Gas turbine combustion chamber

Details Gas turbine combustion chamber Gas turbine combustion chamber

1979-05-03

1981-11-24

Garrett, Robert E.

Power plants

Combustion products used as motive fluid

Combustion products generator

60750, 60758, 60759, F02C 722

Patent

active

043016570

ABSTRACT:
A gas turbine combustion chamber in which the primary air inlets in a peripheral wall of the combustion chamber are defined by open-ended tubes extending inwardly from the peripheral wall by a substantial distance into the combustion chamber and having their inner, that is their outlet, ends facing in an upstream direction within the combustion chamber, whereby each of the tubes will introduce a stream of air with at least a component of motion in the upstream direction along or parallel with the longitudinal axis of the combustion chamber, thereby to effect recirculation of fuel, air and combustion gases within the combustion chamber. Similar air inlet tubes may be provided for introducing secondary and tertiary air into the combustion chamber.

REFERENCES:
patent: 2510645 (1950-06-01), McMahan
patent: 2601000 (1952-06-01), Nerad
patent: 2807139 (1957-09-01), Jackson
patent: 3099134 (1963-07-01), Calder et al.
patent: 3134229 (1964-05-01), Johnson
patent: 3656297 (1972-04-01), Monk
patent: 4054028 (1977-10-01), Kawaguchi

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