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Fragility Analysis of the Reactor Steel Shaft Door Due to Accidental Extreme Overpressure

Králik, Juraj

Abstract

This paper describes the probabilistic nonlinear analysis of the hermetic steel door of the reactor shaft failure due to extreme pressure and temperature. The probabilistic assessment of NPP structures for Probabilistic Safety Analysis (PSA2) level 2 of VVER 440/213 in the case of the technology accidents is presented. The scenario of the hard accident in nuclear power plant (NPP) and the methodology of the calculation of the fragility curve of the failure overpressure using the probabilistic safety assessment PSA 2 level is presented. The nonlinear deterministic and probabilistic analysis based on the response surface method (RSM) were considered.

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SECTION BUILDING STRUCTURES & STRUCTURAL MECHANICS VOLUME: 23 | NUMBER: 2 | 2023 | DECEMBER © 2023 VSB - TECHNICAL UNIVERSITY OF OSTRAVA FACULTY OF CIVIL ENGINEERING 5 FRAGILITY ANALYSIS OF THE REACTOR STEEL SHAFT DOOR DUE TO ACCIDENTAL EXTREME OVERPRESSURE Ju aj KRÁLIK 1 , Joze BOČKAJ 1 1 Ins i u e o Fo ensic Enginee ing, Facul y o Ci il Enginee ing, Slo ak Uni e si y o Technology, Radlinského 11, 810 05 B a isla a, Slo akia ju aj.k alik@s uba.sk, joze .b[email p o ec ed]k DOI: 10.35181/ ces-2023-0008 Abs ac . This pape desc ibes he p obabilis ic nonlinea analysis o he he me ic s eel doo o he eac o sha ailu e due o ex eme p essu e and empe a u e. The p obabilis ic assessmen o NPP s uc u es o P obabilis ic Sa e y Analysis (PSA2) le el 2 o VVER 440/213 in he case o he echnology acciden s is p esen ed. The scena io o he ha d acciden in nuclea powe plan (NPP) and he me hodology o he calcula ion o he agili y cu e o he ailu e o e p essu e using he p obabilis ic sa e y assessmen PSA 2 le el is p esen ed. The nonlinea de e minis ic and p obabilis ic analysis based on he esponse su ace me hod (RSM) we e conside ed. Keywo ds Ansys, agili y, he me ic doo , nuclea sa e y, nonlinea analysis, p obabili y, PSA, RSM, echnology acciden . 1. In oduc ion The IAEA (In e na ional A omic Ene gy Agency) in Vienna [1] adop ed a la ge-scale p ojec "S ess Tes s o NPP", which de ines new equi emen s o he e i ica ion o he sa e y and eliabili y o NPP due o he acciden o NPP in Fukushima. Based on he ecommenda ions o he IAEA in Vienna [1], he p obabilis ic me hodology o he sa e y and eliabili y o he NPP s uc u es was accep ed o he p oblem o he sa e y o he c i ical s uc u es. The sa e y documen s o NRC [2], [3] and IAEA [1] ini ia e he equi emen s o e i y he he me ic s uc u es o NPP loaded by wo combina ions o he ex eme ac ions. Fi s ex eme loads a e conside ed o he p obabili y o exceedance 10-4 by yea and second o 10-2 by yea . O he ac ion e ec s a e conside ed as he cha ac e is ic loads du ing he acciden . In he case o he loss-o -coolan acciden (LOCA) he s eam p essu e expands om he eac o hall o he bubble condense [4]. The eac o and he bubble condense ein o ced s uc u es wi h s eel line a e he c i ical s uc u es o he NPP he me ic zone [4]. Nex , one om he c i ical echnology s uc u es a e he eac o he me ic co e s and doo s. Fig. 1: Sec ion plane o he NPP wi h eac o VVER440/213. The NPP wi h he eac o VVER440 consis o ou buildings – eac o building, leng hwise side building, c oss side building and u bine hall (Fig.1). The FEM model o he NPP was c ea ed in he so wa e ANSYS. Fig. 2: Scheme o he sa e y sys em o he he me ic zone. On he base o he global analysis o he sa e y o he NPP s uc u es unde he echnology acciden in SECTION BUILDING STRUCTURES & STRUCTURAL MECHANICS VOLUME: 23 | NUMBER: 2 | 2023 | DECEMBER © 2023 VSB - TECHNICAL