Turbojet-engine thrust reverser with internal clamshells

Power plants – Reaction motor – Interrelated reaction motors

Patent

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Details

60232, 244110B, 23926529, 23926531, F02K 160

Patent

active

061518859

ABSTRACT:
A turbojet-engine thrust reverser comprises a displaceable sub-assembly including two internal clamshells (12) mounted on stationary pivots (18) of a stationary structure (1) and an annular, axially displaceable structure (11). The displaceable structure forms the external, downstream part (13) of a cowling. In the forward-thrust mode, the displaceable structure forms a downstream portion (15) of a radial outer wall of the flow path and forms the entire trailing edge by covering the clamshells (12) such that the clamshells form part of the radial outer wall of the flow path.

REFERENCES:
patent: 2847823 (1958-08-01), Brewer
patent: 2950595 (1960-08-01), Laucher et al.
patent: 2972681 (1961-03-01), Bennett et al.
patent: 3550855 (1970-12-01), Feld et al.
patent: 4183478 (1980-01-01), Rudolph
patent: 4340178 (1982-07-01), Lawson
patent: 4410152 (1983-10-01), Kennedy et al.
patent: 4790495 (1988-12-01), Greathouse et al.
patent: 4860956 (1989-08-01), Fage
patent: 5181676 (1993-01-01), Lair
patent: 5392991 (1995-02-01), Gatti et al.
patent: 5806302 (1998-09-01), Cariola et al.
patent: 5853148 (1998-12-01), Standish et al.
patent: 5863014 (1999-01-01), Standish

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