Louver construction for liner of gas turbine engine combustor

Details Louver construction for liner of gas turbine engine combustor Louver construction for liner of gas turbine engine combustor

1977-08-30

1980-01-22

Garrett, Robert E.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60 3966, F02C 718

Patent

active

041843266

ABSTRACT:
This invention relates to an improved combustor liner for a gas turbine power plant which liner is constructed from a plurality of louvers that include a lip and cooling means for defining a cooling film of air flow adjacent the liner. Means are provided for preventing lip closure which in turn is detrimental to film cooling.

REFERENCES:
patent: 2268464 (1941-12-01), Seippel
patent: 2477584 (1949-08-01), De Zubay
patent: 2670601 (1954-03-01), Williams et al.
patent: 2858673 (1958-11-01), Wirt
patent: 3038309 (1962-06-01), Waters
patent: 3408812 (1968-11-01), Stenger
patent: 3618316 (1971-11-01), Taylor
patent: 3672162 (1972-06-01), Rygelis et al.
patent: 3706203 (1972-12-01), Goldberg et al.
patent: 3845620 (1974-11-01), Kenworthy
patent: 3899876 (1975-08-01), Williamson

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