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ASTM B637-12e1

Historical Revision

Standard Specification for Precipitation-Hardening and Cold Worked Nickel Alloy Bars, Forgings, and Forging Stock for Moderate or High Temperature Service

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1.1 This specification2 covers hot- and cold-worked precipitation-hardenable nickel alloy rod, bar, forgings, and forging stock for moderate or high temperature service (Table 1).

TABLE 1 Chemical Requirements

 

Element

Composition Limits, %

 

UNS N07022

UNS N07208

UNS N07252
(Formerly
Grade 689)

UNS N07001
(Formerly
Grade 685)

UNS N07500
(Formerly
Grade 684)

UNS N07750
(Formerly
Grade 688)

UNS N07718
(Formerly
Grade 718)

Carbon

0.010 max

0.04–0.08

0.10–0.20

0.03–0.10

0.15 max

0.08 max

0.08 max

Manganese

0.5 max

0.3 max

0.50 max

1.00 max

0.75 max

1.00 max

0.35 max

Silicon

0.08 max

0.15 max

0.50 max

0.75 max

0.75 max

0.50 max

0.35 max

Phosphorus

0.025 max

0.015 max

0.015 max

0.030 max

0.015 max

...

0.015 max

Sulfur

0.015 max

0.015 max

0.015 max

0.030 max

0.015 max

0.01 max

0.015 max

Chromium

20.0–21.4

18.5–20.5

18.00–20.00

18.00–21.00

15.00–20.00

14.00–17.00

17.0–21.0

Cobalt

1.0 max

9.0–11.0

9.00–11.00

12.00–15.00

13.00–20.00

1.00 maxA

1.0 maxA

Molybdenum

15.5–17.4

8.0–9.0

9.00–10.50

3.50–5.00

3.00–5.00

...

2.80–3.30

Columbium
 (Nb) + tantalum

...

...

...

...

...

0.70–1.20

4.75–5.50

Titanium

...

1.90–2.30

2.25–2.75

2.75–3.25

2.50–3.25

2.25–2.75

0.65–1.15

Aluminum

0.5 max

1.38–1.65

0.75–1.25

1.20–1.60

2.50–3.25

0.40–1.00

0.20–0.80

Zirconium

...

0.020 max

...

0.02–0.12

...

...

...

Boron

0.006 max

0.003–0.010

0.003–0.01

0.003–0.01

0.003–0.01

...

0.006 max

Iron

1.8 max

1.5 max

5.00 max

2.00 max

4.00 max

5.00–9.00

remainderB

Copper

0.5 max

0.1 max

...

0.50 max

0.15 max

0.50 max

0.30 max

Nickel

remainderB

remainderB

remainderB

remainderB

remainderB

70.00 min

50.0–55.0

Tantalum

0.2 max

0.1 max

...

...

...

...

...

Columbium   (Niobium)

...

0.2 max

...

...

...

...

...

Tungsten

0.8 max

0.5 max

...

...

...

...

...

 

UNS N07080
(Formerly
Grade 80A)

UNS N07752

UNS N09925

UNS N07725

 

 

 

Carbon

0.10 max

0.020–0.060

0.03 max

0.03 max

 

 

 

Manganese

1.00 max

1.00 max

1.0 max

0.35 max

 

 

 

Silicon

1.00 max

0.50 max

0.5 max

0.20 max

 

 

 

Phosphorus

  ...

0.008 max

0.03 max

0.015 max

 

 

 

Sulfur

0.015 max

0.003 max

0.03 max

0.010 max

 

 

 

Chromium

18.00–21.00

14.50–17.00

19.5–22.5†

19.00–22.50†

 

 

 

Cobalt

...

0.050 max

...

...

 

 

 

Molybdenum

...

...

2.5–3.5

7.00–9.50

 

 

 

Columbium
 (Nb) + tantalum

...

0.70–1.20

0.5 max (Nb only)

2.75–4.00

 

 

 

Titanium

1.80–2.70

2.25–2.75

1.9–2.40

1.00–1.70

 

 

 

Aluminum

0.50–1.80

0.40–1.00

0.1–0.5

0.35 max

 

 

 

Boron

...

0.007 max

...

...

 

 

 

Iron

3.00 max

5.00–9.00

22.0 min

remainderB

 

 

 

Copper

...

0.50 max

1.5–3.0

...

 

 

 

Zirconium

...

0.050 max

...

...

 

 

 

Vanadium

...

0.10 max†

...

...

 

 

 

Nickel

remainderB

70.0 min

42.0–46.0

55.0–59.0

 

 

 

A If determined.
B The element shall be determined arithmetically by difference.
† Chromium content was corrected editorially.
† Vanadium content was corrected editorially

1.2 The values stated in inch-pound units are to be regarded as standard. The values given in parentheses are mathematical conversions to SI units that are provided for information only and are not considered standard.

1.3 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to become familiar with all hazards including those identified in the appropriate Material Safety Data Sheet (MSDS) for this product/material as provided by the manufacturer, to establish appropriate safety and health practices, and determine the applicability of regulatory limitations prior to use.


This specification covers hot- and cold-worked precipitation-hardenable nickel alloy rod, bar, forgings, and forging stock for high-temperature service. Chemical analysis shall be performed on the alloy and shall conform to the chemical composition requirement in carbon, manganese, silicon, phosphorus, sulfur, chromium, cobalt, molybdenum, columbium, tantalum, titanium, aluminum, zirconium, boron, iron, copper, and nickel. The material shall follow recommended annealing treatment, solution treatment, stabilizing treatment, and precipitation hardening treatment. Tension testing, hardness testing and stress-rupture testing shall be performed on the material and shall comply to the required tensile strength, yield strength, elongation, reduction in area, and Brinell hardness.


SDO ASTM: ASTM International
Document Number B637
Publication Date May 1, 2012
Language en - English
Page Count 7
Revision Level 12e1
Supercedes
Committee B02.07
Publish Date Document Id Type View
Dec. 1, 2023 B0637-23 Revision
Nov. 1, 2018 B0637-18 Revision
Oct. 1, 2016 B0637-16 Revision
Oct. 1, 2015 B0637-15 Revision
May 1, 2012 B0637-12E01 Revision
May 1, 2012 B0637-12 Revision
Dec. 1, 2006 B0637-06E01 Revision
Dec. 1, 2006 B0637-06 Revision
June 10, 2003 B0637-03 Revision
April 10, 1998 B0637-98 Revision
June 1, 2011 B0637-06R11 Reaffirmation