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SAE AMS4917

Titanium Alloy Sheet, Strip, and Plate 13.5V - 11Cr - 3.0Al Solution Heat Treated

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Organization: SAE
Publication Date: 1 June 2017
Status: active
Page Count: 8
scope:

Form

This specification covers a titanium alloy in the form of sheet, strip, and plate through 4.000 inches (101.6 mm) nominal thickness.

Application

This material has been used typically for parts to be formed in the solution heat treated condition and subsequently precipitation heat treated, requiring high strength-to-weight ratio and stability up to 550 °F (288 °C) in the precipitation heat treated condition, but usage is not limited to such applications.

This alloy may have poor crack propagation resistance in the precipitation heat treated condition.

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

Document History

SAE AMS4917
June 1, 2017
Titanium Alloy Sheet, Strip, and Plate 13.5V - 11Cr - 3.0Al Solution Heat Treated
Form This specification covers a titanium alloy in the form of sheet, strip, and plate through 4.000 inches (101.6 mm) nominal thickness. Application This material has been used typically for...
October 1, 2012
Titanium Alloy Sheet, Strip, and Plate 13.5V - 11Cr - 3.0Al Solution Heat Treated
Form This specification covers a titanium alloy in the form of sheet, strip, and plate through 4.00 inches (101.6 mm). Application This material has been used typically for parts to be formed in...
March 1, 2008
Titanium Alloy Sheet, Strip, and Plate 13.5V - 11Cr - 3.0Al Solution Heat Treated
Form This specification covers a titanium alloy in the form of sheet, strip, and plate. Application This material has been used typically for parts to be formed in the solution heat treated...
March 1, 2003
Titanium Alloy Sheet, Strip, and Plate 13.5V - 11Cr - 3.0Al Solution Heat Treated
Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: This material has been used typically for parts to be formed in the solution heat treated...
April 1, 1990
Titanium Alloy Sheet, Strip, and Plate 13.5V - 11Cr - 3.0Al Solution Heat Treated
SCOPE: Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: Primarily for parts to be formed in the solution heat treated condition and subsequently...
October 1, 1984
TITANIUM ALLOY SHEET, STRIP, AND PLATE 13.5V - 11Cr - 3.0Al Solution Heat Treated
Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: Primarily for parts to be formed in the solution heat treated condition and subsequently...
July 16, 1979
TITANIUM ALLOY SHEET, STRIP, AND PLATE 13.5V - 11Cr - 3.0Al Solution Heat Treated
Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: Primarily for parts to be formed in the solution heat treated condition and subsequently...
May 1, 1969
TITANIUM ALLOY SHEET, STRIP, AND PLATE 13.5V - 11Cr - 3Al Solution Heat Treated
APPLICATION: Primarily for parts to be formed in the solution heat treated condition and subsequently precipitation heat treated; suitable for parts, such as pressure vessels and missile and aircraft...
November 1, 1968
TITANIUM ALLOY SHEET, STRIP, AND PLATE 13.5V - 11Cr - 3Al Solution Heat Treated
Application: Primarily for parts to be formed in the solution heat treated condition and subsequently precipitation heat treated; suitable for parts, such as pressure vessels and missile and aircraft...
January 15, 1963
TITANIUM ALLOY SHEET, STRIP, AND PLATE 13.5V - 11Cr - 3Al Solution Treated
APPLICATION: Primarily for parts to be formed in the solution treated condition and subsequently precipitation heat treated; suitable for parts, such as pressure vessels and missile and aircraft...

References

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