| 摘要 |
FIELD: mechanical engineering; turbojet engines. SUBSTANCE: turbojet engine thrust reverser has outer fixed support 10 whose outlet end is made in form of evolute out 14 which does not lie in plane square to reverser perpendicular axle 15, and movable part consisting of single shell 16 forming, when closed, outlet part of straight flow nozzle. Shell is able to turn around side axles 22, arranged on fixed support 10, under action of control system including at least one jack installed between axle engaging with fixed support and axle engaging with shell to form obstacle, when unfolded, thus providing reversing of thrust by shifting gas flow. EFFECT: enhanced reliability of operation. 7 cl, 8 dwg
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