Analog Computers

Reference / Paper · 1968

Analysis of Rolling Theory by Analog Computer — Karman's Differential Equation —

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Technical Information Series No. 8 from Hitachi's Analog-Hybrid Computer line, demonstrating how an analog computer automatically solves Karman's differential equation to determine pressure distribution and rolling load during metal rolling. The document derives the governing equations (boundary-value problem, projected contact length, elastic deformation), describes the analog circuit design with five integrators and a program controller, and validates results against digital computer solutions across six parametric cases. Computation time is on the order of seconds versus minutes for digital approaches.

Manufacturer
Hitachi
Year
1968
Type
Reference / Paper
Language
English
Learning track
specific applications
Pages
14
Credit
Hitachi, Ltd. Analog-Hybrid Computer Technical Information Series No. 8, 1968. Printed in Japan.
  • Hitachi
  • rolling theory
  • Karman differential equation
  • pressure distribution
  • analog computation

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Analysis of Rolling Theory by Analog Computer — Karman's Differential Equation —

HITACHI Analog-Hybrid Computer Technical Information Series No.8 Analysis of Rolling Theory by Analog Computer — Karman's Differential Equation — 1968 Hitachi, Ltd. printed in Japan Analysis of Rolling Theory by Analog Computer (Karman's Differential Equation) §1. Introduction Since Karman's differential equation cannot be solved strictly analytically, Tselikov, Trinks, Nadai, Hill and others obtained its solution through approximation or construction by various means, which, however, require considerable labor. The analysis by analog computer presented here is an automatically converging calculation system using an auto- matic programming system, markedly saving calculation time, e.g. determination of a pressure distribution curve, roll radius or projected contact length etc. takes only 1 ~ 2 minutes. Besides, in the logical operation and control of analog computer, reverse time operation system is adopted, widely differing from the conventional boundary value problem. The outline of this analysis will be described below. §2. Outlines of Rolling Assume that a plate of thickness h; is rolled to thickness h,. While circumferential speed of roll, v, is constant everywhere, material speed at roll exit v', is always faster than that at roll entrance v',, since the material is elongated by rolling. In Fig. 1, there- fore, material speed of hatched area A is slower than v, and material is drawn in toward roll exit by frictional force against the roll face, while material speed of hatched area B is faster than v, preventing flow of material due to frictional force against the roll face. At the mid-point between A and B, e.g., Y in Fig. 1, material speed is equal to v, elimi- nating mutual slipping. Hence point Y is called neutral point or watershed, and ¢, roll angle at neutral point. The absolute value of frictional force between roll and material is represented by a single-peaked curve with maximum at neutral point, as illustrated in Fig. 1. When horizontal pressure q is applied to a block of material which is deformed by vertical pressure p as shown in Fig.2, deformation requires vertical pressure ptq to overcome the effect of horizontal pressure q. Accordingly, distribution of vertical pressure takes thatch-shaped curve as shown in Fig. 1. - §3. Derivation of Equation eo Ns Projected Contact Length Frictional force at roll face If the roll is assumed not to deform in the course of rolling, projected contact length L (to be represented by X hereinafter) is given by Eq. (1), Distribution of vertical Pressure between roll and material exactly, or by Eq. (2), in approximation. Fig. 1. Rolling Process 2 X, = / RAh - Bie (1) 4 P p+q X, =. RAh (2) ee cel In case that the segment of roll in contact with —+ —¢ material is elastically deformed in the course of roll- — ing, such as cold rolling of thin plate, the actual | | | I projected contact length is longer than X,, as given by p ptq Hitchcock's formula, Eq. (3) F = 2 = ' Fig. 2. Deformation under - /[8R (1 -7?)p'm 8R (1 -7*)p'm g. 2. sat i xE | +Rah+ xE (3) Plane Stress a Or, more frequently, using modified roll radius R' caused by elastic deformation, which can be represented by Eq. (4) according to Hitachicock, X ' may be represented by Eq. (5) in place of Eq. (3). pile 16:(1-=72): “p (4) R TE bAh Xt= [R'Ah (5) where +: - Poisson's ratio E: Young's modulus b: Width of material pm: mean rolling pressure Ps rolling load Rolling load P is represented by Eq. (6) as a function of rolling pressure p as in Eq. (6). x" P = bf pdx (6) fe) 3-2. Karman's Differential Equation In discussion of stress equilibrium at a minute segment bounded by sections parallel to roll shaft, as the hatched area in Fig.3, Karman derived a differential equation in the following way, assuming 9 hypotheses given below. 