FR2999656B1 - Optimisation de la disponibilite d'un inverseur de poussee - Google Patents

Optimisation de la disponibilite d'un inverseur de poussee

Info

Publication number
FR2999656B1
FR2999656B1 FR1262148A FR1262148A FR2999656B1 FR 2999656 B1 FR2999656 B1 FR 2999656B1 FR 1262148 A FR1262148 A FR 1262148A FR 1262148 A FR1262148 A FR 1262148A FR 2999656 B1 FR2999656 B1 FR 2999656B1
Authority
FR
France
Prior art keywords
thrust reverser
equipment
optimizing
availability
malfunction
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
FR1262148A
Other languages
English (en)
Other versions
FR2999656A1 (fr
Inventor
Sebastien Chalaud
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 FR1262148A priority Critical patent/FR2999656B1/fr
Priority to RU2015129112A priority patent/RU2660719C2/ru
Priority to PCT/FR2013/052987 priority patent/WO2014096619A1/fr
Priority to US14/651,746 priority patent/US9464595B2/en
Priority to GB1510329.4A priority patent/GB2523688B/en
Publication of FR2999656A1 publication Critical patent/FR2999656A1/fr
Application granted granted Critical
Publication of FR2999656B1 publication Critical patent/FR2999656B1/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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • Safety Devices In Control Systems (AREA)
  • Train Traffic Observation, Control, And Security (AREA)
  • Operation Control Of Excavators (AREA)
  • Elevator Control (AREA)
  • Inverter Devices (AREA)
  • Fluid-Pressure Circuits (AREA)

Abstract

Procédé de commande d'un inverseur de poussée comportant une pluralité d'équipements dans lequel lorsque l'on détecte qu'un de ces équipements n'est pas activé à l'issu d'un délai d'activation prédéterminé, un message d'erreur relatif au dysfonctionnement de l'inverseur de poussée est généré et, malgré la génération de ce message d'erreur, on poursuit l'activation de l'équipement et si l'équipement est finalement activé avant un délai maximal prédéterminé de déploiement de l'inverseur de poussée, on poursuit le déploiement de cet inverseur de poussée et on retire le message d'erreur relatif au dysfonctionnement de l'inverseur de poussée.
FR1262148A 2012-12-17 2012-12-17 Optimisation de la disponibilite d'un inverseur de poussee Active FR2999656B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR1262148A FR2999656B1 (fr) 2012-12-17 2012-12-17 Optimisation de la disponibilite d'un inverseur de poussee
RU2015129112A RU2660719C2 (ru) 2012-12-17 2013-12-06 Оптимизация готовности к работе реверсора тяги
PCT/FR2013/052987 WO2014096619A1 (fr) 2012-12-17 2013-12-06 Optimisation de la disponibilite d'un inverseur de poussee
US14/651,746 US9464595B2 (en) 2012-12-17 2013-12-06 Optimising the availability of a thrust reverser
GB1510329.4A GB2523688B (en) 2012-12-17 2013-12-06 Optimising the availability of a thrust reverser

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1262148A FR2999656B1 (fr) 2012-12-17 2012-12-17 Optimisation de la disponibilite d'un inverseur de poussee

Publications (2)

Publication Number Publication Date
FR2999656A1 FR2999656A1 (fr) 2014-06-20
FR2999656B1 true FR2999656B1 (fr) 2017-11-17

Family

ID=47833275

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1262148A Active FR2999656B1 (fr) 2012-12-17 2012-12-17 Optimisation de la disponibilite d'un inverseur de poussee

Country Status (5)

Country Link
US (1) US9464595B2 (fr)
FR (1) FR2999656B1 (fr)
GB (1) GB2523688B (fr)
RU (1) RU2660719C2 (fr)
WO (1) WO2014096619A1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10443540B2 (en) * 2015-05-08 2019-10-15 United Technologies Corporation Thrust reversal for turbofan gas turbine engine
US10054079B2 (en) 2016-02-09 2018-08-21 Woodward, Inc. Thrust reverser actuating

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2706536B1 (fr) * 1993-06-16 1995-07-21 Snecma Vérin d'inverseur de poussée comportant un dispositif de verrouillage interne et un dispositif de détection de la panne du dispositif de verrouillage interne.
US6526744B2 (en) * 2001-04-30 2003-03-04 Honeywell International Inc. System and method for controlling the stowage of jet engine thrust reversers
US7251550B2 (en) * 2003-10-01 2007-07-31 Honeywell International Inc. Aircraft accessory monitor
FR2920201B1 (fr) * 2007-08-20 2013-08-23 Aircelle Sa Systeme de commande d'au moins un actionneur de capots d'un inverseur de poussee pour turboreacteur et procede de test du systeme
FR2922959B1 (fr) * 2007-10-31 2009-12-04 Airbus France Systeme de controle et procede de controle.
FR2930973B1 (fr) * 2008-05-06 2010-04-23 Airbus France Procede et dispositif de mise en oeuvre des inverseurs de poussee d'un aeronef
FR2943732B1 (fr) * 2009-03-25 2011-04-22 Snecma Procede de surveillance 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

Also Published As

Publication number Publication date
WO2014096619A1 (fr) 2014-06-26
US9464595B2 (en) 2016-10-11
RU2660719C2 (ru) 2018-07-09
GB2523688B (en) 2019-10-02
GB2523688A (en) 2015-09-02
FR2999656A1 (fr) 2014-06-20
GB201510329D0 (en) 2015-07-29
RU2015129112A (ru) 2017-01-23
US20150361920A1 (en) 2015-12-17

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