Combustor-turbine nozzle interconnection

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

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Details

60 3966, 415115, 415138, F02C 720, F02C 712, F02C 718

Patent

active

039650669

ABSTRACT:
A seal for use between an annular combustor and a turbine nozzle, disposed downstream of the combustor, is provided with means for effectively innerconnecting the combustor with a sidewall surrounding the nozzle. The sidewall includes an upstream extending radially projecting flange and the combustor includes an axially projecting downstream extending flange. The seal includes means for frictionally engaging each of these flanges and retaining them in a sealing relationship while permitting axial and radial frictional sliding motion therebetween. In addition, the present invention provides means for passing cooling air from a surrounding plenum through the seal in a cooling fashion to a pocket formed between the combustor-associated flange and a film-promoting lip which comprises a portion of the combustor liner.

REFERENCES:
patent: 733065 (1903-07-01), Martin, Jr.
patent: 1543348 (1925-06-01), Venton
patent: 3286461 (1966-11-01), Johnson
patent: 3363416 (1968-01-01), Heybyrne et al.
patent: 3670497 (1972-06-01), Sheldon
patent: 3843279 (1974-10-01), Crossley et al.

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