FR2407463A1 - Poste de controle pour moteurs a turbine a gaz - Google Patents

Poste de controle pour moteurs a turbine a gaz

Info

Publication number
FR2407463A1
FR2407463A1 FR7822090A FR7822090A FR2407463A1 FR 2407463 A1 FR2407463 A1 FR 2407463A1 FR 7822090 A FR7822090 A FR 7822090A FR 7822090 A FR7822090 A FR 7822090A FR 2407463 A1 FR2407463 A1 FR 2407463A1
Authority
FR
France
Prior art keywords
gas turbine
turbine engines
control station
variable
turboreactors
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
FR7822090A
Other languages
English (en)
Other versions
FR2407463B1 (fr
Inventor
Ivan Ray Anderson
Frederick Clifford Mckinley
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2407463A1 publication Critical patent/FR2407463A1/fr
Application granted granted Critical
Publication of FR2407463B1 publication Critical patent/FR2407463B1/fr
Granted legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M15/00—Testing of engines
    • G01M15/04—Testing internal-combustion engines
    • G01M15/05—Testing internal-combustion engines by combined monitoring of two or more different engine parameters

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Indication And Recording Devices For Special Purposes And Tariff Metering Devices (AREA)
  • Testing Of Engines (AREA)
  • Control Of Turbines (AREA)

Abstract

POSTE DE CONTROLE PORTATIF POUR MOTEURS A TURBINE A GAZ. IL COMPREND UN PANNEAU DE COMMANDE QUI COMPORTE EN PARTICULIER DES COMMUTATEURS ET DES AFFICHEURS 102, 104, 106 QUI PERMETTENT D'AFFICHER SELECTIVEMENT LES VITESSES DE DIVERS ORGANES DU MOTEUR, LES TEMPERATURES FOURNIES PAR DIVERS CAPTEURS, ET LA POSITION DES AUBES DIRECTRICES A CALAGE VARIABLE. APPLICATION AU REGLAGE DES TURBOREACTEURS.
FR7822090A 1977-10-31 1978-07-26 Poste de controle pour moteurs a turbine a gaz Granted FR2407463A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/846,957 US4158884A (en) 1977-10-31 1977-10-31 Gas turbine engine trim test set apparatus

Publications (2)

Publication Number Publication Date
FR2407463A1 true FR2407463A1 (fr) 1979-05-25
FR2407463B1 FR2407463B1 (fr) 1983-09-30

Family

ID=25299416

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7822090A Granted FR2407463A1 (fr) 1977-10-31 1978-07-26 Poste de controle pour moteurs a turbine a gaz

Country Status (8)

Country Link
US (1) US4158884A (fr)
JP (1) JPS5467814A (fr)
CA (1) CA1120155A (fr)
DE (1) DE2833147A1 (fr)
FR (1) FR2407463A1 (fr)
GB (1) GB1600585A (fr)
IT (1) IT1097896B (fr)
SE (1) SE439992B (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2476850C1 (ru) * 2011-11-30 2013-02-27 Федеральное Государственное Унитарное Предприятие "Научно-Производственное Объединение "Техномаш" Способ контроля и диагностирования ракетного двигателя
RU2758781C1 (ru) * 2020-07-24 2021-11-01 Акционерное общество "НПО Энергомаш имени академика В.П. Глушко" Способ контроля технического состояния жидкостного ракетного двигателя на переходных режимах стендового испытания

