Title:
翼型胴体無翼航空機
Document Type and Number:
Japanese Patent JP6735022
Kind Code:
B2
Abstract:
To increase transportation performance of an aircraft relatively to a size of a fuselage.SOLUTION: An aircraft has a fuselage of which longitudinal section has an airfoil profile and of which transverse section has a rectangular shape. In the aircraft, a fin 2 is installed in the whole line of both right and left ends of a top face and an under face of the airfoil profile fuselage 1 while being perpendicular to a fuselage surface. Part of the fin in front, back, right and left parts of the top face and the under face of the fuselage is configured to be a movable fin. A suction direction (opposite direction of combustion gas jet or propeller air blowing direction) of an engine installed in a rear end of the top face of the fuselage is configured to be movable.SELECTED DRAWING: Figure 2
Inventors:
Raw Takeshi
Application Number:
JP2018248906A
Publication Date:
August 05, 2020
Filing Date:
December 18, 2018
Export Citation:
Assignee:
Raw Takeshi
International Classes:
B64C39/10; B64C5/06; B64C9/02; B64D33/02
Domestic Patent References:
| JP7196095A | ||||
| JP10194198A | ||||
| JP63291799A | ||||
| JP8310498A | ||||
| JP5155387A | ||||
| JP1195200A | ||||
| JP1093199U |
Foreign References:
| US20050116087 | ||||
| US20180170508 | ||||
| US20100019081 | ||||
| CN108528717A | ||||
| KR101219172B1 |