Inlet for annular gas turbine combustor

Details Inlet for annular gas turbine combustor Inlet for annular gas turbine combustor

1977-12-19

1979-12-11

Croyle, Carlton R.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60 3974R, F02C 306, F02C 308

Patent

active

041776372

ABSTRACT:
Combustion equipment for a gas turbine engine comprises an annular flame tube having a circumferential array of upstream projecting pots or vortex generators at its upstream end, an annular diffusing passageway located upstream of the pots and terminating adjacent the upstream ends of the pots, and a plurality of tubular ducts, one extending from the annular diffusing passageway to the upstream end of each pot.

REFERENCES:
patent: 3026675 (1962-03-01), Vesper et al.
patent: 3372542 (1968-03-01), Sevetz
patent: 3394543 (1968-07-01), Slattery
patent: 3398529 (1968-08-01), Schmitz et al.
patent: 3667221 (1972-06-01), Taylor
patent: 3738106 (1973-06-01), Stein et al.
patent: 3834159 (1974-09-01), Vdoviak

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