Heat treatment for dual alloy turbine wheels

Details Heat treatment for dual alloy turbine wheels Heat treatment for dual alloy turbine wheels

F - Mech Eng,Light,Heat,Weapons

01

D

26/148, 170/72,

F01D 5/34 (2006.01) C22C 19/05 (2006.01) C22F 1/10 (2006.01) F01D 5/28 (2006.01)

Patent

CA 1310274

HEAT TREATMENT FOR DUAL ALLOY TURBINE WHEELS ABSTRACT OF THE DISCLOSURE A dual alloy gas turbine rotor is heat treated by HIP bonding a case superalloy blade ring to a consolidated, powdered-metal hub. After bonding, the assembly is solution treated and aged at certain specific temperatures so as to optimize the mechanical properties of the dual alloy assembly for use in a high performance gas turbine engine.

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