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Metal additive manufacturing for particle accelerator applications

Romano, Tobia; Pikurs, Guntis; Ratkus, Andris; Torims, Toms; Delerue, Nicolas; Vretenar, Maurizio; Stepien, Lukasz; Lopez, Elena; Vedani, Maurizio

Abstract

Metal additive manufacturing technologies are rapidly becoming an integral part of the advancedtechnological portfolio for the most demanding industrial applications. These processes are capable offabricating three-dimensional components with near-net shape quality by depositing the constituentmaterials in a layer-by-layer fashion. This fabrication approach provides numerous advantages overconventional manufacturing methods, including enhanced design flexibility, reduced production costs andlead times, rapid prototyping, and the possibility to repair damaged parts. In recent years, the growingdemand for novel accelerator components with improved performance characteristics, integratingstructures such as drift tubes and internal cooling channels, has prompted the exploration of additivemanufacturing in the field of particle accelerators. Radio-frequency components, beam interceptingdevices, and vacuum systems have been prototyped using various metallic materials and additivemanufacturing technologies, demonstrating performance levels comparable to the conventionally manu-factured counterparts in preliminary tests. However, the absence of established qualification protocols andthe uncertain reliability of additively manufactured parts under the demanding conditions typical ofaccelerator applications pose significant challenges to the integration of additive manufacturing processesinto the fabrication practices of these components. This paper provides a comprehensive review ofdocumented applications of metal additive manufacturing in particle accelerators, highlighting benefits,challenges, and opportunities for future improvements. The main requirements and currently available testsetups for the assessment of additively manufactured components in applications involving ultrahighvacuum and intense electromagnetic fields are also discussed.

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Metal additive manufacturing for particle accelerator applications Tobia Romano ,1,2,* Guntis Pikurs ,2,3 Andris Ratkus ,2Toms Torims ,2,3 Nicolas Delerue ,4 Maurizio Vretenar ,3Lukas Stepien ,5Elena López ,5and Maurizio Vedani 1 1Department of Mechanical Engineering, Politecnico di Milano, 20156 Milan, Italy 2Institute of Particle Physics and Accelerator Technologies, Riga Technical University, LV-1048 Riga, Latvia 3The European Organization for Nuclear Research (CERN), 1211 Meyrin, Switzerland 4Laboratoire de Physique des 2 Infinis Ir`ene Joliot-Curie (IJCLab), 91400 Orsay, France 5Fraunhofer Institute for Material and Beam Technology, IWS, Winterbergstraße 28, 01277 Dresden, Germany (Received 22 February 2024; accepted 23 April 2024; published 17 May 2024) Metal additive manufacturing technologies are rapidly becoming an integral part of the advanced technological portfolio for the most demanding industrial applications. These processes are capable of fabricating three-dimensional components with near-net shape quality by depositing the constituent materials in a layer-by-layer fashion. This fabrication approach provides numerous advantages over conventional manufacturing methods, including enhanced design flexibility, reduced production costs and lead times, rapid prototyping, and the possibility to repair damaged parts. In recent years, the growing demand for novel accelerator components with improved performance characteristics, integrating structures such as drift tubes and internal cooling channels, has prompted the exploration of additive manufacturing in the field of particle accelerators. Radio-frequency components, beam intercepting devices, and vacuum systems have been prototyped using various metallic materials and additive manufacturing technologies, demonstrating performance levels comparable to the conventionally manufactured counterparts in preliminary tests. However, the absence of established qualification protocols and the uncertain reliability of additively manufactured parts under the demanding conditions typical of accelerator applications pose significant challenges to the integration of additive manufacturing processes into the fabrication practices of these components. This paper provides a comprehensive review of documented applications of metal additive manufacturing in particle accelerators, highlighting benefits, challenges, and opportunities for future improvements. The main requirements and currently available test setups for the assessment of additively manufactured components in applications involving ultrahigh vacuum and intense electromagnetic fields are also discussed. DOI: 10.1103/PhysRevAccelBeams.27.054801 I. INTRODUCTION Particle accelerators play a crucial role across various scientific disciplines, including fundamental physics and materials science [1,2], and practical applications, such as radiation therapy for cancer treatment, ion implantation in electronics, and food sterilization [3–5]. According to the International Atomic Energy Agency (IAEA), over 30,000 accelerators are currently in operation worldwide [6]. The increasing deployment of accelerator facilities in diverse fields of applied science has raised the demand for innovative technologies to meet current needs for compact designs, increased energy efficiency, and reduced commissioning and maintenance costs [7]. This has prompted the exploration of novel accelerator component concepts boasting superior performance characteristics to enable a new generation of resource-efficient devices with extended operating times and capable of pushing beyond the current energy frontiers, to pave the way for new discoveries in particle physics research [8,9]. The development of novel designs for complex accelerator components with enhanced performance, incorporating structures such as drift tubes, vacuum connectors, and cooling channels, has required the adoption of advanced manufacturing routes involving several fabrication steps and highly skilled labor for precise machining and joining operations [10,11]. In this context, the opportunity to integrate metal additive manufacturing (AM) technologies into the fabrication practices of accelerator *Corresponding author: tob[email protected] Published by the American Physical Society under the terms of the Creative Commons Attribution 4.0 International license. Further distribution of this work must maintain attribution to the author(s) and the published article’s title, journal citation, and DOI. PHYSICAL REVIEW ACCELERATORS AND BEAMS 27, 054801 (2024) Review Article 2469-9888=24=27(5)=054801(38) 054801-1 Published by the American Physical Society components has emerged in the past few years, aiming to simplify the production processes, reduce costs and lead times, and eliminate the design constraints imposed by conventional methods [7,12]. AM processes create three-dimensional objects by depositing the constituent materials layer after layer, following the geometry outlined in computer-aided design (CAD) models. This approach enables the one-step fabrication of complex structures with a near-net shape quality, opening up possibilities for topological optimization based on the functional requirements of the intended component, no longer limited by technology-related restrictions [13]. These may include, for example, the integration of conformal cooling channels for enhanced thermal efficiency and lattice structures to minimize weight and material usage while providing adequate structural properties. In AM, geometric complexity is not usually associated with significantly higher production costs. Moreover, it is particularly suited for rapid prototyping and for the production of one-off parts and limited series, as is frequently the case for accelerator components designed for specific particle beam characteristics [9]. In contrast, the fabrication of complex parts with conventional methods often entails multiple expensive and time-consuming machining and joining operations. The large amount of scrap produced during machining is particularly impactful for parts made from expensive raw materials, such as niobium superconducting radio-frequency (SRF) cavities [14]. Additionally, the production of small batches may not warrant the initial investment for dedicated molds and tools. Figure 1qualitatively compares the unit cost as a function of part complexity and production volume for AM and conventional manufacturing methods. The monolithic fabrication of seamless structures enabled by AM can improve component reliability by preventing possible misalignments and the formation of detrimental phases at interface regions during joining operations. This holds particular relevance for rf applications, where surface discontinuities can compromise device performance [16]. The demonstrated capability of AM to repair high-value industrial components further emphasizes its potential [17]. Since accelerator components account for a significant portion of the overall cost of accelerator facilities [9,18], repair opportunities through AM methods may be considered aiming at reducing the maintenance expenses. Major challenges to the integration of metal AM technologies into the manufacturing routes of accelerator components are related to the absence of established protocols for qualification, the uncertain reliability of parts produced by AM under the demanding service conditions often encountered in accelerator applications, and the still open questions regarding the process-microstructureproperty relationship in additively manufactured parts. The latter aspect is still the subject of ongoing scientific research due to the multitude of experimental parameters and postprocessing operations that can influence the quality of parts produced by AM, including surface