UNIVERSITY OF OSTRAVA FACULTY OF CIVIL ENGINEERING 6 acco dance wi h he in e na ional s anda ds [1], [5] he de ailed analysis o he he me ic co e , p o ec i e hood, and doo s. The sa e y scheme o he he me ic doo s and he he me ic zone a e p esen ed in Fig.2. The nonlinea analysis and he ull p obabilis ic analysis we e used as he inpu da a o he nex isk analysis o he NPP s uc u es in acco dance wi h he in e na ional s anda ds. Tab.1: The assumed scena ios o he acciden s in he he me ic zone The Commission NRC [2] uses he p obabilis ic isk assessmen (PRA) o es ima e isk by compu ing eal numbe s o de e mine wha can go w ong, how likely is i , and wha a e i s consequences. Thus, PRA p o ides insigh s in o he s eng hs and weaknesses o he design and ope a ion o a nuclea powe plan . Fo he ype o NPP a PRA can es ima e h ee le els o isk: • A Le el 1 PRA es ima es he equency o acciden s ha cause damage o he nuclea eac o co e. This is commonly called co e damage equency (CDF). • A Le el 2 PRA, which s a s wi h he Le el 1 co e damage acciden s, es ima es he equency o acciden s ha elease adioac i i y om he nuclea powe plan . • A Le el 3 PRA, which s a s wi h he Le el 2 adioac i i y elease acciden s, es ima es he consequences in e ms o inju y o he public and damage o he en i onmen . The de ini ion o he agili y cu e o NPP gene ally ep esen s a c ucial s ep o he le el 2 p obabilis ic sa e y assessmen (PSA2), whe e he p obabili y o s uc u e ailu e can be e alua ed as he con olu ion o he agili y cu e wi h he load cu e. The assessmen o he s uc u al s eng h o he nuclea powe plan has acqui ed e en a g ea e impo ance in he amewo k o pos -Fukushima s ess es s whe e he assessmen o he sa e y ma gin and o -design condi ions [6]. 2. Scena io o he echnology acciden The p e ious analysis was achie ed o he o e p essu e alue o 100kPa due o design basic acciden (DBA), which co esponds o he loss o coolan acciden due o guillo ine cu ing o he coolan pipe [4]. When he ba bo age owe ope a es in he pa ial o ze o pe o mance he o e p essu e is equal o he 150 - 300 kPa. The ENEL p opose he maximum empe a u e in he eac o sha is equal abou o 1.800oC and in he con ainmen a ound he eac o sha is equal abou o 350oC [4]. The possibili y o he empe a u e inc easing o he con ainmen ailu e s a e is conside ed in he scena io oo. In he case o he ha d acciden he o e p essu e can be inc eased linea ly, and he in e nal and ex e nal empe a u e a e cons an . Th ee ypes o he scena ios we e conside ed (Tab.1). The c i ical was he acciden du ing 7 days wi h he o e p essu e 250kPa, in e nal empe a u e 150oC and ex e nal empe a u e -28oC. 3. Calcula ion model The echnology segmen s o he NPP he me ic zone a e made om he s eel. The he me ic s eel doo s ype A262 (wi h dimension 1600/900/150 mm) a e loca ed a he eac o sha . The s eel doo s ul il bo h he sealing and shielding unc ions. The echnology segmen s o he NPP he me ic zone a e made om he s eel (S235). Fig. 3: Scheme o he eac o sha he me ic doo - ype A262. Fig. 4: FEM model o he eac o sha he me ic doo . The s eel doo is i ed in he ame cas in conc e e and Type Du a ion O e p essu e in HZ [kPa] Ex eme empe a u es [oC] I. 1hou - 1day 150 127 II. 2hou s - 7days 250 150 III. 1yea - 80 - 120 SECTION BUILDING STRUCTURES & STRUCTURAL MECHANICS VOLUME: 23 | NUMBER: 2 | 2023 | DECEMBER © 2023 VSB - TECHNICAL UNIVERSITY OF OSTRAVA FACULTY OF CIVIL ENGINEERING 7 sealed o he ame wi h double ubbe packing o 150 mm in wid h. The FEM model o he he me ic s eel doo is shown in Fig.4. The de ailed FEM model has 199.469 SOLID185 and CONTA173 elemen s. 4. Accep ance c i e ia In he case o he nonlinea analysis he he mal depended ma e ial p ope ies a e used ollowing he inpu da a o ma e ial 08CH18N10T