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

1976-09-07

1978-03-07

Garrett, Robert E.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60 3965, 60 3966, F02C 718, F02C 720

Patent

active

040772055

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: 2670601 (1954-03-01), Williams et al.
patent: 2692478 (1954-10-01), Hill
patent: 2840989 (1958-07-01), Macaulay
patent: 2884759 (1959-05-01), Sevcik
patent: 3307354 (1967-03-01), Macaulay et al.
patent: 3408812 (1968-11-01), Stenger
patent: 3844116 (1974-10-01), Matto
patent: 3978662 (1976-09-01), DuBell et al.

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