Gas turbine engine combustion liner float wall cooling arrangeme

Details Gas turbine engine combustion liner float wall cooling arrangeme Gas turbine engine combustion liner float wall cooling arrangeme

1994-12-15

1995-10-31

Thorpe, Timothy S.

Power plants

Combustion products used as motive fluid

Combustion products generator

F23R 342

Patent

active

054618665

ABSTRACT:
When second shell section 18 diverges with respect to first shell section 16, the second liner panel 50 is located with a changing spacing from the shell. The liner is close to the shell at the upstream edge 68, and farther from the liner at the downstream end 57. The downstream end of the first liner panel 64 overlaps the second liner panel 50 on the gas side.

REFERENCES:
patent: 4104874 (1978-08-01), Caruel et al.
patent: 4109459 (1978-08-01), Ekstedt et al.
patent: 4302941 (1984-05-01), Du Bell
patent: 4446693 (1984-05-01), Pidcock et al.
patent: 4567730 (1986-02-01), Scott
patent: 4614082 (1986-09-01), Sterman et al.
patent: 4790140 (1988-12-01), Sato et al.
patent: 5083422 (1992-01-01), Vogt
patent: 5388412 (1995-02-01), Schulte-Werning et al.

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