Abstract

HYLITE 20 is a titanium-aluminum-tin alloy with properties of medium tensile strength, good weldability and non-embrittlement under service conditions. It is recommended for aircraft and missile components. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep and fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ti-47. Producer or source: Jessop-Saville Ltd, Brightside Works.

aircraft components, chemical composition, corrosion-resistant alloys, creep properties, elasticity, fatigue properties, heat treatability, high-temperature alloys, Hylite 20, joinability, machinability, missiles, physical properties, tensile strength, weldability, workability
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Copyright © ASM International® 1996
1996
ASM International
Topics
Aircraft components Missiles Corrosion-resistant alloys High-temperature alloys Titanium alloys Chemical composition Heat treatability Joinability Machinability Weldability Workability Creep properties Elastic modulus Fatigue properties Tensile strength Physical properties Thermal properties
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