roughness, thermal stresses causing deformations in printed parts, peculiar microstructures, and defects developing from the complex physical phenomena involved in the processes [15,19,20]. An additional source of the challenge is the increasing demand for design expertise to fully leverage the flexibility of AM through topological optimization based on mechanical, thermal, thermodynamic, electromagnetic, and beam dynamics simulations, pursuing the so-called design for AM paradigm [21]. Despite these challenges, there are specific scenarios in which AM can offer considerable advantages for the manufacturing of particle accelerator components over conventional fabrication methods. This work provides a comprehensive review of applications of metal AM in the accelerator sector, documenting the benefits and challenges evidenced to date in the literature. II. METAL ADDITIVE MANUFACTURING TECHNOLOGIES Metal AM technologies can be divided into single-stage and multistage processes [22]. In single-stage processes, FIG. 1. Unit cost as a function of (a) part complexity and (b) production volume for AM and conventional manufacturing methods [15]. TOBIA ROMANO et al. PHYS. REV. ACCEL. BEAMS 27, 054801 (2024) 054801-2 parts with the basic geometry and material properties are manufactured in a single operation starting from a feedstock material in the form of powder or wire. On the other hand, multistage processes typically involve an initial printing operation providing the basic geometry of the desired product, followed by consolidation procedures to impart the required structural integrity and properties. A. Single-stage processes Depending on the material feeding strategy, the most established single-stage (or direct) metal AM processes can be classified as powder bed fusion (PBF) and direct energy deposition (DED). Both classes include techniques that can process various metallic materials, such as iron, aluminum, titanium, nickel, and copper alloys, as well as precious and refractory metals. In PBF processes, the powder feedstock is spread onto a build platform in layers of controlled thickness to generate a so-called powder bed. After the deposition of each layer, a heat source selectively melts the powder according to the designed model to build a three-dimensional part layer by layer. The process is called laser beam powder bed fusion of metals (PBF-LB/M) [27] or electron beam powder bed fusion (PBF-EB) depending on the nature of the heat source used. FIG. 2. Schematic diagrams of single-stage AM processes: (a) PBF-LB/M [23], (b) PBF-EB [24], (c) LMD [23], (d) WAAM [25], and (e) CSAM [26]. METAL ADDITIVE MANUFACTURING …PHYS. REV. ACCEL. BEAMS 27, 054801 (2024) 054801-3 In PBF-LB/M [Fig. 2(a)], the printing procedure is usually conducted inside a closed chamber filled with inert gas to prevent material contamination. The use of highly focused laser beams (∼30–100 μm spot size), fine powders ranging from 5 to 60 μm in size, and layer thicknesses generally below 50 μm allows realizing minute details with a resolution of up to 0.2–0.4 mm [15,28,29]. In recent years, commercial machines with large build volumes also became available for the fabrication of parts with up to 800 mm base diameter and 850 mm height [29]. Most systems are equipped with one or multiple infrared laser sources with a wavelength of around 1000 nm and a maximum power of up to 1 kW, suitable for the processing of most engineering metallic materials. However, highly reflective metals, like pure copper, exhibit a limited absorption rate in the infrared range (Fig. 3)[30], which often results in defects in the printed parts due to incomplete fusion of the powder [31]. High laser powers (1 kW or higher) can be used to compensate for the low absorption [32–34]. PBF-LB/M machines using green laser sources have also been developed to improve the processability of materials with maximum absorbance in this wavelength range [35,36]. In PBF-EB [Fig. 2(b)], the use of a high-energy electron beam requires the printing process to occur in vacuum, ensuring a high material purity. The electron beam is scanned across the powder bed using magnetic coils, which can move it almost instantaneously by properly varying the input parameters [37]. This aspect, combined with the very effective absorption of the beam energy by the powder material, results in higher production rates compared to PBF-LB/M, as complete fusion is guaranteed even when selecting high scanning speeds [23]. In order to prevent a negative electric charge from accumulating on the surface of the powder bed, each layer is preheated by the electron beam at high power and high scanning speed. Preheating is beneficial for materials sensitive to hot cracking, which require relatively longer times at high temperatures and slower cooling rates to ensure defect-free parts upon solidification. In addition, the preliminary electron beam scans partially sinter the powder particles before the actual selective melting procedure. The slightly consolidated powder bed provides an electrical connection for better charge dissipation and can serve as a support for the creation of inclined overhang structures at angles that cannot be achieved by PBF-LB/M without the use of supports conveniently included in the model. However, it results in a high surface roughness of as-printed parts [38]. This effect is further accentuated by the preferred use of relatively coarse powders (typically, 45–100 μm[39]), having a lower tendency to be ejected from the powder bed due to electrostatic repulsion. The maximum build volume of commercially available PBF-EB systems is comparable to that of PBF-LB/M machines, with a 350 mm base diameter and 380 mm height [15]. In DED processes, the feedstock material in powder or wire form is simultaneously melted by a focused heat source (laser beam, electron beam, or electric arc) while it is being deposited only in the desired locations with a nozzle system. Examples of DED technologies include laser metal deposition (LMD), which employs a coaxial nozzle equipped with a laser source to melt the material fed to the molten region [Fig. 2(c)], and wire arc additive manufacturing (WAAM), which uses an electric arc to deposit metallic filaments [Fig. 2(d)]. Compared to PBF, DED techniques can fabricate larger freeform parts because the printing process does not necessarily require an enclosed work chamber. The direct deposition approach is also suitable for printing additional features on existing parts without the need for a flat base surface and it opens up the possibility to repair high-value components and fabricate multimaterial structures by varying the composition of the material fed during the deposition process [40,41]. Although DED technologies usually have a lower resolution compared to PBF methods (∼1mm minimum feature size [15]), the deposition head can be combined with milling tools to machine finer features and mechanically finish the as-printed surfaces as the part is built up layer after layer, thus alternating printing and milling operations [42]. A single-stage AM method similar to DED processes, but not involving the complete melting of the powder feedstock material, is cold spray additive manufacturing (CSAM). During the process, fine metal or ceramic powders are accelerated within a compressed gas stream toward a substrate (a build platform for fabricating standalone parts or an existing component for feature addition or repair). Upon high-velocity impact on the substrate surface, the particles plastically deform and bond together, FIG. 3. Absorbance of metal powders as a function of laser wavelength; the green and red lines indicate typical green (λ¼515 nm) and IR (λ¼1070 nm) laser wavelengths, respectively, employed in commercial PBF-LB/M machines [30]. TOBIA ROMANO et al. PHYS. REV. ACCEL. BEAMS 27, 054801 (2024) 054801-4 generating a layer of consolidated material [Fig. 2(e)]. CSAM features high material efficiency and low energy consumption. It can provide certain design flexibility through configurations that allow the motion of both the spray gun and the substrate. Similar to DED techniques, it also enables the fabrication of discrete, functionally graded, and even metal-ceramic multimaterial parts by varying the powder composition during the process [43,44]. B. Multistage processes Multistage (or indirect) AM processes include different technologies which, unlike direct processes, usually do not involve the complete melting and solidification of the initial material. Among them, it is worth mentioning bound metal deposition (BMD) and ultrasonic additive manufacturing (UAM), which have already been studied for applications in the field of particle accelerators [45,46]. BMD uses wax and polymer filaments loaded with a metallic powder as feedstock material. A deposition head heats the filament to make it fluid and deposits it onto a build plate to create a three-dimensional part layer after layer. The printing operation is followed by hightemperature debinding and sintering to remove the polymeric fraction and consolidate the metal powder, respectively [Fig. 4(a)]. The slow and uniform heating of the material during the sintering step results in stress-free products. On the other hand, residual porosity is often observed in the sintered parts [49] and impurities produced by incomplete combustion of the polymer may affect the material properties. UAM is a hybrid process that combines ultrasonicassisted welding and computer numerical control machining. Three-dimensional parts are built by stacking thin metal foils (∼100–150 μm thickness [50]) welded together using a sonotrode. The strong interface friction generated by the rotating and vibrating sonotrode induces plastic deformation and intimate contact between the metal foils, resulting in metallurgical bonding. After stacking a certain number of foils, a machine tool is used to trim the deposit to create one slice of the designed part [Fig. 4(b)]. This alternation