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Title:
STEERING/THRUST CONTROLLER
Document Type and Number:
Japanese Patent JP3486302
Kind Code:
B2
Abstract:

PROBLEM TO BE SOLVED: To provide a steering/thrust controller capable of being miniaturized by reducing the power of a driving motor for controlling the flight of an airframe.
SOLUTION: The centers CPs of applying powers of aerodynamic forces, generated on an aerodynamic wing 5 and a thrust deflecting vane 07, are set so that the direction of an external load torque Tef due to aerodynamic load generated on the aerodynamic wing 5 and generated in the output shaft 06 of a driving motor 01, and the direction of another external load torque Tev due to an aerodynamic load generated in a thrust deflecting steering vane 07, become reverse mutually. According to this method, the load of the driving motor 01 becomes a difference between external load torque Tef and the same Tev whereby the output and the size of the driving motor can be reduced.


Inventors:
Satoshi Shinohara
Application Number:
JP19200996A
Publication Date:
January 13, 2004
Filing Date:
July 22, 1996
Export Citation:
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Assignee:
MITSUBISHI HEAVY INDUSTRIES,LTD.
International Classes:
F42B10/60; F42B15/01; (IPC1-7): F42B10/60; F42B15/01
Domestic Patent References:
JP5296699A
JP2217799A
JP62102100A
JP542895A
Attorney, Agent or Firm:
Arata Ishikawa