de ined in s anda d CSN 413240, CSN 411700, CSN 413230, CSN 413240 and NTD SAI Sec ion II. The c i e ion o he max. s ess alues is limi ed by he H-M-H plas ic po en ial [4], [8] and [9]. The ailu e o he s eel s uc u e is limi ed by he max. s ain alues o by he s abili y o he nonlinea solu ion [10] and [11]. The s anda d STN EN 1993 1-2 [9] de ine ollowing cha ac e is ic alues o he s ain o he s uc u al s eel : - yield s ain , 0.02 ay    - ul ima e s ain , 0.15 au    - max. limi s ain , 0.20 ae    Fig. 5: S ess-s ain ela ionship o he s eel dependen on empe a u e. The s ess-s ain ela ionship o he s eel (Fig.5) a e conside ed in acco dance wi h Eu ocode [9] and [10] on dependency o empe a u e le el o hea ing a es be ween 2 and 50K/min. In he case o he s eel he s ess-s ain diag am is di ided on ou egions. The s ess-s ain ela ions a e de ined in ollowing o m in egion I:   2 2 ,,,aay aya b c a a      , (1)  2 ,,,, ,ay ap ay ap a acE      ,  22 ,, ,aay ap bE cc     ,   2 ,, ,, , , , 2 ay ap aay ap ay ap cE         . and in egion III: ,,aay    . (2) 5. Nonlinea analysis The nonlinea analysis based on po en ial heo y conside ing he iso opic ma e ial p ope ies was made o he solid elemen s SOLID185 and CONTA173 elemen s [8] in he FEM model. The s eel is ypical iso opic ma e ial. The elas ic- plas ic beha iou o he iso opic ma e ials is desc ibed by he HMH yield c i e ion [8]. Consequen ly, he s ess-s ain ela ions a e ob ained om he ollowing ela ions:        pl el el Q dDdd Ddd            , (3) whe e ep D   is elas ic-plas ic ma ix in he o m :     T ee ep e T e QF DD DD FQ AD                   . (4) The ha dening pa ame e A depends on he yield unc ion and model o ha dening (iso opic o kinema ic). Hube -Mises-Hencky (HMH) de ine he yield unc ion in he o m:  eq T  , (5) whe e eq  is equi alen s ess in he poin and   o   is yield s ess depends on he ha dening. In he case o kinema ic ha dening by P age ( e sus Ziegle ) and he ideal Bauschinge ’s e ec is gi en 2 2 9 T AH E    . (6) The ha dening modulus H’ o his ma e ial is de ined in he o m: eq T pp eq eq dd Hdd    . (7) When his c i e ion is used wi h he iso opic ha dening op ion, he yield unc ion is gi en by:      0 T oep FM    , (8) whe e   oep is he e e ence yield s ess,  ep is he equi alen plas ic s ain and he ma ix [M] is diagonal. On he base o he elas ic-plas ic heo y and he HMH unc ion o plas ici y he ex eme s ain and s ess o he SECTION BUILDING STRUCTURES & STRUCTURAL MECHANICS VOLUME: 23 | NUMBER: 2 | 2023 | DECEMBER © 2023 VSB - TECHNICAL UNIVERSITY OF OSTRAVA FACULTY OF CIVIL ENGINEERING 8 eac o he me ic doo o he acciden scena io ype II we e calcula ed. The ma ix [M] is de ined as ollows:  100000 010000 001000 000200 000020 000002 M           . (9) 6. P obabili y nonlinea assessmen The p obabilis ic me hods a e e y e ec i e o analyze o he sa e y and eliabili y o he s uc u es conside ing he unce ain ies o he inpu da a [11], [12], [13], [14], [15], [16], [17], [18], [19], [20], [21], [22] and [23]. The p obabili y analysis o he loss o he eac o co e in eg i y was [4], made o he o e p essu e loads om 250 kPa o 7000 kPa using he nonlinea solu ion o he s a ic equilib ium conside ing he geome ic and ma e ial nonlinea i ies o he s eel shell and beam elemen s. The p obabili y nonlinea analysis o he echnology segmen s is based on he p oposi ion ha he ela ion be ween he inpu and ou pu da a can be app oxima ed by he app oxima ion unc ion in he o m o he polynomial [7, 8]. The ull p obabilis ic assessmen was used o ge he p obabili y o echnology segmen ailu e. The sa e y o he echnology segmen s was de e mined by he sa e y unc ion SF in he o m [10] SF E R and 01SF, (10) whe e E is he ac ion unc ion and R is he esis ance unc ion. The eliabili