BR112014028184A2 - processo de monitoramento de uma degradação de um dispositivo integrado de uma aeronave - Google Patents

processo de monitoramento de uma degradação de um dispositivo integrado de uma aeronave

Info

Publication number
BR112014028184A2
BR112014028184A2 BR112014028184A BR112014028184A BR112014028184A2 BR 112014028184 A2 BR112014028184 A2 BR 112014028184A2 BR 112014028184 A BR112014028184 A BR 112014028184A BR 112014028184 A BR112014028184 A BR 112014028184A BR 112014028184 A2 BR112014028184 A2 BR 112014028184A2
Authority
BR
Brazil
Prior art keywords
integrated device
aircraft
degradation
monitoring
decision threshold
Prior art date
Application number
BR112014028184A
Other languages
English (en)
Other versions
BR112014028184B1 (pt
BR112014028184B8 (pt
Inventor
Grallmaes Edith
André Masse Jean-Rémi
Hmad Ouadi
Jean Emile Beauseroy Pierre
Boulet Xavier
Original Assignee
Snecma
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 filed Critical Snecma
Publication of BR112014028184A2 publication Critical patent/BR112014028184A2/pt
Publication of BR112014028184B1 publication Critical patent/BR112014028184B1/pt
Publication of BR112014028184B8 publication Critical patent/BR112014028184B8/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00Aircraft indicators or protectors not otherwise provided for
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B23/00Testing or monitoring of control systems or parts thereof
    • G05B23/02Electric testing or monitoring
    • G05B23/0205Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
    • G05B23/0218Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterised by the fault detection method dealing with either existing or incipient faults
    • G05B23/0224Process history based detection method, e.g. whereby history implies the availability of large amounts of data
    • G05B23/0227Qualitative history assessment, whereby the type of data acted upon, e.g. waveforms, images or patterns, is not relevant, e.g. rule based assessment; if-then decisions
    • G05B23/0235Qualitative history assessment, whereby the type of data acted upon, e.g. waveforms, images or patterns, is not relevant, e.g. rule based assessment; if-then decisions based on a comparison with predetermined threshold or range, e.g. "classical methods", carried out during normal operation; threshold adaptation or choice; when or how to compare with the threshold
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00Aircraft indicators or protectors not otherwise provided for
    • B64D2045/0085Devices for aircraft health monitoring, e.g. monitoring flutter or vibration
    • GPHYSICS
    • G07CHECKING-DEVICES
    • G07CTIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
    • G07C5/00Registering or indicating the working of vehicles
    • G07C5/08Registering or indicating performance data other than driving, working, idle, or waiting time, with or without registering driving, working, idle or waiting time
    • G07C5/0808Diagnosing performance data

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Alarm Systems (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Testing And Monitoring For Control Systems (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
  • Emergency Alarm Devices (AREA)

Abstract

1 / 1 resumo “processo de monitoramento de uma degradaã‡ãƒo de um dispositivo integrado de uma aeronave” um processo de monitoramento de uma degradaã§ã£o de um dispositivo integrado de uma aeronave compreendendo uma etapa de comparaã§ã£o de uma marcaã§ã£o de anormalidade obtida para um voo dado da aeronave a um limiar de decisã£o (s) e uma etapa de emissã£o de um alarme em caso de ultrapassagem do limiar de decisã£o (s), o limiar de decisã£o (s) sendo determinado automaticamente para uma probabilidade de alarme dada pa, correspondente ã  probabilidade que um alarme seja emitido no curso do processo de monitoramento enquanto que o dispositivo integrado ã© nã£o danificado, por meio das etapas seguintes: uma etapa de cã¡lculo de uma pluralidade de marcaã§ãµes de anormalidade para uma pluralidade de voos da aeronave sem degradaã§ã£o de maneira a obter uma distribuiã§ã£o da densidade de probabilidade da marcaã§ã£o de anormalidade, a distribuiã§ã£o sendo prã³pria para a natureza fã­sica do dispositivo integrado; uma etapa de ajuste da distribuiã§ã£o por um estimador nã£o paramã©trico da densidade de probabilidade de maneira a obter uma funã§ã£o de distribuiã§ã£o ajustada contã­nua; uma etapa de cã¡lculo de uma funã§ã£o de repartiã§ã£o ajustada contã­nua a partir da funã§ã£o de distribuiã§ã£o ajustada contã­nua; e uma etapa de leitura do antecedente da funã§ã£o de repartiã§ã£o ajustada contã­nua para o valor 1-pa, o antecedente correspondendo ao limiar de decisã£o (s).
BR112014028184A 2012-05-16 2013-05-15 Processo de monitoramento de uma degradação de um dispositivo integrado de uma aeronave BR112014028184B8 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1254506 2012-05-16
FR1254506A FR2990725B1 (fr) 2012-05-16 2012-05-16 Procede de surveillance d'une degradation d'un dispositif embarque d'un aeronef avec determination automatique d'un seuil de decision
PCT/FR2013/051059 WO2013171427A1 (fr) 2012-05-16 2013-05-15 Procédé de surveillance d'une dégradation d'un dispositif embarque d'un aéronef avec détermination automatique d'un seuil de décision

