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Effect of high-speed steel screw drill geometry on cutting performance when machining austenitic stainless steel

Abstract

Drilling into the solid material is one of the basic technological operations, which creates a cylindrical hole in an appropriate time with required quality. Drilling operation demands a favourable removal of chips from the cutting area because a creation of an undesirable shape of chips can impart a lower quality of the drilled hole corresponding with the generation of excess heat due to the intense contact of the chip with drill. The solution for a proper machining is a suitable modification of the drill geometry i.e., point and clearance angles as presented in current study. The tested drills are made of M35 high-speed steel characterized by a very thin core at the point of the drill. An interesting feature of the drills is the use of cutting speed higher than 30 m min(-1), with the feed of 0.2 mm per revolution. The surface roughness (Ra and Rz lower than 1 mu m and 6 mu m respectively), cylindricity (0.045 mm), roundness (0.025 mm), perpendicularity of the hole axis (0.025 mm), diameters and position of the individual holes were achieved for a drill with point angle 138.32 degrees and clearance angle 6.92 respectively. The increase of the drill point angle by 6 degrees resulted in the decrease in the feed force of more than 150 N. In addition, an increase of the clearance angle by 1 degrees resulted with a decrease in the feed force of 70 N. The results of the experiment showed that with the correct geometry of the tool the effective machining without using internal cooling can be realised.

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Effect of high-speed steel screw drill geometry on cutting performance when machining austenitic stainless steel

Author: Sedlák, Josef; Zouhar, Jan; Kolomý, Štěpán; Slaný, Martin; Nečesánek, Emil
Publisher: Springer Nature
Year: 2023
DOI: 10.1038/s41598-023-36448-y
Source: https://dspace.vut.cz/bitstreams/38153a28-39c9-44ef-ba51-864dea36533e/download
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E ec o high‑speed s eel
sc ew d ill geome y on cu ing
pe o mance when machining
aus eni ic s ainless s eel
Jose Sedlak
1, Jan Zouha
1*, S epan Kolomy
1, Ma in Slany
1 & Emil Necesanek
2
D illing in o he solid ma e ial is one o he basic echnological ope a ions, which c ea es a cylind ical
hole in an app op ia e ime wi h equi ed quali y. D illing ope a ion demands a a ou able emo al
o chips om he cu ing a ea because a c ea ion o an undesi able shape o chips can impa a
lowe quali y o he d illed hole co esponding wi h he gene a ion o excess hea due o he in ense
con ac o he chip wi h d ill. The solu ion o a p ope machining is a sui able modi ica ion o he d ill
geome y i.e., poin and clea ance angles as p esen ed in cu en s udy. The es ed d ills a e made
o M35 high‑speed s eel cha ac e ized by a e y hin co e a he poin o he d ill. An in e es ing
ea u e o he d ills is he use o cu ing speed highe han 30 m min−1, wi h he eed o 0.2 mm pe
e olu ion. The su ace oughness (Ra and Rz lowe han 1 µm and 6 µm espec i ely), cylind ici y
(0.045 mm), oundness (0.025 mm), pe pendicula i y o he hole axis (0.025 mm), diame e s and
posi ion o he indi idual holes we e achie ed o a d ill wi h poin angle 138.32°and clea ance angle
6.92 espec i ely. The inc ease o he d ill poin angle by 6° esul ed in he dec ease in he eed o ce o
mo e han 150 N. In addi ion, an inc ease o he clea ance angle by 1° esul ed wi h a dec ease in he
eed o ce o 70 N. The esul s o he expe imen showed ha wi h he co ec geome y o he ool
he e ec i e machining wi hou using in e nal cooling can be ealised.
S ainless s eels a e used in a wide ange o indus ies due o hei excep ional p ope ies in he ield o esis ance
o he ex e nal en i onmen and ele a ed empe a u e. This s eel can be used as su gical ins umen s in medi-
cine, componen s o he exhaus sys em o ca s o la ge ese oi s and pipelines in he pe ochemical indus y.
When d illing s ainless s eel, se e al limi a ions can ac on he ool. These limi a ions include low he mal
conduc i i y, high duc ili y, suscep ibili y o s ain ha dening and high ab asi eness o he machined ma e ial.
