JPS5698535A - System for controlling starting operation of ceramic gas-turbine engine - Google Patents

System for controlling starting operation of ceramic gas-turbine engine

Info

Publication number
JPS5698535A
JPS5698535A JP39480A JP39480A JPS5698535A JP S5698535 A JPS5698535 A JP S5698535A JP 39480 A JP39480 A JP 39480A JP 39480 A JP39480 A JP 39480A JP S5698535 A JPS5698535 A JP S5698535A
Authority
JP
Japan
Prior art keywords
starter
turning force
fuel
resistance
relay
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.)
Pending
Application number
JP39480A
Other languages
Japanese (ja)
Inventor
Toru Takeuchi
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.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor 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 Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Priority to JP39480A priority Critical patent/JPS5698535A/en
Publication of JPS5698535A publication Critical patent/JPS5698535A/en
Pending legal-status Critical Current

Links

Landscapes

  • Output Control And Ontrol Of Special Type Engine (AREA)

Abstract

PURPOSE: To prevent the ceramic material from being applied with drastic thermal shock, by lowering the turning force of the starter and reducing the fuel supply rate for a predetermined period of time at the time of starting engine.
CONSTITUTION: When a starter switch 1 is turned ON, a relay 3 is closed and a timer 14 is set into operation for shifting a selector switch 15 to the side of a resistance 17. At the same time, a relay 13 is closed. Since electric current is thus supplied to a starter 4 via the resistance 17, the starter 4 is set into rotation but its turning force is low. On the other hand, since a start fuel signal CVset2 is transmitted to a fuel control valve 7 after it is reduced by a subtracter 12 by a level determined by a variable resistance 16, the fuel flow rate is lowered. By thus lowering the turning force of the starter 4 and the fuel flow rate, high-temperature combustion gas after ignition flows at a low speed in an engine 8.
COPYRIGHT: (C)1981,JPO&Japio
JP39480A 1980-01-07 1980-01-07 System for controlling starting operation of ceramic gas-turbine engine Pending JPS5698535A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP39480A JPS5698535A (en) 1980-01-07 1980-01-07 System for controlling starting operation of ceramic gas-turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP39480A JPS5698535A (en) 1980-01-07 1980-01-07 System for controlling starting operation of ceramic gas-turbine engine

Publications (1)

Publication Number Publication Date
JPS5698535A true JPS5698535A (en) 1981-08-08

Family

ID=11472582

Family Applications (1)

Application Number Title Priority Date Filing Date
JP39480A Pending JPS5698535A (en) 1980-01-07 1980-01-07 System for controlling starting operation of ceramic gas-turbine engine

Country Status (1)

Country Link
JP (1) JPS5698535A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5915639A (en) * 1982-07-19 1984-01-26 Yanmar Diesel Engine Co Ltd Control device of gas turbine engine
JPS5915638A (en) * 1982-07-19 1984-01-26 Yanmar Diesel Engine Co Ltd Control device of gas turbine engine
CN108708790A (en) * 2018-04-19 2018-10-26 中国航发南方工业有限公司 The progress of starting sequence control device and control method of fanjet

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5915639A (en) * 1982-07-19 1984-01-26 Yanmar Diesel Engine Co Ltd Control device of gas turbine engine
JPS5915638A (en) * 1982-07-19 1984-01-26 Yanmar Diesel Engine Co Ltd Control device of gas turbine engine
JPH0355654B2 (en) * 1982-07-19 1991-08-26
JPH0355653B2 (en) * 1982-07-19 1991-08-26
CN108708790A (en) * 2018-04-19 2018-10-26 中国航发南方工业有限公司 The progress of starting sequence control device and control method of fanjet

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