y unc ion RF is de ined in he o m:  ,1 0RF g R E SF R E , (11) whe e  , g RE is he eliabili y unc ion. The p obabili y o ailu e can be de ined by he simple exp ession:    0 PPREPRE    . (12) The eliabili y unc ion RF can be exp essed gene ally as a unc ion o he s ochas ic pa ame e s X1, X2 o Xn, used in he calcula ion o R and E. 12 ( , ,..., ) n RF g X X X. (13) The ailu e unc ion g({X}) ep esen s he condi ion (capaci y ma gin) o he eliabili y, which can be ei he an explici o implici unc ion o he s ochas ic pa ame e s and can be single (de ined on one c oss-sec ion) o complex (de ined on se e al c oss-sec ions, e.g., on a complex ini e elemen model). In he case o he nonlinea analysis he co ec solu ion o he elas ic-plas ic beha io o he s uc u es is de e mined by he unc ion plas ici y. The HMH unc ion o he plas ici y was used o he nonlinea solu ion o he s eel echnology segmen s. This plas ici y unc ion is de ined in he o m: y R  and e E  , (14) whe e he e ec i e s ess e  (Von Mises s ess) is de ined as ollows  1 2 222 12 21 31 1 2 e        . (15) The ailu e o he s eel echnology segmen s in he ame o he PSA analysis is de ined by he ul ilimi e alues o he maximal s ain de o ma ion. This ailu e unc ion is de ined in he o m: ,ay R    and e E  , (16) whe e he e ec i e s ain e  (Von Mises s ain) is de ined as ollows  1 2 222 12 21 31 11 12 e          , (17) whe e   is he e ec i e Poisson cons an . The ailu e p obabili y is calcula ed om he e alua ion o he s a is ical pa ame e s and heo e ical model o he p obabili y dis ibu ion o he eliabili y unc ion Z = g(X) using he simula ion me hods. The ailu e p obabili y is de ined as he bes es ima ion on he base o nume ical simula ions in he o m:  1 10 N i i pIgX N    , (18) whe e N in he numbe o simula ions, g(.) is he ailu e unc ion, I[.] is he unc ion wi h alue 1, i he condi ion in he squa e b acke is ul illed, o he wise is equal 0. The ull p obabilis ic analysis esul om he nonlinea analysis o he se ies simula ed cases conside ed he unce ain ies o he inpu da a. The a ious simula ion me hods (di ec , modi ied o app oxima ion me hods) can be used o he conside a ion o he in luences o he unce ain y o he inpu da a [4]. In case o he nonlinea analysis o he ull FEM model he app oxima ion me hod RSM (Response su ace me hod) is he mos e ec i e me hod [8]. The RSM me hod assumes ha i is possible o de ine he dependency be ween he a iable inpu and he ou pu da a h ough he app oxima ion unc ions in he ollowing o m: 1 2 11 1 NNNN oiiiii ijij ii iji Yc cX cX cXX         , (19) whe e co is he index o he cons an membe ; ci a e he indices o he linea membe and cij he indices o he SECTION BUILDING STRUCTURES & STRUCTURAL MECHANICS VOLUME: 23 | NUMBER: 2 | 2023 | DECEMBER © 2023 VSB - TECHNICAL UNIVERSITY OF OSTRAVA FACULTY OF CIVIL ENGINEERING 9 quad a ic membe , which a e gi en o p ede e mined schemes o he op imal dis ibu ion o he a iables o o using he eg ession analysis a e calcula ing he esponse. App oxima e polynomial coe icien s a e gi en om he condi ion o he e o minimum, usually by he "Cen al Composi e Design Sampling" (CCD) me hod o he "Box- Behnken Ma ix Sampling" (BBM) me hod [8]. On base o expe imen al design, he unknown coe icien s a e de e mined due o he andom a iables selec ed wi hin he expe imen al egion. The unce ain y in he andom a iables can be de ined in he model by a ying in he a bi a y amoun p oducing he whole expe imen al egion. The o al ec o o he de o ma ion pa ame e s { s} in he FEM is de ined o he s h-simula ion in he o m:       1 ,,,, sGNs ssss KEF FGQPT     , (20) and he s ain ec o     s ss B  , (21) whe e   GN K is he nonlinea s i ness ma ix depending on he a iable pa ame e s and s EF  , F is he HMH yield unc ion de ined in he s ess componen s,   F is he ec o o he gene al o ces depending on he a iable pa ame e s ,,and s ss s GQP T o he s h-simula ion. 7. Unce ain ies o he inpu da a The unce ain ies a e coming om he ollowing sou ces [4], [7], [10] and [14]:  Pa ame e s o ma e ial p ope ies. Based on expe imen s wi h conc e e elemen s he s anda d de ia ion is 11.1%. In case o o he ma e ials his alue is abou 5%.  