Gas turbine combustor air inlet

Details Gas turbine combustor air inlet Gas turbine combustor air inlet

1977-08-29

1980-03-11

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Combustion products generator

431351, F02C 700

Patent

active

041921380

ABSTRACT:
A covered air scoop for a gas turbine combustor comprising a tubular member radially extending through the combustor shell to define an air inlet. A symmetrical cap member is disposed in spaced, overhanging relationship over the inlet. To enter the combustor, the air must flow into the cap member, thereby causing all air to enter the tube in a substantially uniform manner so that the air flow through all similarly constructed air tubes at a common axial location of the combustor is substantially equal at all times.

REFERENCES:
patent: 2601390 (1952-06-01), Hague
patent: 3158114 (1964-11-01), Nikodem
patent: 3477358 (1969-11-01), Howard
patent: 3899882 (1975-08-01), Parker

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