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Title:
CONTROL DEVICE OF FLYING MACHINE
Document Type and Number:
Japanese Patent JP2007154708
Kind Code:
A
Abstract:

To provide technique enabling respective gas turbine engines to equally share and output the power demanded by an aircraft in the flying machine equipped with the plurality of gas turbine engines controlled under pressure ratio constant control.

A thrust control signal from a pilot inputted to an aircraft control ECU 41 is inputted also to engine control ECUs 40A/40B, which control the respective gas turbine engines 10, to enable the engine control ECUs 40 to acquire information of the aircraft demand power. Each engine control ECU 40 controls rotation speed of each gas turbine engine 10 so that the gas turbine engine 10 outputs a half of the aircraft demand power.


Inventors:
FUKUDA HIROYOSHI
Application Number:
JP2005348828A
Publication Date:
June 21, 2007
Filing Date:
December 02, 2005
Export Citation:
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Assignee:
TOYOTA MOTOR CORP
International Classes:
F02C6/08; B64C29/00; B64D31/00; F02K1/28
Attorney, Agent or Firm:
Yoshiyuki Kawaguchi
Hidemi Matsukura
Mayuko Wakuda
Kazunobu Sera
Tsutomu Toyama



 
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