Combustion liner swirler

Details Combustion liner swirler Combustion liner swirler

1974-06-25

1976-08-17

Camby, John J.

Combustion

Flame holder having protective flame enclosing or flame...

Including means feeding air axially spaced points of the flame

431353, 60 3974R, 431182, 239406, F02C 324, F23R 110

Patent

active

039751414

ABSTRACT:
In the use of combustion apparatus with hot gas turbines it is desirable to e able to efficiently burn fuel at widely ranging rates (pounds per hour) in accordance with varying demands on the turbine. The present invention proposes a combustor wherein stable combustion is achieved over a wide range of fuel flows. Combustion air is introduced as a circumferential swirl around the sprayed fuel to promote a high tangential velocity and low core velocity.

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patent: 3845903 (1974-11-01), Runninger
patent: 3853456 (1974-12-01), Mutchler
patent: 3922137 (1975-11-01), Peczeli et al.

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