of additive and subtractive operations is repeated until achieving the final geometry. One advantage of UAM is that accuracy and surface quality do not depend on the thickness of the metal foils used, but only on the machining tool and strategy adopted. Inclined and curved surfaces can be easily milled, faithfully reproducing the geometry of the component model. Also, thanks to the building approach based on foil piling, multifunctional parts made of multiple materials or embedded electronic components like fiber optics and sensors can be manufactured. FIG. 4. Schematic diagrams of multistage AM processes: (a) BMD [47], (b) UAM [48], and (c) BJT [38]. METAL ADDITIVE MANUFACTURING …PHYS. REV. ACCEL. BEAMS 27, 054801 (2024) 054801-5 However, very complex geometries and overhanging elements cannot usually be integrated into the design due to the inherent lack of support structures [50]. Another indirect AM technology that has experienced rapid development in recent years for the processing of both metallic and ceramic materials is binder jetting (BJT) [51]. BJT is based on the same powder bed approach of PBF processes. However, a print head selectively deposits a polymeric binder to join the powder particles in each powder layer and between adjacent layers, instead of melting them with a high-energy beam. Following the printing step, the so-called green parts are first subjected to a curing treatment at a moderate temperature to reticulate the binder and provide sufficient mechanical strength for handling operations [38]. Then, high-temperature debinding and sintering cycles are applied to burn off the polymer and densify the material [Fig. 4(c)], like in the BMD process. Unlike PBF methods, the powder bed can support overhang elements during the BJT process, eliminating the need for further support structures [52]. Several parts can also be printed stacked on top of each other in a single job, resulting in higher productivity and lower fabrication costs [51]. The main challenges are to obtain fully dense products from green parts, with typical relative densities of around 50%, and to control the size and geometry of the components during densification to ensure a good accuracy [52,53]. III. METALLIC MATERIALS FOR ACCELERATOR APPLICATIONS The variety of metallic materials used in the fabrication of accelerator components is not very large [54]. It mainly includes pure copper and copper-based alloys, niobium and other superconducting materials, stainless steel, aluminum alloys, titanium alloys, nickel-based alloys and superalloys, and refractory metals. Many of these materials are commercially available as feedstock for various AM systems and have already been studied in this framework in terms of processability and achievable properties [15,23,55]. A. Pure copper and copper alloys High-purity copper is used for the fabrication of several accelerator components, such as rf cavities and quadrupoles, waveguides, vacuum seals, klystrons, and various types of cathodes [56–60] because it has excellent electrical and thermal properties, good formability, workability and solderability, and a relatively high corrosion resistance. The combination of high thermal conductivity and low electrical resistivity is crucial for increasing the sustainable electric fields in high-gradient normal-conducting accelerators, in order to enhance efficiency and avoid overheating caused by ohmic losses, which can cause significant thermal expansion and distortions that can change the rf phase response of the accelerating structures [61,62]. Pure copper grades that are typically used in accelerator applications are oxygen-free (OF, >99.95% Cu) and oxygen-free electronic (OFE, >99.99% Cu) copper, having a low outgassing tendency [63] due to the stringent limits on the content of oxygen and other impurities. OFE copper is preferred in cryogenic applications requiring a large residual resistivity ratio (RRR) [56]. A limitation of pure copper is that its mechanical properties degrade at relatively low temperatures (softening already occurs around 250 °C [64]). For this reason, copper alloys with better mechanical properties are often preferred in applications involving thermal cycling and pulsed heating. The long straight sections (LSS) of the drift chambers of the vacuum system of the Large Hadron Collider (LHC) were manufactured in C10700 Cu-Ag alloy because the inner walls were coated by a nonevaporable getters (NEG) coating having an activation temperature in the range of 200–300 °C [56]. A small addition of silver (0.085%) can in fact improve softening and creep resistance of the base material while keeping comparable electrical and thermal properties [63,64]. Precipitation-hardening CuCr, CuZr, and CuCrZr alloys also exhibit higher hardness and strength, resulting in low susceptibility to surface damage during pulsed heating [65]. Excellent high-temperature performance is also shown by oxide dispersion-strengthened (ODS) coppers, in which nanometric ceramic particles reinforce the metal matrix. Alumina-reinforced Glidcop®has been used to fabricate crotches for the absorption of synchrotron radiation [64] and is normally employed when vacuum brazing is required [66] as the finely dispersed particles prevent recrystallization and softening of the copper matrix even at typical brazing temperatures (∼600 °C) at which precipitation-hardening alloys start becoming unstable [56]. However, in these systems, the gain in mechanical properties is inevitably accompanied by a slight reduction in the electrical conductivity. B. Niobium and niobium-based superconducting systems Pure niobium (>99.95% Nb) is primarily used to manufacture rf cavities and magnets for superconducting accelerator facilities [67] since it is able to generate very high accelerating electric fields with little heat dissipation. Historically, niobium has been used for these applications because, among pure metals, it has the highest critical temperature (∼9.2K), the highest lower critical magnetic field, and the highest superheating field [68]. It also features good formability and can be easily molded into cavity shapes [69]. Copper cavities internally coated with a thin film of pure niobium have also been developed since the 1980s [70] and employed at CERN in several experiments [71]. Such structures offer some advantages over bulk niobium cavities, including the reduction of costs associated with both raw materials and manufacturing TOBIA ROMANO et al. PHYS. REV. ACCEL. BEAMS 27, 054801 (2024) 054801-6 routes and a better thermal stability, resulting from the superior thermal conductivity of copper, and the easier implementation of optimally designed cryomodules [68,70,72]. Nb-Ti alloy and Nb3Sn intermetallics are also used for the fabrication of superconducting joints, wires, and Rutherford cables [73–75]. C. Stainless steel Stainless steel is a crucial material for the construction of new generation accelerators [56]. It is widely employed to manufacture waveguides, beampipes, flanges, and vacuum connectors, as well as structural components also working at cryogenic temperatures, like the standard dipole magnet collars of the LHC [76–79]. The grades mainly used in accelerator applications are 304L and 316L austenitic stainless steels because they combine high strength, ductility, toughness, and corrosion resistance. They can also be easily machined to create the sharp edges typically required in vacuum seals [56]. A major limitation is that the metastable austenitic phase is susceptible to martensitic transformation when cooled to cryogenic temperatures. Martensite has a higher magnetic susceptibility compared to austenite and is brittle at cryogenic temperatures. 304L steel suffers from martensitic transformation already at liquid nitrogen temperature (∼77 K) [79]. Small additions of nitrogen can significantly increase austenite stability against martensitic transformation in 316L. Nitrogenstrengthened 316LN steel with ∼0.2% N content can retain a large ductility even at liquid helium temperature (∼4K) [79,80]. The superior corrosion resistance and resistance to softening of 316LN also make it suitable for vacuumfiring operations, i.e., heating the component at ∼1000 °C for several hours to remove dissolved gases (mainly hydrogen) and improve its outgassing performance [81]. D. Pure aluminum and aluminum alloys Pure aluminum and aluminum alloys are largely employed to manufacture waveguides, microwave cavities, and casings for superconducting quantum devices [82–86]. Aluminum combines good electrical and thermal properties with a higher transparency to radiation and a lower residual radioactivity compared to other structural materials like copper and stainless steel [56,87]. Depending on their chemical composition, aluminum alloys can be plastically deformed or welded to produce parts with relatively complex geometry. However, their use should be carefully considered for components subjected to high temperature cycles, such as vacuum chambers undergoing firing and NEG coating activation, as they may suffer from temperature-induced softening and creep [56]. E. Titanium alloys Titanium alloys find many structural applications in high-energy physics facilities because they combine good mechanical properties, like specific strength, ductility, and fatigue endurance limit, with excellent high-temperature stability and corrosion resistance [15,88]. Their relatively low elastic modulus and coefficient of thermal expansion also result in a high resistance to thermal shocks induced by pulsed beams, making them a preferred material for beam dumps and windows [89,90]. Since they do not show ductile-to-brittle transition at low temperatures [91],various titanium grades have been used to produce liquid helium storage vessels and cryomodules for cryogenic cooling of superconducting accelerator components [92–94]. Ti-45Nb alloy is often employed to manufacture type-II superconducting magnets and wires because it is