Gas turbine blade shroud support

Details Gas turbine blade shroud support Gas turbine blade shroud support

1989-10-24

1991-06-11

Kwon, John T.

Rotary kinetic fluid motors or pumps

With passage in blade, vane, shaft or rotary distributor...

4151821, F04D 2940

Patent

active

050228161

ABSTRACT:
Tip shroud segments (26) are supported in support ring (24). The ring has at its downstream end conical surface (32) mating and in interference fit with conical surface (16). When flange (20) is torqued, face (22) aligns and forces support ring (24) into the interference fit. Concentricity and rigidity of the shroud support is obtained in a structure easily assembled and disassembled.

REFERENCES:
patent: 2858104 (1958-10-01), Kelk et al.
patent: 3085398 (1963-04-01), Ingleson
patent: 3990807 (1976-11-01), Sifford
patent: 3992126 (1976-11-01), Brown et al.
patent: 4566851 (1986-01-01), Comeau et al.
patent: 4627233 (1986-12-01), Baran, Jr.

Affiliated with

Also associated with

Rating

Gas turbine blade shroud support does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Gas turbine blade shroud support, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Gas turbine blade shroud support will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-779762