Title:
AIRCRAFT
Document Type and Number:
Japanese Patent JP2020001509
Kind Code:
A
Abstract:
To provide an aircraft that includes a pair of left and right rotors, a rotor disposed on the airframe centerline, and a fixed wing and excels in the airframe stability during vertical takeoff and landing.SOLUTION: An aircraft includes: a fuselage 10; a fixed wing 20 comprising a swept-back wing; a propeller 40 generating forward thrust; a left rotor 31 disposed on the left side of the airframe centerline CL; a right rotor 32 disposed on the right side of the airframe centerline CL; and a central rotor 33 disposed on the airframe centerline CL. The center of gravity CG of an airframe is located inside a triangle 50 that is formed by connecting the rotation center line 31c of the left rotor 31, the rotation center line 32c of the right rotor 32 and the rotation center line 33c of the central rotor 33.SELECTED DRAWING: Figure 1
More Like This:
Inventors:
ONISHI YUSUKE
MIYAUCHI SORANO
MIYAKOSHI TETSUYA
HATTORI SATORU
SHIBATA MITOMU
MIYAUCHI SORANO
MIYAKOSHI TETSUYA
HATTORI SATORU
SHIBATA MITOMU
Application Number:
JP2018121641A
Publication Date:
January 09, 2020
Filing Date:
June 27, 2018
Export Citation:
Assignee:
SHIN MEIWA IND CO LTD
International Classes:
B64C29/00; B64C3/10; B64C27/08; B64C27/20
Foreign References:
| FR3020622A1 | 2015-11-06 | |||
| US20070057113A1 | 2007-03-15 | |||
| FR3020039A1 | 2015-10-23 |
Attorney, Agent or Firm:
Takashi Goto
Hiroaki Yamane
Hiroaki Yamane