Double jet gas turbine engine equipped with a thrust reverser

Power plants – Reaction motor – Interrelated reaction motors

Patent

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Details

60230, 60232, 60262, 23926529, F02K 306

Patent

active

043620159

ABSTRACT:
The present invention relates to a gas turbine engine which is provided with a thrust reverser with unfoldable doors and which is of the double jet type, i.e. comprising a central generator emitting a jet of hot gas and surrounded by an annular by-pass conduit through which a jet of relatively cold gas passes, wherein said turbine engine comprises means for restricting the passage of the jet of relatively cold gas in said annular by-pass conduit when the doors of the thrust reverser are unfolded. The invention results in a simplification of the structure of the doors of the thrust reverser.

REFERENCES:
patent: 3100627 (1963-08-01), Wilde
patent: 3196609 (1965-07-01), Ingram
patent: 3660982 (1972-05-01), Gozlan
patent: 4069663 (1978-01-01), Harper
patent: 4072008 (1978-02-01), Kenworthy
patent: 4073440 (1978-02-01), Hapke

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