Deflecting feeder bowl assembly for a turbojet engine combustion

Details Deflecting feeder bowl assembly for a turbojet engine combustion Deflecting feeder bowl assembly for a turbojet engine combustion

1997-07-22

1999-08-24

Kim, Ted

Power plants

Combustion products used as motive fluid

Combustion products generator

60754, 60755, F23R 310

Patent

active

059410760

ABSTRACT:
A combustion chamber is disclosed for a gas turbine engine having a feeder owl interposed between the forward end wall of the combustion chamber and an associated air and fuel injection device, the feeder bowl having a generally annular configuration with spaced apart outer and inner walls forming a chamber. A baffle is formed integrally with the feeder bowl and extends outwardly from a merging zone in a direction generally parallel to the forward end wall of the combustion chamber. The outer wall of the feeder bowl has a plurality of air intake orifices communicating with the chamber and located adjacent to the merging zone. The inner wall of the feeder bowl has a plurality of first and second air outlet orifices, both communicating with the chamber and the second air outlet orifices being spaced from the first air outlet orifices.

REFERENCES:
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patent: 5484263 (1996-01-01), Nagaraj et al.
patent: 5623827 (1997-04-01), Monty
patent: 5765376 (1988-04-01), Zarzalis et al.

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