Specially configured deflection edge thrust reverser for jet eng

Aeronautics and astronautics – Retarding and restraining devices – Friction brakes

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Details

23926529, 23926541, 602262, 60230, B64C 3304, F02K 164

Patent

active

057160252

ABSTRACT:
The reverser includes a partition (28) exhibiting openings (19) and separating the cavity (16) which exists, when the doors (2) are in the closed position, between the front part (7) of the internal panel (11) of the door and the stream of gaseous flow (15) flowing in direct jet mode through the jet pipe CA, thus overcoming the aerodynamic losses which result from the presence of this cavity.

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patent: 4093122 (1978-06-01), Linderman et al.
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patent: 4485970 (1984-12-01), Fournier et al.
patent: 4922712 (1990-05-01), Matta et al.
patent: 4976466 (1990-12-01), Vauchel
patent: 5003770 (1991-04-01), Schegerin et al.
patent: 5224342 (1993-07-01), Lair
patent: 5372006 (1994-12-01), Lair

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