a I ;T_r -ra _ _l-.-rx.,'0!.$/d i_ l-^-lt.r-0.rnD/d i | \dw(nca1 ! -- t-- f -o- I -l- . :.; _,;--- -;2-! - - | --t/,---z i ,--' ,----i -t/.--' ,''-/''i 0.1 1l r I. I - -a-t1 r-10a56/l|u1 .;;' 'a'' *d\doa.t I a: l 1i a- I f-"* l-^-u ' lllf Fig. 8. lhr<strong>in</strong>tion of irc nonnal force to the flnnk suiace as a functiott of cutl<strong>in</strong>g paranrctet: a - speed; b - feed; c - depth ofcuu<strong>in</strong>g rioration of the physical cornponents is much weaker. As a result, the fnction force J? <strong>in</strong>creases for 337o,while the normal force F17 is approximately constant ancj so their ratio is situated between 0.15...0.21. The feed's <strong>in</strong>fluence on the friction force F (figure 7b), the normal force Fry (figure Bb) and the ratio between them (figure 9b) is expla<strong>in</strong>ed based on rhe fact that the tear<strong>in</strong>g angle ((p) irtcreases and the longitud<strong>in</strong>al coefficient of plastical cornpression (Cni) decreases as the feeci is higher. When the feed <strong>in</strong>creases frorn 0.1 to 0.-i mn/rot, the friction force,tr and the normal one,l.y <strong>in</strong>crease fronl 25.7 N to 62.1/y' and fron 103.1 N to 351.2 { respecrively. The decreas<strong>in</strong>g tendency of the friction coefficient as the feed <strong>in</strong>creases can be expla<strong>in</strong>ed because of the slower <strong>in</strong>crease of the tangential friction stress on that surface, ascrib<strong>in</strong>q to the normal stress due to thermal effect. The <strong>in</strong>fluence of the cutt<strong>in</strong>g depth on the friction force I (figure 7c), the normal force -[,y (figure 8c) and the ratio betu,een thern (figure 9c) <strong>in</strong> oblique turn<strong>in</strong>g of OLC 45 steel, shows that the values of these components <strong>in</strong>crease clue to thernlal stress, as a result oflclrver snecific prcssitlns on c()ntirct srrrftrcc ,4. Fig. 9. Variation of tltc cutt<strong>in</strong>g specd and the ftictiort coefJicicnt as jitnctiott of cutt<strong>in</strong>g paranrcters: a - spced: l> - fced: c - tleptlt of cuuitrg 5. CONCI,USION The results obta<strong>in</strong>ed us<strong>in</strong>g the methodology proposed above are close enough to those obta<strong>in</strong>ed by other authors <strong>in</strong> their exper<strong>in</strong>rents [4]. The friction force and the friction coefficient on the flank surface of the tool depend on the cutt<strong>in</strong>g pzrrameters. and their values decrease with an average of 251)b for 100-800 rnlrnitt cuttiug speeds, as a result of a rnuch lnore ilttense therntal effect, <strong>in</strong>fluenc<strong>in</strong>g the mechanical chiiracter-istic.s of the material. NOTATIONS: l) - cutt<strong>in</strong>g speed; f ,, n Fa lty Ty, oy Tn, o,z Tt,r,r, (Pd - ship's section; - friction coefficient on the flank surface; - fricrtion coefficient on the rake surface; - tangential, notrr. al stress to the flank surface; - tangeritial. nolllal stress to the rake surface; - maximum tangential stress to rake sur{ace; - base plune; 1A t+ Ii'ibolog, itt itftlustty, \blunre 20, <strong>No</strong>. l, 199g.
(A") - tangent plane to the flank surface, <strong>in</strong> Nl; (,\) - tangent plane to the rake surface, <strong>in</strong> M; (P) - pressure p)ane (normal to the effect. speed) vector i. - the resriltant speed, <strong>in</strong> M; T - tool angles: cutt<strong>in</strong>g edge angle, rake angle, tlank angle, cutt<strong>in</strong>g edge <strong>in</strong>cl<strong>in</strong>ation angle; K,f ,G,,1 - tool angles: cutt<strong>in</strong>g edge angle, rake angle, tlank angle, cutt<strong>in</strong>g edge <strong>in</strong>cl<strong>in</strong>ation angle; Ke,Te, ee,,l.. - work<strong>in</strong>g angles: i,r'ork<strong>in</strong>g cutt<strong>in</strong>g edge angle, rvork<strong>in</strong>g m<strong>in</strong>or cutt<strong>in</strong>g edge <strong>in</strong>cl<strong>in</strong>ation angle; rl - angle bchveen the chip's flow<strong>in</strong>g direction and the vector N, measured <strong>in</strong> (Ay) plane; fu - cutt<strong>in</strong>g force; FD Fv Fz - conponents r.lf the cutt<strong>in</strong>g force along lhe axes of the lvl.ryz si/stem: Fy - plastic deformation force; f,f -tnctr()nforce; Cat - plastic c.leformation coefficient. 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