more affordable than pure niobium while offering an accessible critical temperature (∼10 K), a high upper critical magnetic field, and a high critical current density [95]. Due to its higher mechanical properties [96], it is also preferred to unalloyed niobium for making flanges and connectors in multicell superconducting cavities [97]. F. Nickel alloys and superalloys Nickel-based alloys are high-performance materials often used in demanding applications, as they display excellent mechanical properties, high creep resistance, and good corrosion resistance even in harsh environments [15,98]. Nickel superalloys are one of the main materials of choice for beam windows [99,100], because they retain high strength and ductility even after exposure to intense irradiation, resulting in great window durability and resistance to high dose levels for high-power beam applications [101–103]. They are also used to produce high-strength support frames to be integrated with superconducting coil structures [104]. Thanks to their high magnetic permeability, which is maintained even at cryogenic temperatures [105], Ni-Fe alloys are the preferred material for passive magnetic shielding of superconducting cavities cooled with liquid helium [106,107]. G. Refractory metals and alloys Besides niobium, other refractory metallic materials are of particular interest for high-energy accelerator facilities. Refractory metals, such as tungsten, molybdenum, and tantalum, feature an extremely high melting point (well above 2000 °C) and can exhibit an excellent performance under various extreme conditions. Tungsten and molybdenum have been studied for the manufacturing of components directly exposed to high-energy beams, like beam intercepting devices [108], while tungsten-copper alloys are often employed for arcing contacts in high-voltage circuit breakers [109]. The materials used in these applications must withstand extreme thermomechanical stresses, as well as resist radiation damage. Tungsten, molybdenum, and tantalum find applications as electrode materials in high-voltage devices, such as ion sources and traveling wave tubes [110,111], and in high accelerating gradient and METAL ADDITIVE MANUFACTURING …PHYS. REV. ACCEL. BEAMS 27, 054801 (2024) 054801-7 high rf power structures [112,113] because they can guarantee low breakdown rates during operation [114]. Molybdenum and tantalum are also widely employed in electron guns due to their good thermal conductivity and dimensional stability [115]. Various combinations of refractory metals and alloys are good candidates as antiproton target materials because their high density allows the production of compact targets that prevent antiproton reabsorption into the surrounding material [116]. IV. REQUIREMENTS FOR ACCELERATOR COMPONENTS Due to the extreme conditions to which accelerator components are often subjected during operation, there are several stringent requirements that the materials used in their production have to fulfill. This translates into a long list of aspects that need to be considered for the qualification of AM technologies for accelerator applications. They can be grouped into three key categories, relating, respectively, to the material properties, the manufacturing process, and the specific service conditions to which accelerator components are exposed. A. Material properties 1. Chemical composition and purity Materials used in particle accelerators usually have a tightly controlled chemical composition. Many applications require the use of pure metals with stringent limits on the impurity content, as they can dramatically alter the properties of the base material. For example, small contents of oxygen, carbon, and especially phosphorus can significantly reduce the thermal and electrical conductivity of copper [52,55,117], while hydrogen degrades the performance of superconducting niobium cavities by forming hydride precipitates that act as normal-conducting sites [118,119]. The quality factor (Q-factor) of niobium cavities is also affected by magnetic impurities, which cause inelastic scattering of the Cooper pairs and increase the surface resistance [120], thus locally increasing the rf losses and suppressing superconductivity. The number of contaminants prone to activation should be minimized in components exposed to irradiation to avoid the uncontrolled generation of radionuclides with a long half-life, which may cause safety concerns during maintenance and disposal [121]. Contaminants are a major source of outgassing in ultrahigh vacuum (UHV) systems [122], while surface impurities may promote vacuum electrical breakdown in high-voltage applications due to local field enhancement [123]. Achieving a well-controlled chemical composition in additively manufactured parts is often challenging, due to both feedstock quality and contamination or uncontrolled changes in element concentration that can occur during the fabrication process. Keeping the oxygen content within specifications is particularly critical in powder-based AM processes because oxidation can already occur during powder production, sieving, transport, and handling due to the high surface area of powder particles [117,124].The pickup of impurities during PBF processing of sensitive materials, like titanium and aluminum alloys, can be limited by minimizing the content of residual oxygen and other contaminants in the build chamber [125]. In DED processes, however, this is more challenging because the shielding gas only provides a partial protection during material deposition [38,126]. The reuse of powder collected from previous printing operations should be approached with caution because the content of interstitial elements usually increases with each successive print cycle [127]. Special attention should also be paid to the possible loss of volatile elements, like zinc and magnesium, in processes that use high-energy beams, as selective vaporization may alter the chemical composition of the printed parts compared to the initial feedstock material [128]. 2. Microstructure A homogenous microstructure is a key requirement for accelerator components, as it provides increased formability, which is particularly important when the manufacturing process involves severe plastic deformation operations [129] and uniform mechanical and physical properties. These are crucial to avoid hot spots that may arise due to localized variation in electrical resistivity or thermal conductivity, as well as having a beneficial effect on the thermo-mechanical fatigue behavior of components exposed to pulsed beams [130]. In UHV applications, products with fine and uniform grain size distribution are mandatory, especially when the design involves thinwalled regions [56]. Microstructural anisotropy should also be avoided to ensure consistent thermal expansion properties, thus preventing the buildup of severe internal stresses during temperature fluctuations. In superconducting systems, local textures with low electron work function (like h100ifiber in pure niobium) may compromise the device efficiency [131]. In applications that involve high accelerating gradients, when using multiphase alloys, the different phases should be intimately mixed to prevent breakdown from occurring selectively at the dielectrically weaker phase [132]. Although the specific grain morphology depends on the nature of the material and the selected process parameters, it is not common to observe homogeneous microstructures in parts produced with the most established metal AM technologies due to their inherent layer-by-layer approach. In direct processes, relatively large columnar grains typically develop along the build direction and can traverse several layers. This may result in markedly different mechanical and physical properties along different directions [133]. TOBIA ROMANO et al. PHYS. REV. ACCEL. BEAMS 27, 054801 (2024) 054801-8 3. Defects Accelerator components must comply with strict limits on defect content. Porosity and nonmetallic inclusions should be minimized as they affect thermal, electrical, and mechanical properties of metallic materials. A high porosity may also compromise the outgassing performance in UHVapplications [134], while relatively large inclusions may cause leakages [56]. Manufactured parts should also be free of residual stresses to prevent uncontrolled deformations that deviate from the geometric tolerances specified in the design and to ensure a high dimensional stability even for components subjected to high thermomechanical loads. Typical defects observed in additively manufactured parts are gas porosity and the so-called lack-of-fusion. Round pores may be generated from gas entrapped in the feedstock material or absorbed during the printing process by the molten material [Fig. 5(a)], while lack-of-fusion defects are caused by incomplete melting of the powder and appear as irregularly shaped cavities [Fig. 5(b)][23]. When employing high power densities and low scanning speeds in PBF-LB/M, the melting of the material can occur through keyhole formation. A keyhole is a deep and narrow cavity generated by the rapid evaporation of the metallic material, which pushes the surrounding melt enabling penetration and multiple reflections of the laser beam [135]. Although this results in excellent laser absorption efficiency, without careful control of the process parameters, the keyhole can become unstable and repeatedly collapse during the scanning process, producing round voids in the deposit due to entrapped vapor [Fig. 5(c)][23]. Cracking may also occur if the process parameters are not properly adjusted, especially in the most crack-sensitive alloys. Delamination, as well as macroscopic distortion and geometrical inaccuracies, may result from thermal stresses developing during single-stage AM processes. Nonuniform and time-dependent stresses are generated from the repeated heating and cooling cycles the material experiences during the printing process. Understanding