FIELD: engines and pumps.
SUBSTANCE: this thrust reverser comprises fixed structure, deflectors, moving cowl and reversing flaps. The latter are arranged to turn in the area of upstream top end at moving cowl and driven by actuator levers. Moving cowl is driven by actuating cylinders. Note here that reversing flaps are coupled with appropriate actuating cylinders by actuator levers. Linear displacement of moving cowl actuating cylinders and those of recessing flaps allows displacement of moving cowl from closed position to open position. Closed moving cowl closes deflectors while reversing flaps are retracted. Open moving cowl opens deflectors to open passage in nacelle while reversing flaps are turned up to block nacelle outer edge section. Deflectors and their drive cylinders are located in two, in fact, parallel planes located one above the other in radial direction of nacelle. At least one of said reversing flaps is driven by adjacent reversing flaps actuated by drive cylinder. Another invention of the set relates to bypass turbojet with above described thrust reverser.
EFFECT: simplified assembly, decreased weight.
16 cl, 12 dwg
