HELICOPTER CABIN WITH TRAUMA-RESISTANT CONTROLS Russian patent published in 2005 - IPC

Abstract RU 2265556 C1

FIELD: aeronautical engineering; helicopter controls.

SUBSTANCE: cabin is provided with longitudinal and lateral control stick 5 and collective-pitch stick 29 kinematically connected with leverage mechanism located under seat 1 and connected with movable member 2 of shock absorber of seat 1 by means of rod 12. Leverage mechanism is connected with directional control pedals 36 and 37 which are made according to parallel-motion linkage.

EFFECT: reduced probability of pilot trauma in case of emergency fall of helicopter.

3 cl, 2 dwg

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RU 2 265 556 C1

Authors

Gubarev B.A.

Dates

2005-12-10—Published

2004-05-06—Filed