Assessmen o mechanical cha ac e is ics e o ac o s a e abou 8-12%, i depends on he cons uc ion ma e ial di e ences used o he di e en uni s wi h VVER 440/213. In some cases, i can be conse a i e, in o he cases non-conse a i e impac .  Unce ain ies in he nume ical esul s in he alue o 10-15%. In his a ea we can ake in o conside a ion he s eel line wi h he conc e e elemen s.  Unce ain ies a ising om he empe a u es impac in he alue o 10%.  O he calcula ions assump ions 3-5%. The mean alues and s anda d de ia ions we e de ined in acco dance o he expe imen al es and design alues o he ma e ial p ope ies and he ac ion e ec s [6 and 8] (see Tab.3). Based on he esul s om he simula ed nonlinea analysis o he echnology segmen s and he a iabili y o he inpu pa ame e s 106 Mon e Ca lo simula ions we e pe o med in he sys em ANSYS [8]. Tab.2: Va iabili y o inpu pa ame e s. Quan i y Cha ac . alue Va ia ble Type Mean  De ia [%] Min. alue Max. alue Ma e ial S eng h F k a N 1.10 6.6 0.77 1.35 Ac ion e ec s Dead load G k g a N 1 5 0.81 1.20 Li e load Qk q a GU 0.64 22.6 0.23 1.36 P essu e LOCA p k p a N 1 8 0.70 1.33 Tempe a u e T k a GU 0.67 14.2 0.40 1.15 Model unce ain ies Ac ion E k e a N 1 5 0.81 1.19 Resis ance R k a N 1 5 0.81 1.20 8. P obabili y nonlinea analysis o he eac o doo The calcula ion o he p obabili y o he eac o doo ailu e is based on he esul s o he nonlinea analysis o a ious le el o he acciden p essu e and mean alues o he ma e ial p ope ies. The c i ical a ea o he echnology segmen s de ined om he nonlinea de e minis ic analysis a e he mechanical closu es. The CCD me hod o he RSM app oxima ion is based on 45 nonlinea simula ions depending on he 6 a iable inpu da a. The nonlinea solu ion o he one simula ion consis s abou he 50 o 150 i e a ions depending on he scope o he plas ic de o ma ions in he calcula ed s uc u es. The sensi i i y analysis gi es us he in o ma ion abou he in luences o he a iable p ope ies o he inpu da a o he ou pu da a. These analyses a e based on he co ela ion’s ma ixes. 9. F agili y cu es o ailu e p essu e The PSA app oach o he e alua ion o p obabilis ic p essu e capaci y in ol es limi s a e analyses [4], [7], [10] and [11]. The limi s a es should ep esen possible ailu e modes o he con inemen unc ions. The con ainmen [4] may ail a di e en loca ions unde di e en ailu e modes. Conside wo ailu e modes A and B, each wi h n agili y cu es and espec i e p obabili ies pi (i = 1,…, n) and qj (j = 1,…, n). Then he union C = AB, he agili y FCij (x) is gi en by           Cij Ai Bj Ai Bj F xFxFxFxFx, (22) whe e he subsc ip s i and j indica e one o he n agili y cu es o he ailu e modes and x deno e a speci ic alue o he p essu e wi hin he con ainmen . The p obabili y pij associa ed wi h agili y cu e FCij.(x) is gi en by pi. qj i he median capaci ies o he ailu e modes a e independen . The esul o he in e sec ion e m in (22) is FAj(x), FBj(x) when he andomness in he ailu e mode capaci ies is independen and min [FAi.(x), FBj.