SAE AS4877C

Bolts and Screws, Nickel Alloy UNS N07718, Classification: 185 ksi/1200 Â°F, Procurement Specification

SAE International , 03/10/2012

Publisher: SAE

File Format: PDF

$42.00$85.00

Description

Standard By:SAE International , 03/10/2012

Published:03/10/2012

File Size:1 file , 1.3 MB

Language:English

Note:This product is unavailable in Ukraine, Russia, Belarus

This procurement specification covers bolts and screws made from a corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07718. Classification: a. tensile strength at room temperature 185 ksi minimum, b. maximum test temperature of parts 1200 degrees F, c. tensile strength at 1200 degrees F 145 ksi minimum, and d. stress rupture: 100 ksi stress rupture strength at 1200 degrees F.

Primarily for use in aerospace propulsion systems as follows: a. for use up to approximately 1200 degrees F where elevated temperature tensile strength, stress-rupture strength, and resistance to relaxation are required, and b. for use up to approximately 800 degrees F where fatigue resistance and tensile strength are required.

SAE AS4877C

Bolts and Screws, Nickel Alloy UNS N07718, Classification: 185 ksi/1200 Â°F, Procurement Specification

SAE AS4877C History

SAE AS4877J

SAE AS4877H

SAE AS4877G

SAE AS4877F

SAE AS4877E

SAE AS4877D

SAE AS4877C

SAE AS 4877B

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