Title:
SHORT DISTANCE TAKEOFF AND LANDING AIRPLANE
Document Type and Number:
Japanese Patent JP2008162539
Kind Code:
A
Abstract:
To provide an airplane capable of generating climbing power with a simple device, and taking off and landing by a short distance.
This airplane has a rotary airfoil orthogonal to the travelling direction and rotating around a horizontal axis other than lifting power by a fixed airfoil. The rotary airfoil adds the climbing power.
More Like This:
JP6567054 | Multi-rotor with sloping wings |
JPH04317891 | AIRCRAFT FOR VERTICAL TAKE-OFF AND LANDING |
WO/2007/018559 | TANDEM ROTOR WING ROTATIONAL POSITION CONTROL SYSTEM |
Inventors:
HASEGAWA TAKASHI
Application Number:
JP2006357525A
Publication Date:
July 17, 2008
Filing Date:
December 28, 2006
Export Citation:
Assignee:
HASEGAWA TAKASHI
International Classes:
B64C27/24
Previous Patent: METHOD FOR REINFORCING HOLLOW DOUBLE WALL STRUCTURE
Next Patent: TARPAULIN FOR VESTIBULE DIAPHRAGM
Next Patent: TARPAULIN FOR VESTIBULE DIAPHRAGM