Title:
テイルシッター
Document Type and Number:
Japanese Patent JP7433254
Kind Code:
B2
Abstract:
A tail sitter aircraft (1, 1') is described that comprises: a fuselage (2) arranged vertically in a Take-off/landing position and transversely to a vertical direction in a cruising position of the aircraft (1, 1'); a single wing (4); two first engines (15a, 15b) configured to exert respective first thrusts directed along respective first axes (A) on the tail sitter (1, 1'); and at least two second engines (15c, 15d) rotating about respective second axes (A) arranged above the first axes (A) of the first engines (15a, 15b), with reference to the cruising position; the at least two second engines being configured to exert respective second thrusts directed along respective second axes (A) on the tail sitter (1, 1'); the first and second engines (15a, 15b; 15c, 15d) being carried by the single wing (4); the first axes (A) of the first engines (15a, 15b) and the second axes (A) of the second engines (15c, 15d) being arranged along said front section (C) of the single wing (4).
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Inventors:
Riccardo Bianco Mengotti
Application Number:
JP2020572754A
Publication Date:
February 19, 2024
Filing Date:
June 28, 2019
Export Citation:
Assignee:
Leonardo Esse Pi A
International Classes:
B64C29/02; B64C1/26; B64C11/30; B64C39/02; B64D27/40
Foreign References:
| WO2016005954A1 | ||||
| US20180044011 | ||||
| US3350035 | ||||
| EP3243750A1 | ||||
| EP3263445A1 | ||||
| US20110042510 | ||||
| CN206327567U | ||||
| WO2018152258A1 |
Other References:
Vikram Hrishikeshavan and Inderjit Chopra,“High-Speed Quad-Rotor Biplane Micro Air Vehicle for Multiple-Role Missions”,Proceedings of the 4th Asian-Australian Rotorcraft Forum,IN,2015年11月
Attorney, Agent or Firm:
Yasuhiko Murayama
Shinya Mihiro
Tatsuhiko Abe
Shinya Mihiro
Tatsuhiko Abe