Gas turbine engines

Details Gas turbine engines Gas turbine engines

1994-03-09

1995-03-21

Thorpe, Timothy S.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60752, F02C 700

Patent

active

053984960

ABSTRACT:
A gas turbine engine component support assembly (30) comprises a pair of ring members (64) and (74) defining a slot in which a cranked flange (28) extending from the inner surfaces of an array of combustion chamber discharge nozzles (22) is located. One part (28B) of the cranked flange has projections (28C) which engage with radial slots (76) formed in one of the ring members (74) to provide cross-key location of the discharge nozzles. The support assembly (30) is located adjacent the radially inner platform of an array of nozzle guide vanes (20), and also provides support and location for the vanes.

REFERENCES:
patent: H903 (1991-04-01), Weinstein
patent: 3186168 (1965-06-01), Ormerod et al.
patent: 3959966 (1976-06-01), Pearce et al.
patent: 3965066 (1976-06-01), Sterman et al.
patent: 4739621 (1988-04-01), Pettengill et al.
patent: 4798514 (1989-01-01), Pask
patent: 4821522 (1989-04-01), Matthews et al.

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