| Product Name |
Notes |
|
SP - 700 -- Aircraft Quality Sheet
|
Superior strength & creep resistance to 400°C, limited weldability
|
|
Ti - 10V - 2Fe - 3Al -- Aircraft Quality Sheet
|
Good ductility & fatigue resistance, use: space vehicles/structures
|
|
Ti - 17 -- Aircraft Quality Sheet
|
Excellent superplastic formability & thermal stability, space vehicles
|
|
Ti - 5Al - 2.5Sn - Grade 6
|
Weldable, non-ageable, offering good high temperature stability, strength
|
|
Ti - 6Al - 2Sn - 4Zr - 2Mo - 0.1Si
|
Excellent strength & creep resistance to temp. as high as 550°C
|
|
Ti - 6Al - 2Sn - 4Zr - 2Mo - 0.1Si -- Aircraft Quality Sheet
|
High creep-resistant, non-ageable, weldable, app: gas turbine engine comp.
|
|
Ti - 6Al - 2Sn - 4Zr - 6Mo -- Aircraft Quality Sheet
|
Application: airframe components
|
|
Ti - 6Al - 4V - Grade 5
|
"Workhorse" alloy for aerospace applications for use up to 400°C
|
|
Ti - 6Al - 4V ELI - Grade 23
|
Improved ductility and fracture toughness in air and saltwater environments
|
|
Ti - 6Al - 6V - 2Sn
|
Application: airframe components
|
|
Ti - 6Al - 6V - 2Sn -- Aircraft Quality Sheet
|
Excellent strength & creep resistance to temp. as high as 550°C
|
|
Ti - 8Al - 1Mo - 1V
|
High creep-resistant, non-ageable, weldable, app: gas turbine engine comp.
|
|
Ti - 8Al - 1Mo - 1V -- Aircraft Quality Sheet
|
Excellent combination of toughness and strength at cryogenic temperatures
|
|
Ti Beta-C™ - Grade 19 -- Aircraft Quality Sheet
|
Superior fatigue & strength/toughness combinations
|
|
Ti-6Al-2Sn-2Zr-2Mo-2Cr-0.15Si -- Aircraft Quality Sheet
|
Improved strength to temp 450°C, app: gas turbine engine components
|
