Premixed combustor

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

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Details

60 3971, F02C 722

Patent

active

040819574

ABSTRACT:
A combustion system for a gas turbine engine is disclosed. Fluid transfer and premixing techniques are developed. The combustion system is specifically adapted, in one embodiment, to an engine having a centrifugal or an axial/centrifugal compressor including a pipe diffuser at the downstream end thereof. Flow transfer tubes are shown between the pipe diffuser and a radial inflow combustor.

REFERENCES:
patent: 2567079 (1951-09-01), Owner et al.
patent: 2920449 (1960-01-01), Johnson
patent: 3238718 (1966-03-01), Hill
patent: 3283502 (1966-11-01), Lefebvre
patent: 3584791 (1971-06-01), Stratton et al.

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