Login| Sign Up| Help| Contact|

Patent Searching and Data


Title:
TRANSLATIONAL WING AIRCRAFT
Document Type and Number:
Japanese Patent JP2006291796
Kind Code:
A
Abstract:

To provide a translational wing aircraft simplifying mechanism, reducing weight, improving reliability, and reducing a manufacturing cost.

This translational wing aircraft employs a method for controlling output not by pitch angle control but by rotational speed control, a method for positioning a blade by pinching the upper part of one guide plate by more than one roller, and a method for changing a pitch angle by changing the angles of two arms installed fixedly on a blade shaft when pitch angle control is unescapable.


Inventors:
KUBOMURA KENJI
UCHIDA TAKASHI
Application Number:
JP2005111895A
Publication Date:
October 26, 2006
Filing Date:
April 08, 2005
Export Citation:
Click for automatic bibliography generation   Help
Assignee:
KUBOMURA KENJI
UCHIDA TAKASHI
International Classes:
F03D5/02; F03B9/00; F03D7/06; F04D33/00



 
Previous Patent: KNOCKING SUPPRESSING DEVICE

Next Patent: INLET FLOW VALVE SYSTEM