Method of manufacturing a rotor assembly

Details Method of manufacturing a rotor assembly Method of manufacturing a rotor assembly

1990-10-01

1991-07-16

Cuda, Irene

Metal working

Method of mechanical manufacture

Impeller making

2988922, 29428, 29505, 228112, 228115, B21K 304

Patent

active

050312880

ABSTRACT:
A compressor rotor structure for a gas turbine engine is made by linear friction bonding stub rooted blades and separate platform pieces, to lands between slots in a compressor disc periphery. These results an integral structure in which the periphery of the disc has had metal removed so as to form the slots and the disc is thus lightened, and the stub roots and platform pieces cooperate to form the airflow inner annulus wall.

REFERENCES:
patent: 3768147 (1973-10-01), Berry et al.
patent: 4096615 (1978-06-01), Cross
patent: 4529452 (1985-07-01), Walker
patent: 4736504 (1988-04-01), Jones
patent: 4864706 (1989-09-01), Jenkel
patent: 4874031 (1989-10-01), Janney

Affiliated with

Also associated with

Rating

Method of manufacturing a rotor assembly does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Method of manufacturing a rotor assembly, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method of manufacturing a rotor assembly will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-121640