JPS5762933A - Control device for aircraft engine - Google Patents

Control device for aircraft engine

Info

Publication number
JPS5762933A
JPS5762933A JP13685680A JP13685680A JPS5762933A JP S5762933 A JPS5762933 A JP S5762933A JP 13685680 A JP13685680 A JP 13685680A JP 13685680 A JP13685680 A JP 13685680A JP S5762933 A JPS5762933 A JP S5762933A
Authority
JP
Japan
Prior art keywords
circuit
control device
systems
electric
circuits
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP13685680A
Other languages
Japanese (ja)
Other versions
JPS5928741B2 (en
Inventor
Masanori Endo
Mineo Kishimoto
Makoto Endo
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
National Aerospace Laboratory of Japan
IHI Corp
Original Assignee
National Aerospace Laboratory of Japan
Ishikawajima Harima Heavy Industries Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by National Aerospace Laboratory of Japan, Ishikawajima Harima Heavy Industries Co Ltd filed Critical National Aerospace Laboratory of Japan
Priority to JP13685680A priority Critical patent/JPS5928741B2/en
Publication of JPS5762933A publication Critical patent/JPS5762933A/en
Publication of JPS5928741B2 publication Critical patent/JPS5928741B2/en
Expired legal-status Critical Current

Links

Landscapes

  • Safety Devices In Control Systems (AREA)
  • Control Of Transmission Device (AREA)

Abstract

PURPOSE: To permit the high accurate and high reliable control by a digital electronic control device which comprises a monitoring circuit for electric and hydraulic systems adapted to detect troubles of a microcomputer for the respective control systems, a mutual transmission circuit between both the electric and hydraulic systems and so.
CONSTITUTION: This control device comprises a first system including an input signal processing circuit 1, No.1DEC (digital electronic control device) 3 and an output circuit 11, a second system including an input signal processing circuit 2, No.2 DEC4 and an output circuit 12, and parts common to both the systems. The common parts comprise a bi-directional memory 5 having such a function as to exhange informations between both the DEC's 3, 4 synchronous monitoring control circuit 6, electric system monitoring control circuits 7, 8, hydraulic switching system monitoring control circuits 8, and a switching circuit 10. The respective DEC's 3, 4 receive a signal A from various sensors 17 mounted on an engine body 16 and a signal B from a fleight Machmeter through mutual transmission circuits 19, 20. Thus, if becomes also able to detect troubles of the sensor 17 as early as possible.
COPYRIGHT: (C)1982,JPO&Japio
JP13685680A 1980-10-01 1980-10-01 Aircraft engine control device Expired JPS5928741B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13685680A JPS5928741B2 (en) 1980-10-01 1980-10-01 Aircraft engine control device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13685680A JPS5928741B2 (en) 1980-10-01 1980-10-01 Aircraft engine control device

Publications (2)

Publication Number Publication Date
JPS5762933A true JPS5762933A (en) 1982-04-16
JPS5928741B2 JPS5928741B2 (en) 1984-07-16

Family

ID=15185102

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13685680A Expired JPS5928741B2 (en) 1980-10-01 1980-10-01 Aircraft engine control device

Country Status (1)

Country Link
JP (1) JPS5928741B2 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS57176341A (en) * 1981-04-21 1982-10-29 Nippon Denso Co Ltd Internal combustion engine control computer device having mutual diagnostic device
JP2006316773A (en) * 2005-05-16 2006-11-24 Honda Motor Co Ltd Control device for aircraft gas turbine engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS57176341A (en) * 1981-04-21 1982-10-29 Nippon Denso Co Ltd Internal combustion engine control computer device having mutual diagnostic device
JP2006316773A (en) * 2005-05-16 2006-11-24 Honda Motor Co Ltd Control device for aircraft gas turbine engine
US7840336B2 (en) 2005-05-16 2010-11-23 Honda Motor Co., Ltd. Control system for gas turbine aeroengine

Also Published As

Publication number Publication date
JPS5928741B2 (en) 1984-07-16

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