An aircraft (100) comprising a wing (10); a tractor propulsion means (TPM, 20); a pusher propulsion means (PPM, 30); a cruising propulsion means (CPM, 40); and wherein the TPM is capable of providing a thrust, the direction of thrust reversibly movable from a forward propelling direction, to an upward propelling direction; and wherein the PPM is capable of providing a thrust, the direction of thrust reversibly movable from a forward propelling direction, to an upward propelling direction; and wherein the CPM is capable of providing a thrust, the direction of thrust being in a forward propelling direction; and wherein the TPM and PPM are connected to the wing, and wherein the TPM is located in fore of the wing and the PPM is located in aft of the wing.
一种飞行器(100),包括:翼(10);牵引式推进装置(TPM,20);推进式推进装置(PPM,30);巡航推进装置(CPM,40);并且其中,所述TPM能够提供一推力,该推力的方向能够可逆地从向前推进方向移动到向上推进方向;并且其中,所述PPM能够提供一推力,该推力的方向能够可逆地从向前推进方向移动到向上推进方向;并且其中,所述CPM能够提供一推力,该推力的方向在向前推进方向上;并且其中,所述TPM和所述PPM连接到所述翼,并且其中,所述TPM位于所述翼的前部,并且所述PPM位于所述翼的后部。
Aircraft and modular propulsion unit
飞行器和模块化推进单元
2021-07-23
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |