FR2374513A1 - Procede et appareil de detection et de correction de pannes pour commande de moteur a turbine a gaz - Google Patents

Procede et appareil de detection et de correction de pannes pour commande de moteur a turbine a gaz

Info

Publication number
FR2374513A1
FR2374513A1 FR7738477A FR7738477A FR2374513A1 FR 2374513 A1 FR2374513 A1 FR 2374513A1 FR 7738477 A FR7738477 A FR 7738477A FR 7738477 A FR7738477 A FR 7738477A FR 2374513 A1 FR2374513 A1 FR 2374513A1
Authority
FR
France
Prior art keywords
control
gas turbine
faults
correction
detection
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
FR7738477A
Other languages
English (en)
French (fr)
Other versions
FR2374513B1 (de
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 FR2374513A1 publication Critical patent/FR2374513A1/fr
Application granted granted Critical
Publication of FR2374513B1 publication Critical patent/FR2374513B1/fr
Granted legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/46—Emergency fuel control
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B9/00—Safety arrangements
    • G05B9/02—Safety arrangements electric
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/50—Control logic embodiments
    • F05D2270/54—Control logic embodiments by electronic means, e.g. electronic tubes, transistors or IC's within an electronic circuit
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/70—Type of control algorithm
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/70—Type of control algorithm
    • F05D2270/71—Type of control algorithm synthesized, i.e. parameter computed by a mathematical model

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Feedback Control In General (AREA)
  • Control Of Turbines (AREA)
  • Safety Devices In Control Systems (AREA)
FR7738477A 1976-12-20 1977-12-20 Procede et appareil de detection et de correction de pannes pour commande de moteur a turbine a gaz Granted FR2374513A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US75205076A 1976-12-20 1976-12-20

Publications (2)

Publication Number Publication Date
FR2374513A1 true FR2374513A1 (fr) 1978-07-13
FR2374513B1 FR2374513B1 (de) 1984-10-19

Family

ID=25024630

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7738477A Granted FR2374513A1 (fr) 1976-12-20 1977-12-20 Procede et appareil de detection et de correction de pannes pour commande de moteur a turbine a gaz

Country Status (7)

Country Link
JP (1) JPS5395410A (de)
BE (1) BE862071A (de)
CA (1) CA1188775A (de)
DE (1) DE2756681C2 (de)
FR (1) FR2374513A1 (de)
GB (1) GB1597129A (de)
IT (1) IT1088432B (de)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2424998A1 (fr) * 1978-05-01 1979-11-30 United Technologies Corp Dispositif de commande a parametre simule pour moteur du type turbine a gaz
FR2494007A1 (fr) * 1980-11-11 1982-05-14 Sulzer Ag Montage de regulation a grandeur reglee auxiliaire
FR2512565A1 (fr) * 1981-09-05 1983-03-11 Lucas Ind Plc Systeme de commande numerique de pleine autorite
EP0344389A1 (de) * 1987-06-01 1989-12-06 United Technologies Corporation Verfahren und Vorrichtung zur Steuerung eines Flugzeugs

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4228650A (en) * 1978-05-01 1980-10-21 United Technologies Corporation Simulated parameter control for gas turbine engine
JPS5894004A (ja) * 1981-11-30 1983-06-04 Hitachi Ltd プラント制御系調節器最適パラメ−タ探索装置
JPS6045733A (ja) * 1983-08-23 1985-03-12 Toyota Motor Corp 電子制御ガスタ−ビンエンジンの可動部制御装置
JPS6047824A (ja) * 1983-08-25 1985-03-15 Toyota Motor Corp 電子制御ガスタ−ビンエンジンの可動部制御方法
JPS6047825A (ja) * 1983-08-26 1985-03-15 Toyota Motor Corp 電子制御ガスタ−ビンエンジンの可動部制御方法
US4992946A (en) * 1988-06-20 1991-02-12 General Electric Company Data link for gas turbine engine control
DE19729101A1 (de) * 1997-07-08 1999-01-14 Bosch Gmbh Robert System zum Betreiben einer Brennkraftmaschine insbesondere eines Kraftfahrzeugs
US6568166B2 (en) 2000-12-22 2003-05-27 Pratt & Whitney Canada Corp. Back-up control apparatus for turbo machine
US6687596B2 (en) * 2001-08-31 2004-02-03 General Electric Company Diagnostic method and system for turbine engines
US7216071B2 (en) * 2002-04-23 2007-05-08 United Technologies Corporation Hybrid gas turbine engine state variable model
DE102007025447A1 (de) * 2006-10-09 2008-04-17 Siemens Ag Verfahren zur Steuerung und/oder Regelung eines industriellen Prozesses
US7630820B2 (en) * 2007-04-24 2009-12-08 Honeywell International Inc. Feedback control system and method that selectively utilizes observer estimates
DE102008041571B4 (de) 2008-08-26 2019-12-05 Robert Bosch Gmbh Verfahren und Vorrichtung zur Fehlerbehandlung beim Betrieb eines Verbrennungsmotors
CN111475889B (zh) * 2020-03-30 2022-12-06 西安交通大学 一种物理与数据驱动的航空发动机数字孪生建模方法
CN114508421B (zh) * 2021-12-14 2023-05-05 泸州懋威科技有限公司 一种微小型航空发动机控制系统及其运行方法

