Computation of the Leuven milling machine
Citation for published version (APA):
Bosma, W. D. G., Hijink, J. A. W., & van der Wolf, A. C. H. (1973). Computation of the Leuven milling machine:
status results of Eindhoven. (TH Eindhoven. Afd. Werktuigbouwkunde, Laboratorium voor mechanische
technologie en werkplaatstechniek : WT rapporten; Vol. WT0309). Technische Hogeschool Eindhoven.
Document status and date:
Published: 01/01/1973
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technische hogeschoo( eindhoven
laboratoriwm voar mechc'I1!sche technologie en werkplaotstechniek
van de seetie:
t,{T
COHPUTATION OF THE LEUVEN HIlLING f-1ACHINE
sornerwotti ng
prognose
•
'if"
D
(I Bo~,maIr .. J.A.W. Hi
Profcdr"iro A .. C .. H. van del' Wolf
S'I'ATIC RESULTS.
z.
1
van
11
codering:
trefwoord:
datum:
jan"
'73
aantol biz.
geschikt vear
publicatie in:
C.I.R.P. GROUP Ma, CO-OPERATIVE WORK ON
COMPUTER AIDED DESIGN AND ANALYSIS
OF
MACHINE TOOL STRUCTURES
COMPUTATION
OF
THE LEUVEN MILLING MACHINE
STATIC RESULTS OF EINDHOVEN
UNIVERSITY
OF
TECHNOLOGY
JANUARY, 1973
W.D.G.
BOSMA
J.A.W.
HIJINK
2
PREFACE
This report deals with the results of two models.
The characteristic values of model 1 ,.Jere derived by just
looking at the drawings.
Because this model did not fit when comparing the computed
deflections with the measured ones, a second model was made
in which model 1 values of 1Y, 1Z and
J
were adapted on a
try and error base to match the measured deflections.
This meant that the column had to be stiffened considerably
and the support made much more flexible.
Also the stiff element nr. 33 between column and support was
shortened.
3
12
@
36
11
TOLERANTIES VLGS Nl:N 2365 PROjECTlE BENAMING
MATHEMATICAL MODEL
FOR
b.v.8 :l:: 0.15 8':'
~:~ ~_
300 10' :l:: 30"AM
STATIC CALCULATIONS OF
lEUVEN
MILLING
MACHINE
?ASSINGfN VLGS N SOL
I
RUWHE1DSWAARDEN VlGS NEN 630I
AANTAI. MATERIAAl
-I:~
TECHNISCHE HOGESCHOOl EINDHOVEN
SCHAAl. DATUM TEKENINGNR.AFDEl.Il'>IG:
W
GET.: '~7:~'~//{tt~ /./1A4
4
CHARACTERISTICS OF ELEMENTS FROM DRAWINGS (model
1 )
ELEMENT
L(m)
A(m2)
IY(m4)
IZ(m4)
J(m4)
1
0.195
0.10E-t
0.48E-5
0.47E-4
0.52E-4
2
0.195
O. 10E-l
O.48E-5
0.47E-4
0.52E-4
3
0.280
0.16E-l
0.90E-5
0.10E-4
0.98E-4
4
0.280
0.16E-l
0.90E-5
0.IOE-4
0.98E-4
5
0.120
0.90E-i
0.10E-Z
0.10E-2
0.20E-2
6
0.189
0.10E-l
0.38E-4
0.35E-4
0.46E-4
7
O. 136
0.12E-I
0.59E-4
0.45E-4
