JPS5781131A - Starting time fuel control circuit for gas turbine - Google Patents

Starting time fuel control circuit for gas turbine

Info

Publication number
JPS5781131A
JPS5781131A JP15691380A JP15691380A JPS5781131A JP S5781131 A JPS5781131 A JP S5781131A JP 15691380 A JP15691380 A JP 15691380A JP 15691380 A JP15691380 A JP 15691380A JP S5781131 A JPS5781131 A JP S5781131A
Authority
JP
Japan
Prior art keywords
gas turbine
inlet temperature
hot start
starting time
comparator
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
JP15691380A
Other languages
Japanese (ja)
Other versions
JPS624540B2 (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 JP15691380A priority Critical patent/JPS5781131A/en
Publication of JPS5781131A publication Critical patent/JPS5781131A/en
Publication of JPS624540B2 publication Critical patent/JPS624540B2/ja
Granted legal-status Critical Current

Links

Abstract

PURPOSE: To prevent excessive heating of the gas turbine materials at the time of hot start by providing a fuel-variable vane control circuit to input the compressor inlet temperature and the gas turbine outlet temperature and output the fuel flow reduction signal.
CONSTITUTION: A fuel-variable vane control 20 has a reference inlet temperature setter 51, a comparator 52 which compares the output signal T1D of said setter 51 with a compressor inlet temperature measured value T1, and an adjuster 53 which receives the output of said comparator 52 and outputs the starting time fuel flow reduction signal ΔGf1. The control 20 also has a pre-start gas turbine inlet temperature memory circuit 54, a hot start determination reference temperature setter 55, a comparator 56 which compares the hot start determination reference temperature T7IS with the gas turbine inlet temperature T7I, and a adjuster 57 which outputs the starting time fuel flow reduction signal ΔGf2. A minimum value selection circuit 58 receives these two signals, ΔGf1 and ΔGf2, and sends out a smaller signal of the two to an adder 26 as a hot start time fuel reduction signal.
COPYRIGHT: (C)1982,JPO&Japio
JP15691380A 1980-11-10 1980-11-10 Starting time fuel control circuit for gas turbine Granted JPS5781131A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15691380A JPS5781131A (en) 1980-11-10 1980-11-10 Starting time fuel control circuit for gas turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15691380A JPS5781131A (en) 1980-11-10 1980-11-10 Starting time fuel control circuit for gas turbine

Publications (2)

Publication Number Publication Date
JPS5781131A true JPS5781131A (en) 1982-05-21
JPS624540B2 JPS624540B2 (en) 1987-01-30

Family

ID=15638113

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15691380A Granted JPS5781131A (en) 1980-11-10 1980-11-10 Starting time fuel control circuit for gas turbine

Country Status (1)

Country Link
JP (1) JPS5781131A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6196141A (en) * 1984-10-15 1986-05-14 Mitsubishi Electric Corp Control system of fuel controller
JP2016521396A (en) * 2013-03-15 2016-07-21 ユナイテッド テクノロジーズ コーポレイションUnited Technologies Corporation A small aerothermal model based control system estimator initiation algorithm

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6196141A (en) * 1984-10-15 1986-05-14 Mitsubishi Electric Corp Control system of fuel controller
JP2016521396A (en) * 2013-03-15 2016-07-21 ユナイテッド テクノロジーズ コーポレイションUnited Technologies Corporation A small aerothermal model based control system estimator initiation algorithm
US10087846B2 (en) 2013-03-15 2018-10-02 United Technologies Corporation Compact aero-thermo model stabilization with compressible flow function transform
US10107203B2 (en) 2013-03-15 2018-10-23 United Technologies Corporation Compact aero-thermo model based engine power control
US10107204B2 (en) 2013-03-15 2018-10-23 United Technologies Corporation Compact aero-thermo model base point linear system based state estimator
US10145307B2 (en) 2013-03-15 2018-12-04 United Technologies Corporation Compact aero-thermo model based control system
US10161313B2 (en) 2013-03-15 2018-12-25 United Technologies Corporation Compact aero-thermo model based engine material temperature control
US10190503B2 (en) 2013-03-15 2019-01-29 United Technologies Corporation Compact aero-thermo model based tip clearance management
US10196985B2 (en) 2013-03-15 2019-02-05 United Technologies Corporation Compact aero-thermo model based degraded mode control
US10400677B2 (en) 2013-03-15 2019-09-03 United Technologies Corporation Compact aero-thermo model stabilization with compressible flow function transform
US10480416B2 (en) 2013-03-15 2019-11-19 United Technologies Corporation Compact aero-thermo model based control system estimator starting algorithm
US10539078B2 (en) 2013-03-15 2020-01-21 United Technologies Corporation Compact aero-thermo model real time linearization based state estimator
US10753284B2 (en) 2013-03-15 2020-08-25 Raytheon Technologies Corporation Compact aero-thermo model base point linear system based state estimator
US10767563B2 (en) 2013-03-15 2020-09-08 Raytheon Technologies Corporation Compact aero-thermo model based control system
US10774749B2 (en) 2013-03-15 2020-09-15 Raytheon Technologies Corporation Compact aero-thermo model based engine power control
US10844793B2 (en) 2013-03-15 2020-11-24 Raytheon Technologies Corporation Compact aero-thermo model based engine material temperature control
US11078849B2 (en) 2013-03-15 2021-08-03 Raytheon Technologies Corporation Compact aero-thermo model based engine power control

Also Published As

Publication number Publication date
JPS624540B2 (en) 1987-01-30

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