FIELD: aviation.
SUBSTANCE: rescue system with an external suspension bracket of aircraft contains a folding platform self-revealing during descent and an inhaul rope. The platform is fitted with a ring clamp fixing top ends of the spokes rigidly fixed on the top end of the bearing rod together with the lower end of inhaul rope. The lower ends of spokes are hingedly fixed on the lower slide, which is coaxial and mobile with reference to the bearing rod and which is in spring-loaded interaction with it within the stroke of releasing of spokes from the ring clamp. Each spoke is implemented in the form of the two-arm lever the lower end of which is hingedly connected to the lower slider of the rod. The hinge of the central part of each spoke interacts through rod pushers with the top slide of the rod synchronising simultaneous folding and unfolding of spokes at relative shift of both slides.
EFFECT: decrease of hazard for life during evacuation.
10 cl, 18 dwg
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Authors
Dates
2015-09-20—Published
2014-05-14—Filed