SAE AMS4950

Titamium Alloy, Bars, Wire, Forgings, and Rings 6.0al 4.0v Solution Heat Treated and Aged Modified Strenght.

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Standard:
  • AMS4950
Revised:
  • 1996-08-01
Revision:
  • Historical. Access the latest revision: AMS4950C
Issuing:
  • Ams G Titanium And Refractory Metals Committee
Scope:

This specification covers a titanium alloy in the form of bars, wire, forgings, and flash welded rings 4.000 inches (101.60 mm) and under in nominal diameter or least distance between parallel sides and of stock for foging or flash welded rings.

These products have been used typically for parts which are machined after being solution heat treated and aged, and are suitable for parts requiring high strength-to-weight ratios at or near room temperature, but usage is not limited to such applications.

Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking; ARP982 recommends practices to minimize such conditions.

History:
StandardPublishedRevisionStatus
AMS4950C2011-06-23LatestRevised
AMS4950B2007-06-27HistoricalRevised
AMS4950A2002-07-23HistoricalRevised
AMS49501996-08-01HistoricalIssued
AKA:
  • SAE AMS 4950
Sector:
  • Aerospace
Topic:
  • Nonferrous alloys
  • Titanium alloys

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