JPS55146235A - Temperature protector circuit for two-shaft gas turbine - Google Patents

Temperature protector circuit for two-shaft gas turbine

Info

Publication number
JPS55146235A
JPS55146235A JP5145579A JP5145579A JPS55146235A JP S55146235 A JPS55146235 A JP S55146235A JP 5145579 A JP5145579 A JP 5145579A JP 5145579 A JP5145579 A JP 5145579A JP S55146235 A JPS55146235 A JP S55146235A
Authority
JP
Japan
Prior art keywords
temperature
inlet
comparator
setter
δtm
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
JP5145579A
Other languages
Japanese (ja)
Other versions
JPS5949413B2 (en
Inventor
Teruo Miyata
Nobuichi Okamoto
Etsuji Kino
Arata Suminoe
Noboru Fujii
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.)
Mitsubishi Motors Corp
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Motors Corp
Mitsubishi Heavy Industries 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 Mitsubishi Motors Corp, Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Motors Corp
Priority to JP5145579A priority Critical patent/JPS5949413B2/en
Publication of JPS55146235A publication Critical patent/JPS55146235A/en
Publication of JPS5949413B2 publication Critical patent/JPS5949413B2/en
Expired legal-status Critical Current

Links

Landscapes

  • Control Of Turbines (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

PURPOSE: To prevent overheating of gas turbine and to keep a high accelerating performance of the same independently of the change in the temperature of intake air, by detecting the temperature at the inlet of compressor, comparing the same with a reference temperature, and determining the allowance for the temperature at the inlet of gas generator from the above comparison of temperatures.
CONSTITUTION: Temperature T1 at the inlet of compressor 1, detected by temperature detector 51, is directed to comparator 53 and compared with output T1D of reference temperature setter 52. From the comparator 53, deviation signal (T1- T1D) is afforded to gain setter 57, which in turn produces a correction signal ΔTM for the allowance of the temperature at the inlet of gas generator on the basis of deviation (T1-T1D) of the intake temperature and furnishes it to comparator 59. Comparator 59 calculates the deviation between output ΔTD of reference signal setter 58 and output ΔTM of setter 57 and affords allowance for the temperature at the inlet of gas generator (ΔT=ΔTD-ΔTM) to adder 29.
COPYRIGHT: (C)1980,JPO&Japio
JP5145579A 1979-04-27 1979-04-27 Temperature protector circuit for dual-shaft gas turbine Expired JPS5949413B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5145579A JPS5949413B2 (en) 1979-04-27 1979-04-27 Temperature protector circuit for dual-shaft gas turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5145579A JPS5949413B2 (en) 1979-04-27 1979-04-27 Temperature protector circuit for dual-shaft gas turbine

Publications (2)

Publication Number Publication Date
JPS55146235A true JPS55146235A (en) 1980-11-14
JPS5949413B2 JPS5949413B2 (en) 1984-12-03

Family

ID=12887399

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5145579A Expired JPS5949413B2 (en) 1979-04-27 1979-04-27 Temperature protector circuit for dual-shaft gas turbine

Country Status (1)

Country Link
JP (1) JPS5949413B2 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58176422A (en) * 1982-04-07 1983-10-15 Toyota Motor Corp Fuel control device for gas turbine engine
JPS58222924A (en) * 1982-06-22 1983-12-24 Toyota Motor Corp Controller of gas turbine engine
CN113740068A (en) * 2021-08-31 2021-12-03 重庆长安汽车股份有限公司 Method for identifying influence of engine intake along-way temperature on vehicle acceleration performance

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58176422A (en) * 1982-04-07 1983-10-15 Toyota Motor Corp Fuel control device for gas turbine engine
JPS58222924A (en) * 1982-06-22 1983-12-24 Toyota Motor Corp Controller of gas turbine engine
CN113740068A (en) * 2021-08-31 2021-12-03 重庆长安汽车股份有限公司 Method for identifying influence of engine intake along-way temperature on vehicle acceleration performance
CN113740068B (en) * 2021-08-31 2024-02-09 重庆长安汽车股份有限公司 Method for identifying influence of engine air inlet along-path temperature on vehicle acceleration performance

Also Published As

Publication number Publication date
JPS5949413B2 (en) 1984-12-03

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