(x)] when he ailu e SECTION BUILDING STRUCTURES & STRUCTURAL MECHANICS VOLUME: 23 | NUMBER: 2 | 2023 | DECEMBER © 2023 VSB - TECHNICAL UNIVERSITY OF OSTRAVA FACULTY OF CIVIL ENGINEERING 10 modes a e pe ec ly dependen . The ollowing is and he consequence o an acciden depends on he o al leak a ea. Mul iple leaks a di e en loca ions o he con ainmen (e.g., bellows, ha ch, and ai lock) may con ibu e o he o al leak a ea. Using he me hodology desc ibed abo e, we can ob ain he agili y cu es o leak a each loca ion. Fo a gi en acciden sequence, he induced acciden p essu e p obabili y dis ibu ion, h ( x ), is known. This is con ol ed wi h he agili y cu e o each leak loca ion o ob ain he p obabili y o leak om ha loca ion ( P Li) . I is unde s ood ha he e is no b eak o con ainmen up u e a his p essu e. Fig. 6: Family o agili y cu es showing modelling unce ain y.    0 1 Li b l phxFxFxdx     , (23) he e  b Fx is he agili y o b eak a he loca ion and  l Fx is he agili y o leak. The leak is o each loca ion speci ied as a andom a iable wi h a p obabili y dis ibu ion. The p obabili y o eac o co e ailu e is calcula ed om he p obabili y o he eliabili y unc ion RF in he o m, P = P ( RF < 0), (24) whe e he eliabili y condi ion RF is de ined depending on a conc e e ailu e condi ion , 1e a y RF    , (25) whe e he ailu e unc ion was conside ed in he o m (16). The agili y cu e o he ailu e p essu e was de e mined using 45 p obabilis ic simula ions using he RSM app oxima ion me hod wi h he expe imen al design CCD o 10 6 Mon e Ca lo simula ions o each model and 5 le el o he o e p essu e. The a ious p obabilis ic calcula ions o 5 cons an le el o o e p essu e nex o he a iable o e p essu e o gauss and uni o m dis ibu ion we e aken ou . The ailu e c i e ion o he s eel s uc u es using HMH (Von Mises) plas ic c i e ion wi h he mul ilinea kinema ic ha dening s ess-s ain ela ions o he a ious le el o he empe a u es and he deg ada ion o he s eng h we e conside ed. The unce ain y o he inpu da a ( ab.2) and he esul s o he nonlinea analysis o he echnological s uc u es o a ious le el o he acciden p essu e we e aken. Fig. 7: F agili y cu es o he s eel eac o sha doo . Fig. 8: F agili y cu es o he conc e e ame abou he eac o sha doo . The idealized agili y cu es o he eac o sha doo a e p esen ed in Fig.7. In case o he ein o ced s uc u e ame abou o he doo he idealized agili y cu es a e p esen ed in Fig.8. 10. Conclusion This epo is based on me hodology o he p obabilis ic analysis o s uc u es o he me ic zone o NPP wi h eac o VVER440/213 de ailed desc ibed in wo k [4]. The nonlinea p obabilis ic analysis o he eac o sha doo ailu e is in acco dance wi h he equi emen s IAEA [1] and NRC [2], expe iences om he simila analysis NPP in ab oad [21], new knowledges om he p obabilis ic analysis o s uc u es [7], [10], [11], [12], [14] and ou expe iences om he p e ious analysis [4]. These analyses go ou om he p e ious esul s o he moni o ing o ma e ial p ope ies [4], and NPP s uc u es, as well as om he esul s o he esis ance analysis o he impo an s uc u al componen s om he poin o he ini ia ed acciden s. The s uc u es we e analysed on impac o he ex eme load’s si ua ion de ined in he scena ios o he in e nal acciden s. Acco ding o he nonlinea de e minis ic analysis we e SECTION BUILDING STRUCTURES & STRUCTURAL MECHANICS VOLUME: 23 | NUMBER: 2 | 2023 | DECEMBER © 2023 VSB - TECHNICAL UNIVERSITY OF OSTRAVA FACULTY OF CIVIL ENGINEERING 11 de ined he mos c i ical s uc u al componen s o which he alues o he ailu e p essu e o he acciden a e de e mined on base o he bes es ima ion. We p opose om he supposi ion ha he loss o con ainmen in eg i y occu and he pe o mance o he NPP can be unsa e. The c i ical elemen s we e iden i ied aking in o conside a ion also unce ain ies o he inpu da a in he esul s. The nonlinea analysis o he loss o he con ainmen in eg i y was made o he o e p essu e loads om 250kPa using he nonlinea solu ion o he s a ic equilib ium conside ing he geome ic and ma e ial nonlinea i ies o he s eel shell and solid elemen s. The nonlinea analyses we e pe o med in he ANSYS p og am using he HMH plas ic condi ion [8]. The s anda d STN EN 1993 1-2 [9] de ine ollowing cha ac e is ic alues o he s ain o he s uc u al s eel - yield s ain and ul ima e s ain. The p obabili y analysis o he loss o he conc e e con ainmen in eg i y was made o he o e p essu e loads om 250kPa o 7.000kPa using he nonlinea solu ion o he s a ic equilib ium. The unce ain ies o he loads le el ( empe a u e, dead and li e loads), he ma e ial model o he s eel s uc u es as well as he inaccu acy o he calcula ion model and he nume ical me hods [4] we e conside ed in he app oxima ion RSM me hod o CCD expe imen al design and 106 Mon e Ca lo simula ions. This epo is based on he me hodology o he p obabilis ic analysis o s uc u es o he he me ic zone o NPP wi h eac o VVER44/213 de ailed desc ibed in he wo k [4]. The unce ain ies o he loads le el, he ma e ial model o he s eel s uc u es as well as he inaccu acy o he calcula ion model and he nume ical me hods we e conside ed in he app oxima ion RSM me hod o CCD expe imen al design and 106 Mon e Ca lo simula ions [7] and [8]. One om he c i ical echnology segmen s o he con ainmen is he he me ic s eel doo ype A252 wi h he ailu e p essu e pu.0,05 = 4.78MPa. The mean alue o p essu e capaci y o he s eel doo ype A252 is pu.0,50= 5.88MPa, he uppe bound o 95% is pu.0,95= 6.75Ma. These agili y cu es (Fig.7, 8) a e he inpu da a o he ollowing isk analysis o he NPP. Acknowledgmen s The p ojec was ealized wi h he inancial suppo o he G an Agency o he Slo ak Republic (VEGA). The p ojec egis a ion numbe is VEGA No. 1-0453-20. Re e ences [1] IAEA/TA-2488. Guidelines o WWER 440/213 Con ainmen E alua ion, TC P ojec RER/9/035, WWER-SC-l70, Rep. o Consul ans Mee ing, Vienna, augus 1996. [2] NRC, RG 1.200, An App oach o De e mining he Technical Adequacy o P obabilis ic Risk Assessmen Resul s o Risk-In o med Ac i i ies, U.S. Nuclea Regula o y Commission, Washing on, DC. 2009. [3] NUREG/CR-4839, Me hods o Ex e nal E en Sc eening Quan i ica ion: Risk Me hods In eg a ion and E alua ion P og am (RMIEP) Me hods De elopmen , Repo , Sandia Na ional Labo a o ies and U.S. Nuclea Regula o y Commission, 1992. [4] KRÁLIK, J. Risk Assessmen o NPP Sa e y in Case o Eme gency Si ua ions on Technology, In: Monog aph “Recen Imp o emen s o Powe Plan s Managemen and Technology”, Ed. A.B.Nikolic, Z.S.Janda, Pp. 69-96, Pub. INTECH, Sep . 2017, ISBN 978-953-51-3357-5. [5] ASME, Sec ion III, Di . 1, Appendix F, “Rules o E alua ion o Se ice Loadings wi h Le el D Se ice Limi s,” Ame ican Socie y o Mechanical Enginee s, 1998.NRA SR, The s ess es s o Nuclea Powe Plan s Slo akia, ÚJD B a isla a, Sep embe 2011. [6] HALDAR, A. S. MAHADEVAN, P obabili y, Reliabili y and S a is ical Me hods in Enginee ing Design, John Wiley & Sons, New Yo k, 2000. [7] KOHNKE, P. ANSYS, Theo y, SAS IP Inc. Canonsbu g, 2008. [8] STN EN 1993-1-2. Eu ocode 3: Design o s eel s uc u es. Pa 1-2 Gene al ules — S uc u al i e design. [9] HANBOOK 5. Implemen a ion o Eu ocodes Reliabili y Backg ounds. Design o Buildings o he Fi e Si ua ion. De elopmen o Skills Facili a ing Implemen a ion o Eu ocodes. Leona do Da Vinci Pilo P ojec CZ/02/B/F/PP-134007. P ague, CR, 2005. [10] MELCHERS, R. E. S uc u al Reliabili y: Analysis and P edic ion, John Wiley & Sons, Chiches e , 1999, U.K. [11] NOVÁK, D. e al. Small-sample P obabilis ic Asses- smen – so wa e FReET, ICASP 9, 9 h In e na ional Con e ence on Applica ions o S a is ics and P obabili y in Ci il Enginee ing, San F ancisco, USA, July 6-9, 2003, pp. 91-96. [12] NOVÁK, D. BERGMEISTER, K. PUKL, R. ČERVENKA, V., S uc u al assessmen and eliabili y analysis o exis ing enginee ing s uc u es, Theo e ical backg ound. S uc u e and in as uc u e enginee ing, Vol. 9, No. 2, 2009, pp. 