Combustor

Details Combustor Combustor

1988-05-31

1996-01-09

Walsh, Donald P.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60 3927, 60 3929, 60 3937, F02C 306

Patent

active

054818672

ABSTRACT:
An annular combustor for a gas turbine engine is constructed to include a sector that has a reduced airflow distribution than the remainder of the circumference by supplying a reduced airflow in a judiciously located portion of the fuel nozzles and the single stage of radially ingested combustion airflow. This single stage circumferential zoned annular combustor serves to accommodate higher fuel/air ratios.

REFERENCES:
patent: 4255927 (1981-03-01), Johnson et al.
patent: 4417439 (1983-11-01), Sepulveda et al.
patent: 4499735 (1985-02-01), Moore et al.
patent: 4696157 (1987-09-01), Barbier et al.
patent: 4720970 (1988-01-01), Hudson et al.

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