Fuel distribution manifold to an annular combustion chamber

Details Fuel distribution manifold to an annular combustion chamber Fuel distribution manifold to an annular combustion chamber

1975-04-25

1977-06-14

Croyle, Carlton R.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60 3936, 60 3974R, 239550, 285 32, 285 89, 285224, F02C 722

Patent

active

040288889

ABSTRACT:
A fuel distribution system for a gas turbine-compressor includes means permitting ready replacement and maintenance of individual fuel nozzles without disassembly of the entire fuel nozzle system. The gas turbine-compressor finds particularly useful application in areas where high power, compact, relatively maintenance-free units are required, as, for example, on offshore platforms in the natural gas industry.

REFERENCES:
patent: 691246 (1902-01-01), Cram
patent: 2344698 (1944-03-01), Howe
patent: 2359846 (1944-10-01), Hayman
patent: 2672727 (1954-03-01), Brown
patent: 2690648 (1954-10-01), Pearce et al.
patent: 2795106 (1957-06-01), Martin
patent: 2970438 (1961-02-01), Howald

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