Bypass augmentation burner arrangement for a gas turbine engine

Details Bypass augmentation burner arrangement for a gas turbine engine Bypass augmentation burner arrangement for a gas turbine engine

1974-12-12

1976-12-28

Freeh, William L.

Power plants

Combustion products used as motive fluid

External-combustion engine type

60 3974R, 60224, F02C 722

Patent

active

039993787

ABSTRACT:
A two stage bypass augmentation burner is provided for a gas turbine engine wherein the downstream end of the primary burner is convoluted to define alternating cold and hot chutes.

REFERENCES:
patent: 2647369 (1953-08-01), Leduc
patent: 2704440 (1955-03-01), Nicholson
patent: 2780060 (1957-02-01), Griffith
patent: 3048014 (1962-08-01), Schmidt
patent: 3100627 (1963-08-01), Wilde
patent: 3714778 (1973-02-01), Howald
patent: 3788065 (1974-01-01), Markowski

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