0.68E-4
8
0.127
O.13E-i
0.93E-4
0.62E-4
0.10E-3
9
0.180
0.17E-l
0.40E-3
0.IOE-2
0.10E-3
10
0.217
0.19E-i
0.46E-4
0.45E-4
0.40E-5
11
0.622
0.23E-l
0.40E-3
0.] OE-2
0.10E-3
12
0.135
O.20E-I
O.5IE-4
O.35E-4
0.80E-4
13
0.100
O.20E-l
0.50E-4
O.30E-4
O.70E-4
14
0.175
0.21E-I
0.50E-4
0.30E-4
0.80E-4
15
O. 148
0.27E-)
0.61E-3
O. 25E- 3
0.56E-3
16 x)
0.348
O.35E-2
0.10E-5
O.10E-5
0.20E-5
17
0.120
0.24E-1
0.43E-3
0.I6E-3
0.42E-3
18
x)
0.315
0.80E-3
0.52E-7
0.52E-7
0.10E-6
19 x)
0.113
0.80E-3
0.52E-7
0.52E-7
0.10E-6
20
0.430
0.90E-2
0.1
0.27E-4
0.29E-4
2]
0.065
0.50E-2
o
.12E-4
0.34E-5
0.1
22
0.055
0.2SE-2
0.29E-5
0.36E-6
0.40E-5
23
0.010
24
0.050
25
0.148
26
O. ]88
27
0.050
28
0.188
29
0.160
30
0.030
31
0.030
32
0.087
33
0.213
34
0.243
35
0.325
L
=
length
A
=beam cross sectional area
IY, 1Z
=second moment of area about Y- and Z- axis respectively
J
=effective second polar moment of area
E
=
0.90E+ll N/m2
G
=O.35E+ll N/m2
x) E
=
2.06E+ll N/m2
Load +lOOON at 37 and -1000N at 20 in the X-direction (model 1)
displac0,menc rotation rotation
(m) (rad) Crad)
joint in X-direction a:,out Y-axis about Z-axis
1 +.135£-4 +.507;::-4 .485£-5 2 +.135E-4 +.507E-4 -.4851'-5 3 +.120£-4 + ~ 507 E-!+ - .l.85E-S 4 +.1 +.507£-4 - .48.3E-5 5 ~. I +.507£-4 - ./,85E-5 6 +.590£-5 +. .485£-5 7 +.329E-S +.5021':-4 .[,85E-5
8 +.357E-6 +.197 E-4 .396E-S
9 0.0 0.0 0.0 10 -.242E-7 .935::-7 -.219£-11 II +.129£-15 " J99E-7 -.131 E-It, J 2 -.152E-5 .211 £-4 +. 13 0.0 0.0 0.0 14 -.435E-5 -.349E-4 + ./,23£-4 15 -.120:::-4 -.502£-4 +.720E-4 16 -.524[-5 -. 507~:-4 +.756E-4 ! 7 -.19L..E-4 +.756E-4 I -.315£-4 +.873£-4 19 .2S0E-4 .503E-4 +.790£-4 -.897£-/, -.507£-4 -.278£-4 21 +.728[-5 +.101 E-3 22 -.833E-4 -.507T::-4 +.738E-4 23 -.816E-/, + .1 ISE-l, + 53£-4 21, .83')1::-4 + .161 +.738£-4 25 .810E-4 +.728£-5 +.10IE-3 26 -.825£-4 +.IISE-4 +.953E-4
27 -.397E-4 .503E-I, +.790E-4
28 -.132[-4 -.503E-4 +.798E-4 29 -.255E-4 -.503E-4 +.7901:-4 30 -.S24E-5 -.507£-4 +. 31 -.315£--4 -.507E-4 +.756£-4 32 +.135£-4 +.507l::-L, -.485E-5 33 +.135£-4 +.507E-4 .485E-5 34 +.153E-5 +.502E-4 .485,,-5 35 -.242E-7 -.9351'-7 -.21')£-11 36 -.969£-8 .399£-7 -.13IE-14 37 +.284E-4 +.507F.-4 -.4851::-5
--
----r--_
I ~---...---...
---....
TOL£RANT~ES VlGS N~N 2165 +010A
b.'I, a::f: 0.1S Ii -0:15
L-L
JOO 10' ±-30"PRorECTIE B~NAMlNG
AM
!\UWHEtDSWAAF\OEN VlGS N£N 4JQ AfDElING; W GI\OEP: WT LOAD--.
----...
