Title:
VERTICAL TAKEOFF AND LANDING (VTOL) AIR VEHICLE
Document Type and Number:
Japanese Patent JP2019142501
Kind Code:
A
Abstract:
To design and manufacture aerial vehicles that are 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), the first port electric motor 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), the first starboard electric motor 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:
JP2019082535A
Publication Date:
August 29, 2019
Filing Date:
April 24, 2019
Export Citation:
Assignee:
AEROVIRONMENT INC
International Classes:
B64C29/02; B64C11/30; B64C27/605; B64D27/24
Domestic Patent References:
| JP2002362496A | 2002-12-18 | |||
| JPH08310498A | 1996-11-26 | |||
| JP2009083798A | 2009-04-23 | |||
| JP2012198883A | 2012-10-18 |
Foreign References:
| US20100252690A1 | 2010-10-07 | |||
| US20120043413A1 | 2012-02-23 | |||
| US3181810A | 1965-05-04 | |||
| US20120248259A1 | 2012-10-04 | |||
| US5765783A | 1998-06-16 | |||
| US20050178879A1 | 2005-08-18 |
Attorney, Agent or Firm:
Patent business corporation Kita Aoyama International