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No. 1, 1998 - Tribology in Industry

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a<br />

I<br />

;T_r -ra _<br />

_l-.-rx.,'0!.$/d i_<br />

l-^-lt.r-0.rnD/d i<br />

| \dw(nca1 !<br />

-- t--<br />

f<br />

-o-<br />

I<br />

-l-<br />

. :.; _,;--- -;2-! - -<br />

| --t/,---z<br />

i ,--'<br />

,----i<br />

-t/.--'<br />

,''-/''i<br />

0.1<br />

1l<br />

r I. I -<br />

-a-t1 r-10a56/l|u1<br />

.;;'<br />

'a''<br />

*d\doa.t<br />

I<br />

a:<br />

l<br />

1i<br />

a- I<br />

f-"*<br />

l-^-u<br />

'<br />

lllf<br />

Fig. 8. lhr<strong>in</strong>tion of irc nonnal force to the flnnk<br />

suiace as a functiott of cutl<strong>in</strong>g paranrctet:<br />

a - speed; b - feed; c - depth ofcuu<strong>in</strong>g<br />

rioration of the physical cornponents is much weaker. As<br />

a result, the fnction force J? <strong>in</strong>creases for 337o,while the<br />

normal force F17 is approximately constant ancj so their<br />

ratio is situated between 0.15...0.21.<br />

The feed's <strong>in</strong>fluence on the friction force F (figure 7b),<br />

the normal force Fry (figure Bb) and the ratio between<br />

them (figure 9b) is expla<strong>in</strong>ed based on rhe fact that the<br />

tear<strong>in</strong>g angle ((p) irtcreases and the longitud<strong>in</strong>al coefficient<br />

of plastical cornpression (Cni) decreases as the feeci<br />

is higher. When the feed <strong>in</strong>creases frorn 0.1 to 0.-i mn/rot,<br />

the friction force,tr and the normal one,l.y <strong>in</strong>crease fronl<br />

25.7 N to 62.1/y' and fron 103.1 N to 351.2 { respecrively.<br />

The decreas<strong>in</strong>g tendency of the friction coefficient<br />

as the feed <strong>in</strong>creases can be expla<strong>in</strong>ed because of the<br />

slower <strong>in</strong>crease of the tangential friction stress on that<br />

surface, ascrib<strong>in</strong>q to the normal stress due to thermal<br />

effect.<br />

The <strong>in</strong>fluence of the cutt<strong>in</strong>g depth on the friction force<br />

I (figure 7c), the normal force -[,y (figure 8c) and the<br />

ratio betu,een thern (figure 9c) <strong>in</strong> oblique turn<strong>in</strong>g of OLC<br />

45 steel, shows that the values of these components<br />

<strong>in</strong>crease clue to thernlal stress, as a result oflclrver snecific<br />

prcssitlns on c()ntirct srrrftrcc ,4.<br />

Fig. 9. Variation of tltc cutt<strong>in</strong>g specd and the ftictiort<br />

coefJicicnt as jitnctiott of cutt<strong>in</strong>g paranrcters:<br />

a - spced: l> - fced: c - tleptlt of cuuitrg<br />

5. CONCI,USION<br />

The results obta<strong>in</strong>ed us<strong>in</strong>g the methodology proposed<br />

above are close enough to those obta<strong>in</strong>ed by other authors<br />

<strong>in</strong> their exper<strong>in</strong>rents [4]. The friction force and the<br />

friction coefficient on the flank surface of the tool depend<br />

on the cutt<strong>in</strong>g pzrrameters. and their values decrease<br />

with an average of 251)b for 100-800 rnlrnitt cuttiug<br />

speeds, as a result of a rnuch lnore ilttense therntal effect,<br />

<strong>in</strong>fluenc<strong>in</strong>g the mechanical chiiracter-istic.s of the material.<br />

NOTATIONS:<br />

l) - cutt<strong>in</strong>g speed;<br />

f ,, n<br />

Fa<br />

lty<br />

Ty, oy<br />

Tn, o,z<br />

Tt,r,r,<br />

(Pd<br />

- ship's section;<br />

- friction coefficient on the flank surface;<br />

- fricrtion coefficient on the rake surface;<br />

- tangential, notrr. al stress to the flank surface;<br />

- tangeritial. nolllal stress to the rake surface;<br />

- maximum tangential stress to rake sur{ace;<br />

- base plune;<br />

1A<br />

t+<br />

Ii'ibolog, itt itftlustty, \blunre 20, <strong>No</strong>. l, 199g.

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