Door thrust reverser for a jet engine

Fluid sprinkling – spraying – and diffusing – Reaction motor discharge nozzle – With means controlling amount – shape or direction of...

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60230, 23926537, B64C 1500

Patent

active

046714600

ABSTRACT:
The invention provides a thrust inverser for a jet engine comprising doors 5-6 pivotably mounted at 14 on two beams diametrically opposite with respect to the gas discharge channel 2. The mechanism for operating the doors is entirely contained in the closed caisson formed by one of the beams 3, this mechanism comprising an actuating cylinder 15 driving a transmission piece 21 suspended from the beam 3, the transmission piece being coupled to two links 28 pivotably secured to the doors 5 and 6.

REFERENCES:
patent: 2839891 (1958-06-01), Drakeley
patent: 3002342 (1961-10-01), Schatzki
patent: 3531049 (1970-09-01), Hom
patent: 3532275 (1970-10-01), Hom et al.
patent: 3550855 (1970-12-01), Feld et al.
patent: 3567128 (1971-03-01), Urguhart et al.
patent: 3576337 (1971-04-01), Gudde
patent: 4147027 (1979-04-01), Greathouse
patent: 4212442 (1980-07-01), Fage

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