Turbojet engine thrust reverser with rear support structure

Details Turbojet engine thrust reverser with rear support structure Turbojet engine thrust reverser with rear support structure

1994-11-25

1996-08-27

Bertsch, Richard A.

Power plants

Reaction motor

Interrelated reaction motors

60230, 24411013, 23926529, F02K 302

Patent

active

055489540

ABSTRACT:
A thrust reverser for a turbojet engine is disclosed in which the actuator for the thrust reverser is attached to a second support frame located downstream of the reverse thrust opening. A plurality of longitudinally extending beams interconnect the downstream support frame to an upstream support frame which is located upstream of the reverse thrust opening. A cylinder of the actuating device is attached to the downstream support frame and the extendible and retractable piston rod is attached to the moveable thrust reverser element. The location of the actuating device allows for a better stress distribution and enables the weight to be reduced as compared to prior art thrust reversers.

REFERENCES:
patent: 3172256 (1965-03-01), Kerry et al.
patent: 3262270 (1966-07-01), Beavers
patent: 3279181 (1966-10-01), Beavers et al.
patent: 3600894 (1971-08-01), McClain
patent: 3610533 (1971-10-01), Johnson
patent: 3614037 (1971-10-01), Vdolek
patent: 3747855 (1973-07-01), Vdoviak et al.
patent: 3815357 (1974-06-01), Brennan
patent: 3831376 (1974-08-01), Moorehead
patent: 4026105 (1977-05-01), James
patent: 4030291 (1977-06-01), Sargisson
patent: 4407120 (1983-10-01), Timms
patent: 4858430 (1989-08-01), Belbouche
patent: 4894985 (1990-01-01), Dubois et al.
patent: 4914905 (1990-04-01), Dubois et al.
patent: 4916895 (1990-04-01), Dubois
patent: 4960243 (1990-10-01), Dubois et al.
patent: 4976466 (1990-12-01), Vauchel
patent: 5039171 (1991-08-01), Lore
patent: 5046307 (1991-09-01), Matta et al.
patent: 5235807 (1993-08-01), Nightingale

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