the evolution of these stresses, also by means of multiphysics simulations, is crucial to optimize part design and support structure configuration to improve heat dissipation and reduce distortions [23]. B. Manufacturing process The characteristics of parts made by AM significantly depend on the technology and the process parameters employed. While PBF processes can provide superior dimensional accuracy, the limited volume of the build chamber of most commercially available systems may be insufficient for the fabrication of large accelerator components. On the other hand, DED and multistage processes do not usually have strict dimensional constraints but at the expense of resolution and design freedom. Meeting the stringent surface roughness requirements typical of accelerator components poses a significant challenge for most available AM processes. The surface quality of additively manufactured parts in as-built conditions results from the interaction of a large number of factors related to feedstock material, part design, production technology, and process parameters [23,137]. A major source of surface roughness common to most AM methods is the so-called staircase effect, which results from converting three-dimensional models into stacks of discrete layers that approximate the ideal surface contour by steps [Fig. 6(a)][138]. The staircase effect can be mitigated by reducing the layer thickness, which, however, increases the overall processing time, and by properly orienting the part to avoid highly inclined surfaces relative to the build direction [137]. In powder-based processes, another contribution to roughness comes from powder particles that adhere and partially sinter on the surface of the consolidated material at high temperature [Fig. 6(b)]. This effect is particularly severe in downward-facing surfaces because the solid material lies on a layer of loose powder that does not allow for effective heat dissipation [139]. Before complete solidification, the molten material may also partially penetrate into the powder bed due to gravity and capillarity effects, promoting dross formation [140].In PBF-LB/M, supports are often added in the design to secure overhanging surfaces and improve heat dissipation. However, the removal of these sacrificial structures at the end of the printing process can be challenging, especially in small and intricate parts [141], and leave macroscopic marks, thus requiring significant postprocessing efforts to achieve a good quality in downward facing surfaces [142]. The top surface, on the other hand, may exhibit discontinuities caused by instabilities in the melt track due to improper selection of the laser scanning parameters. This phenomenon is known as balling [Fig. 6(c)][143]. Proper calibration of the process parameters is also crucial for producing high-quality parts, with optimized characteristics for the specific application and minimal defect content. While the possibility to tune numerous settings with a certain degree of freedom allows for adjustments based on design specifications, understanding FIG. 5. (a) Gas-induced pores [126], (b) lack-of-fusion defect [42], and (c) keyhole-induced porosity [136] observed in additively manufactured deposits. METAL ADDITIVE MANUFACTURING …PHYS. REV. ACCEL. BEAMS 27, 054801 (2024) 054801-9 manufactured without any support [184], an innovative noncontact structure was integrated into the design of the niobium cavities [Fig. 15(c)] to act as a support for surfaces inclined by less than 35° relative to the build platform. The support structure followed the profile of the inner surface of the cavity’s upper shell while remaining separated by a few layers of loose powder. The presence of this bulk structure improved the heat dissipation during the printing process, resulting in a lower roughness of down-skin regions of the cavities compared to nonsupported samples. Moreover, as it was not welded to the cavity’s internal walls, it could be easily extracted from inside at the end of the printing process without the need for complex cutting operations. A novel PBF-LB/M approach was also adopted by Riensche et al. [186] to fabricate AlSi10Mg prototypes of rf quarterwave cavity resonators (QWRs). They employed a commercial hybrid PBF-LB/M machine integrating a vertical three-axis milling tool for in situ machining of specific features, critical for the rf performance of QRWs, including the outer conductor, central pin, shorting plane, and service surfaces. A milling operation was performed after every ten layers of deposition, corresponding to a thickness of ∼0.5mm. Thanks to their superior surface finish, the QRWs manufactured with the hybrid process exhibited a significantly higher and more stable Q-factor compared to their counterparts made by standard PBF-LB/M, as well as a resonant frequency closer to the ideal value. Another aluminum alloy, the Al12Si grade, was employed by Creedon et al. [187] to manufacture superconducting microwave cavities by PBF-LB/M [Fig. 16(a)]. Si-containing aluminum alloys arewell suited for the PBF-LB/M process because the high silicon content promotes the formation of a eutectic phase with a narrow solidification range and higher fluidity in the molten state, thus preventing hot cracking during solidification [188,189], resulting in excellent laser processability. Subsequent annealing of the printed device at ∼600 °C for 4 h significantly improved the Q-factor from 1.6×106to 3.8×106,as the high temperature promoted the diffusion of silicon out of the supersaturated solid solution, leaving behind a purer aluminum matrix with higher electrical conductivity. A superconducting microwave cavity was also manufactured by Holland et al. [190]. They developed a novel design for a conical resonator and printed it by PBF-LB/M in a monolithic piece employing a Ti6Al4V powder [Fig. 16(b)]. The measured resonance of the device (ω0=2π¼7.50 GHz) was in good agreement with the simulated data. PBF-LB/M has also been used to manufacture normalconducting linear accelerator (linac) structures. Mayerhofer et al. [154] prototyped a five-cell drift tube linac (DTL) comprising four drift tubes and a network of cooling channels running through the cavity (Fig. 17). In the standard DTL design, each drift tube is supported by two stems to ensure stability during the brazing operations. However, the one-stem geometry allowed by PBF-LB/M results in a lower electromagnetic field interference, increasing the predicted shunt impedance by ∼18% compared to the two-stem configuration. They also slightly modified the shape of the upper region of the cavity and cooling channels to eliminate significant overhanging features and facilitate the printing of the DTL without the need for additional support structures. The additively manufactured DTL exhibited a ∼15% lower unloaded Q-factor and ∼4% lower shunt impedance compared to its conventionally produced counterpart. This was primarily attributed to the larger surface roughness, causing higher ohmic rf power losses at the cavity walls and promoting the occurrence of breakdown phenomena. A comparable performance was achieved after improving the surface quality by means of a commercially available chemical-electrochemical process [191]. Moreover, the production costs were reduced to one-third of those of the reference cavity. A similar strategy was adopted to prototype biperiodic side-coupled linac structures, highlighting the potential of PBF-LB/M in manufacturing each cell with optimal length in terms of particle energy without additional cost or effort (Fig. 18)[9]. On the other hand, this approach is impractical with conventional methods, as the fabrication of several individual parts with dissimilar geometries would be economically unsustainable. FIG. 16. (a) Additively manufactured Al12Si superconducting cavities in as-built condition, after annealing and machining, and in annealed and polished condition [187], and (b) Ti-6Al-4V conical resonator made by PBF-LB/M [190]. TOBIA ROMANO et al. PHYS. REV. ACCEL. BEAMS 27, 054801 (2024) 054801-16 The economic advantage and ease of production of AM were also emphasized by Wehner et al. [192,193] who exploited the flexibility of PBF-LB/M to manufacture a complex klystron circuit with multiple rf cavities in only two parts with well-aligned matching features, which were subsequently brazed in a hydrogen furnace [Figs. 19(a) and 19(b)]. This approach provided significant benefits over the conventional fabrication process, which involves numerous intermediate machining and brazing operations, carrying the risk of vacuum and water leakage due to minor misalignments. The assembled circuit displayed no indication of leakage during the helium leak test, nor significant outgassing when placed in vacuum. The rf cavities, on the other hand, showed a substantial deviation in resonant frequency compared to the intended design. Further experiments conducted on test cavities with the same geometry as cavity 2 of the full klystron circuit [Fig. 19(c)] revealed a lower Q-factor and higher frequency than simulated values [Figs. 19(d) and 19(e)]. This was primarily attributed to the surface roughness of as-built cavity walls and inaccuracies of the PBF-LB/M process in reproducing the 3D model geometry. In a series of publications, Hähnel et al. [194–198] demonstrated the manufacturing of 316L stainless steel and pure copper Interdigital H-mode (IH) DTL structures using PBF-LB/M. The 316L cavity was equipped with CF40 flanges for vacuum testing and rf coupler and tuner for low-level rf measurements. The structure also included cooling channels extending to the stems of the additively manufactured drift tubes [Fig. 20(a)]. An ultimate pressure of ∼10−7was reached during vacuum tests after approximately 120 h pumpdown while the measured operating frequency and Q-factor showed good agreement with the expected values [198]. An improved design with smoothed surfaces was also developed to facilitate