Dolinšek1 examined s ain ha dening du ing d illing o aus eni ic s ainless s eel. Wi h he help o he cu b eake ,
i was ound ha he highes in ensi y o de o ma ion ha dening occu ed in he icini y o he axis o he d ill
close o he poin o he c oss cu ing edge. The esul o s ain ha dening was ha he mic oha dness o he
ma e ial inc eased om 300 o 600HV 50. Aus eni ic s ainless s eel is cha ac e ized by up o ou imes lowe
he mal conduc i i y compa ed o low-ca bon s eel, which causes an in ense inc ease in empe a u e a he edge
o he cu ing ool2. The highes hea occu s on he pe iphe y o he ool in he a ea o he ou e poin due o he
inc easing cu ing speed ou wa ds o he d ill pe ime e 3. Acco ding o he simula ion based on he expe imen
in he s udy3 pe o med on AISI 1045 ca bon s eel, almos 50% o he gene a ed hea ans e ed in o he ool.
The in ensi y o hea gene a ion can be educed by dec easing he a ea o he ine icien ly machining co e o he
d ill, as in he case o he CZ005 ool om his s udy, o by using he app op ia e clea ance angle o he d ill4.
E ec i e cooling o he ool edge is ano he op ion o elimina ing he gene a ed hea . In he s udy4, he e ec o
in e nal cooling wi h he p essu e o 80ba owa ds o he cu ing edge was analysed expe imen ally and h ough
he simula ion. I was ound ha , despi e he high speed o liquid supply h ough he cooling channels, ine icien
cooling o he ool edge occu ed due o an undesi able luid u bulence and ic ion on he d ill. Acco ding o he
esul s o a s udy5 conduc ed on aus eni ic s ainless s eel, an inc ease in he alue o he poin angle in he ange
o 82°–118° led o he inc ease in he empe a u e a he cu ing edge. Unde ce ain condi ions, he e may be a
educ ion in cu ing o ces due o he so-called so ening e ec 6 leading o an imp o emen o su ace oughness.
The e ec o he cu ing speed on he oughness o he machined su ace depends on he empe a u e a which
i occu s o p e en he o ma ion o g ow h in he gi en ma e ial, he alues o he cu ing speed used and he
OPEN
1Facul y o Mechanical Enginee ing, B no Uni e si y o Technology, B no, Czech Republic. 2NÁSTROJE CZ, s. .o.,
Kyjo , Czech Republic. *email: zouha @ me. u b .cz
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machined ma e ial. In he s udy7, he lowe su ace oughness o aus eni ic s ainless s eel (abou 20–50%) was
obse ed when he cu ing speed inc eased om 18 o 30m min−1. On he con a y, in he s udy8 when d illing
low-alloy s eel, he e was an inc ease in oughness mo e han 50% when he cu ing speed inc eased om 32 o
51m min−1. The so ening e ec ea u ed a majo impac in he expe imen used by Huang e al.9. They analysed
he in luence o indi idual pa ame e s on he magni ude o he eed o ce when d illing hin pla es made o
composi e ma e ial ein o ced wi h silicon ca bides. Inc easing he cu ing speed om 50m min−1 o he double
alue ea u ed a di e en e ec on he amoun o eed o ce a di e en s ages o d illing. Be o e en ance o he
en i e ool ip, he e was a sligh inc ease in eed o ce due o he inc ease o cu ing speed. In case o d illing
wo kpiece wi h a hickness highe han 1mm, when he cu ing speed inc eased, he empe a u e inc eased and,
bu due o he so ening e ec , he eed o ce dec eased by mo e han 15%.
The di icul condi ions o d illing aus eni ic s ainless s eel desc ibed in he p e ious pa ag aph equi e he
co ec selec ion o indi idual geome ic pa ame e s o he ool, o he wise he apid wea is obse ed. The ool
wea is accompanied wi h he lowe quali y o he hole co esponding wi h he inc ease o he empe a u e and
he high oughness o he ma e ial. F om he complex geome y o he helical d ill, he in luence o he poin
angle on he cu ing p ocess is mos o en discussed in he s udies. The i s pa ame e analysed is he eed o ce.
The dependence o he size o he poin angle on he eed o ce a ies in each s udy. I was ound ha when he
poin angle inc eased, he eed o ce sligh ly dec eased10,11. The same end was obse ed in he cu en s udy.