1. Transverse expansion of material can be neglected. 2. Coefficient of friction «is uniform everywhere. 3. Additional shearing strain does not occur. 4. Elastic deformation does not occur. 5. Material is plastic-rigid. hy h+dh h < he dx-=) 6. Since two-dimensional constraint strain resistance (two-dimensional yielding stress S) is 1.15 times simple compressive strain resistance <——— FE Eke (So), the following formula holds be- tween maximum and minimum principal stress, S, and S;, respective- Fig.3 Pressure Equilibrium ly. _ in Rolling S=1.15S)=Si -S; 7. Strain resistance S is uniform throughout arc of contact. 8. Roll speed is constant. 9. Horizontal stress q of material distributes uniformly in the direction of thickness. That is, in discussing the equilibrium of horizontal stress at the hatched area in Fig. 3, transverse extension can be assumed always 1, to omit calculation. Horizontal stress 4Q acting on the small portion of material through the cross- section is: ; AQ = (h+dh)(q+dq) - h-q dx F Pr ae r *sing Hence, 4Q = hq + dh-q + dq-h+ dh-dq - hq = dh-q + dq-h d(h-q) (7) Since horizontal component AQ of stress acting on the small portion of material through the surface is the sum of horizontal component of pressure vertical to roll face pr and of horizontal h+dh q+dq—™ component of frictional force pr acting to the sur- oe face of material, horizontal stress on the one side of material 4 Q/2 is given by (8), (8') or (8"). a2 aQ dx dx 5 7 ese ) wine = # (Pray) cos 6 (8) Fig.4 Details of Stress =?,(tang - tan f) dx (8!) Equilibrium where # = tané. While Fig. 4 gives stress equilibrium at the entrance of roll, the direction of frictional force is Ap=APreosé nee reversed at the exit of roll, thus giving Eq. (8") from Eq. (8'). Pr A = ?; (tan oytan f) dx (8") yi = : 2255) Furthermore, putting compressive force and iy compressive stress acting on material in dx from the HII | roll surface in Fig.5 as Apr and pr, respectively, Pp the following relation holds: dx dx Fig.5 Relation between p If vertical component of Apr is put as and pr Ap = Apr cos @ and compressive stress in the vertical direction as p Ap = Apr cos 6 = p.dx (10) Accordingly, the following relation always holds from Eq. (9) and (10), p=pr y (11) Hence, p and pr will not be distinguished in the subsequent discussion. From Eqs. (7) and (8'), Karman's differential equation is derived as an equation for equilibrium of AQ as below: d (39) = p(tano Ftan 1) dx (12) where minus sign refers to entrance side and plus sign to exit side. Since vertical compressive stress p is sum of horizontal compressive stress and of stress due to two-dimensional constraint strain resistance, q+k=P (13) where k is a function of h, as represented below k=k@) (14) 1 From Fig. 6, R ae R'cos @ Be Bet R' - R'cos@ ie h 4/2 hd [_h/2) | ha/2 hence=—>4 RV = RPS ei bait ert) | Do R Sir ; Fe tee iez ioe sB+R'-R! (1-32)") 2 a Fig.6 Deformation Process And tan @ = x of Material R' cos@ xX i ri (16) 1x TP siege R 2R! As boundary conditions, tension to material at entrance and exit, ,, and o2, should satisfy the following relations: where X = 0, Ps Io kyi=" g22 BP Cr) k = ke h = he P where X=X,', P=1.15k: - o=B Ph he vw k = ki (18) ac ve NS 7 ~“ 7 h =h, Sie? p+ Pz 1 § 4. Operation of Analog Computer ‘ xX 0 1 4-1. Construction of Automatic Program . Since pressure distribution p is as illustrated in Fig. 7, for projected contact length X, of roll without Fig.7. Pressure elastic strain, p” value is calculated starting from the distribution given initial value p, in the direction of Xi: ~ 0, and the value p' at X= 0 is memorized. Then at X = 0, Giving initial values p, for p* and p' for p’, calculating simultaneously in the direction 0 >X:, to obtain pressure distribu- tion curve p as shown by thick lines in Fig.7. At the same time, determining rolling load P, radius R! of roll with elastic strain is obtained from Eq. (4). From R! and Eq.