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D11AE - Copper-Nickel-Tin Alloy, Tubes, Solution Annealed, Cold Finished and Spinodal Hardened (TXTS)

Details
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Document Number: D11AE
Project Initiation: 04-19-2011
Project Number:
Revision Number:
Sponsor Name: W Raymond Cribb
Title
Copper-Nickel-Tin Alloy, Tubes, Solution Annealed, Cold Finished and Spinodal Hardened (TXTS)
Scope
This new specification is for high strength cold worked tube of Cu-15Ni-8Sn (C72900) alloy after spinodal hardening for use in highly loaded bushing/bearing components. Outside diameter includes1.625 to 2.500 inch with wall thickness less than 20% of the outside diameter.
Rationale
This SAE Aerospace Material Specification is intended to provide technical requirements such as composition, casting practices and heat treatment as well as Quality Assurance provisions drawn C72900 alloy.
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