A short take-off and landing (STOL) vehicle includes a tail having a surface and a fuselage having a surface, where the tail and fuselage have continuous surfaces, where the surface of the tail is directly coupled to the surface of the fuselage. The vehicle further includes a sweepforward wing having a trailing edge and a rotor attached to the trailing edge of the sweepforward wing via a pylon, where the rotor has a maximum downward angle from the horizontal plane that is less than or equal to 60 degrees, and the STOL vehicle takes off and lands using at least some lift from the sweepforward wing and at least some lift from the rotor.
一种短距起降(STOL)载具,其包括具有表面的机尾和具有表面的机身,其中机尾和机身具有连续表面,其中机尾的表面直接联接到机身的表面。载具进一步包括具有后缘的前掠翼和经由挂架附接到前掠翼的后缘的旋翼,其中旋翼具有小于或等于60°的与水平面的最大向下角度,并且STOL载具使用来自前掠翼的至少一些升力和来自旋翼的至少一些升力来起飞和降落。
Short-distance take-off and landing carrier with forward swept wings
具有前掠翼的短距起降载具
2025-03-11
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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