On he o he hand, he inc ease o he eed o ce when he poin angle inc eased was p esen ed by he o he
esea che s6,12,13. When he poin angle inc eased om 82° o 118° in he s udy5 and 110° o 118° in14 he in ense
de o ma ion o he ma e ial a he poin o he c oss edge caused he highe empe a u e. Ka pa 6 pe o med a
de elopmen o he special d ills wi h a double edge aimed o machining composi e ma e ials. The d ills ea u ed
he diame e o 6.4mm, while he leng h o each d ill a ied as well as he leng h o he cu ing edge, which
enabled o change he dependence o he eed o ce on ime. The d ill wi h a lowe poin angle exhibi ed lowe
eed o ce compa ed o he d ill wi h he highe poin angle. They ound ou ha he bes esul s we e achie ed
when he d ill had he longes cu ing edge wi h a poin angle o 120°6. The lowe eed o ce can dec ease he
delamina ion o he composi e laye s, o he o ma ion o bu s when d illing duc ile me al ma e ials. Mu ad
e al.15 p esen ed he pape e alua ing an e ec o poin angle when d illing o he i anium Ti6Al4V alloy. Due
o he empe a u e inc ease in he hole su ace, he hole ea u ed he ha dening laye . The highe poin angle
caused an inc ease in he hickness o he ha dened laye o he hole om 0.05 o 0.1mm. The inc ease in laye
hickness was also obse ed when ool wea inc eased.
When machining ough s ainless s eel, long helical chips, which causes ab asi e e ec in he d ill g oo e
and in he d illed hole a e o med. Due o he ic ion be ween he chip and he ool, an excess hea is gene -
a ed, and he su ace o he d illed hole may be damaged3. A he same ime, he long chip can block he access
o he cu ing luid in o he cu ing a ea4. When he con en ional d illing o ough ma e ials, i is no possible
o p e en he o ma ion o long chips. The solu ion can be ul asonic d illing echnology, whe e ib a ions a
he equency o ul asound a e in oduced in o he classic d illing p ocess. Zhu e al.16 ocused on d illing he
0.5mm diame e holes in nickel supe alloy wi h he ul asound echnology. The ib a ion added o he d illing
p ocess b oke he chip in o small pieces and he high-densi y ene gy inpu dis up s he ma e ial unde he ool
edge esul ing in lowe eed o ce.
The in luence o he poin angle se ing on he achie ed su ace oughness o he d illed hole a ies in indi-
idual s udies. In he case o he s udies8,11, hey obse ed an inc ease in su ace oughness when he alue o he
poin angle inc eased, bu con a y in s udies10,15 he au ho s p esen ed a dec ease in su ace oughness when he
poin angle inc eased. In he s udy16, au ho s ound ha he su ace oughness dec eased abou 20–30% when
implemen ing ul asonic d illing echnology.
Accu a e d illing o he ool is a p e equisi e o p oduce a high-quali y hole, when d illing o -axis, he diam-
e e o he en ance pa o he hole inc eases and he geome ic ole ances o he hole de e io a e. The ma e ial
wi h lowe ha dness de e io a es he s abiliza ion o he d ill in he d illed hole. Üllen e al.17 examined an e ec o
ma e ial s uc u e on he quali y o d illed holes when d illing low-alloy ch omium-molybdenum s eel subjec ed
o di e en hea ea men s. The moni o ed hole quali y pa ame e s we e ci cula i y, cylind icali y, de ia ion o
he diame e om he nominal alue and oughness o he machined su ace. I was ound ha he quali y o
d illed holes depends on he ha dness o he ma e ial. When he ha dness o he d illed ma e ial inc eased om
34 o 67 HRC (by applied hea ea men ), he e was an imp o emen o each indi idual pa ame e in he ange
30–50%, bu con e sely, when he ha dness o he ma e ial dec eased om 34 o 24 HRC (by applied annealing),
he dec ease in hole quali y o mo e han 15% was de ec ed17. Imp o ing he abili y o d ill in o so ma e ial can
be achie ed by implemen ing ul asonic d illing echnology. In he expe imen (ca ied ou by16) he e was he
dec ease in he de ia ion om he nominal diame e om 25 o 5µm and he conici y o he hole mo e han 30%.
The main aim o his pape is o s udy an e ec o he di e en d ill geome y (especially he poin and clea -
ance angle) on he quali y o d illed holes. The quali y o d illed holes was assessed by he su ace oughness,
cylind ici y, oundness, pe pendicula i y o he hole axis, he diame e s and posi ion o he indi idual holes and
hei mu ual compa ison. The cu ing o ces we e measu ed du ing he d illing ope a ion o e i y he e ec
o di e en d ill geome y. The in luence o he es ed ma e ial su ace ha dness was e alua ed. The no el y o
p esen wo k is a special design o es ed d ills, which ea u e a hin co e co esponding wi h he possibili y o
se he highe cu ing speed wi h espec o he inal hole quali y. The hin co e u ilises o p oduce a deepe heli-
cal g oo e, which p o ides he be e access o he g inding wheel enabling highe p oduc i i y o HSS d ills.
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Expe imen al se up and ma e ial
Expe imen al ma e ial. The ma e ial o d illing was he AISI 304 aus eni ic s ainless s eel. The ma e ial
was in he o m o olled pla es wi h dimensions o 206 × 120 × 20mm, which we e used o he expe imen . The
d illing ope a ions we e ca ied ou in o he solid ma e ial (wi hou he cen e ing o he hole). The mic oha d-
ness was measu ed on bo h si es o he es ed ma e ial, which ea u ed he signi ican di e ence on he bo om
and op si e. The mic oha dness ( he cou se o he mic oha dness ac oss he ma e ial) was obse ed on he
c oss-sec ion o he ma e ial, in which he mic oha dness exhibi ed he ange 200–400 HV 0.1 (Fig.1).
In o de o cla i y he cause o he change in ha dness, he s uc u e obse a ion was ca ied ou . The posi-
ion o indi idual mic oha dness measu emen s and mic os uc u e we e ealised on he c oss-sec ion o he
ma e ial ma ked in Fig.2a–d.
On he i s side o he pla e, he mic os uc u e consis s o aus eni e (Fig.2a), bu owa ds o he second side
o he pla e he needles o ma ensi e appea ed in he s uc u e (Fig.2b,c). The ma ensi ic s uc u e was ound
on he edge o he semi- inished p oduc in he place whe e he mic oha dness eached 400 HV 0.1 (Fig.2d).
The o ma ion o a ma ensi ic s uc u e in he semi- inished aus eni ic s eel was appa en ly caused by une en
s ain ha dening du ing shee olling. The side wi h he highe mic oha dness exhibi ed a highe deg ee o shee
olling de o ma ion. The simila e ec o he o ma ion o he ma ensi ic s uc u e connec ed wi h he inc ease
in he mic oha dness caused by s ain ha dening du ing olling echnology was also obse ed in he s udy18.
D illing ools. Fo he expe imen , 8 d ills (model CZ005) manu ac u ed by he company NÁSTROJE CZ,
s. .o. we e used. The d ills we e made o M35 high-speed s eel wi h di e en poin angle and clea ance angle on
he main cu ing edge (Fig.3). These angles we e used o e i y he in luence o he d ill geome y du ing he
d illing p ocess.
The poin angle o indi idual d ills was in ange 135°–145° and he clea ance angle was in ange 7° o 15° (see
Table1). The ange o a clea ance angle was selec ed as a minimum and maximum alue (and alues wi hin he
ange), which can be g inded wi h he g inding wheel and he poin angle was chosen as he simila angle used
o sin e ed ca bide d ill p oduc ion Each d ill (A–G) was p oduced wice due o e i ica ion o hei epea abili y.
The geome y o he d ill was based on he CZ005 model se ies o d ills designed o machining s ainless
s eel. The speci ica ions o he d ills used in he expe imen (see Table2) we e he same o all he es ed samples.
The geome y o indi idual d ills was measu ed on a HELICHECK PLUS op ical measu ing machine om
he company Wal e . The geome y o he CZ005 d ill is pa icula ly cha ac e ized by a e y hin co e, whe e he
diame e o he co e is 0.07–0.08 × D. Due o he hin co e, i is possible o p oduce a deepe helical g oo e in he
Figu e1. Ma e ial mic oha dness dis ibu ion on he c oss-sec ion o he d illed ma e ial.
Figu e2. Mic os uc u e o aus eni ic s ainless s eel in indi idual sec ions o he c oss-sec ion.
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d ill. The deepe g oo e he mo e posi i e geome y can be g inded (see Fig.4). The dependence o clea ance
angle on he dep h o he g oo e is gi en by he g inding p ocess. The deepe g oo e he bigge space o he
g inding wheel enabling be e g inding p ocess o he cu ing edge19.
The posi i e clea ance angle along he en i e leng h o he edge plays a signi ican ole in case o he machining
aus eni ic s ainless s eel. A posi i e clea ance angle o he main cu ing edge educes he none ec ual zone wi hin
he a ea in he icini y o he d ill axis. Wi h his geome y i is possible o each he educ ion o he cu ing
o ces, de o ma ion ha dening and hea gene a ion wi hin he a ea o he d ill ip. These aspec s a e conside ed
o cause a poo machinabili y o aus eni ic s ainless s eel20. The educ ion o he co e c oss-sec ion a he poin
o he d ill causes a signi ican educ ion eed o ce21.
The clea ance o he d ill CZ005 is c ea ed by h ee indi idual ace s depic ed in Fig.4, while he ace along
he main edge ea u es he o iginal shape. The second edge exhibi s he ace wi h i s wid h co esponding wi h
he d ill co e diame e . The ace is dec easing owa ds o he ou e pe ime e o he d ill o cause he lowe ic-
ion be ween he clea ance and he bo om o he d illing hole19.
The shape o he main edge is c ea ed om he 2/3 by he con ex cu e, which is ollowed wi h he la a ea
o he main edge co esponding o he es o 1/3 o he main edge19.
Figu e3. D ill geome y used in he expe imen wi h he clea ance angle α and poin angle ω.
Table 1. The alues o he poin angle and he clea ance angle o he indi idual compa ed d ills.
A B C D E F G
Poin angle ω (°) 135.68 135.62 138.32 138.35 141.61 142.14 145.03
Clea ance angle α (°) 8.09 7.20 6.92 7.07 7.76 8.37 14.65
Table 2. Speci ica ions o expe imen ally used d ills.
D ill diame e 13mm Helix angle 29.40 ± 0.40°
O e all d ill leng h 151mm Clea ance angle in he axis o he d ill 1.70 ± 0.80°
Flu e leng h 101mm D ill co e hickness 1.00 ± 0.10mm
Figu e4. De ail geome y o used d ill CZ005.
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Expe imen al and measu emen design. Tes ing o he indi idual lis ed d ills was ca ied ou on he
mul i unc ional e ical machining cen e TAJMAC ZPS MCV 1210 (BUT, Czech Republic, B no). To al o 14
holes (see Fig.5) we e d illed wi h each o he men ioned ools as pa o he expe imen . The numbe o 14 holes
was se o e alua e he geome ical ole ances and ind ou how hey change du ing he d illing ( om he 1s o
14 h hole). The d ill was no wo n a e he 14 h hole, bu he es was ended ( he necessa y da a o e alua ion
o he p ope ool geome y we e ob ained).
The d illed holes we e analysed conside ing he ollowing ac o s:
• cu ing o ces (1s and 14 h hole),
• oughness (1s and 14 h hole),
• geome ic ole ances—ci cula i y, cylind icali y, and pe pendicula i y o he axis o he hole o he su ace
o he pla e (1, 2, 5, 6, 9, 10, 12, 13 and 14 hole),—diame e (1, 2, 5, 6, 9, 10, 12, 13 and 14 holes),
• pi ch (x1, x2, x3, x4, x5).
Cu ing o ces measu emen . A KISTLER 9272 dynamome e (Feed o ce in ange − 5 o 5kN < 0.02, o que in
ange − 200 o 200 < 0.2Nm) wi h accesso ies was used o he pu pose o he expe imen o measu e he cu ing
o ces. The dynamome e was clamped o he wo k able o he machining cen e using T-slo sc ews, a ice was
a ached o he dynamome e o clamping he d illed pla e. Cu ing o ces we e measu ed only when d illing
in o he side co esponding wi h he highe obse ed mic oha dness (400HV). The cu ing o ces we e a ec ed
only by he change in he geome y o he d ill, he o he pa ame e s o he p ocess we e cons an du ing he
expe imen .
