ASTM B564-22

Standard Specification for Nickel Alloy Forgings

ABSTRACT
This specification covers nickel alloy forgings. These alloys are classified into different grades according to their chemical composition. A chemical analysis shall be employed on each alloy in order to determine its chemical composition. Grain size and mechanical properties like tensile strength, yield strength, and elongation shall be measured. A tension test and nondestructive ultrasonic test shall be done on each specimen.
SCOPE
1.1 This specification2 covers forgings of:    
Alloy Type  
UNS Number(s)  
Fe-Ni-Cr-Mo-N  
N08367  
Low-carbon Cr-Ni-Fe-N  
R20033  
Low-carbon Ni-Cr-Mo  
N06035, N06058, N06059, N06044  
Low-carbon Ni-Cr-Mo-Cu  
N06200  
Low-carbon Ni-Cr-Mo-W  
N06686  
Low-carbon Ni-Fe-Cr-Mo-Cu  
N08031, N08034  
Low-carbon Ni-Mo-Cr  
N10276, N06022, N10362  
Low-carbon Ni-Mo-Cr-Ta  
N06210  
Ni  
N02200  
Ni-Co-Cr-Si  
N12160  
Ni-Cr-Al  
N06699  
Ni-Cr-Co-Mo  
N06617  
Ni-Cr-Fe  
N06600, N06603, N06690  
Ni-Cr-Fe-Al  
N06025  
Ni-Cr-Fe-Si  
N06045  
Ni-Cr-Mo-Nb  
N06625  
Ni-Cr-Mo-Si  
N06219  
Ni-Cr-Mo-W  
N06110  
Ni-Cr-W-Mo  
N06230  
Ni-Cu  
N04400  
Ni-Fe-Cr  
N08120, N08800, N08810, N08811  
Ni-Fe-Cr-Mo-Cu  
N08825, N08827  
Ni-Fe-Cr-W  
N06674  
Ni-Mo  
N10665, N10675, N10629  
Ni-Mo-Cr-Fe  
N10242, N10624  
1.1.1 The nickel-iron-chromium alloys are UNS N08120, UNS N08800, UNS N08810, and UNS N08811. Alloy UNS N08800 is normally employed in service temperatures up to and including 1100 °F (593 °C). Alloys UNS N08810, N08120, and UNS N08811 are normally employed in service temperatures above 1100 °F (593 °C) where resistance to creep and rupture is required, and are annealed to develop controlled grain size for optimum properties in this temperature range.  
1.1.2 Nickel-iron-chromium-tungsten alloy UNS N06674 is normally employed in service temperatures above 1100 °F (593 °C) where resistance to creep and rupture is required, and is annealed to develop optimum properties in this temperature range.  
1.1.3 Nickel-chromium-molybdenum-columbium (UNS N06625) products are furnished in two grades of different heat-treated conditions:
1.1.3.1 Grade 1 (Annealed)—Material is normally employed in service temperatures up to 1100 °F (593 °C).
1.1.3.2 Grade 2 (Solution annealed)—Material is normally employed in service temperatures above 1100 °F (593 °C) where resistance to creep and rupture are required.
Note 1: Hot-working or reannealing may change properties significantly, depending on working history and temperatures.  
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 Safety Data Sheet (SDS) for this product/material as provided by the manufacturer, to establish appropriate safety, health, and environmental practices, and determine the applicability of regulatory limitations prior to use.  
1.4 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

General Information

• Status: Published
• Publication Date: 31-Mar-2022
• ICS: 77.150.40 - Nickel and chromium products
• Technical Committee: B02 - Nonferrous Metals and Alloys
• Drafting Committee: B02.07 - Refined Nickel and Cobalt and Their Alloys

Standards Content (Sample)

This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the
Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
Designation:B564 −22
Standard Specification for
1
Nickel Alloy Forgings
This standard is issued under the fixed designation B564; the number immediately following the designation indicates the year of
original adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. A
superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
This standard has been approved for use by agencies of the U.S. Department of Defense.
1. Scope* 1.1.3 Nickel-chromium-molybdenum-columbium (UNS
2 N06625) products are furnished in two grades of different
1.1 This specification covers forgings of:
heat-treated conditions:
Alloy Type UNS Number(s)
1.1.3.1 Grade 1 (Annealed)—Material is normally em-
Fe-Ni-Cr-Mo-N N08367
Low-carbon Cr-Ni-Fe-N R20033 ployed in service temperatures up to 1100 °F (593 °C).
Low-carbon Ni-Cr-Mo N06035, N06058, N06059, N06044
1.1.3.2 Grade 2 (Solution annealed)—Material is normally
Low-carbon Ni-Cr-Mo-Cu N06200
employed in service temperatures above 1100 °F (593 °C)
Low-carbon Ni-Cr-Mo-W N06686
Low-carbon Ni-Fe-Cr-Mo-Cu N08031, N08034 where resistance to creep and rupture are required.
Low-carbon Ni-Mo-Cr N10276, N06022, N10362
Low-carbon Ni-Mo-Cr-Ta N06210 NOTE 1—Hot-working or reannealing may change properties
Ni N02200 significantly, depending on working history and temperatures.
Ni-Co-Cr-Si N12160
1.2 The values stated in inch-pound units are to be regarded
Ni-Cr-Al N06699
Ni-Cr-Co-Mo N06617 as standard. The values given in parentheses are mathematical
Ni-Cr-Fe N06600, N06603, N06690
conversions to SI units that are provided for information only
Ni-Cr-Fe-Al N06025
and are not considered standard.
Ni-Cr-Fe-Si N06045
Ni-Cr-Mo-Nb N06625
1.3 This standard does not purport to address all of the
Ni-Cr-Mo-Si N06219
safety concerns, if any, associated with its use. It is the
Ni-Cr-Mo-W N06110
Ni-Cr-W-Mo N06230
responsibility of the user of this standard to become familiar
Ni-Cu N04400
with all hazards including those identified in the appropriate
Ni-Fe-Cr N08120, N08800, N08810, N08811
Safety Data Sheet (SDS) for this product/material as provided
Ni-Fe-Cr-Mo-Cu N08825, N08827
Ni-Fe-Cr-W N06674
by the manufacturer, to establish appropriate safety, health,
Ni-Mo N10665, N10675, N10629
and environmental practices, and determine the applicability
Ni-Mo-Cr-Fe N10242, N10624
of regulatory limitations prior to use.
1.1.1 The nickel-iron-chromium alloys are UNS N08120,
1.4 This international standard was developed in accor-
UNS N08800, UNS N08810, and UNS N08811. Alloy UNS
dance with internationally recognized principles on standard-
N08800 is normally employed in service temperatures up to
ization established in the Decision on Principles for the
and including 1100 °F (593 °C). Alloys UNS N08810,
Development of International Standards, Guides and Recom-
N08120, and UNS N08811 are normally employed in service
mendations issued by the World Trade Organization Technical
temperatures above 1100 °F (593 °C) where resistance to creep
Barriers to Trade (TBT) Committee.
and rupture is required, and are annealed to develop controlled
grain size for optimum properties in this temperature range.
2. Referenced Documents
1.1.2 Nickel-iron-chromium-tungsten alloy UNS N06674 is
3
2.1 ASTM Standards:
normally employed in service temperatures above 1100 °F
B880 Specification for General Requirements for Chemical
(593 °C) where resistance to creep and rupture is required, and
Check Analysis Limits for Nickel, Nickel Alloys and
is annealed to develop optimum properties in this temperature
Cobalt Alloys
range.
E8/E8M Test Methods for Tension Testing of Metallic Ma-
terials
1
This specification is under the jurisdiction of ASTM Committee B02 on
E29 Practice for Using Significant Digits in Test Data to
Nonferrous Metals and Alloys and is the direct responsibility of Subcommittee
B02.07 on Refined Nickel and Cobalt and Their Alloys.
Current edition approved April 1, 2022. Published April 2022. Originally
3
approved in 1972. Last previous edition approved in 2019 as B564 – 19. DOI: For referenced ASTM standards, visit the ASTM website, www.astm.org, or
10.1520/B0564-22. contact ASTM Customer Service at [e-mail]. For Annual Book of ASTM
2
For ASME Boiler and Pressure Vessel Code applications see related Specifi- Standards volume information, refer to the standard’s Document Summary page on
cation SB-564 in Section II of that Code. the ASTM website.
*A Summary of Changes section appears at the end of this standard
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1

...

This document is not an ASTM standard and is intended only to provide the user of an ASTM standard an indication of what changes have been made to the previous version. Because
it may not be technically possible to adequately depict all changes accurately, ASTM recommends that users consult prior editions as appropriate. In all cases only the current version
of the standard as published by ASTM is to be considered the official document.
Designation: B564 − 19 B564 − 22
Standard Specification for
1
Nickel Alloy Forgings
This standard is issued under the fixed designation B564; the number immediately following the designation indicates the year of
original adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. A
superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
This standard has been approved for use by agencies of the U.S. Department of Defense.
1. Scope*
2
1.1 This specification covers forgings of:
Alloy Type UNS Number(s)
Fe-Ni-Cr-Mo-N N08367
Low-carbon Cr-Ni-Fe-N R20033
Low-carbon Ni-Cr-Mo N06035, N06058, N06059, N06044
Low-carbon Ni-Cr-Mo-Cu N06200
Low-carbon Ni-Cr-Mo-W N06686
Low-carbon Ni-Fe-Cr-Mo-Cu N08031, N08034
Low-carbon Ni-Mo-Cr N10276, N06022, N10362
Low-carbon Ni-Mo-Cr-Ta N06210
Ni N02200
Ni-Co-Cr-Si N12160
Ni-Cr-Al N06699
Ni-Cr-Co-Mo N06617
Ni-Cr-Fe N06600, N06603, N06690
Ni-Cr-Fe-Al N06025
Ni-Cr-Fe-Si N06045
Ni-Cr-Mo-Nb N06625
Ni-Cr-Mo-Si N06219
Ni-Cr-Mo-W N06110
Ni-Cr-W-Mo N06230
Ni-Cu N04400
Ni-Fe-Cr N08120, N08800, N08810, N08811
Ni-Fe-Cr-Mo-Cu N08825, N08827
Ni-Fe-Cr-W N06674
Ni-Mo N10665, N10675, N10629
Ni-Mo-Cr-Fe N10242, N10624
1.1.1 The nickel-iron-chromium alloys are UNS N08120, UNS N08800, UNS N08810, and UNS N08811. Alloy UNS N08800
is normally employed in service temperatures up to and including 1100°F (593°C).1100 °F (593 °C). Alloys UNS N08810,
N08120, and UNS N08811 are normally employed in service temperatures above 1100°F (593°C)1100 °F (593 °C) where
resistance to creep and rupture is required, and are annealed to develop controlled grain size for optimum properties in this
temperature range.
1
This specification is under the jurisdiction of ASTM Committee B02 on Nonferrous Metals and Alloys and is the direct responsibility of Subcommittee B02.07 on Refined
Nickel and Cobalt and Their Alloys.
Current edition approved Nov. 1, 2019April 1, 2022. Published November 2019April 2022. Originally approved in 1972. Last previous edition approved in 20182019 as
B564 – 18.B564 – 19. DOI: 10.1520/B0564-19.10.1520/B0564-22.
2
For ASME Boiler and Pressure Vessel Code applications see related Specification SB-564 in Section II of that Code.
*A Summary of Changes section appears at the end of this standard
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1

---------------------- Page: 1 ----------------------
B564 − 22
1.1.2 Nickel-iron-chromium-tungsten alloy UNS N06674 is normally employed in service temperatures above 1100°F
(593°C)1100 °F (593 °C) where resistance to creep and rupture is required, and is annealed to develop optimum properties in this
temperature range.
1.1.3 Nickel-chromium-molybdenum-columbium (UNS N06625) products are furnished in two grades of different heat-treated
conditions:
1.1.3.1 Grade 1 (Annealed)—Material is normally employed in service temperatures up to 1100 °F (593 °C).
1.1.3.2 Grade 2 (Solution annealed)—Material is normally employed in service temperatures above 1100 °F (593 °C) where
resistance to creep and rupture are required.
NOTE 1—Hot-working or reannealing may change properties significantly, depending on working history and temperatures.
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 Safety Data Sheet
(SDS) for this product/material as provided by the manufacturer, to establish appropriate safety, health, and environmental
practices, and determine the applicability of regulatory limitations prior to use.
1.4 This international standard was developed in accordance with internationally recognized principles on standardization
established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued
by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
2. Referenced Documents
3
2.1 ASTM Standards:
B880 Specification for General Requirements for Chemical Check Analysis Limits for Nickel, Nickel Alloys and Cobalt Alloys
E8/E8M Test Methods for Tension Testing of Metallic Materials
E29 Practice for
...