postprocessing operations, such as surface finishing and copper plating, and reduce the peak field for the benefit of high-power rf operation [Fig. 20(b)] [196]. The pure copper specimens [Fig. 20(c)], on the other hand, exhibited a lower Q-factor than expected. This was attributed to the peculiar microstructure resulting from the PBF-LB/M process, affecting the electrical conductivity of the material. Although the ideal value was not achieved, an improvement in the Q-factor of FIG. 18. (a) Additively manufactured side-coupled linac structures and (b) half-cells after cutting [9]. FIG. 17. Design of (a) DTL cavity and (b) cooling system and (c) front and (d) rear view of the fully equipped prototype [154]. METAL ADDITIVE MANUFACTURING …PHYS. REV. ACCEL. BEAMS 27, 054801 (2024) 054801-17 ∼18% was observed after annealing the parts at 300–400 °C for 1 h to induce recrystallization. Another core element of many linac facilities, the radiofrequency quadrupole (RFQ), was prototyped by Torims et al. [13,199] using a commercial PBF-LB/M machine equipped with a high-power green laser source to process an electrolytic tough-pitch pure copper powder. In the first iteration, they printed one-quarter of a 750 MHz RFQ [Fig. 21(a)][13]. The implementation of topologically optimized cooling channels and internal honeycomb structure replacing the massive walls of the standard design led to a weight reduction of ∼37%, also resulting in significant material saving and reduction of printing time. The required geometrical accuracy of 20 μm was successfully achieved for the vane tip. Subsequently, a four-vane RFQ demonstrator of 250 mm length and 148 mm cross-section diameter was manufactured in a single piece, without the need for complex and time-consuming brazing operations [Fig. 21(b)]. This improved design included flanges and orifices for vacuum and rf testing, respectively [199]. A larger version of 400 mm in length was showcased at the Formnext exhibition in 2022 [Fig. 21(c)][200]. The research on AM of rf devices led to the filing of a European patent describing a “method of manufacturing a radio-frequency cavity resonator having a tubular structure extending along a longitudinal axis and a plurality of tubular elements, in particular drift tubes, arranged within the tubular structure, […], that is more cost efficient than the manufacture according to prior art”[201]. PBF-LB/M of copper and copper alloys is also being investigated for the production of acceleration grids for nuclear fusion reactors [202,203]. FIG. 19. Photographs of the (a) additively manufactured klystron circuit half-piece, (b) full circuit after brazing operation, (c) test cavities, (d) frequency, and (e) Q-factor measured on test cavities compared to simulated values [193]. FIG. 20. Additively manufactured IH-type DTL drift tube structure made of (a),(b) 316L stainless steel and (c) pure copper [194,195]. TOBIA ROMANO et al. PHYS. REV. ACCEL. BEAMS 27, 054801 (2024) 054801-18 C. Radio-frequency waveguides and loads rf waveguides are structures designed to guide and manipulate electromagnetic waves, playing a crucial role in accelerator facilities by delivering the rf power from external sources, such as klystrons and magnetrons, to rf cavities for the acceleration of charged particles [204]. While conventional waveguides are established components in rf systems, ongoing research is exploring innovative designs to enhance their functionality [205], for example, for the delivery of THz radiation to high-field gradient accelerator and beam manipulation facilities [155,206]. However, the manufacturing of such devices poses challenges for conventional fabrication methods due to their geometrical complexity and small feature size (on the mm scale), resulting in high production costs and limited design flexibility. Hence the growing interest in recent years in AM applied to the fabrication of waveguides and other rf components. The first additively manufactured prototypes of an rf waveguide were showcased by Grudiev [207] during the CLIC14 workshop. 20 cm long Ti6Al4V WR90 waveguides were produced using PBF-LB/M and PBF-EB technologies. Extensive testing of printed samples involved the characterization of shape accuracy, surface roughness, microstructure and mechanical properties, dc conductivity, rf loss, leak tightness, and outgassing rate. Further development led to the manufacturing and testing of an improved design, featuring an additional cooling jacket, increased wall thickness, and vacuum flange implementation (Fig. 22)[208]. A prototype made of 316L stainless steel was also fabricated by PBF-LB/M. The outputs of the experimental campaign suggested that the PBF-EB technology was not as mature as the laser-based process. Moreover, issues regarding surface roughness and geometrical tolerances were identified as the next challenges to face for part validation. A similar conclusion was drawn by Kellermeier et al. [155], who fabricated 316L stainless steel horn waveguides using PBF-LB/M [Fig. 23(a)]. As expected, dispersion measurements showed that the phase velocity of the printed devices decreased with increasing the nominal inner radius from 0.75 to 0.95 mm [Fig. 23(b)]. However, microscopic inspection revealed a systematic deviation of ∼0.07 mm in the effective radius. This shift caused the waveguides to be inherently overmoded, exhibiting wiggles explainable by multimode excitation. Various types of waveguides made of pure copper were also manufactured using PBF-EB. Horn et al. [210] produced a WR10 waveguide and polished it employing magnetically driven abrasive media. rf testing results FIG. 22. (a) CAD model and (b) photograph of additively manufactured Ti6Al4V WR90 waveguides [209]. FIG. 23. (a) Photograph of additively manufactured horn waveguides and (b) measured dispersion of printed waveguides with varying inner radius [155]. FIG. 21. Photographs of (a) one-quarter [13], (b) 250 mm long [199], and (c) 400 mm long four-vane RFQ prototypes made by PBF-LB/M [200]. METAL ADDITIVE MANUFACTURING …PHYS. REV. ACCEL. BEAMS 27, 054801 (2024) 054801-19 indicated comparable losses (0.8dB cm−1) to conventionally produced reference parts. In another study, Lomakin et al. [205] fabricated two WR12 waveguides using different electron beam scan strategies to evaluate their effect on the performance of the printed devices. In the first approach, they rotated the scan direction by 90° between layers, while the second approach involved creating a contour around the region already processed with the electron beam in each deposited layer. Since both specimens were printed vertically (i.e., with the build direction parallel to the wave propagation direction), the same wavy pattern caused by the layer-wise fabrication was observed on their outer surface. However, the part manufactured with the first strategy also exhibited marked grooves at crosssectional edges, resulting in a significantly higher attenuation compared to the reference waveguide. On the other hand, the contour strategy produced even cross-sectional edges, leading to an attenuation coefficient closer to the ideal value. Lanza et al. [211] also conducted helium leak and outgassing tests on copper X-band waveguides made by PBF-EB to demonstrate their suitability for implementation in UHV systems. Following printing, the parts were annealed at 900 °C in UHV to reduce the oxygen content to 20 ppm. During leakage testing, the waveguides were successfully pumped down to a pressure lower than 10−4Torr, displaying a helium background of 4×10−9Torr l s−1. Outgassing measurements conducted after baking the specimens at 250 °C for 48 h did not reveal any significant outgassing, indicating an outgassing rate below that of the testing chamber walls. A significant impetus for the research on AM for the production of rf components stemmed from CERN’s investment in the Compact Linear Collider (CLIC), which demanded the development of compact devices capable of operating at more than 50 MW peak power and few kW average power to minimize the machine footprint [209,212,213]. Within this framework, Grudiev et al. published various reports showcasing the results progressively achieved in designing and manufacturing a novel X-band rf spiral load [Fig. 24(a)][208,214,215]. This load was devised for implementation in the CLIC facility, aiming to absorb residual rf power not used for beam acceleration nor dissipated in the module walls [213]. The innovative concept behind this design was to make a long taper waveguide more compact by wrapping it inwards. Conveniently positioned holes on the load walls allowed the main vacuum pump placed at the center of the spiral to effectively communicate with the whole internal volume [Fig. 24(b)][204]. A water cooling system was also integrated into the design [209]. The first load prototype, manufactured in 316L stainless steel via PBF-LB/M, exhibited high reflection during low-power rf testing, due to traces of contaminants on the internal surfaces. A second load, made of Ti6Al4V alloy [Fig. 24(c)], was successfully tested in the high-capacity X-band facility Xbox3 with up to 35.5 MW peak power for 50 ns pulses and 25 MW peak power for 200 ns pulses, at a repetition rate of 200 Hz [209]. Following the validation of the spiral rf load and registration under the terms of CERN’s open hardware license [209], Bursali et al. [213] developed an improved design to facilitate the fabrication of multiple parts in a single print run. In the standard design, only one load can be manufactured in each cycle, as the part is constructed with an orientation of 45° relative to the build direction to avoid horizontal surfaces that would compromise quality. This orientation requires substantial support structures [Fig. 25(a)] that need to be removed at the end of the printing process, thereby increasing production costs and generating a large amount of waste material. An iterative optimization process, involving mechanical modeling and