Su ace oughness measu emen . The su ace oughness o he holes was measu ed using a Taylo Hobson
Talysu CLI 1000 oughness de ice. Acco ding o he ČSN EN ISO 4288 s anda d, he indica i e alue o he
RSm pa ame e was i s measu ed and he co esponding basic and e alua ed leng h was chosen based on he
measu ed alues. A e le elling he su ace o a ho izon al posi ion, he p o ile o he en i e leng h o he hole
was measu ed. To ob ain he oughness p o ile, i was necessa y o pe o m h esholding, emo e he shape o
he measu ed p o ile using a 5 h-o de polynomial, and il e he measu ed da a using a Gaussian il e . The
e alua ed leng hs we e ex ac ed om he ob ained oughness p o ile (see Fig.6), and he equi ed oughness
pa ame e s Ra and Rz we e subsequen ly measu ed.
Geome ic ole ances measu emen . Measu emen s o geome ic ole ances i.e., hole diame e s and pi ches
we e pe o med on he Lei z Re e ence Xi coo dina e measu ing de ice. The ci cula i y, he pe pendicula i y
o he hole axis o he su ace and he spacing o he holes we e measu ed in wo places along he leng h o he
hole in places 3mm om bo h sides o he ma e ial (see Fig.7). Roundness was e alua ed based on he cen e o
he leas squa es acco ding o he ČSN ISO 4291 s anda d. The spacing o he pai o holes is conside ed as he
spacing o a pai o ci cles a he same heigh le el c ea ed du ing he oundness e alua ion. The ole ance ield
o he hole pe pendicula i y is conside ed as he cylinde in which he axis o he cylinde o he app oxima ed
hole alls.
Figu e5. Scheme o he expe imen ally d illed holes on he d illed pla e.
Figu e6. Me hodology used o he measu ing o he su ace oughness o d illed holes.

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The e alua ion o he cylind ici y and diame e o he d illed holes ook place in h ee places along he leng h
o he holes (3mm om he op o he hole, he middle heigh and 3mm om he bo om o he hole, he scheme
is depic ed in Fig.7). The cylind ici y o he holes was de e mined based on he c ea ion o he so-called w ap-
ping cylind ical su aces c ea ed by ex ac ing he ci cula i y p o ile acco ding o he ČSN ISO 12180-2 s anda d.
The diame e o he holes is conside ed as he diame e o a ci cle app oxima ed by he me hod o leas squa es.
De e mining he accu acy o he posi ion and dimension o he holes. The posi ion o he holes was assessed
based on he measu emen o he de ia ion o he pai o holes om he nominal alue o he spacing. In he case
o he dimension, he pa ame e was he de ia ion om he nominal alue o he diame e .
Cu ing condi ions. The cu ing condi ions we e se o he indica ed alues and emained cons an
h oughou he expe imen i.e., cu ing speed c = 32m min−1 (co esponding e olu ions n = 784 min−1) and
eed pe o a ion = 0.2mm (co esponding eed a e = 157mm min−1). Quake Cool 7350BFF cu ing luid
wi h a concen a ion o 5% ( ecommended by he p oduce o he d ills) was used du ing d illing.
Resul s and discussion
The ollowing chap e p esen s he ob ained esul s based on obse ing he in luence o he poin angle and he
clea ance angle on he quali y o he d illed holes. Using he simula ion in he Heli onic ool s udio p og am, he
e ec o bo h men ioned angles on he size o he angle o he c oss edge o he d ill was de e mined (see Fig.8).
Feed o ce and o que e alua ion. The eed o ce and o que we e measu ed o indi idual d ills used in
he expe imen . The Figs.9 and 10 a e depic ed o he d illing o 1s hole (new ool). The boxplo cha was used
o isualize he da a, due o he possibili y o display he agg ega ed s a is ical da a. Indi idual blocks ep esen
50% o he da a se , alling be ween he 1s and 3 d qua iles. The lines leading om he blocks show he dis ibu-
ion o he es o he alues o he se , he ou lie s a e exp essed by sepa a e poin s. The s aigh line inside he
block ep esen s he median o he se and he black block he mean alue o he da a se . The a e age alue o
he eed o ce when d illing wi h indi idual d ills was in he anged 2481–2929 N (see Fig.9).
Based on he acqui ed da a, i can be s a ed ha poin and clea ance angles in luenced he applied eed o ce
(compa e d ill A and d ill G, whe e he maximum di e ence 420 N was obse ed). When he clea ance angle
inc eased by less han 1° in d ills A and B, he eed o ce dec eased mo e han 70 N. The example o he in luence
Figu e7. Me hodology used o he measu ing o he ole ances o he geome y o d illed holes.
