FR2943732B1 - Procede de surveillance d'un inverseur de poussee - Google Patents

Procede de surveillance d'un inverseur de poussee

Info

Publication number
FR2943732B1
FR2943732B1 FR0951916A FR0951916A FR2943732B1 FR 2943732 B1 FR2943732 B1 FR 2943732B1 FR 0951916 A FR0951916 A FR 0951916A FR 0951916 A FR0951916 A FR 0951916A FR 2943732 B1 FR2943732 B1 FR 2943732B1
Authority
FR
France
Prior art keywords
monitoring
thrust inverter
thrust
inverter
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
FR0951916A
Other languages
English (en)
Other versions
FR2943732A1 (fr
Inventor
Nicolas Alain Bader
Thomas Deguin
Xavier Regis Flandrois
Jean Remi Andre Masse
Mickael Yves Maurice Sauzedde
Jean Julien Camille Vonfelt
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
Priority to FR0951916A priority Critical patent/FR2943732B1/fr
Priority to US12/728,641 priority patent/US8275507B2/en
Publication of FR2943732A1 publication Critical patent/FR2943732A1/fr
Application granted granted Critical
Publication of FR2943732B1 publication Critical patent/FR2943732B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/76—Control or regulation of thrust reversers
    • 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
    • G05B23/00—Testing or monitoring of control systems or parts thereof
    • G05B23/02—Electric testing or monitoring
    • G05B23/0205—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
    • G05B23/0208—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterized by the configuration of the monitoring system
    • G05B23/021—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterized by the configuration of the monitoring system adopting a different treatment of each operating region or a different mode of the monitored system, e.g. transient modes; different operating configurations of monitored system
    • 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
    • G05B23/00—Testing or monitoring of control systems or parts thereof
    • G05B23/02—Electric testing or monitoring
    • G05B23/0205—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
    • G05B23/0259—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterized by the response to fault detection
    • G05B23/0283—Predictive maintenance, e.g. involving the monitoring of a system and, based on the monitoring results, taking decisions on the maintenance schedule of the monitored system; Estimating remaining useful life [RUL]
    • 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
FR0951916A 2009-03-25 2009-03-25 Procede de surveillance d'un inverseur de poussee Active FR2943732B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0951916A FR2943732B1 (fr) 2009-03-25 2009-03-25 Procede de surveillance d'un inverseur de poussee
US12/728,641 US8275507B2 (en) 2009-03-25 2010-03-22 Method of monitoring a thrust reverser

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0951916A FR2943732B1 (fr) 2009-03-25 2009-03-25 Procede de surveillance d'un inverseur de poussee

Publications (2)

Publication Number Publication Date
FR2943732A1 FR2943732A1 (fr) 2010-10-01
FR2943732B1 true FR2943732B1 (fr) 2011-04-22

Family

ID=41449598

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0951916A Active FR2943732B1 (fr) 2009-03-25 2009-03-25 Procede de surveillance d'un inverseur de poussee

Country Status (2)

Country Link
US (1) US8275507B2 (fr)
FR (1) FR2943732B1 (fr)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080114507A1 (en) * 2006-11-10 2008-05-15 Ruth Robert S System and method for situational control of mobile platform maintenance and operation
FR2922959B1 (fr) * 2007-10-31 2009-12-04 Airbus France Systeme de controle et procede de controle.
FR2999656B1 (fr) * 2012-12-17 2017-11-17 Snecma Optimisation de la disponibilite d'un inverseur de poussee
GB2510635B (en) * 2013-02-12 2017-11-01 Ge Aviat Systems Ltd Method for predicting faults in an aircraft thrust reverser system
GB2513133B (en) 2013-04-16 2015-07-08 Ge Aviat Systems Ltd Methods for predicting a speed brake system fault
FR3008741B1 (fr) 2013-07-17 2017-04-28 Aircelle Sa Systeme inverseur de poussee electrique pour nacelle de moteur d'aeronef et nacelle de moteur d'aeronef ainsi equipee
FR3016191B1 (fr) * 2014-01-08 2019-07-05 Safran Aircraft Engines Procede et programme d'ordinateur pour la surveillance d'un inverseur de poussee a actionneurs hydrauliques
US10443509B2 (en) * 2014-10-31 2019-10-15 General Electric Company System and method for turbomachinery vane prognostics and diagnostics
US10443540B2 (en) * 2015-05-08 2019-10-15 United Technologies Corporation Thrust reversal for turbofan gas turbine engine
US10125779B2 (en) 2016-12-06 2018-11-13 General Electric Company System and method for turbomachinery vane diagnostics
US10519964B2 (en) 2016-12-06 2019-12-31 General Electric Company System and method for turbomachinery rotor and blade prognostics and diagnostics
EP3404502B1 (fr) * 2017-05-17 2021-03-03 Caverion Oyj Maintenance basée sur l'état du dispositif
RU2719778C1 (ru) * 2019-09-05 2020-04-23 Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") Способ управления реверсивным устройством авиационного двигателя при торможении самолета
US20220206486A1 (en) * 2020-12-31 2022-06-30 Infosys Limited Method and system for predictive maintenance of a machinery asset
FR3130383A1 (fr) * 2021-12-10 2023-06-16 Safran Nacelles Procédé de diagnostic numérique d’un système d’actionneurs électromécaniques d’un aéronef en maintenance

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6408258B1 (en) * 1999-12-20 2002-06-18 Pratt & Whitney Canada Corp. Engine monitoring display for maintenance management
US7124059B2 (en) * 2000-10-17 2006-10-17 Accenture Global Services Gmbh Managing maintenance for an item of equipment
US7251550B2 (en) * 2003-10-01 2007-07-31 Honeywell International Inc. Aircraft accessory monitor

Also Published As

Publication number Publication date
US20100242434A1 (en) 2010-09-30
FR2943732A1 (fr) 2010-10-01
US8275507B2 (en) 2012-09-25

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