FIELD: heavier-than-air flying vehicles; dropping glide rockets from aircraft.
SUBSTANCE: proposed device includes wing turn mechanism 2 and slide block 11 with articulated rods 13 mounted symmetrically on longitudinal axles. Wings in form of first-order lever are kinematically linked with articulated rod of slide block which is secured through cross-piece supports on rod of pneumatic cylinder brought into communication with high-pressure source. Slide block is mounted for longitudinal motion on pneumatic cylinder and is connected with transversal base by means of bursting screws. Said transversal base carries wing turn axles. Pneumatic cylinder body has radial slot for forcing the wings of locking rod mounted in slide block and loaded with plate spring 19.
EFFECT: enhanced reliability.
2 cl, 3 dwg
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