electromagnetic simulations, resulted in a new design that can be manufactured horizontally [Fig. 25(b)], allowing the stacking of several units within the powder bed. This can potentially reduce the cost per unit and enable faster manufacturing for mass production. A spiral design was also developed by Mathesen et al. [206] for the rf loads of the Cool Copper Collider (C3), a compact TeV accelerator planned to operate in the C-band frequency of 5.712 GHz to produce Higgs bosons. A load prototype was manufactured in two halves using PBF-LB/M to eliminate the need for internal support and ease the removal of excess powder at the end of the process. The printed parts were then welded together, and vacuum FIG. 24. (a) CAD model, (b) cross section showing the spiralized waveguide and vacuum pumping holes, and (c) photograph of additively manufactured spiral rf load [209]. FIG. 25. (a) Photograph of additively manufactured spiral rf showing the supports and (b) CAD model of the novel design developed for mass production [213]. TOBIA ROMANO et al. PHYS. REV. ACCEL. BEAMS 27, 054801 (2024) 054801-20 pump port was added (Fig. 26). Preliminary cold tests conducted before and after welding operations displayed an increase in the S11 value from −38.7dB to −25.1. The load underwent initial conditioning with 200 ns pulses up to 8 MW power and 20 Hz repetition rate. The pulse width was then increased up to 700 ns during high-power testing, demonstrating the load’s capability to terminate a peak power of 8.1 MW. However, further testing with 1000 ns pulses could not be completed due to significant heating of the outer turns of the spiral and loss of vacuum pressure. Future design improvements include the integration of cooling channels and the optimization of waveguide geometry to enhance heat dissipation and prevent local loss concentrations. D. Beam instrumentation and diagnostics In recent years, AM has been used to manufacture prototypes and functional instruments employed in the management and characterization of particle beams in accelerators. In 2012, Veness et al. [216] suggested integrating AM in the fabrication route of advanced wire scanners to be installed in the pre-injectors of the LHC, aiming for high scanning speeds while providing high position and time accuracy [217]. They devised a novel design for the wire-supporting forks, considering stiffness requirements to keep the wire under tension and minimize vibrations during motion across the beam. Topological optimization of the fork geometry was also conducted to minimize its mass, thus reducing the inertial load on the motor during wire acceleration and deceleration phases [Figs. 27(a) and 27(b)]. The first prototype, printed in Ti6Al4V alloy using PBF-LB/M and postprocessed to machine precision details [Figs. 27(c) and 27(d)], was installed in the Super Proton Synchrotron (SPS) ring in 2015 [218]. Over the following 2 years, slightly different designs were developed to produce wire-supporting forks for the proton synchrotron booster (PSB) and the proton synchrotron, each tailored to the specific aperture of the machine [219]. The cost of each printed fork [Fig. 27(e)] was ∼35% of the conventionally manufactured counterpart. The economic advantages associated with AM were also emphasized by Jenzer et al. [220] in the production of a stripline beam position monitor (BPM). The standard manufacturing routes typically involve welding together four different parts. However, the subsequent machining of the thin cylindrical striplines [Fig. 28(a)] poses significant challenges. On the other hand, thin-walled devices were readily fabricated by PBF-LB/M using a 316L stainless steel powder. The shape of the flange was topologically optimized to allow the fabrication of the BPM in a single print cycle without the need for support structures (Figs. 28(b)–28(d)). Since no additional space was needed for welding the flanges onto the BPM body, the part length could be reduced by 20 mm [Figs. 28(a) and 28(b)], resulting in a weight reduction of ∼40% compared to the original design. The design improvements enabled by the flexibility of PBF-LB/M process approximately halved the production costs and reduced lead times by a factor of 3. Following preliminary Lambertson and stretched wire tests, which demonstrated performance comparable to the reference component, a triplet comprising of two conventionally manufactured BPM and the additively manufactured BPM in between was installed in the PHIL (Photo-Injecteur au LAL) accelerator beam line [Fig. 28(e)]. All BPMs exhibited similar accuracy in position measurements during tests with 3.5 MeV beam energy [221]. PBF-LB/M was also employed by Grazzi et al. [222] to produce the exit snout of the MACHINA (Movable Accelerator for Cultural Heritage In-situ Non-destructive Analysis) transportable particle accelerator, which was installed on the beamline to extract the beam into the atmosphere. The exit snout design comprised two hollow focusing elements with a conical shape intersecting at the extraction window, as shown in Fig. 29. FIG. 26. Additively manufactured spiral rf load, with the inner structure shown in the inset [206]. FIG. 27. (a) Topological optimization, (b) finite element analysis, (c) as-built, and (d) postprocessed wire scanner forks made by PBF-LB/M [218], and (e) series of printed forks with different geometries [219]. METAL ADDITIVE MANUFACTURING …PHYS. REV. ACCEL. BEAMS 27, 054801 (2024) 054801-21 As part of the SOLEIL synchrotron upgrade program, Tavakoli et al. additively manufactured compact crotch absorbers in CuCr1Zr alloy to be inserted downstream of the dipoles [Fig. 30(a)][223]. Cooling channel optimization allowed reducing the maximum temperature by more than 30 °C compared to the conventional absorber design. In another study, Sinico et al. [224] prototyped a copper beam dump using PBF-LB/M. The device served to stop the proton beam at the end of a cyclotron beamline and dissipate the generated heat. It comprised a bulky disc with one face to be exposed to the beam and the other accommodating a cooling system. The cooling system, featuring a spiral geometry for water circulation, was printed using a pure copper powder on a build platform also made of copper, which served as the beam dump front [Figs. 30(b) and 30(c)]. A spiral channel configuration was also integrated into the PROTAD targets for antiproton production developed within the RaDIATE collaboration at CERN [225,226]. These targets consisted of a Ta/Ir core embedded in a matrix of expanded graphite and encapsulated in a double wall assembly with an internal spiral channel for compressed air cooling, which was manufactured by PBF-LB/M using a Ti6Al4V powder. Chan et al. [227] adopted a similar approach to develop a compact target holder design for the IBA Cyclone®18=18 cyclotron, incorporating an internal cooling system for water circulation [Figs. 30(d) and 30(e)]. The sterling silver prototype fabricated by PBF-LB/M exhibited ∼60% higher cooling FIG. 28. Drawings of the (a) standard BPM and (b) topologically optimized design with (c) 3D CAD model, (d) photograph of BPM prototype made by PBF-LB/M [220], and (e) BPM triplet installed in PHIL accelerator [221]. FIG. 29. (a) CAD model and (b) photograph of the additively manufactured beam exit snout of the MACHINA transportable accelerator [222]. FIG. 30. (a) Additively manufactured crotch absorbers, (b) CAD design and (c) photograph of copper beam dump made by PBF-LB/ M[224], (d) photograph of target assembly of the IBA Cyclone®18=18 cyclotron with (e) detail of the internal cooling system of the additively manufactured target holder [227], and (f) cylindrical magnetic shielding structures made by PBF-LB/M [149]. TOBIA ROMANO et al. PHYS. REV. ACCEL. BEAMS 27, 054801 (2024) 054801-22 efficiency compared to the standard target system, thereby enabling higher target currents. Additionally, the novel design allowed moving the target material closer to the exit port of the cyclotron, significantly reducing the beam losses caused by divergence. PBF-LB/M was also employed by Vovrosh et al. [149] to fabricate cylindrical magnetic shielding components with a compact and lightweight design that could be tailored to the specific structure to be shielded [Fig. 30(f)]. The as-printed permalloy samples exhibited a preferential grain orientation along the Ni hard axis [100] resulting from the layer-wise fabrication, which negatively impacted the shielding properties of the material. HIP and annealing treatments mitigated this microstructural anisotropy, increasing the shielding factors (ratio between nonshielded magnetic field amplitude and residual field amplitude after field installation) to ∼150 and ∼260, respectively. E. Vacuum devices A variety of components is employed in particle accelerator facilities to provide the UHVenvironment required for their operation. These include, for example, gates, valves, seals, pumps, and other equipment essential for achieving and maintaining low-pressure levels [147]. Vacuum devices are often custom-made and produced in limited batches, employing sophisticated routes that involve multipart assembly operations and often result in high manufacturing costs. AM’s inherent ability to create complex monolithic structures can help overcome these challenges [147]. Vovrosh et al. [149] demonstrated the possibility of using PBF-LB/M to manufacture UHV components made of Ti6Al4V alloy. They fabricated a test piece with a top hat profile and sealed it to a DN40CF flange using an indium wire [Figs. 31(a) and 31(b)]. The assembly was installed in an ion pump with triode configuration, with an additional reference branch equipped with a standard flange for comparison purposes [Fig. 31(c)], and the setup was baked out at 130 °C for 160 h. An ultimate pressure of 5×10−10 mbar was achieved at both the test and reference branches, with an outgassing rate of ∼4×10−12 mbar l s−1cm−2. It should be noted that the contact surface of