The present invention relates to an airplane capable of hyper-short / vertical takeoff and landing (hyper-STOL / VTOL) and having a positive tilt angle applied to the 5 horizontal propulsors (104A, 104B). A positive tilt angle may also be applied to the vertical propulsors (106A, 106B, 106A1, 106A2, 106B1, 106B2). This invention attempts to reduce pitch angle during hovering and vertical flight.
本发明涉及一种能够超短距/垂直起飞和着陆(hyper‑STOL/VTOL)并且具有向水平推进器(104A,104B)施加的正倾角的飞机。正倾角也可以施加到垂直推进器(106A、106B、106A1、106A2、106B1、106B2)。本发明试图减小悬停和垂直飞行期间的俯仰角。
Airplane capable of hyper-short / vertical takeoff and landing
具有倾斜推进器的垂直起飞和着陆能力飞机
2021-09-28
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2023
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