ASTM B564-00a

Standard Specification for Nickel Alloy Forgings

SCOPE
1.1 This specification covers forgings of nickel alloy UNS N02200, Ni-Cu alloy UNS N04400, Ni-Cr-Fe alloys UNS N06600, UNS N06603, and UNS N06690, Ni-Cr-Mo-Nb alloy UNS N06625, Ni-Cr-Mo-Si alloy UNS N06219, low-carbon Ni-Mo-Cr alloys UNS N10276 and UNS N06022, Ni-Cr-Mo-W alloy UNS N06110, low-carbon Ni-Cr-Mo-W alloy UNS N06686, Ni-Fe-Cr-Mo-Cu alloy UNS N08825, Fe-Ni-Cr-Mo-N alloy UNS N08367, low-carbon Ni-Cr-Mo alloy UNS N06058, low-carbon Ni-Cr-Mo alloy UNS N06059, low carbon Ni-Cr-Mo-Cu alloy UNS N06200, Ni-Mo-Cr-Fe alloy UNS N10242, Ni-Mo alloys UNS N10665 and UNS N10675, low-carbon Ni-Fe-Cr-Mo-Cu alloy UNS N08031, Ni-Cr-W-Mo alloy UNS N06230, Ni-Cr-Co-Mo alloy UNS N06617, Ni-Co-Cr-Si alloy UNS N12160, Ni-Fe-Cr alloys, Ni-Mo alloy UNS N10629, Ni-Cr-Fe-Al alloy UNS N06025, Ni-Cr-Fe-Si alloy UNS N06045, Low-Carbon Ni-Mo-Cr-Ta alloy UNS N06210, Ni-Mo-Cr-Fe alloy UNS N10624, and low-carbon Cr-Ni-Fe-N alloy UNS R20033*.
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 1100oF (593oC). Alloys UNS N08810, N08120, and UNS N08811 are normally employed in service temperatures above 1100oF where resistance to creep and rupture is required, and are annealed to develop controlled grain size for optimum properties in this temperature range.
1.2 The values stated in inch-pound units are to be regarded as the standard. The values given in parentheses are for information only.

General Information

• Status: Historical
• Publication Date: 09-Oct-2000
• 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

Relations

• Replaced By: ASTM B564-04 - Standard Specification for Nickel Alloy Forgings
• Effective Date: 01-Feb-2004
• Referred By: ASTM B366/B366M-23 - Standard Specification for Factory-Made Wrought Nickel and Nickel Alloy Fittings
• Effective Date: 10-Oct-2000
• Referred By: ASTM F1387-23 - Standard Specification for Performance of Piping and Tubing Mechanically Attached Fittings
• Effective Date: 10-Oct-2000

Standards Content (Sample)

NOTICE: This standard has either been superseded and replaced by a new version or withdrawn.
Contact ASTM International (www.astm.org) for the latest information
Designation: B 564 – 00a
Standard Specification for
Nickel Alloy Forgings
This standard is issued under the fixed designation B 564; 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 (e) indicates an editorial change since the last revision or reapproval.
This standard has been approved for use by agencies of the Department of Defense.
1. Scope B 880 Specification for General Requirements for Chemical
2 Check Analysis Limits for Nickel, Nickel Alloys and
1.1 This specification covers forgings of nickel alloy UNS
Cobalt Alloys
N02200, Ni-Cu alloy UNS N04400, Ni-Cr-Fe alloys UNS
E 8 Test Methods for Tension Testing of Metallic Materials
N06600, UNS N06603, and UNS N06690, Ni-Cr-Mo-Nb alloy
E 29 Practice for Using Significant Digits in Test Data to
UNS N06625, Ni-Cr-Mo-Si alloy UNS N06219, low-carbon
Determine Conformance with Specifications
Ni-Mo-Cr alloys UNS N10276 and UNS N06022, Ni-Cr-
E 76 Test Methods for Chemical Analysis of Nickel-Copper
Mo-W alloy UNS N06110, low-carbon Ni-Cr-Mo-W alloy
Alloys
UNS N06686, Ni-Fe-Cr-Mo-Cu alloy UNS N08825, Fe-Ni-Cr-
E 112 Test Methods for Determining the Average Grain
Mo-N alloy UNS N08367, low-carbon Ni-Cr-Mo alloy UNS
Size
N06058, low-carbon Ni-Cr-Mo alloy UNS N06059, low car-
E 350 Test Methods for Chemical Analysis of Carbon Steel,
bon Ni-Cr-Mo-Cu alloy UNS N06200, Ni-Mo-Cr-Fe alloy
Low-Alloy Steel, Silicon Electrical Steel, Ingot Iron, and
UNS N10242, Ni-Mo alloys UNS N10665 and UNS N10675,
Wrought Iron
low-carbon Ni-Fe-Cr-Mo-Cu alloy UNS N08031, Ni-Cr-
E 1473 Test Methods for Chemical Analysis of Nickel,
W-Mo alloy UNS N06230, Ni-Cr-Co-Mo alloy UNS N06617,
Cobalt, and High-Temperature Alloys
Ni-Co-Cr-Si alloy UNS N12160, Ni-Fe-Cr alloys, Ni-Mo alloy
2.2 Military Standards:
UNS N10629, Ni-Cr-Fe-Al alloy UNS N06025, Ni-Cr-Fe-Si
MIL-STD-129 Marking for Shipment and Storage
alloy UNS N06045, Low-Carbon Ni-Mo-Cr-Ta alloy UNS
MIL-STD-271 Nondestructive Testing Requirements for
N06210, Ni-Mo-Cr-Fe alloy UNS N10624, and low-carbon
Metals
Cr-Ni-Fe-N alloy UNS R20033*.
1.1.1 The nickel-iron-chromium alloys are UNS N08120,
3. Ordering Information
UNS N08800, UNS N08810, and UNS N08811. Alloy UNS
3.1 It is the responsibility of the purchaser to specify all
N08800 is normally employed in service temperatures up to
requirements that are necessary for the safe and satisfactory
and including 1100°F (593°C). Alloys UNS N08810, N08120,
performance of material ordered under this specification.
and UNS N08811 are normally employed in service tempera-
Examples of such requirements include, but are not limited to,
tures above 1100°F where resistance to creep and rupture is
the following:
required, and are annealed to develop controlled grain size for
3.1.1 Alloy (Table 1).
optimum properties in this temperature range.
3.1.2 Condition (Table 2).
1.2 The values stated in inch-pound units are to be regarded
3.1.3 Quantity (mass or number of pieces).
as the standard. The values given in parentheses are for
3.1.4 Forging, sketch or drawing.
information only.
3.1.5 Certification— State if certification or a report of test
2. Referenced Documents results is required (14.1).
3.1.6 Samples for Product (Check) Analysis—Whether
2.1 ASTM Standards:
samples for product (check) analysis should be furnished (see
4.2).
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. Annual Book of ASTM Standards, Vol 02.04.
Current edition approved Oct. 10, 2000. Published November 2000. Originally Annual Book of ASTM Standards, Vol 03.01.
published as B 564 – 72. Last previous edition B 564 – 00. Annual Book of ASTM Standards, Vol 14.02.
2 6
For ASME Boiler and Pressure Vessel Code applications see related Specifi-
Annual Book of ASTM Standards, Vol 03.05.
cation SB-564 in Section II of that Code. Annual Book of ASTM Standards, Vol 03.06.
* New designations established in accordance with ASTM E527 and SAE J1086, Available from Standardization Documents Order Desk, Bldg. 4, Section D,
Practice for Numbering Metals and Alloys (UNS). 700 Robbins Ave., Philadelphia, PA 19111–5094, Attn: NPODS.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.
B 564
TABLE 1 Chemical Requirements
Composition, %
Nickel- Nickel- Nickel- Low-
Chromium- Chromium- Chromium- Carbon
Nickel- Nickel-
Nickel- Nickel-Iron Nickel-Iron- Nickel-Iron- Iron- Iron- Iron-Silicon Nickel-
Chromium- Chromium-
Copper Chromium Chromium Chromium Aluminum Aluminum Alloy UNS Molybdenum-
Element Iron Alloy Iron Alloy
Alloy UNS Alloy UNS Alloy UNS Alloy UNS Alloy UNS Alloy UNS N06045 Chromium-
UNS UNS
N04400 N08120 N08800 N08810 N06603 N06025 Tantalum
N06600 N06690
Alloy UNS
N06210
A A A A A
Nickel 63.0 min 72.0 min 58.0 min 35.0–39.0 30.0–35.0 30.0–35.0 balance balance 45 min remainder
Copper 28.0–34.0 0.5 max 0.5 max 0.50 max 0.75 max 0.75 max 0.5 max 0.10 max 0.3 max .
A A
Iron 2.5 max 6.0–10.0 7.0–11.0 remainder 39.5 min 39.5 min 8.0–11.0 8.0–11.0 21.0–25.0 1.0 max
Manganese 2.0 max 1.0 max 0.5 max 1.5 1.5 max 1.5 max 0.15 max 0.15 1.0 0.5 max
Carbon 0.3 max 0.15 max 0.05 max 0.02–0.10 0.10 max 0.05–0.10 0.20–0.40 0.15–0.25 0.05–0.12 0.015 max
Silicon 0.5 max 0.5 max 0.5 max 1.0 1.0 max 1.0 max 0.5 max 0.5 2.5–3.0 0.08 max
Sulfur, max 0.024 0.015 0.015 0.03 0.015 0.015 0.010 0.01 0.010 0.02
Chromium . 14.0–17.0 27.0–31.0 23.0–27.0 19.0–23.0 19.0–23.0 24.0–26.0 24.0–26.0 26.0–29.0 18.0-20.0
Aluminum . . . 0.40 max 0.15–0.60 0.15–0.60 2.4–3.0 1.8–2.4 . .
Titanium . . . 0.20 max 0.15–0.60 0.15–0.60 0.01–0.25 0.1–0.2 . .
Columbium . . . 0.4–0.9 . . . . . .
(Nb) +
tantalum
Molybdenum . . . 2.50 max . . . . . 18.0-20.0
Phosphorus . . . 0.040 max . . 0.02 max 0.02 max 0.02 max 0.02 max
Tungsten . . . 2.50 max . . . . . .
Cobalt, max . . . 3.0 . . . . . 1.0
Vanadium, . . . . . . . . . 0.35
max
Nitrogen . . . 0.15–0.30 . . . . . .
Boron . . . 0.010 max . . . . . .
Lanthanum . . . . . . . . . .
Aluminum + . . . . . . . .
Titanium
Nickel + . . . . . . . . . .
Molybdenum
Columbium . . . . . . . . . .
(Nb) max
Tantalum . . . . . . . . . 1.5-2.2
Zirconium, max . . . . . . 0.01–0.10 0.01–0.10 . .
Cerium . . . . . . . . 0.03–0.09 .
Yttrium . . . . . . 0.01–0.15 0.05–0.12 . .
A
Element shall be determined arithmetically by difference.
B 564
TABLE 1 Chemical Requirements (continued)
Composition, %
Low-
Low- Iron-Nickel- Low- Low-
Carbon
Nickel- Nickel- Carbon Chromium- Carbon Carbon
Nickel-Iron Nickel-
Nickel-Iron- Chromium- Chromium- Nickel- Molyb- Nickel- Nickel-
Chromium- Molyb-
Element
Chromium Molybdenum- Molybdenum- Molyb- denum- Chromium Chromium
Molybdenum- denum-
Alloy UNS Columbium Tungsten denum- Nitrogen Molyb- Molyb-
Copper Alloy Chro-
N08811 Alloy UNS Alloy UNS Chromium Alloy denum denum
UNS N08825 mium
N06625 N06110 Alloy UNS UNS Alloy UNS Alloy UNS
Alloy UNS
N10276 N08367 N06059 N06058
N06022
A A A A A
Nickel 30.0–35.0 58.0 min 51.0 min 38.0–46.0 remainder remainder 23.50–25.50 balance balance
Copper 0.75 max . 0.50 max 1.5–3.0 . . 0.75 max 0.50 max 0.50 max
A A A
Iron 39.5 min 5.0 max 1.0 max 22.0 min 4.0–7.0 2.0–6.0 remainder 1.5 max 1.5 max
Manganese 1.5 max 0.5 max 1.0 max 1.0 max 1.0 max 0.50 max 2.00 max 0.5 max 0.50 max
Carbon 0.06–0.10 0.10 max 0.15 max 0.05 max 0.010 max 0.015 max 0.030 max 0.010 max 0.010 max
Silicon 1.0 max 0.5 max 1.0 max 0.5 max 0.08 max 0.08 max 1.00 max 0.10 max 0.10 max
Sulfur, max 0.015 0.015 0.015 0.03 0.03 0.02 0.030 0.010 0.010
Chromium 19.0–23.0 20.0–23.0 28.0–33.0 19.5–23.5 14.5–16.5 20.0–22.5 20.0–22.0 22.0–24.0 20.0–23.0
Aluminum 0.15–0.60 0.4 max 1.0 max 0.2 max . . . 0.1–0.4 0.40 max
Titanium 0.15–0.60 0.4 max 1.0 max 0.6–1.2 . . . . .
