Alloy turbine disk

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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170/78

F02C 7/00 (2006.01) B23K 20/22 (2006.01) F01D 5/28 (2006.01)

Patent

CA 2021625

13DV-10058 ALLOY TURBINE DISK ABSTRACT OF THE DISCLOSURE A dual alloy disk made from a rim alloy having high stress rupture and creep resistance as well as good hold time fatigue crack resistance and a hub alloy having high tensile strength and good low cycle fatigue crack resistance is described. The dual alloy disk is designed for use as a disk in gas turbine engines operating as high as 1500°F. The hub and rim are joined together at a substantially defect-free joint to form a turbine disk having improved properties in both the hub and rim regions.

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