Figu e8. Dependence o he angle size o he c oss blade on he se ing he alue o he poin angle and he
clea ance angle o he d ill CZ005.
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o he size o he poin angle can be obse ed in d ills A and E, whe e he poin angle inc eased by 6°, he eed
o ce dec eased mo e han 150N (see Fig.9). An inc ease o he clea ance angle ( om 8.37° co ela es wi h d ill
F o 14.65°co esponds wi h d ill G) caused a dec ease (270 N, calcula ed om a e age alues) o he eed o ce,
which can be impa ed by he c ea ion o a sha pe cu ing edge esul ing in lowe esis ance agains pene a ion
in o he wo kpiece ma e ial. The o que was less a ec ed by he change o angles compa ed o he eed o ce.
The o que alue a ied be ween 10.5 and 11.1Nm, depending on he selec ed alue o he clea ance angle and
poin angle (see Fig.10). The highes o que alue was measu ed in case o d ill G, which is cha ac e ized by he
highes alue o bo h angles (poin and clea ance angle).
Hole su ace oughness. The su ace oughness o he d illed holes was e alua ed based on he pa ame e s
Ra and Rz, he measu emen was ca ied ou acco ding o he me hodology desc ibed in chap e 2.3.1. Using
he lowe alues o bo h obse ed angles esul ed in su ace oughness lowe han 1µm conside ing h ee com-
pa ed d ills i.e., A, B and C. The dependence o su ace oughness on he poin and clea ance angle is depic ed in
Fig.11a. D ill F exhibi ed he highes de ia ion ( ep esen ed by he ed line depic ed in each d ill) in ega ds o
oughness Ra, bu con a y he lowes de ia ion ea u ed d ill B wi h he lowes poin angle (132.62°). Figu e11b
shows oughness o he 1s and he 14 h hole eached o each d ill.
The obse ed dependence o su ace oughness on he poin and clea ance angles, showed he same end in
case o Rz pa ame e , he e o e he display o he measu ed alues o Rz was no pe o med. The su ace ough-
ness pa ame e Rz was e alua ed in he ange 5.7–11.7µm. The in luence o he angles on he su ace oughness
is based on he p emise o main ain a smoo h machining p ocess wi hou in oducing addi ional ib a ions
and une en o ce s ess. The d ill geome y wi h he lowe clea ance angle shows he sha pe cu ing wedge
and makes i easie o he ool o cu in o he wo kpiece ma e ial. Choosing a lowe poin angle in luences he
abili y o s abilize he d ill in he hole due o mo e a ou able o ce ac ion. When bo h angles desc ibed abo e
a e changed, he eme ging phenomena in e ac wi h each o he . In he case o choosing a lowe alue o he
angle o he poin and he clea ance angle (in case o A and B d ills, see Fig.11), he d ill is su icien ly s able
when cu ing in o he ma e ial. In he case o he highe alue o he poin and clea ance angle he cu ing edge
epea edly cu s in o he wo kpiece ma e ial and hen cause undesi able ib a ions. The desc ibed e ec esul ed
in highe su ace oughness no iceable in case o d ills E, F and G.
Geome ic ole ances o holes. The geome ic shape was assessed using he measu ed geome ic ole -
ances o he holes—ci cula i y (see Fig.12), cylind ici y (see Fig.13) and pe pendicula i y o he hole axis o he
su ace (see Fig.14). The lowes alues o geome ic ole ances we e measu ed in case o he d ill C, bu con a y
he highes alues o geome ic ole ances we e ound in case o uns able d ill G.
Figu e9. The in luence o he d ill bi geome y on he magni ude o he applied eed o ce.
Figu e10. The in luence o he d ill geome y on he applied o que magni ude.
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The measu ed alues o he geome ical ole ance (calcula ed as an a e age alue om holes desc ibed in
“Expe imen al and measu emen design” sec ion) o oundness anged om 0.025 (d ill C) o 0.045mm (d ill
G). Changing he angle o he poin and he clea ance angle on he main edge o d ills A o F ea u ed no e ec
on he oundness o he measu ed holes. A signi ican e ec o inc easing he clea ance angle was ound in case
o d ill G (Fig.12). D ill A exhibi ed he highes de ia ion conside ing a hole ci cula i y, bu con a y he lowes
de ia ion ea u ed d ill C wi h he lowes clea ance angle (6.92°).
