FIELD: aircraft jet engines. SUBSTANCE: device includes movable housing 2 articulated with swivel doors 9. Each swivel door is articulated with fixed housing 1 by means of two levers 3 and 4 and compensator 5. Levers of each door are mounted on limiting stop 12, 18 fitted on one of levers. Each door is mounted in movable housing by means of stop 11 and is closed by folded levers. Stops are adjustable in height. Housing of compensator is rigidly secured on fixed housing. Working member is made in form of two pistons 14 which are located on either side of first lever and are interconnected by means of common base 17 which is articulated with first lever. EFFECT: reduction of losses in engine thrust, reduction of vibrations and enhanced reliability. 6 cl, 6 dwg
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