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2851855A (en) * 1953-03-27 1958-09-16 Curtiss Wright Corp Fuel control system for jet engines
US3851157A (en) * 1973-07-09 1974-11-26 United Aircraft Corp Self-correcting feedback control system

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1523275A (en) * 1974-08-20 1978-08-31 Cav Ltd Digital control system for a gas turbine engine

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2851855A (en) * 1953-03-27 1958-09-16 Curtiss Wright Corp Fuel control system for jet engines
US3851157A (en) * 1973-07-09 1974-11-26 United Aircraft Corp Self-correcting feedback control system
FR2325096A1 (fr) * 1973-07-09 1977-04-15 United Aircraft Corp Systeme de commande auto-corrigeant

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
EXBK/75 *

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2424998A1 (fr) * 1978-05-01 1979-11-30 United Technologies Corp Dispositif de commande a parametre simule pour moteur du type turbine a gaz
FR2494007A1 (fr) * 1980-11-11 1982-05-14 Sulzer Ag Montage de regulation a grandeur reglee auxiliaire
FR2512565A1 (fr) * 1981-09-05 1983-03-11 Lucas Ind Plc Systeme de commande numerique de pleine autorite
EP0344389A1 (de) * 1987-06-01 1989-12-06 United Technologies Corporation Verfahren und Vorrichtung zur Steuerung eines Flugzeugs

Also Published As

Publication number Publication date
FR2374513B1 (de) 1984-10-19
IT1088432B (it) 1985-06-10
GB1597129A (en) 1981-09-03
JPS5395410A (en) 1978-08-21
DE2756681A1 (de) 1978-06-22
CA1188775A (en) 1985-06-11
BE862071A (fr) 1978-04-14
DE2756681C2 (de) 1986-06-05

Similar Documents

Publication Publication Date Title
FR2374513A1 (fr) Procede et appareil de detection et de correction de pannes pour commande de moteur a turbine a gaz
FR2406728A1 (fr) Appareil de commande electronique de moteur
BE901402A (fr) Systeme de detection et d'avertissement de calage de rotation d'un compresseur.
FR2408820A1 (fr) Dispositif pour mesurer un debit d'air, notamment pour mesurer le debit d'air aspire par un moteur a combustion interne
FR2398895A1 (fr) Procede et appareil de commande automatique du point d'allumage d'un moteur a combustion interne
FR2390781A1 (fr) Perfectionnements aux systemes de commande d'appareils
US3406562A (en) On-line exhaust data analysis system
FR2548274B1 (fr) Appareil de detection d'anomalies d'un dispositif de detection de parametres de fonctionnement d'un moteur a combustion interne
FR2412848A1 (fr) Circuit d'essai et de diagnostic in situ et procede applicable a des circuits logiques integres fonctionnant en mode de courant
FR2357739A1 (fr) Regulateur de poussee pour un moteur a turbine a gaz
FR2435079A1 (fr) Circuit de compensation de l'erreur de phase residuelle pour un asservissement numerique
FR2449287A1 (fr) Circuit de detection de l'etat de fonctionnement de dispositifs resistifs
KR900006878B1 (ko) 전자배선 백업장치
GB1384931A (en) Method and apparatus for determining pressures in and the thrust of a jet engine
FR2398185A1 (fr) Commande de secours pour systeme de commande de moteur a turbine a gaz
FR2361550A1 (fr) Dispositif pour la mesure numerique de caracteristiques d'installations d'allumage de moteurs a combustion interne
FR2409504A1 (fr) Procede et dispositif de test de compression pour un moteur a combustion interne
FR2445897A1 (fr) Testeur de systeme de commande electrique pour moteur a combustion interne
JPS57127820A (en) Method of monitoring cyclically moving body
FR2418461A1 (fr) Appareil de mesure d'isolement acoustique
CA1119301A (en) Variometer
FR2401318A1 (fr) Dispositif d'arret et indicateur de premiere panne pour moteur a combustion interne
JPS53121429A (en) Duplex memory unit
ES462412A1 (es) Un metodo y un equipo para medicion, durante perforaciones de pozos, de condiones del interior de los mismos.
FR2373099A1 (fr) Appareil de commande synchrone dans un dispositif multi-circuits

Legal Events

Date Code Title Description
ST Notification of lapse