The cylind ici y o he analysed holes (calcula ed as an a e age alue om holes desc ibed in “Expe imen al
and measu emen design” sec ion) was measu ed in a ange o alues om 0.045 (d ill C) o mo e han 0.095mm
Figu e11. (a) The dependence o he de ia ion alue om he nominal alue o he poin angle and he
clea ance angle o he d ill on he achie ed su ace oughness and (b) oughness o he 1s and he 14 h hole
eached o each d ill.
Figu e12. The dependence o he de ia ion alue om he nominal alue o he ci cula i y alue o he d illed
holes on he choice o poin angle and clea ance angle.
Figu e13. The dependence o he de ia ion alue om he nominal alue o he poin angle and he clea ance
angle o he d ill on he size o he d illed hole cylind ici y.
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(d ill G). Highe cylind ici y alues we e eached when using d ills wi h poin angle alues o 138°–142° and
clea ance angle alues om 7° o 8° (Fig.13). D ill B exhibi ed he highes de ia ion conside ing a hole cylind ic-
i y, bu con a y he lowes de ia ion showed d ill E (poin angle 141.61 and clea ance angle 7.76° espec i ely).
The measu ed alues o he pe pendicula i y (calcula ed as an a e age alue om holes desc ibed in “Expe i-
men al and measu emen design” sec ion) o he hole axis o he su ace anged om 0.025 (d ill C) o 0.06mm
(d ill G). The bes alues we e ob ained using a poin angle in he ange o 138°–140° (Fig.14). D ill E ea u ed
he highes de ia ion conside ing a hole pe pendicula i y (opposi e o hole cylind ici y), bu con a y he lowes
de ia ion ea u ed d ill C as in case o hole cylind ici y.
D ill G achie ed signi ican ly wo se hole quali y esul s in e ms o su ace oughness and geome ic ole -
ances compa ed o d ill D wi h a e y simila geome y. The cause o he desc ibed anomaly is appa en ly a
de ec in he d ill caused du ing i s p oduc ion i.e., ele a ion o he blade, when he ou e ips o he d ill ha e
a di e en heigh . This de ec causes a di e en engagemen o he wo edges o he ool, esul ing in he ib a-
ions and egula misalignmen o he d ill bi du ing d illing. The achie ed alues o geome ic ole ances a e
mainly in luenced by he abili y o accu a ely d ill in o he ma e ial and he subsequen s abili y o he cu ing
p ocess du ing d illing. Imp ope en e ing o he d ill in o he ma e ial can impa he axis o he hole o de ia e
and in oduce ib a ions.
Posi ion and size o holes. The alues o he de ia ion om he nominal alue o he hole pi ch we e o
indi idual holes om 0.06mm (in case o d ill C) o 0.1 o d ill E (see Fig.15). The bes alues we e achie ed
wi h d ills C and G. In he case o hole machined by d ill C, his alue was assumed as he high-quali y d illed
holes. The alue o he d ill G hole is no conside ed due o he e y poo quali y o he hole in e ms o assessed
pa ame e s. The s anda d de ia ion o he se o measu ed da a o pi ch de ia ions om he nominal alue is
only 0.01mm, his ac con i ms he s abili y o he d ill du ing d illing in o he ma e ial. D ill B ea u ed he
highes de ia ion conside ing a hole space de ia ion, bu he lowes de ia ion alue was eached by d ill C.
In e ms o he accu acy o he dimension o he d illed holes, he bes esul s we e ound o d ills C and
D, wi h a poin angle o 138° and he clea ance angle o 7° (see Fig.16). The de ia ion alues o he measu ed
da a om he nominal alue o he diame e a e 0.03mm and 0.036mm espec i ely o he men ioned d ills,
Figu e14. The dependence o he de ia ion alue om he nominal alue o he chosen geome y o he
compa ed angles on he achie ed pe pendicula i y o he axis o he hole o he su ace o he d illed pla e.
Figu e15. The dependence o he de ia ion alue om he nominal alue o he d illed holes spacing on he
choice o he poin angle and he clea ance angle on he d ill.