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IONITRIDING MATERIAL GUIDE

MATERIAL CORE Rc SURFACE HV`5
(Rc equiv.)

TOTAL CASE mm
(inches)

1020,1045, CAST IRON 14-18 FILE HARD 0.0005" 0.05-0.25

(0.002 - 0.010)

8620, 9310, 9315, P6 26-32 500-653 (49-58) 0.30-0.71

(0.012 - 0.028)

4130,4140 28-32 550-653 (52-58) 0.20-0.61

(0.008 - 0.024)

4340 28-32 500-600 (49-55) 0.20-0.61

(0.008 - 0.024)

P20 28-36 636-745 (57-62) 0.20-0.50

(0.008 - 0.020)

NITRALLOY 135M 28-36 900- 1150 (67-71) 0.20-0.50

(0.008 - 0.020)

A2 54-56 820- 1076 (65-70) 0.13-0.25

(0.005 - 0.010)

D2, D4, D6 57-59 820-1076 (65-70) 0.13-0.25

(0.005 - 0.010)

H13, S7 45-50 900-1150 (67-71) 0.10-0.30

(0.004 - 0.012)

M2, M42, ASP 60-65 1000- 1250 (69-72) 0.013-0.05

(0.0005-0.002)

304, 316 S.S. 0 (Rb 80) 745-865 (62-66) 0.05-0.10

(0.002 - 0.004)

15-5, 17-4 PH S.S. 31 -38 745-865 (62-66) 0.10-0.20

(0.002 - 0.008)

420, 436 S.S. 24-38 950-1100 (68-70) 0.10-0.20

(0.004 - 0.008)

TOTAL CASE DEPTH: Aerospace material specification AMS 2759/8 defines as the maximum depth below a surface at which Rc 5, or equivalent hardness, above core hardness is achieved.

EFFECTIVE CASE DEPTH: Aerospace material specification AMS 2759/8 defines as the maximum depth below a surface at which Rc 50, or equivalent hardness, is achieved.

HARDNESS LEVEL: Dependant on chemistry of the material ionitrided; readings are taken in Vickers(HV5), Rockwell(R15N) and Knoops.

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