Turbo fan engine mixer

Power plants – Reaction motor – With thrust direction modifying means

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Details

60262, 23926537, F02K 100

Patent

active

042928036

ABSTRACT:
A turbo fan engine has a fan gas duct surrounding the exhaust or primary gas stream. The primary gas stream leaves the engine through a plurality of nozzles terminating within the fan gas stream. The nozzles are positioned so that mixing of the two gas streams is accomplished and, when utilized with a pair of clam shells for thrust reversing, cool air from the fan stream cools the inner surface of the clam shells and insulates the inner surface from the hot primary gas stream. The mixing of the streams is accomplished substantially within the fan gas duct.

REFERENCES:
patent: 3084505 (1963-04-01), Cherchi
patent: 3113428 (1963-12-01), Colley et al.
patent: 3587777 (1971-06-01), Ellis
patent: 3625008 (1971-12-01), Hewson et al.
patent: 3673803 (1972-07-01), Macdonald
patent: 4117671 (1978-10-01), Neal et al.
patent: 4135363 (1979-01-01), Packman
patent: 4147027 (1979-04-01), Greathouse

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