AIRCRAFT TURBOJET ENGINE POD, A POWER PLANT AND AN AIRCRAFT CONTAINING SUCH A POD Russian patent published in 2021 - IPC B64D29/06 

FIELD: aviation.

SUBSTANCE: invention relates to a turbojet engine pod, a power plant equipped with such a pod, and an aircraft containing such a power plant. The pod of a turbojet engine of an aircraft consists of a rear section without a lower bifurcation, which contains a thrust reversal system containing a movable hood. In this case, the pod contains a guiding system having a movable part and a fixed part. In this case, the movable part is connected in translational motion with the movable hood and interacts with the stationary part. Moreover, the stationary part is stationary relative to the pod. In this case, the guiding system is located near the so-called "six o'clock" position. In this case, the length of the stationary part of the guide system is greater than or equal to 50% of the length of the movable part. The group of inventions also relates to an aircraft power plant containing a bypass turbojet engine, wherein the power plant contains the above-described pod as well as an aircraft containing at least one above-described power plant.

EFFECT: invention proposes to eliminate the disadvantages of the known technical solutions due to the correct transfer of all forces acting on the sliding hood and on the reversing grilles to the lower part of the pod.

15 cl, 9 dwg