Title:
飛翔機の制御装置
Document Type and Number:
Japanese Patent JP4207039
Kind Code:
B2
Abstract:
The thrust control signal transmitted from the operator of an aircraft is input in both an aircraft control ECU and engine control ECUs that control respective gas-turbine engines such that the engine control ECUs can obtain information concerning the aircraft required output. The engine control ECUs control speeds of the respective gas-turbine engines such that each of the gas-turbine engines half the aircraft required output.
More Like This:
Inventors:
Daiki Fukuda
Application Number:
JP2005348828A
Publication Date:
January 14, 2009
Filing Date:
December 02, 2005
Export Citation:
Assignee:
TOYOTA JIDOSHA KABUSHIKI KAISHA
International Classes:
F02C6/08; B64C29/00; B64D31/00; F02K1/28
Domestic Patent References:
| JP9032581A | ||||
| JP2003206806A |
Attorney, Agent or Firm:
Yoshiyuki Kawaguchi
Hidemi Matsukura
Mayuko Wakuda
Kazunobu Sera
Tsutomu Toyama
Hidemi Matsukura
Mayuko Wakuda
Kazunobu Sera
Tsutomu Toyama