CA2889122C - Procede de differenciation de pannes de commande dans un systeme de commande d'un actionneur, notamment de stator de moteur a turbine a gaz - Google Patents

Procede de differenciation de pannes de commande dans un systeme de commande d'un actionneur, notamment de stator de moteur a turbine a gaz Download PDF

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Publication number
CA2889122C
CA2889122C CA2889122A CA2889122A CA2889122C CA 2889122 C CA2889122 C CA 2889122C CA 2889122 A CA2889122 A CA 2889122A CA 2889122 A CA2889122 A CA 2889122A CA 2889122 C CA2889122 C CA 2889122C
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CA
Canada
Prior art keywords
control
actuator
failure
electrical
speed
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.)
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Application number
CA2889122A
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English (en)
French (fr)
Other versions
CA2889122A1 (fr
Inventor
Severine Chevalier
Jose Rodrigues
Alain Tiepel
Original Assignee
SNECMA SAS
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Publication of CA2889122A1 publication Critical patent/CA2889122A1/fr
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Publication of CA2889122C publication Critical patent/CA2889122C/fr
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/003—Arrangements for testing or measuring
    • 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
    • F02C9/16—Control of working fluid flow
    • F02C9/20—Control of working fluid flow by throttling; by adjusting vanes
    • 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
    • F05D2260/00—Function
    • F05D2260/80—Diagnostics
    • 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
    • F05D2260/00—Function
    • F05D2260/84—Redundancy

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Control Of Turbines (AREA)
  • Safety Devices In Control Systems (AREA)
  • Control Of Electric Motors In General (AREA)
  • Supercharger (AREA)
CA2889122A 2012-09-26 2013-09-24 Procede de differenciation de pannes de commande dans un systeme de commande d'un actionneur, notamment de stator de moteur a turbine a gaz Active CA2889122C (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1259038A FR2995947B1 (fr) 2012-09-26 2012-09-26 Procede de differenciation de pannes de commande dans un systeme de commande d'un actionneur, notamment de stator de moteur a turbine a gaz
FR1259038 2012-09-26
PCT/FR2013/052238 WO2014049260A1 (fr) 2012-09-26 2013-09-24 Procede de differenciation de pannes de commande dans un systeme de commande d'un actionneur, notamment de stator de moteur a turbine a gaz

Publications (2)

Publication Number Publication Date
CA2889122A1 CA2889122A1 (fr) 2014-04-03
CA2889122C true CA2889122C (fr) 2020-02-25

Family

ID=47902054

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2889122A Active CA2889122C (fr) 2012-09-26 2013-09-24 Procede de differenciation de pannes de commande dans un systeme de commande d'un actionneur, notamment de stator de moteur a turbine a gaz

Country Status (7)

Country Link
US (1) US9976439B2 (https=)
EP (1) EP2900981B1 (https=)
CN (1) CN104736818B (https=)
CA (1) CA2889122C (https=)
FR (1) FR2995947B1 (https=)
IN (1) IN2015DN03148A (https=)
WO (1) WO2014049260A1 (https=)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10190440B2 (en) * 2015-06-10 2019-01-29 Rolls-Royce North American Technologies, Inc. Emergency shut-down detection system for a gas turbine
US20180023414A1 (en) * 2016-07-25 2018-01-25 United Technologies Corporation Oil debris monitoring for failure detection isolation
US11440677B2 (en) * 2018-11-16 2022-09-13 Rolls-Royce Corporation Secured backup feature for an embedded system
FR3092170B1 (fr) * 2019-01-24 2022-08-19 Safran Helicopter Engines Procédé de surveillance de l’état de fonctionnement d’un système de positionnement d’organes à géométrie variable d’une turbomachine
FR3094807B1 (fr) * 2019-04-05 2021-03-12 Safran Aircraft Engines Dispositif de commande d'un moteur d'un aéronef comprenant deux voies de commande redondées
FR3094790B1 (fr) * 2019-04-05 2021-03-05 Safran Aircraft Engines Système de surveillance d’un système d’actionnement d’un élément d’une turbomachine
US11720067B2 (en) * 2020-03-30 2023-08-08 General Electric Company Method for handling a simultaneous failure of all channels of a multi-channel engine controller for a gas turbine engine

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3023782A (en) 1959-11-13 1962-03-06 Moog Servocontrols Inc Mechanical feedback flow control servo valve
DE19651882A1 (de) * 1996-12-13 1998-06-18 Asea Brown Boveri Verfahren zur Frequenzstützung beim Betrieb einer Kraftwerksanlage
US5938401A (en) * 1998-02-03 1999-08-17 United Technologies Corporation Automatic engine hydro-mechanical control unit preflight test
US6341238B1 (en) * 1998-10-01 2002-01-22 United Technologies Corporation Robust engine variable vane monitor logic
FR2870000B1 (fr) * 2004-05-05 2006-08-11 Hispano Suiza Sa Controle de la robustesse d'une modelisation d'un systeme physique
US7927067B2 (en) * 2007-05-01 2011-04-19 United Technologies Corporation System and method for controlling stator assemblies
CN101694182A (zh) * 2009-09-29 2010-04-14 上海中科清洁能源技术发展中心 中/小型燃气轮机在线故障诊断、预测、反馈控制方法及装置
FR2963948B1 (fr) * 2010-08-17 2014-04-25 Snecma Systeme de commande distribue pour turbomachine
US9726035B2 (en) * 2015-04-15 2017-08-08 Honeywell International Inc. Hard-stop position detection methods and systems

Also Published As

Publication number Publication date
CN104736818B (zh) 2016-09-21
US20150285092A1 (en) 2015-10-08
CA2889122A1 (fr) 2014-04-03
IN2015DN03148A (https=) 2015-10-02
CN104736818A (zh) 2015-06-24
FR2995947B1 (fr) 2018-03-16
WO2014049260A1 (fr) 2014-04-03
EP2900981A1 (fr) 2015-08-05
EP2900981B1 (fr) 2017-07-26
US9976439B2 (en) 2018-05-22
FR2995947A1 (fr) 2014-03-28

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