FIELD: aircraft engineering.
SUBSTANCE: invention relates to the field of aviation, in particular to the design of devices for assisting in the manoeuvring of a cover of a nacelle of a turbojet engine. Assistance device comprises bent part (13-15) mounted on hinge (41, 75) coaxial with hinge (5, 6) of connecting element (4, 7). Hinge of the device is rigidly connected to bent part (13-15), one end of which rests on connecting element coupling (35, 38) of cover (1, 2) and one point of which is pivotally connected to compression spring (17, 27) so as to apply assistance momentum to the connecting element when lifting of cover (1, 2).
EFFECT: weight of the aircraft is reduced.
8 cl, 9 dwg
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