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Title:
VERTICAL TAKEOFF AND LANDING AIRCRAFT
Document Type and Number:
Japanese Patent JP2013010466
Kind Code:
A
Abstract:

To provide a vertical takeoff and landing aircraft capable of safely taking-off or landing even in a narrow space in which an obstacle is present while performing thrust control with a simple configuration.

A vertical takeoff and landing aircraft includes: a propeller 2 having a fan 21 for generating lift and thrust; a motor 3 for supplying power to the propeller 2; a frame 4 for coupling the propeller 2 and the motor 3; a seat 5 coupled so as to be able to turn forward and backward in relation to the frame 4, being suspended from and supported by the frame 4; a control stick 6 coupled with the frame 4; and a grounding leg 7 connected to the seat 5. The propeller 2 is coupled to the frame 4 such that the drive axis of the fan 21 is vertical during landing. Operation of the control stick 6 moves the frame 4 relative to the seat 5, changing the orientation of the propeller 2.


Inventors:
TSUNEKAWA MASAYOSHI
TAMURA TETSUYA
Application Number:
JP2011145525A
Publication Date:
January 17, 2013
Filing Date:
June 30, 2011
Export Citation:
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Assignee:
IHI CORP
International Classes:
B64C29/00; B64C27/20
Domestic Patent References:
JPH0391895U1991-09-19
JP2009137319A2009-06-25
JP2006015971A2006-01-19
JPS59501202A1984-07-12
JPH0692294A1994-04-05
JP4223921B22009-02-12
JPH0391895U1991-09-19
Attorney, Agent or Firm:
Koji Nagato
Echizen Masahiro