SAE AMS5852D
Current
The latest, up-to-date edition.
Nickel Alloy, Corrosion and Heat Resistant, Billets and Preforms 55ni 15cr 17co 5.0mo 3.5ti 4.0al 0.025b, Powder Metallurgy Product, Hot Isostatically Pressed
01-10-2001
1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGEMENT
7. REJECTIONS
8. NOTES
Specifies a corrosion and heat resistant nickel alloy powder-metallurgy product in the form of billets and preforms. Mainly for highly-stressed parts, such as rotating parts of gas turbine engines, needing high strength and corrosion and oxidation resistance up to 1400 Deg F (760 Deg C).
| DocumentType |
Standard
|
| PublisherName |
SAE International
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| Status |
Current
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| Supersedes |
This specification covers a corrosion and heat resistant nickel alloy powder-metallurgy product in the form of billets and preforms.
| SAE AMS 2269 : 2006 | CHEMICAL CHECK ANALYSIS LIMITS, NICKEL, NICKEL ALLOYS, AND COBALT ALLOYS |
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| MIL-STD-163 Revision C:1978 | STEEL MILL PRODUCTS PREPARATION FOR SHIPMENT AND STORAGE |
| SAE ARP1313D | Determination of Trace Elements in High Temperature Alloys |
| SAE MAM2261D | Tolerances, Metric, Nickel, Nickel Alloys, and Cobalt Alloy Bars, Rods, and Wire |
| ASTM E 8 : 2004 | Standard Test Methods for Tension Testing of Metallic Materials |
| ASTM E 354 : 2014 : REDLINE | Standard Test Methods for Chemical Analysis of High-Temperature, Electrical, Magnetic, and Other Similar Iron, Nickel, and Cobalt Alloys |
| SAE AMS 5851 : D2001 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, POWDER 55NI 15CR 17CO 5.0MO 3.5TI 4.0AI 0.025B, AS FABRICATED |
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