267-275. [13] SÝKORA, M. M. HOLICKÝ, Assessmen o Unce ain ies in Mechanical Models, In: Applied Mechanics and Ma e ials, Vol. 378, pp 13-18, © TTP, Swi ze land, 2013. SECTION BUILDING STRUCTURES & STRUCTURAL MECHANICS VOLUME: 23 | NUMBER: 2 | 2023 | DECEMBER © 2023 VSB - TECHNICAL UNIVERSITY OF OSTRAVA FACULTY OF CIVIL ENGINEERING 12 [14] KALA, Z. Sensi i i y analysis o s eel plane ames wi h ini ial impe ec ions, Enginee ing S uc u es, 33, 8, pp.2342-2349, 2011. [15] KALA, Z. J. KALA, Sensi i i y Analysis o S abili y P oblems o S eel Columns using Shell Fini e Elemen s and Nonlinea Compu a ion Me hods, In p oc. Enginee ing mechanics 2011, 17 h In e na ional Con e ence, ISBN 978-80-87012-33-8, S a ka, 2011. [16] KONEČNÝ, P. e al. Towa ds Pa allel Compu ing using he Simula ion-based Reliabili y Assessmen Me hod. In. P oceedings o he Fi s In e na ional Con e ence on Pa allel, Dis ibu ed and G id Compu ing o Enginee ing, Ci il Comp P ess, p. 542-549. ISBN 978-1-905088-29-4, 2009. [17] KREJSA, M. J. KRÁLIK. P obabilis ic Compu a- ional Me hods in S uc u al Failu e Analysis, Jou nal o Mul iscale Modelling, Vol. 6, No. 2 (5 pages), Impe ial College P ess, DOI: 10.1142/S1756973715500067, 2015. [18] KREJSA, M. e al. P obabilis ic Calcula ion Using Pa allel Compu ing, In Enginee ing mechanics 2016, 22nd In e na ional con e ence. S a ka, ČR, 9. - 12. 5. 2016. 1s . ed. P ague, ITAM AS CR, 2016, p. 347- 350. ISSN 1805-8248. ISBN 978-80-87012-59-8. [19] KREJSA, M. e al. P obabilis ic a igue analysis o exis ing s eel s uc u e. In 4 h In e na ional Scien i ic Con e ence - SPACE 2019, EDP Sciences, Londyn, 2020, ISSN 2261-236X. [20] VEJVODA, S., KERŠNER, Z., NOVÁK, D. & TEPLÝ, B. P obabilis ic Sa e y Assessmen o he S eam Gene a o Co e , In P oc. o he 17 h In e na ional Con e ence on S uc u al Mechanics in Reac o Technology (SMiRT 17), P ague, Czech Republic, Augus 17-22, 2003, in CD, M04-4, 10 pp. [21] KRÁL, P. e al. Using he in e se iden i ica ion o pa ame e s o a nonlinea conc e e ma e ial model o analysis o RC s uc u al elemen . In AIP Con e ence P oceedings, 2019, Vol. 2116, 4 pp. ISSN 0094- 243X. [22] SUCHARDOVÁ, P., BERNATÍK, A., SUCHARDA, O. Assessmen o loss esul s by means o mul i - C i e ia analysis. In: Ad ances in Sa e y, Reliabili y and Risk Managemen - P oc. o he Eu opean Sa e y and Reliabili y Con e ence, ESREL 2011. London: CRC P ess-Taylo & F ancis g oup, pp. 1563-1570. ISBN 978-0-415-68379-1. Abou Au ho s Ju aj KRÁLIK was bo n in B a isla a, Slo akia. He ecei ed his Ph.D. om Facul y o Ci il Enginee ing Slo ak Uni e si y o Technology in B a isla a in 1990. He is p o esso o Applied Mechanics in Facul y o Ci il Enginee ing STU in B a isla a. He is Au ho ized Ci il Enginee , Fo ensic Expe in Ci il Enginee ing and Au ho ized Expe o Sa e y Con ol o Nuclea Powe Plan s. His esea ch in e es s include - S a ics and dynamics o he ci il enginee ing s uc u es, Ea hquake enginee ing, Nonlinea mechanics o s eel and ein o ced conc e e s uc u es, Sa e y and eliabili y o he Nuclea Powe Plan s, Soil-s uc u e and Fluid-s uc u e in e ac ion and o he s. He is he au ho o he ollowing publica ions: Books and ex books: 23, Jou nals: 115, Con e ences: 430, P ojec s and expe ’s epo s: 185. Ci a ion in esea ch pape s: Scopus - 238 ci a ions (h - index 11), Web o Science - 182 ci a ions (h -index 8). Scopus Au ho ID: 57000998100, RESEARCH ID: F- 9699-2017 and ORCID ID: 0000-0002-3706-6041. Joze BOČKAJ was bo n in Dolný Kubín, Slo akia. He ecei ed his Ing. om Facul y o Ci il Enginee ing Uni e si y o Technology in Žilina in 2020. He is doc o al s uden in Facul y o Ci il Enginee ing STU in B a isla a. His esea ch in e es s include – Building cons uc ions, The mal mechanics, Fluid mechanics, Wind enginee ing.