SAE AMS 5852D-2001

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SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely

voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.”

SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions.

QUESTIONS REGARDING THIS DOCUMENT: (724) 772-7161 FAX: (724) 776-0243

TO PLACE A DOCUMENT ORDER: (724) 776-4970 FAX: (724) 776-0790

SAE WEB ADDRESS: http://www.sae.org

400 Commonwealth Drive, Warrendale, PA 15096-0001

AEROSPACE

MATERIAL

SPECIFICATION

AMS 5852D

Issued SEP 1977

Revised JUL 1989

Noncurrent APR 1994

Cancelled OCT 2001

Superseding AMS 5852C

Nickel Alloy, Corrosion and Heat Resistant, Billets and Preforms

55Ni - 15Cr - 17Co - 5.0Mo - 3.5Ti - 4.0Al - 0.025B

Power Metallurgy Product, Hot Isostatically Pressed

(Composition similar to UNS N13017)

CANCELLATION NOTICE

This specification has been “CANCELLED” by the Aerospace Materials Division, SAE, as of October

2001. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace

Material Specifications.

Cancelled specifications are available from SAE.

AMS 5852D SAE AMS 5852D

- 2 -

1. SCOPE:

1.1 Form:

This specification covers a corrosion and heat resistant nickel alloy powder-metallurgy product in the

form of billets and preforms.

1.2 Application:

Primarily for highly-stressed parts, such as rotating parts of gas turbine engines, requiring high

strength and corrosion and oxidation resistance up to 1400°F (760°C).

2. APPLICABLE DOCUMENTS:

The following publications form a part of this specification to the extent specified herein. The latest

issue of SAE publications shall apply. The applicable issue of other documents shall be as specified in

AMS 2350.

2.1 SAE Publications:

Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096.

2.1.1 Aerospace Material Specifications:

AMS 2261 Tolerances, Nickel, Nickel Alloy, and Cobalt Alloy Bars and Forging Stock

MAM 2261 Tolerances, Metric, Nickel, Nickel Alloy, and Cobalt Alloy Bars and Forging Stock

AMS 2269 Chemical Check Analysis Limits, Wrought Nickel Alloys and Cobalt Alloys

AMS 2350 Standards and Test Methods

AMS 2374 Quality Assurance Sampling of Corrosion and Heat Resistant Steels and Alloys,

Forgings and Forging Stock

AMS 2630 Ultrasonic Inspection, Product Over 0.5 In. (12.5 mm) Thick

AMS 5851 Alloy Powder, Corrosion and Heat Resistant, 55Ni - 15Cr - 17Co - 5.0Mo - 3.5Ti -

4.0Al - 0.025B, as Fabricated

2.1.2 Aerospace Recommended Practices:

ARP1313 Determination of Trace Elements in High Temperature Alloys

AMS 5852D SAE AMS 5852D

- 3 -

2.2 ASTM Publications:

Available from ASTM, 1916 Race Street, Philadelphia PA 19103.

ASTM E8 Tension Testing of Metallic Materials

ASTM E8M Tension Testing of Metallic Materials (Metric)

ASTM E10 Brinell Hardness of Metallic Materials

ASTM E21 Elevated Temperature Tension Tests of Metallic Materials

ASTM E112 Determining Average Grain Size

ASTM E139 Conducting Creep, Creep-Rupture, and Stress-Rupture Tests of Metallic Materials

ASTM E292 Conducting Time-for-Rupture Notch Tension Tests of Materials

ASTM E354 Chemical Analysis of High-Temperature, Electrical, Magnetic, and Other Similar Iron,

Nickel, and Cobalt Alloys

2.3 U.S. Government Publications:

Available from Commanding Officer, Naval Publications and Forms Center, 5801 Tabor Avenue,

Philadelphia, PA 19120.

2.3.1 Military Standards:

MIL-STD-163 Steel Mill Products, Preparation for Shipment and Storage

3. TECHNICAL REQUIREMENTS:

3.1 Material:

Billets and preforms shall be produced by compaction of AMS 5851 powder by hot isostatic pressing

(HIP) to produce products meeting the requirements of 3.5 and 3.6.

3.2 Composition:

Shall conform to the following percentages by weight, determined by wet chemical methods in

accordance with ASTM E354, by spectrochemical methods, or by other analytical methods

acceptable to purchaser except that lead and bismuth shall be determined in accordance with

ARP 1313 and oxygen and nitrogen shall be determined by Leco gas analyzer or equivalent:

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摘要：

SAE AMS 5852D-2001 是一项由美国汽车工程师学会（SAE）发布的航空航天材料规范标准，主要规定了耐腐蚀钢棒材、线材、锻件及环形件的技术要求。该标准适用于需要高强度和良好耐腐蚀性能的航空航天零部件制造，如发动机部件、紧固件和结构组件。AMS 5852D 版本于2001年发布，替代了之前的版本，更新了化学成分、力学性能及热处理工艺的要求，确保材料在极端温度下保持稳定的性能。本标准中规定的材料为马氏体不锈钢（如 AISI 440C 改进型），具有优异的硬度、耐磨性和抗腐蚀能力。通过严格

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