CN104736818B - 对控制致动器的系统中的控制故障进行区分的方法和系统 - Google Patents

对控制致动器的系统中的控制故障进行区分的方法和系统 Download PDF

Info

Publication number
CN104736818B
CN104736818B CN201380054774.6A CN201380054774A CN104736818B CN 104736818 B CN104736818 B CN 104736818B CN 201380054774 A CN201380054774 A CN 201380054774A CN 104736818 B CN104736818 B CN 104736818B
Authority
CN
China
Prior art keywords
actuator
fault
control
computer
electrical
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.)
Active
Application number
CN201380054774.6A
Other languages
English (en)
Chinese (zh)
Other versions
CN104736818A (zh
Inventor
塞威利娜·舍瓦莱尔
乔斯·罗德里格斯
阿兰·蒂佩尔
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Publication of CN104736818A publication Critical patent/CN104736818A/zh
Application granted granted Critical
Publication of CN104736818B publication Critical patent/CN104736818B/zh
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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)
CN201380054774.6A 2012-09-26 2013-09-24 对控制致动器的系统中的控制故障进行区分的方法和系统 Active CN104736818B (zh)

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
CN104736818A CN104736818A (zh) 2015-06-24
CN104736818B true CN104736818B (zh) 2016-09-21

Family

ID=47902054

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201380054774.6A Active CN104736818B (zh) 2012-09-26 2013-09-24 对控制致动器的系统中的控制故障进行区分的方法和系统

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
US20150285092A1 (en) 2015-10-08
CA2889122A1 (fr) 2014-04-03
IN2015DN03148A (https=) 2015-10-02
CN104736818A (zh) 2015-06-24
CA2889122C (fr) 2020-02-25
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

Similar Documents

Publication Publication Date Title
CN104736818B (zh) 对控制致动器的系统中的控制故障进行区分的方法和系统
US10431019B2 (en) Health monitoring of an actuator in a flying device
EP2837799B1 (en) Engine fuel control system
EP2954297B1 (en) Auto testing system for a gas turbine
US5233512A (en) Method and apparatus for actuator fault detection
EP2273168B1 (en) Valve failure detection
EP4035998B1 (en) System and method for detecting failure of a propeller feedback device
JP5391086B2 (ja) 飛行制御システム
CN106255814A (zh) 用于检测双发动机直升机的第一涡轮发动机的故障且用于运转第二涡轮发动机的方法，以及对应的设备
US10132189B2 (en) Variable vane control system
EP3161381B1 (en) Automatic combustion system characterization
WO2021054861A1 (ru) Способ управления реверсивным устройством газотурбинного двигателя
CN113167304B (zh) 用于控制气缸的方法
RU2631974C2 (ru) Способ управления газотурбинным двигателем с форсажной камерой сгорания и система для его осуществления
CN113167230B (zh) 检测风力涡轮机转子叶片调节故障
EP2458179B1 (en) Method of monitoring an electronic engine control (EEC) to detect fuel screen clogging
EP1753939B1 (en) Overspeed limiter for turboshaft engines
EP4528088A1 (en) Method and system for monitoring a bleed valve of a gas turbine engine
EP3045887B1 (en) Method for detecting a fault, fault detection system and gas turbine engine
CN108945517A (zh) 飞机缝翼倾斜探测装置及其定位方法
US20220082027A1 (en) Method for monitoring the operating state of a system for positioning variable-geometry members of a turbomachine
US9599018B2 (en) Method and device for safely operating a gas turbine plant
CN109642471A (zh) 涡轮控制装置预测
KR101374356B1 (ko) 항공기 공기흡입구의 왜곡 제어방법
RU2710944C1 (ru) Способ управления регулирующими органами гидротурбин (варианты)

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant