Thrust reverser and silencer assembly of turbojet engines

Details Thrust reverser and silencer assembly of turbojet engines Thrust reverser and silencer assembly of turbojet engines

1980-07-15

1982-10-12

Frankfort, Charles E.

Aeronautics and astronautics

Retarding and restraining devices

Friction brakes

181217, 23926513, 23926517, 23926529, 244 53R, B64D 3304, F02K 154

Patent

active

043535160

ABSTRACT:
Two groups of half shells capable of being retracted from the jet flow, in a position closing the jet pipe. The thrust reverser and the silencer are concentric and their axes of rotation are upstream with respect to their position in the jet flow.

REFERENCES:
patent: 3139153 (1964-06-01), De Remer
patent: 3344882 (1967-10-01), Bellion et al.
patent: 3432100 (1969-03-01), Hardy et al.
patent: 3587973 (1971-06-01), Wolf et al.
patent: 3605939 (1971-09-01), Duthion
patent: 3759467 (1973-09-01), Roudil
patent: 3954224 (1976-05-01), Colebrook et al.
patent: 4043121 (1977-08-01), Thomas et al.
patent: 4291782 (1981-09-01), Klees

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