Components for gas turbine engines and methods for...

Details Components for gas turbine engines and methods for... Components for gas turbine engines and methods for...

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/02 (2006.01) B23P 15/00 (2006.01)

Patent

CA 2643631

A method of manufacturing a turbine engine component comprises the steps of fabricating an inner hub, casting a plurality of blades, forming a blade ring, and bonding the blade ring to the inner hub. Each blade comprises a blade root and an airfoil body extending from the blade root. The blade ring comprises, at least in part, the plurality of blades coupled by a first bonding technique. The blade ring is bonded to the inner hub using a second bonding technique.

Affiliated with

Also associated with

Rating

Components for gas turbine engines and methods for... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Components for gas turbine engines and methods for..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Components for gas turbine engines and methods for... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1640375