FIELD: engines and pumps.
SUBSTANCE: aircraft car comprises a bonnet, an engine installed in the inner volume of the bonnet, a circular channel for secondary traction flow passage made between the engine and the bonnet, and also a thrust reverse installed on the rear end of the bonnet for displacement between two positions. In the first closed position the thrust reverse forms a rear end of the bonnet, and in the second open position the thrust reverse blocks the circular channel of passage and sends the secondary traction flow outside the bonnet to the front end to form a reverse flow. The reverse comprises multiple static connection rods, multiple folds and driving facilities. Static connection rods are installed as fixed relative to the bonnet and pass as extension of the bonnet towards the rear part. Folds are installed at two arcs of circumference and are fixed as capable of rotation at two static connection rods, besides, each fold adjoins at least another fold, while the thrust reverse is in closed position. Driving facilities provide for the possibility of simultaneous rotation of folds between the first and second positions. Another invention of the group relates to an aircraft comprising the above car.
EFFECT: inventions make it possible to reduce the possibility of thrust reverse folds deformation and disturbance of the flow when streamlining the car.
17 cl, 14 dwg