Columbium . 3.15–4.15 1.0 max . . . . . .
(Nb) +
tantalum
Molybdenum . 8.0–10.0 9.0–12.0 2.5–3.5 15.0–17.0 12.5–14.5 6.00–7.00 15.0–16.5 19.0 - 21.0
Phosphorus . 0.015 max 0.50 max . 0.04 max 0.02 max 0.040 max 0.015 max 0.015 max
Tungsten . . 1.0-4.0 . 3.0–4.5 2.5–3.5 . . 0.3 max
Cobalt . . . . 2.5 max 2.5 max . 0.3 max 0.3 max
Vanadium, . . . . 0.35 0.35 . . .
max
Nitrogen . . . . . . 0.18–0.25 . 0.02 - 0.15
Boron . . . . . . . . .
Lanthanum . . . . . . . . .
Aluminum + 0.85–1.20 . . . . . . . .
Titanium
Nickel + . . . . . . . . .
Molybdenum
Columbium . . . . . . . . .
(Nb), max
Tantalum . . . . . . . . .
Zirconium, . . . . . . . . .
max
Cerium . . . . . . . . .
Yttrium . . . . . . . . .
A
Element shall be determined arithmetically by difference.
B 564
TABLE 1 Chemical Requirements (continued)
Composition, %
Low- Low-
Carbon Nickel- Carbon Nickel
Nickel
Nickel- Chromium- Nickel-Iron Chro- Nickel- Nickel-
Chromium-
Chromium- Molyb- Chromium- mium- Molyb- Molyb-
Cobalt-
Molyb- dnum- Molyb- Tungsten- denum denum
Element Molyb-
dnum- Silicon dnum- Molyb- Alloy Alloy
denum
Copper Alloy Copper denum UNS UNS
Alloy UNS
Alloy UNS Alloy Alloy UNS N10629 N10665
N06617
UNS N06219 UNS N06230
N06200 N08031
A A A A
Nickel remainder balance 30.0–32.0 remainder 44.5 min balance remainder
Copper 1.3–1.9 0.50 max 1.0–1.4 . 0.5 max 0.5 max .
A
Iron 3.0 max 2.0-4.0 balance 3.0 max 3.0 max 1.0–6.0 2.0 max
Manganese 0.50 max 0.50 max 2.0 max 0.30–1.00 1.0 max 1.5 1.0 max
Carbon 0.010 max 0.05 max 0.015 max 0.05–0.15 0.05–0.15 0.010 max 0.02 max
Silicon 0.08 max 0.70-1.10 0.3 max 0.25–0.75 1.0 max 0.05 0.10 max
Sulfur, max 0.010 0.010 0.010 0.015 0.015 0.01 0.03
Chromium 22.0–24.0 18.0-22.0 26.0-28.0 20.0–24.0 20.0–24.0 0.5–1.5 1.0 max
Aluminum 0.50 max 0.50 max . 0.20–0.50 0.8–1.5 0.1–0.5 .
Titanium . 0.50 max . . 0.6 max . .
Columbium . . . . . . .
(Nb) +
tantalum
Molybdenum 15.0–17.0 7.0-9.0 6.0-7.0 1.0–3.0 8.0–10.0 26.0–30.0 26.0–30.0
Phosphorus 0.025 max 0.020 max 0.020 max 0.030 max . 0.04 max 0.04 max
Tungsten . . . 13.0–15.0 . . .
Cobalt 2.0 max 1.0 max . 5.0 max 10.0 min– 2.5 1.00 max
15.0 max
Vanadium, . . . . . . .
max
Nitrogen . . 0.15-0.25 . . . .
Boron . . . 0.015 max 0.006 max . .
Lanthanum . . . 0.005–0.050 . . .
Aluminum + . . .
Titanium
Nickel + . . . . . . .
Molybdenum
Columbium . . . . . . .
(Nb), max
Tantalum . . . . . . .
Zirconium, . . . . . . .
max
Cerium . . . . . . .
Yttrium . . . . . . .
A
Element shall be determined arithmetically by difference.
B 564
TABLE 1 Chemical Requirements (continued)
Composition, %
Low-
Carbon Nickel-
Nickel- Nickel-
Nickel- Nickel- Molyb-
Molyb- Cobalt- Chromium-
Molyb- Chro- Nickel denum
denum- Chro- Nickel-Iron-
Element
denum mium- Alloy Chro-
Chromium- mium- Nitrogen
Alloy Molyb- UNS mium-
Iron Alloy Silicon Alloy UNS
UNS denum- N02200 Iron
UNS Alloy UNS R20033
N10675 Tungsten Alloy UNS
N10242 N12160
Alloy UNS N10624
N06686
A A A A
Nickel 65.0 min remainder remainder remainder 99.0 min remainder 30.0–33.0
Copper 0.20 max . . . 0.25 max 0.5 max 0.30–1.20
A
Iron 1.0–3.0 2.0 max 5.0 max 3.5 max 0.40 max 5.0-8.0 balance
Manganese 3.0 max 0.80 max 0.75 max 1.5 max 0.35 max 1.0 max 2.0
Carbon 0.01 max 0.03 0.010 max 0.15 max 0.15 max 0.01 max 0.015 max
Silicon 0.10 max 0.80 max 0.08 max 2.4–3.0 0.35 max 0.10 max 0.50
Sulfur, max 0.010 0.015 0.02 0.015 0.01 0.01 max 0.01
Chromium 1.0–3.0 7.0-9.0 19.0–23.0 26.0–30.0 . 6.0-10.0 31.0–35.0
Aluminum 0.50 max 0.50 max . . . 0.5 max .
Titanium 0.20 max . 0.02–0.25 0.20–0.80 . . .
Columbium . . . . . . .
(Nb) +
tantalum
Molybdenum 27.0–32.0 24.0-26.0 15.0–17.0 1.0 max . 21.0-25.0 0.50–2.0
Phosphorus 0.030 max 0.030 max 0.04 max 0.030 max . 0.025 max 0.02 max
Tungsten 3.0 max . 3.0–4.4 1.0 max . . .
†
Cobalt 3.0 max 1.00 max . 27.0–33.0† . 1.0 max .
Vanadium, 0.20 . . . . . .
max
Nitrogen . . . . . . 0.35–0.60
Boron . 0.006 max . . . . .
Lanthanum . . . . . . .
Aluminum + . . . . . .
Titanium
Nickel + 94.0–98.0 . . . . . .
Molybdenum
Columbium 0.20 . . 1.0 . . .
(Nb), max
Tantalum 0.20 max . . . . . .
Zirconium, 0.10 . . . . . .
max
Cerium . . . . . . .
Yttrium . . . . . . .
A
Element shall be determined arithmetically by difference.
B 564
3.1.7 Purchaser Inspection—If the purchaser wishes to
TABLE 2 Continued
witness tests or inspection of material at the place of manu-
Yield Elongation
Maximum Tensile
facture, the purchase order must so state indicating which tests
Strength, in
Section Strength,
Material and Condition 0.2 % 2 in. or 50
or inspections are to be witnessed (12.1).
Thickness, min, ksi
Offset, min, mm or 4D,
in. (mm) (MPa)
ksi (MPa) min, %
4. Chemical Composition
Over 4 90 (621) 40 (276) 50
4.1 The material shall conform to the composition limits
(102) to
10 (254),
specified in Table 1.
incl
4.2 If a product (check) analysis is performed by the
Nickel-iron-chromium- . 85 (586) 35 (241) 30
purchaser, the material shall conform to the product (check)
molybdenum-copper alloy
UNS N08825
analysis variations per B 880.
Low carbon nickel-molyb- . 100 (690) 41 (283) 40
denum-chromium alloy
5. Mechanical Properties and Other Requirements
UNS N10276, annealed
Low-carbon nickel-molyb- . 100 (690) 45 (310) 45
5.1 Mechanical Properties—The material shall conform to
denum-chromium alloy
the mechanical properties specified in Table 2.
UNS N06022
5.2 Grain Size—Annealed alloys (UNS N08810, N08120,
Iron-nickel-chromium-molyb- . 95 (655) 45 (310) 30
denum-nitrogen alloy
and UNS N08811) shall conform to an average grain size of
UNS N08367
ASTM No. 5 or coarser.
Low-carbon nickel-iron- . 94 (650) 40 (276) 40
chromium-molybdenum-
6. Dimensions and P
...