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A comprehensive tool-wear/tool-life performance model in the ...

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ARTICLE IN PRESS<br />

P.W. Marksberry, I.S. Jawahir / International Journal of Mach<strong>in</strong>e Tools & Manufacture 48 (2008) 878–886 883<br />

-Y (j)<br />

4<br />

80˚<br />

+Y (j)<br />

1<br />

2<br />

3<br />

~50-mm<br />

5<br />

16°<br />

+X (i)<br />

+X (i)<br />

4<br />

1<br />

2<br />

5<br />

3<br />

-Z (k)<br />

[1] Removable Hardened Steel Nozzle Holder<br />

[2] Sta<strong>in</strong>less Steel Adjustable Nozzle<br />

[3] Tool Holder<br />

[4] Indexable Cutt<strong>in</strong>g Tool Insert<br />

[5] Tool Holder Carousel (4 qty)<br />

Nozzle to Cutt<strong>in</strong>g Tool Relationship (vector notation)<br />

i, j, k (+X, +Y, +Z) Vectors (+/- 2-mm)<br />

i. = -48-mm j. = -8-mm k. = -14-mm<br />

Fig. 3. Nozzle to cutt<strong>in</strong>g <strong>tool</strong> to workpiece orientation.<br />

Table 4<br />

Fixed mach<strong>in</strong><strong>in</strong>g and mist spray delivery parameters<br />

Table 5<br />

Design of experiments<br />

Parameter<br />

Description<br />

Control factors Levels Description of levels<br />

Cutt<strong>in</strong>g <strong>tool</strong><br />

material<br />

Cutt<strong>in</strong>g <strong>tool</strong><br />

geometry<br />

Cutt<strong>in</strong>g<br />

parameters<br />

Al 2 O 3 , alum<strong>in</strong>um oxide (supplier: Kennametal CNMG<br />

432 ESA AC2000)<br />

Type: grooved chip breaker<br />

Relief angle: 01 (side), 01 (end)<br />

Cutt<strong>in</strong>g edge angle: 51 (side), 51 (end)<br />

Tool nose radius: 0.8 mm<br />

Depth of cut: 3.2 mm<br />

Cutt<strong>in</strong>g speed: 4 m/s<br />

Feed: 0.3 mm/rev<br />

Metal removal rate: 11,520 mm 3 /s<br />

MWF type Straight oil, Cooluble 2210<br />

Soluble—water miscible, Cimperial 1011<br />

Semi-syn<strong>the</strong>tic—water miscible, TRIM SC235<br />

Syn<strong>the</strong>tic—water miscible, Hocut 763<br />

Atomization<br />

system<br />

Atomization type: co-axial air blast atomization<br />

Mach<strong>in</strong>e: MSK-G 100—MicroJet<br />

Air pressure: 5 psi<br />

Nozzle: sta<strong>in</strong>less steel<br />

The 95% confidence <strong>in</strong>terval was determ<strong>in</strong>ed at 0.85 and<br />

1.00-mm for <strong>the</strong> dom<strong>in</strong>ant <strong>tool</strong>-<strong>wear</strong> pattern (W BL ) for dry<br />

cutt<strong>in</strong>g us<strong>in</strong>g a sample size of 20.<br />

Modifications to <strong>the</strong> ASTM tapp<strong>in</strong>g torque procedure<br />

were carried out to dist<strong>in</strong>guish <strong>the</strong> primary MWF functions<br />

us<strong>in</strong>g two different reamed hole diameters 5.55 and<br />

5.48 mm to characterize cool<strong>in</strong>g and lubricity, respectively.<br />

Fig. 4 shows <strong>the</strong> ASTM tapp<strong>in</strong>g torque results for each of<br />

MWF volumetric flow rate (ml/h) 4 (1) 20<br />

(2) 40<br />

(3) 80<br />

(4) 160<br />

MWF type 4 (1) Straight oil<br />

(2) Soluble oil<br />

(3) Semi-syn<strong>the</strong>tic<br />

(4) Syn<strong>the</strong>tic oil<br />

Nozzle position 3 (1) Rake face<br />

(2) Flank face<br />

(3) Chip<br />

<strong>the</strong> MWFs used <strong>in</strong> this work while vary<strong>in</strong>g <strong>the</strong> reamed hole<br />

diameter. Test results were collected from a Microtap<br />

Megatap 2, Labtop II G8 mach<strong>in</strong>e us<strong>in</strong>g standard 1018<br />

steel test bar. A form<strong>in</strong>g tap type was used <strong>in</strong> <strong>the</strong> test at a<br />

size of M6 1 pitch. Tapp<strong>in</strong>g speed was held constant at<br />

1000 rpm or 18.8 m/m<strong>in</strong>.<br />

5. Results<br />

A <strong>comprehensive</strong> study has been conducted to<br />

validate <strong>the</strong> new <strong>tool</strong>-<strong>life</strong>/<strong>tool</strong>-<strong>wear</strong> relationship for<br />

NDM. A summary of <strong>the</strong> study is presented <strong>in</strong><br />

Tables 6–8 and Fig. 5.

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