High intensity slinger type combustor for turbine engines

Details High intensity slinger type combustor for turbine engines High intensity slinger type combustor for turbine engines

1978-12-26

1980-11-11

Garrett, Robert E.

Power plants

Combustion products used as motive fluid

Combustion products generator

F02C 722

Patent

active

042325269

ABSTRACT:
A rotating slinger fuel injector for turbine engines is provided with a plurality of radial holes for distributing and mixing fuel and air throughout the combustor. Fuel is supplied from a stationary fuel manifold through fuel ports in a rotating slinger which distributes the fuel in a plurality of planes throughout the combustor. Air is channeled from the compressor rotor through radially and axially angled air ports provided in the slinger so as to distribute air in a plurality of planes which intersect the planes of distributed fuel at various points throughout the interior combustor. Thus the combustion intensity and efficiency is greatly increased.

REFERENCES:
patent: 3932988 (1976-01-01), Beaufrere
patent: 3983694 (1976-10-01), Bracken
patent: 4040251 (1977-08-01), Heitmann et al.

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