Title:
VERTICAL TAKEOFF AND LANDING (VTOL) AIR VEHICLE
Document Type and Number:
Japanese Patent JP2023082107
Kind Code:
A
Abstract:
To provide an aerial vehicle that is efficient in flight and that can take off and land vertically.SOLUTION: A flight control apparatus for fixed-wing aircraft includes a first port wing 115 and first starboard wing 120, a first port swash plate 145 coupled between a first port rotor 155 and a first port electric motor 135 that is coupled to the first port wing 115, and a first starboard swash plate 150 coupled between a first starboard rotor 130 and a first starboard electric motor 140 that is coupled to the first starboard wing 120.SELECTED DRAWING: Figure 3A
Inventors:
DANA J TAYLOR
PHILLIP T TOKUMARU
BART DEAN HIBBS
WILLIAM MARTIN PARKS
DAVID WAYNE GANZER
CHRISTOPHER EUGENE FISHER
JASON SIDHARTHADEV MUKHERJEE
JOSEPH FREDERICK KING
PHILLIP T TOKUMARU
BART DEAN HIBBS
WILLIAM MARTIN PARKS
DAVID WAYNE GANZER
CHRISTOPHER EUGENE FISHER
JASON SIDHARTHADEV MUKHERJEE
JOSEPH FREDERICK KING
Application Number:
JP2023054895A
Publication Date:
June 13, 2023
Filing Date:
March 30, 2023
Export Citation:
Assignee:
AEROVIRONMENT INC
International Classes:
B64C29/02; B64C11/30; B64C25/02; B64C27/605; B64D27/24; B64U10/20; B64U50/19; B64U60/50
Attorney, Agent or Firm:
Kita Aoyama International Patent Attorney Corporation