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2841220C2 (de) * 1978-09-22 1983-04-28 Robert Bosch Gmbh, 7000 Stuttgart Verfahren zum Prüfen der Funktion eines Regelsystems
US4255790A (en) * 1978-09-25 1981-03-10 Hondeghem Luc M Programmable pulse generating system
US4313167A (en) * 1979-07-27 1982-01-26 General Electric Company Thrust control system for a gas turbine engine
US4274144A (en) * 1979-12-31 1981-06-16 Acf Industries, Incorporated Fuel control system development apparatus
DE3309486A1 (de) * 1983-03-16 1984-10-25 Kraftwerk Union AG, 4330 Mülheim Ueberwachungssystem an elektrohydraulischen kompaktantrieben fuer ventile von turbomaschinen, insbesondere turbinen
US5168447A (en) * 1983-12-27 1992-12-01 The Boeing Company Engine trim control unit
US4641517A (en) * 1984-12-20 1987-02-10 United Technologies Corporation Control system actuator position synthesis for failure detection
US4651563A (en) * 1985-10-16 1987-03-24 Sperry Corporation Jet engine testing apparatus
US4821217A (en) * 1987-01-12 1989-04-11 The Boeing Company Programmable jet engine test station
US4918629A (en) * 1988-04-07 1990-04-17 The Boeing Company Engine trim tachometer unit and calibration method
US5031398A (en) * 1989-11-30 1991-07-16 Sundstrand Corporation Direct controlled control valve with an offset of a digital to analog converter
US5080496A (en) * 1990-06-25 1992-01-14 General Electric Company Method and apparatus for compensated temperature prediction
US5689066A (en) * 1995-08-15 1997-11-18 Stevenson; Dennis B. Method and apparatus for analyzing gas turbine pneumatic fuel system
DE69831593T2 (de) * 1997-10-20 2006-04-27 United Technologies Corp., Windsor Locks Verfahren zum geschwindigkeitsadaptiven Testen einer Steuerung
CN1307424C (zh) * 2002-01-30 2007-03-28 株式会社普利司通 测量值输出装置、测量值监视装置、电流值输出装置以及电流监视装置
FR2841352B1 (fr) * 2002-06-19 2004-08-06 Eurocopter France Dispositif et systeme de maintenance d'un systeme complexe, en particulier d'un aeronef
US8661881B2 (en) * 2010-12-23 2014-03-04 General Electric Company Hub unit for a high temperature electronic monitoring system
US8600642B2 (en) * 2010-12-23 2013-12-03 General Electric Company Hub unit for a high temperature electronic monitoring system
JP2013246534A (ja) * 2012-05-24 2013-12-09 Mitsubishi Electric Corp Ａｉモジュールの調整試験装置
CN104977169B (zh) * 2015-04-15 2017-12-22 北京宇航系统工程研究所 一种火箭发动机冷摆数字试验方法
RU2750874C1 (ru) * 2020-07-24 2021-07-05 Акционерное общество "НПО Энергомаш имени академика В.П. Глушко" Способ контроля характеристик агрегатов жидкостного ракетного двигателя при огневом испытании
RU2755027C9 (ru) * 2020-12-08 2021-10-08 Акционерное общество "ОДК-Климов" Мобильный стенд для тестирования электронной системы управления и способ разработки и испытания системы автоматического управления

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3287965A (en) * 1963-09-27 1966-11-29 United Aircraft Corp Engine performance indicator
US3485093A (en) * 1965-09-16 1969-12-23 Universal Testproducts Inc Engine performance analyzer
FR2152217A6 (fr) * 1970-11-16 1973-04-20 Howell Instruments
US3813647A (en) * 1973-02-28 1974-05-28 Northrop Corp Apparatus and method for performing on line-monitoring and fault-isolation

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3750465A (en) * 1971-09-09 1973-08-07 Howell Instruments Engine performance indicator

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3287965A (en) * 1963-09-27 1966-11-29 United Aircraft Corp Engine performance indicator
US3485093A (en) * 1965-09-16 1969-12-23 Universal Testproducts Inc Engine performance analyzer
FR2152217A6 (fr) * 1970-11-16 1973-04-20 Howell Instruments
US3813647A (en) * 1973-02-28 1974-05-28 Northrop Corp Apparatus and method for performing on line-monitoring and fault-isolation

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
EXBK/76 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2476850C1 (ru) * 2011-11-30 2013-02-27 Федеральное Государственное Унитарное Предприятие "Научно-Производственное Объединение "Техномаш" Способ контроля и диагностирования ракетного двигателя
RU2758781C1 (ru) * 2020-07-24 2021-11-01 Акционерное общество "НПО Энергомаш имени академика В.П. Глушко" Способ контроля технического состояния жидкостного ракетного двигателя на переходных режимах стендового испытания

Also Published As

Publication number Publication date
DE2833147A1 (de) 1979-05-03
IT1097896B (it) 1985-08-31
CA1120155A (fr) 1982-03-16
FR2407463B1 (fr) 1983-09-30
US4158884A (en) 1979-06-19
DE2833147C2 (fr) 1989-10-12
SE439992B (sv) 1985-07-08
JPH0240970B2 (fr) 1990-09-14
SE7806392L (sv) 1979-05-01
JPS5467814A (en) 1979-05-31
GB1600585A (en) 1981-10-21
IT7826244A0 (it) 1978-07-28

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Legal Events

Date Code Title Description
ST Notification of lapse