Title:
ハイブリッド有人飛行体
Document Type and Number:
Japanese Patent JP6751537
Kind Code:
B2
Abstract:
To provide a manned aircraft as new means of moving.SOLUTION: A hybrid manned aircraft of the present invention comprises: an engine; a motor; a first rotary wing unit for generating an aerodynamic lift using the engine; a second rotary wing unit for generating at least a thrust in the front-back direction using the motor; and a control unit for controlling the engine and the motor. In this way, the separation between the rotary wing unit for lift and the rotary wing unit for thrust can achieve an efficient structure of the aircraft according to the power needed.SELECTED DRAWING: Figure 1
Inventors:
Shuhei Komatsu
Application Number:
JP2018175395A
Publication Date:
September 09, 2020
Filing Date:
September 19, 2018
Export Citation:
Assignee:
Alitechnologies inc.
International Classes:
B64D27/02; B64C27/08; B64C27/20; B64C29/00; B64D27/24; H02J7/00
Domestic Patent References:
| JP2015085934A | ||||
| JP2019503941A | ||||
| JP2019501057A | ||||
| JP2000142379A |
Foreign References:
| WO2017105266A1 | ||||
| WO2017087399A1 | ||||
| US20030062442 | ||||
| US20160304193 | ||||
| US20110163199 | ||||
| WO2012026022A1 | ||||
| US20120032032 | ||||
| CN104773290A |
Attorney, Agent or Firm:
Minoru Nakahata