(5), new projected contact length X' is determined, and with this the above calculation is repeated in the same way. By repeating these trial calculations, X', R', p and P converge to finite values, which are solutions of Karman's differential equation. A flow chart for the automatic program and time chart for its control process are given below. & in(p-10) = plian 6 <a) dx Calculator of p™ Calculator of independent variable x 0O>x1' or x;" 70 2 th(p-k)) = p(tang +n) dx Calculator of p* Summation of p- and p*, calculator of pressure distribution p (pressure distribution) x,' (projected contact length) Calculation of X,', calculator R! (Roll radius with elastic strain) Calculation of P, calculator of rolling load load) Calculation of R', calculator of elastic Strain of roll of projected contact length P (rolling Fig. 8 Automatic Program System Calculate HOLD Calculate xX - lat Rest Rest calculator X,' +0 atX=0 0- x; e e Calculate HOLD Calculate = in reversed at in normal js time from x =0 time from Beet nee K=X! xX =0 Calculate 4 in normal P' -calculator Rest Rest timesfrom Rest Rest xX =0 p-calculator Rest Rest Calculate Rest Rest P-calculator Rest Rest Calculate HOLD Rest R'-calculator Rest Rest Calculate HOLD Rest X,'-calculator HOLD HOLD HOLD Calculate HOLD Fig.9 Control Process at the Program Controller Composition of Analog Computer Circuit h (1) Function from for k = k ra 1 While function of k may take various forms, this calculation adopted that given in Fig. 10. k kg/mm? (2) Synthesis circuit for p~ and pt The circuit shown in Fig. 12 is used for synthesis, i.e., in general, taking lower segments of two intersecting curves as illustrated in Fig. 11. 20 (3) Numerical values ; ‘ ; ; bh 0.2 04 0.6 08 1.0 4x hi 1.0 mm Fig.10 Function form of K he 0.7mm Bh 0¢3 b 1,000 mm P- R 270 mm se 8 kg/mm? oo 12kg/mm? Fig.11 Synthesis of p” and p* u 0.07 E 2.1 x 10‘kg/mm’* v 0.3 (4) Block diagram of analog computer Fig.12 Circuit for Synthesis Block diagram of the analog computer is given in Fig.13, in which there are five integrators controlled separately by the sequence shown in Fig. 14. Control time | 3 ~5 sec. | X1' sec/mm |3 ~ 5 sec| X:' sec/mm | 3 ~5 sec etree 2 | RESET | COMPUTE] HOLD | COMPUTE | RESET soa. in| RESET | RESET RESET | COMPUTE | RESET Eh OR in) RESET | RESET RESET | COMPUTE | HOLD Aa awn in| HOLD HOLD HOLD | HOLD COMPUTE oe OFF OFF ON ON OFF Fig.14 Operation control sequence for program controller et 34 nt 00r (74 -4guny)OOt (4) 008 9s (77-9 ues) 4% I ' (7749 wy) g~ y I I Zz. "os\ [euB}s jorjU09 gau+ “Zot T mi9L 34S Z°ON = of ot g 49{]01qU0D wesbosg 4 d I guryt-= Sf ul "Wa {t)}— T Zz \ NSA (:U/e X7- a 00F"0 ENSURE eT Add+ Xo. As2° Riches oset enna JL 9 I is ie x 008 (6) Aga, 1) 008 vos o=¢6 ¢ na: aA td (ea-1)9t'°) 4 OF uz 00S I Wa+ W I ‘ya ( (7-9 ua) or (Se wr 00% 9% } (9) ext Wry 7 1x x soo NO ¥ <i 1G) ac Re Tt 008"0 ° = Rick! em * yo0s I 00s — + or I ee a Om 4” u Aqu- atta *y [euBys jo1;U09 Yr , WAL US FON I 25 6 y Aa[[4WOD wessorg I ost"0 I ws YX 00S (or 4 LL ie! S$ Aaa ba I v »¢ fe N 00s I (*9-"¥ST°0)' 4 T- dnosb_y ZAG I 440 Wg, 008 v = om 06 | 7 rat Ty fi — da fas (4-4) 008. (4-4) 208 aa ne Calculating conditions R=203mm h, =3.63mm Rolling prossure h, =2.54mm (kg/mm? ) wu =0.224 t,=tr=0 60 4 ————— _ Solution obtained by eigital computer If \ == ----- Solution obtained by analog if Computer i ——-——-- Strain resistance Value 40 - y, \ se + L. 5.0 10.0 15.0 Fig 15 Exampls of digital and analog computation 7 Rolling pressure (kg/mm*) 60 = Calculation conditions R =203mm h ,=3.63mm h 2=2.54mm “=0.224 t,=t,=5.0kg/mm* Solution obtained by digital computer ———-——-— Solution obtained by analog computer —— -———- Strain resistance value te 5.0 Fig 16 Examples of digital and analog computation @) 10.0 15.0 (mm) Calculating conditions R=203mm h, =3.63mm h, =2.54mm we =0.224 Rolling pressure Pp t, =t¢ =10kg/mm? (kg/mm? ) S =20kg/mm? —_ Solution obtained by 30-4 digital computer p=. an Le Solution obtained by analog computer — - — - Strain resistance value > —+> 4 5.0 10.0 . 15.0 Fig 17 Examples of digital and analog computation () X (mm) =H6— Rolling pressure | p (kg/mm? ) 30 - / \ Calculating conditions R=203mm h, =3.63mm h, =2.54mm ft =0.112 107 tp =tr= 0 Solution obtained by digital computer -----—-- Solution obtained by analog computer ——— Strain resistance value ~~ + 5.0 10.0 15.0 X ( Fig 18 Examples of digital and analog computation 4 an) -ll- Calculating conditions R=203mm h, =3.63mm h, =2.54mm uw =0.112 Rolling pressure t, =te =5.0kg/mm? (kg mm?) fp ees Solution obtained by digital computer Se Solution obtained by 30- analog computer — -— - Strain resistance value 10- 5.0 10.0 15.0 Fig 19 Examples of digital and analog computation %, i -12- Calculating conditions R=203mm Rolling pressure h, =3.63mm h, =2.54mm 100- # =0.112 S =80.0( 7 +0.00817)°3 aN (kefmm®.) Solution obtained by digital computer Solution obtained by analog computer Strain resistance value 50 0 ~ T 7 5.0 10.0 15.0 ———> X (mn) Fig 20 Examples of digital and analog computation 6 SAVY