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Title:
HYBRID LIGHT MANNED AIRCRAFT HAVING FIXED WINGS AND ROTOR WINGS, AND AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2022/121444
Kind Code:
A1
Abstract:
Disclosed are a hybrid light manned aircraft having fixed wings and rotor wings, and an aircraft, the aircraft comprising: a fuselage, wings, an empennage, a propulsion device and a landing device. Rotor wing assemblies are provided on the wings, and each set of rotor wing assemblies comprises a rotor wing. The aircraft also comprises a flight power system comprising at least one set of power supply devices; the rotor wing assemblies and the power supply devices are detachably mounted on the wings; a manned aircraft combining fixed wings and rotor wings is formed when the rotor wing assemblies and the power supply devices are mounted, and a manned aircraft having fixed wings is formed when the rotor wing assemblies and a battery compartment are dismounted. The present invention creatively proposes a reconfigurable aircraft. By adding components such as power supply devices and rotor wings to wings to form a vertical lift system, the aircraft may vertically take off and land and also take off and land from a runway; in addition, the aircraft is restored to a fixed-wing manned aircraft by dismounting the components mounted on the wings.

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Inventors:
WU BIN (CN)
LV XIZHE (CN)
Application Number:
PCT/CN2021/119936
Publication Date:
June 16, 2022
Filing Date:
September 23, 2021
Export Citation:
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Assignee:
SHANGHAI FLYMAN AVIATION SERVICES CORP (CN)
International Classes:
B64D27/24; B64C27/24; B64D47/00
Foreign References:
CN112407269A2021-02-26
CN112722289A2021-04-30
CN214138980U2021-09-07
CN208530842U2019-02-22
CN206857019U2018-01-09
CN207242030U2018-04-17
CN209814262U2019-12-20
CN110116802A2019-08-13
CN107499506A2017-12-22
KR20200080825A2020-07-07
Attorney, Agent or Firm:
SHANGHAI HANGSOME INTELLECTUAL PROPERTY LTD (CN)
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