Reduced diameter annular combustor

Details Reduced diameter annular combustor Reduced diameter annular combustor

1993-04-22

1994-07-26

Bertsch, Richard A.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60748, F23R 314

Patent

active

053318056

ABSTRACT:
An annular gas turbine engine combustor includes additional axial primary airflow openings, formed as arcuately segmented openings on opposite sides of each of the airblast fuel nozzles of the combustor, for reducing overall combustor diameter while maintaining flame stabilization and avoiding unacceptable thermal variations in the combustion process.

REFERENCES:
patent: 2545495 (1951-03-01), Sforzini
patent: 2867982 (1959-01-01), Clarke et al.
patent: 3512359 (1970-05-01), Pierce
patent: 3834159 (1974-09-01), Vdoviak
patent: 4241586 (1980-12-01), Caruel et al.
patent: 4689961 (1987-09-01), Stratton
patent: 4843825 (1989-07-01), Clark
patent: 4991398 (1991-02-01), Clark et al.
patent: 5129231 (1992-07-01), Becker et al.

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