the additively manufactured flange was milled before the indium sealing operation, while the inner walls were left in as-built conditions. This aligns with findings from other researchers, confirming that machining the inner surfaces of additively manufactured components is not strictly required to ensure vacuum tightness. Jenzer et al. [228] reported that 316L stainless steel DN40KF tubes made by PBF-LB/M [Fig. 32(a)] displayed a vacuum performance comparable with commercial products once machining the knife-edge seals, but leaving the internal walls unaltered. In another study, Cooper et al. [148] manufactured an AlSi10Mg vacuum chamber by PBF-LB/M [Fig. 32(b)] and tested it in a UHV setup [Fig. 32(c)] without further machining operations, except at the mating surfaces between the printed chamber and the components of the experimental apparatus. The chamber design comprised multiple conflat flange ports and integrated a gyroid lattice on the external surface to enhance the stiffness of the thin walls. Following a 120 °C bakeout of 120 h, the assembly was pumped down using a NEG combination ion pump, achieving an ultimate pressure of ∼10−10 mbar and maintaining it for more than 2 h without active pumping. Because of the high system complexity, a precise outgassing rate could not be determined, but its upper limit was estimated to be ∼10−13 mbar l s−1mm−2. Results from spectrometry and spectroscopy analyses attributed the good outgassing performance to the formation of a Mg-rich oxide layer on the material surface, capable of withstanding temperatures up to 350 °C and reducing the release of volatile species. An additively manufactured vacuum chamber was also showcased by Wolf et al. [229], who integrated a system of FIG. 31. (a) 3D model and (b) photograph of vacuum flange assembly with additively manufactured Ti6Al4V test piece and (c) schematic diagram of the experimental setup for vacuum testing [149]. FIG. 32. (a) Additively manufactured DN40KF tubes [228], (b) vacuum chamber, and (c) UHV test setup [148]. METAL ADDITIVE MANUFACTURING …PHYS. REV. ACCEL. BEAMS 27, 054801 (2024) 054801-23 flow channels into the cavity walls to facilitate heating during evacuation phase and cooling when needed during operation (Fig. 33). The design flexibility of AM was also leveraged by Du et al. [230] in developing a stiffening cage to be integrated into the thin-walled dipole-magnet vacuum chambers of the Booster Ring accelerator [Fig. 34(a)]. Two cover panels were added to the initial cage design [Figs. 34(b) and 34(c)] to mitigate beam coupling impedance, affecting beam quality and causing instabilities during high-intensity operation. F. Heat exchangers and cooling systems As demonstrated by the implementation of cooling systems into several accelerator components already discussed, typical applications that greatly leverage the opportunities offered by the design freedom of AM are represented by thermal management devices. Topological optimization can be harnessed to design components with improved heat transfer efficiency, for instance, by integrating intricate structures providing a large surface area for heat dissipation [38]. Of particular interest is the exploration of innovative heat exchanger designs incorporating triply periodic minimal surface (TPMS) structures, such as gyroids and lidinoids, which provide separated interpenetrating channels for efficient heat transfer between fluids at different temperatures [231]. In 2015, within the framework of the LIEBE project, Delonca [232] developed a novel design for Pb-Bi/water heat exchangers and employed PBF-LB/M to manufacture the first prototypes. In another investigation, Sciacca et al. [233] proposed three different heat sink configurations to be embedded in the backside of compact isotopeenriched targets used in the production of radionuclides for nuclear medicine. Two configurations consisted of lattice structures with different cell orientations relative to the inlet coolant flow, while the third configuration comprised individual helical twisted channels [Figs. 35(a) and 35(b)]. The prototypes were manufactured using PBFLB/M with pure copper powder [Fig. 35(c)]. During experimental tests conducted in an in-house designed setup, all the samples exhibited good performance, with heat transfer coefficients exceeding 19 kW m−2K−1.The higher dissipation capacity shown by the heat sink with the third configuration was attributed to the generation of vortices and secondary flows inside the twisted channels. Zhang et al. [234] also demonstrated the capability of topologically optimized cooling channels to reduce hot spot temperature (by ∼24 °C)in704.4MHzCHcopper cavities made by PBF-LB/M [Figs. 35(d)–35(f)], in comparison with the original design featuring nonconformal channels. VI. SURFACE QUALITY IMPROVEMENT FOR ADDITIVELY MANUFACTURED ACCELERATOR COMPONENTS The poor surface quality typically found in additively manufactured parts is a major concern for the application of AM in particle accelerators, as it is generally associated with limited UHV compatibility, sparse rf properties, and low breakdown strength. Moreover, because of their peculiar surface characteristics in both as-printed and postprocessed conditions, it remains uncertain whether established models and characterization techniques can reliably predict the performance of accelerator components produced by AM. For instance, Mayerhofer et al. [9] observed that the rf conductivity of additively manufactured linac cells surprisingly was not affected by the wavy pattern that appeared on their surface as a result of finishing operations, because its characteristic wavelength was much larger than the skin depth. Additionally, they noticed that the cell Q-factor could not be accurately predicted using classic gradient and Hammerstad models based on the measured root-mean-square roughness (Sq) values, suggesting the need to employ alternative measurement settings compared to those typically used for the assessment FIG. 33. (a) CAD model with (b) internal flow channels, and (c) photograph of the additively manufactured vacuum chamber after welding of standard vacuum components [229]. FIG. 34. CAD models of (a) thin-walled dipole-magnet vacuum chamber with internal stiffening cage, (b) initial cage design, and (c) cage design with additional cover panels for coupling impedance reduction [230]. TOBIA ROMANO et al. PHYS. REV. ACCEL. BEAMS 27, 054801 (2024) 054801-24 of conventionally manufactured rf structures. Khan et al. [235] also showed that the typical surface roughness of part made by PBF-LB/M exceeds the applicability range of the Groiss model, a modified version of the Hammerstad model for the prediction of the Q-factor of rf cavity resonators. On the other hand, the one-ball Hurey model, in which the surface is described as a nonuniform distribution of spheres of different sizes, provided more accurate predictions for both the Q-factor and the resonant frequency. In another study, Zhang et al. [234] highlighted the limitations of considering only macroscopic roughness when evaluating the performance of components subjected to intense electromagnetic fields, neglecting the major role played by nanoscale surface protrusions in promoting vacuum breakdown. Regarding postprocessing methods, the applicability of conventional milling is restricted to relatively simple geometries accessible to the machining tools. More sophisticated postprocessing methods have been developed to enhance the surface quality of more complex parts [156–159], with some of them already applied to accelerator component prototypes produced by AM. A. Mechanical treatments Mechanical surface treatments rely on the use of abrasive media to remove or plastically deform the outer layer of material containing the peaks and valleys that contribute to surface roughness, leaving behind a smoother appearance [139]. These methods include, among others, various polishing and tumble finishing techniques [159]. Horn et al. [210] employed a magnetically driven polishing technique to reduce the roughness of the inner surface of a WR10 waveguide produced with PBF-EB. The waveguide was filled with a paste containing magnetic particles mixed with silicon carbide and alumina abrasive particles. An external magnet guided the magnetic particles along the workpiece, inducing the movement of the abrasive media. This process removed the asperities from the surface profile, reducing the average roughness from 36 to 5μm after 10,000 polishing cycles, during which four types of abrasive media with progressively decreasing sizes were used. Torims et al. [199] employed conventional and chemically assisted tumble finishing to enhance the surface quality of RFQ prototypes manufactured using PBF-LB/ M. During the process, the workpieces were inserted into a barrel containing water and proprietary abrasive media and compounds provided by Rösler Italiana S.r.l. The finishing effect was achieved through the relative motion between the parts and the abrasive media inside the barrel [159]. A commercial MMP TECHNOLOGY®mechanicalphysical-catalytic treatment was also tested. All procedures successfully met the requirement for average surface roughness (Ra<0.4μm). However, conventional finishing required a longer processing time and was less effective in removing deep valleys on the part surface, as mechanical abrasion mainly acted on protruding features. This challenge was not faced by the chemically assisted and MMP TECHNOLOGY®processes, which easily removed a relatively thick layer of material containing all surface defects. In addition to conventional tumble finishing, Candela et al. [184] employed an internally developed vibrotumbling process to smooth the inner surface of copper rf cavities made by PBF-LB/M. In the vibro-tumbling system [Fig. 36(a)], the cavity is gripped at the two ends and set into vibration by an eccentric vibrating motor [236]. 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