I
/
I
(
Iff
I / /
'/-I N X - 01 RECT'/-I ON (mode! 1 )Load +j OOON nt 37 and -IOOON at 20 in the Y-dircction (model 1)
displacement displacement rotation
(m) (m) (rad)
joint in Y-d iree t ion in Z-direction nbout X-,:1xis
I +.580[-5 -.256E-S -.227E-4
2 +.580£-5 -.256E-5 .227E-4
3 +.512E-5 -.256E-5 -.227E-4
4 +.512E-3 -.256£-5 .227£-4
5 +. i 2E-5 .256E-5 .227E-4
6 + .. 242E-5 .256E-S .22110-4 7 +. H7'3t:-6 .672£-5 -.221£-4 8 +.14JE-6 -~503[.-6 -.835E-S 0.0 0.0 0.0 10 -.654£-8 +.1 +.543£-7 11 -.344E-15 +.1 +.185£-8 12 -.10'3£-5 +.1 +.1'-5E-4 13 0.0 0.0 0.0 -.291£-5 +.149E-9 +.228E-4 15 +.149E-9 +.319L:-4 I -.604E-5 +.3:: 1 E~t~ 17 .12SE-4 +.111-91:-9 +.32IE-4 18 .. 125[-4 +.514£-5 +.321£-4 19 -.180£-4 +.1491::-9 +.321 20 -.1~5E-4 +.1 +. 1 E-4
21 -.lHOE-4 +.186};-I, +.32IE-4
-.1 +.lS~JL-4 +.32IE-4 23 -.1 +.186E-4 +.32IE-4 24 .125E-4 +. ]89£-£, +.32IE-4 25 -.16!..:;:-4 +.186£-4 + .. 321E-4 26 .143£-4 +.189£-4 +.32IE-4 0 -~I -.180£-4 +.475E-5 +.321£-4 28 .180E-4 -.604£-5 +.321E-4 29 -.164£-4 +.149£-9 +.32IE-4 3D -.1 .604E-S +.321 E-4 31 +.514E-5 +.321E-4 +. .256E-5 -.227E-4 33 +.5801~-5 -.256£-5 - .227£-4 34 +.497£-6 -.256£-5 -.221E-4 35 -.654E-8 +.117E-7 +.543£-7 36 -.450£-9 +.149E-9 +.185£-8 37 +.125E-4 -.256£-5 -.227E-4 TOt.£I\ANr~ES V\.GS Nf;N 1365 +0,10
A
,_
'
b,v.8 ± 0,15 , _ 1),25 ~ _- 10'":t 3(1' PROJECTIE SENAMINGAM
RlJWHEIOSWAARC£N VLGS NEN 410 ... ANTAL
AFOHlNG: W
GRO[P: WT
~CHAAL
--
--lOAD IN y. DIRECTION (mod"l , ) MATEl't,IA.4,1.
LOJd -IOOON at 37 and +IOOON at 20 in the Z-direction (model I) displacement displacement rotat ion
(m) (m) (rad)
joint in Y-d iree ~ ion in Z-direetion about X-axis
+.118[-5 .793[-6 -.475£-5
2 +.IISE-5 -.79JE-6 .475E-5
3 +.104£-5 .7931::-6 -.475E-5 4 +.IO!,£-5 .793E-6 -.475l::-5 5 +.10/,£-5 -.793E-6 -.475E-5 6 +.470£-6 .7781::-6 -.475£-5 7 +. I 38"-6 -.1671':-5 .475£-5 8 +.820E-8 -.2131::-6 -.'302£-5 ':I C.O 0.0 0.0 10 +.20%-14 -.IY,E-16 .131+£-13 II +.81lE-16 -.741£-16 .9991::-15 12 -.943£-6 +.750£-7 +. I/,OE-4 13 0.0 0.0 0.0 14 - .. 287£-5 +.131£-6 +.245E-4 15 -.8781::-5 +.223::-6 +.430£-4 16 -.152[-4 -.804E-5 +.44J£-4 17 -.152[-4 +.284E-6 + . 18 . !52E-4 +.737L-S +.565£-1, 19 -.229£-4 +.328E-6 +.456£-l, 20 .152E-4 +.564 £-4 -.722£-4
21 .229E-4 +.423E-4 +.957E-4
22 -.1521::-4 +.435E-4 -.6lJ7E-6
23 -.1221:-4 +. ~ 2/t [-4 +,,865E-4
-. 983i:- 5 +.435E-4 .607E-b
25 -.181 E-4 +.L.2JE-Q +.957£-4
2fj -~122E-4 +.433E-4 +.865E-4
21 -.229i;-4 +.707£-5 +.456E-4 28 -.229[-4 -.82!,E-S +.456£-4 29 -.206£-4 +.328E-6 +.456£-4 30 -.152[-4 .804£-S +.4!+3E-4 31 -.152£-4 +.737E-S +.4431'-4 32 +.118;:-5 -.793[-6 -.47512-5 33 +.118E-5 -.793£-6 .475£-5 34 +.570f:-7 -.778£-6 -.475£-5
35 +.209E-14 .288E-14 -.13I,.E-13
36 +.324[-15 -.74IE-16 .999£-15 37 +.258E-5 -.793£-6 -.475E-5
---,
TOLEAANT~ES VLGS NEN lJ6.S\
\
,
\
\j
li
i•.•. S"O.1S
B':'::~ ~
lQO\O'"",," F'l<.OJECr-U:AM
"ASSINGfN VLGS N 001J_
~~WHE1PSWAAROEN VLGS NfN ,10I~
TECHNISCHE HOGESCHOOl EINDHOVEN
AFOEUNG: W
CROeP: WT
8ENAMING
LOAD IN Z· DIRECTION (model 1 )
AANTA'.. MATERIAAL
SCHAAL DAtUM Ti:K£NINCNP..
