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SAE AMS4915

Titanium Alloy Sheet, Strip, and Plate 8Al - 1V - 1Mo Single Annealed

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Organization: SAE
Publication Date: 1 June 2017
Status: active
Page Count: 9
scope:

Form

This specification covers a titanium alloy in the form of sheet, strip, and plate up to 4.000 inches (101.60 mm), inclusive

Application

These products have been used typically for parts requiring strength up to 800 °F (427 °C) where fracture toughness is not critical, but usage is not limited to such applications

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 AMS4915
June 1, 2017
Titanium Alloy Sheet, Strip, and Plate 8Al - 1V - 1Mo Single Annealed
Form This specification covers a titanium alloy in the form of sheet, strip, and plate up to 4.000 inches (101.60 mm), inclusive Application These products have been used typically for parts...
March 1, 2013
Titanium Alloy Sheet, Strip, and Plate 8Al - 1V - 1Mo Single Annealed
Form This specification covers a titanium alloy in the form of sheet, strip, and plate up through 4.000 inches (101.60 mm). Application These products have been used typically for parts requiring...
December 1, 2008
Titanium Alloy Sheet, Strip, and Plate 8Al - 1V - 1Mo Single Annealed
Form This specification covers a titanium alloy in the form of sheet, strip, and plate. Application These products have been used typically for parts requiring strength up to 800 °F (427 °C) where...
August 1, 2003
Titanium Alloy Sheet, Strip, and Plate 8Al - 1V - 1Mo Single Annealed
Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: These products have been used typically for parts requiring strength up to 800 °F (427 °C) where...
June 1, 2003
Titanium Alloy Sheet, Strip, and Plate 8Al - 1V - 1Mo Single Annealed
Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: These products have been used typically for parts requiring strength up to 800 °F (427 °C) where...
July 1, 1990
Titanium Alloy Sheet, Strip, and Plate 8Al - 1V - 1Mo Single Annealed
SCOPE: Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: Primarily for parts requiring strength up to 800°F (427°C) where fracture toughness is not...
April 1, 1984
TITANIUM ALLOY SHEET, STRIP, AND PLATE 8Al - 1V - 1Mo Single Annealed
Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: Primarily for parts requiring strength up to 800°F (425°C) where fracture toughness is not...
July 15, 1977
TITANIUM ALLOY SHEET, STRIP, AND PLATE 8Al - 1V - 1Mo Single Annealed
Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Applications: Primarily of parts requiring strength up to 800°F (425°C) where fracture toughness is not...
January 15, 1977
TITANIUM ALLOY SHEET, STRIP, AND PLATE 8Al - 1V - 1Mo Single Annealed
Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: Primarily for parts requiring strength up to 800o F (425o C) where fracture toughness is not...
January 15, 1976
TITANIUM ALLOY SHEET, STRIP, AND PLATE 8Al - 1V - 1Mo Single Annealed
Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: Primarily for parts requiring strength up to 800 F (427° C) where fracture toughness is not...
November 1, 1968
TITANIUM ALLOY SHEET, STRIP, AND PLATE 8Al – 1Mo- 1V Single Annealed
APPLICATION: Primarily for parts requiring strength up to 800 F (427 C) where maximum fracture toughness is not critical.
September 30, 1966
TITANIUM ALLOY SHEET, STRIP, AND PLATE 8Al – 1Mo- 1V Single Annealed
APPLICATION: Primarily for parts requiring high strength up to 800 F (427 C) where maximum fracture toughness is not critical.
March 15, 1966
TITANIUM ALLOY SHEET, STRIP, AND PLATE 8Al – 1Mo - 1V Single Annealed
Application: Primarily for parts requiring strength up to 8000 F (427 C). where maximum fracture toughness is not critical.

References

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