GET. : /);;
(ire. , - f I
WllllG."".l
I
!
1 I
J
8
CHARACTERISTICS OF ELEMENTS ADAPTED TO MEASUREMENTS (model 2)
ELEMENT
L(m)
A(m2)
IY(m4)
IZ(m4)
J(m4)
1
O.
J
95
O.lOE-l
O.48E-5
0.47E-4
0.52E-4
2
0.195
O.IOE-I
0.48E-5
0.47E-4
0.52E-4
3
0.280
0.16E-1
0.90E-5
0.10E-4
0.98E-4
4
0.280
0.16E-1
0.90E-5
0.IOE-4
0.98E-4
5
0.120
0.90E-l
0.25E-3
O.18E-3
0.40E-3
6
0.189
O.lOE-I
0.38E-4
O.35E-4
0.46E-4
7
0.136
0.12E-l
0.30E-4
0.12E-4
0.60E-4
8
0.250
0.13E-1
0.35E-4
0.15E-4
0.85E-4
9
0.180
0.17E-l
0.40E-3
O.10E-2
0.10E-3
10
0.217
0.19E-j
0.46E-4
0.45E-4
0.40E-5
11
0.622
0.23E-]
0.40E-3
0.10E-2
0.10E-3
12
0.135
O.20E-]
0.35E-3
0.25E-3
0.30E-3
13
0.100
0.20E-I
0.25E-3
0.25E-3
0.35E-3
14
0.175
0.21E-I
0.25E-3
0.25E-3
0.30E-3
15
0.148
0.27E-I
0.99E-3
0.35E-3
0.25E-2
16 x)
0.348
0.35E-2
0.IOE-5
0.10E-5
0.20E-5
17
0.120
0.24E-I
0.43E-3
0.28E-3
0.8SE-3
18 x)
0.315
0.80E-3
O.
0.45E-7
0.10E-6
19 x)
0.113
0.80E-3
O.45E-7
0.45E-7
0.IOE-6
20
0.430
0.90E-2
O.60E-S
0.11 E-4
0.22E-4
21
0.065
0.50E-2
o
.12E-4
0.34E-5
0.15E-4
22
0.055
O.25E-2
0.29E-5
0.36E-6
0.40E-5
23
0.010
24
0.050
25
0.148
26
0.188
27
0.050
28
0.188
29
0.160
30
0.030
31
0.030
32
0.087
33
0.090
34
0.243
35
0.325
L
=
lenght
A
=
beam cross sectional area
IY, IZ
=
second moment of area about Y- and Z- axis respectively
J
=effective second polar moment of area
E
=0.90E+l1 N/m2
G
=0.3SE+II N/m2
x) E
=2.06E+ll N,'m2
Load +IOOON at 37 and -1000); at 20 in the X-direction (model 2) joint 3 5 6 7 8 Y 10 II I 1 14 16
,
" , I 20 21 22 23 26 27 23 29 30 3 J 32 33 34 35 36 37 displacement (m) X-direction +.362E-I, +.3621:.-4 "'.3371:-4 +.337E-4 +.337E-4 +.235E-4 +.2Sl/+E-f. +.7:,8E-5 0.0 -.2',2::-7 II} ,3781'-5 -.325E-/t .4S!!l:-!, +.450f.-7 +. +.....
+. ! 63L-I, -.2421'-7 .969E-8 +.613E-4 rotat ion (rad) about Y-axis +.853E-4 +.833E-4 +.8531::-4 +.S53E-4 +.S53E-/' +.S32E-::' +.832E-4 .... i,7 5[-4 0.0 -.935E-7 -.3:J9E-7 0.0 -.653E-5 -.687E-5 -.687E-5 -.687~-5 -.665E-5 -.687E-5 +. 68~ E-L~ -.6371:-5 +.730[-4 +.776E-4 +.688E-4 ~. 73U:c-4 -.665E-5 -.66512-5 -.665£-5 -.637[-5 -.687[-5 +.853E-4 +.8532-4 .... 832E-4 -.935[-7 -.399E-7 +.853E-4 rct.:1tiC'n (rad) about Z-axis -.624E-4 .624E-4 -~624E-4 -.624L-4 -.624E-4 -.624:'-4 .621+1::-4 .50!fE-6. 0.0 -.322E-12 +.611E-5 0.0 +.998£-5 +.179E-4 +.1 +.1871::-4 +. 111::-4 +.204E-4 • 704E-~ +.744E-4 +.472E-I+ +.68610-4 "'.472E-I, +.74t+E-cJ. +. +.204E-4 +. +.204E-4 +.1 +.187£-4 -.624E-4 5 .624E-4 .624E-4 -.32210-12 .2261::-15 -.624F.-4+
TO\.£P.ANTtES VL,.GS NEN 2145 PROJECTf£: 8ENAMtNG
~,v,
a :±: 0,1$ 8 + _ 0°·10 ,B ~~
300 10' ... 30" -AM
RUWHEIOSWAAR.DEJ14 VlG$ NEN t'tlO AANTA!..
AFOEUNG: W GROEP: WT SCHAAL LOAD IN
. /
\
-.\
'~
f
/ '
. / / ' X-DIRECTION (model 2) MATEfU"'AtAi
Load +IOOON tit 37 tlnd -lOGON at 20 in the Y-direction (model 2)
displacement displacement rotation
(m) em) (rad)
joint in Y-c!ircction in Z-direction about X-axis
+.]83£-4 -.132£-4 -.738£-4 2 +.185E-4 -.132£-(+ -.738£-4 3 +. !(j 3£-4 -.132£-4 .738£-4 .~ +. 163E-!; 132[-4 -.7381-4 5 + .1 -. 132E-4 -.738:0-4 6 +.758E-5 -.132£-4 -.709E-4
7 +.2G2E-5 -.265E-~ -.709E-I,
8 +.1~26E-6 -.51.7E-5 ~432E-4
9 0.0 0.0 0.0 10 -.6541::-8 +.149E-9 +. II -.7S2E-16 +.li,YE-\l 12 .162E-6 +.149E-9 13 0.0 0.0 14 -.4b l+£-6 +.149£-9 +.:J:'IlE-5
I
5 -.1 1 £-.5 +. 11,9[-9 +.56SE-5 16 -.21 -.108£-5 +.577E-517 .216E-5 +.149E··9 +.577E-5
IS -.:'1 +.923E-6 +.577[-5 -.314£-5 +. I +.577E-5 20 -.407E-5 +.274E-5 +.577£-5 21 -.314[-5 +.3J3E-5 +.577:':-5 22 -.4D7E-5 +.339E-5 +.5771':-5 23 -.24RE-S +.3331'-5 +.S77E-5 21, -.216[-5 +.339[-5 +.577E-5 2~ .285E-5 T . 3310-5 +.577£-5 26 .248E-5 +.3391::-5 +.57710-5 27 -.]14£-5 +. 85!~E-6 +.577E-5 28 -.314£-5 -.108E-5 +.577E-5 29 -.285"-3 +.149['-9 +.57710-5 30 -.1]6E~5 -.108E-5 +.57710-5 31 .216E-5 +.923[-6 +.577E-5 +.185['-4 -.132£-4 -.738(:-4 33 +.185E-4 -.132£-4 -.73810-4 3/\ +.141 E-5 .1)21::-4 -.709£-4 35 -.654£-8 +.503E-8 +.54310-7 36 -.450E-9 +.1/+9£-9 +.185E-8 37 +.403£-4 -.1321\-4 -.738E-4
+
TOLER .... Nn£S VI..G$ NEN '2365 PROJECTII: BENAMING
b, •• S,.O." •
.:::~:~
L
'O"IO'± 3O"AM
LOAD INy-DIRECTION (model 2)
?ASSING£N VLGS N SOl
I
RVWHElDSWAA"'OE~ VLGS NEN 6.)0 AANTAl MATERIAA!..I
~
TECHNISCHE HOGESCHOOL EINDHOVEN S.CHAAl OA_~ 1"EJ«NINCNR.AFDELlNG W GH.: '7'/VV
tt:.(...-l
A-4
GROEP: WT cve. :
Load -IOOON at 37 and +IOOON at 20 in the Z-direction (model
:D
displacement displacement rotation
(m) (m) (rad)
joint in Y-d irec t ion in Z-dircction about X-axis
I +.615E-5 -.61 1£-5 -.240E-4
2 +.615£-5 -.611£-5 -.240£-4
3 +.543[-5 -.611£-5 -.240E-4
4 +.5/+3£-5 -.611 [;-5 -.2L,0£-4
5 +.543E-5 -.611E-S -.240E-4
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