Publications (3)

Publication Number Publication Date
BR112014028184A2 true BR112014028184A2 (pt) 2017-06-27
BR112014028184B1 BR112014028184B1 (pt) 2021-02-09
BR112014028184B8 BR112014028184B8 (pt) 2022-02-22

Family

ID=48577130

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112014028184A BR112014028184B8 (pt) 2012-05-16 2013-05-15 Processo de monitoramento de uma degradação de um dispositivo integrado de uma aeronave

Country Status (8)

Country Link
US (1) US9346558B2 (pt)
EP (1) EP2850499B1 (pt)
CN (1) CN104303122B (pt)
BR (1) BR112014028184B8 (pt)
CA (1) CA2873689C (pt)
FR (1) FR2990725B1 (pt)
RU (1) RU2629479C2 (pt)
WO (1) WO2013171427A1 (pt)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3022997B1 (fr) * 2014-06-25 2016-06-10 Snecma Procede de surveillance d'une degradation d'un dispositif embarque d'un aeronef incluant la determination d'un seuil de comptage
FR3027417B1 (fr) * 2014-10-20 2016-11-25 Airbus Operations Sas Procede et systeme de generation de rapports d'alertes dans un aeronef
FR3028067B1 (fr) * 2014-11-05 2016-12-30 Snecma Outil de validation d'un systeme de surveillance d'un moteur d'aeronef
JP6649182B2 (ja) * 2016-05-30 2020-02-19 日本電信電話株式会社 確率密度関数推定装置、連続値予測装置、方法、及びプログラム
US10373474B2 (en) * 2017-03-09 2019-08-06 Keithley Instruments, Llc Auto setting of alarm limits
RU2665142C1 (ru) * 2017-08-22 2018-08-28 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Способ полетной диагностики узлов турбореактивного двухконтурного двигателя со смешением потоков
RU2680945C1 (ru) * 2018-04-17 2019-02-28 Закрытое акционерное общество "Туполев-Проект" Интеллектуальная система поиска неисправности на самолёте
RU2729110C1 (ru) * 2019-07-01 2020-08-04 Акционерное общество "Туполев-Проект" Интеллектуальная система технического обслуживания для самолета
CN112100037B (zh) * 2020-09-25 2023-07-25 北京奇艺世纪科技有限公司 告警级别识别方法、装置、电子设备及存储介质

Family Cites Families (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3186866B2 (ja) * 1992-11-20 2001-07-11 株式会社東芝 構造部材の劣化・損傷予測方法およびその予測装置
JPH1055497A (ja) * 1996-08-09 1998-02-24 Yazaki Corp 故障予知方法、及びこれを用いた制御ユニット並びに負荷制御システム
GB9704843D0 (en) * 1997-03-08 1997-04-23 Murphy Graham F Apparatus
GB9910938D0 (en) * 1999-05-11 1999-07-14 Murphy Graham F Diagnostic apparatus
US6532421B2 (en) * 2000-04-07 2003-03-11 Toho Gas Co., Ltd Method for estimating a life of apparatus under narrow-band random stress variation
JP3850311B2 (ja) * 2002-02-21 2006-11-29 オムロン株式会社 残存寿命予測報知方法および電子機器
US6892163B1 (en) * 2002-03-08 2005-05-10 Intellectual Assets Llc Surveillance system and method having an adaptive sequential probability fault detection test
US7451021B2 (en) * 2003-05-06 2008-11-11 Edward Wilson Model-based fault detection and isolation for intermittently active faults with application to motion-based thruster fault detection and isolation for spacecraft
US7440811B2 (en) * 2004-09-28 2008-10-21 Siemens Aktiengesellschaft Dynamic-state waiting time analysis method for complex discrete manufacturing
US7243042B2 (en) * 2004-11-30 2007-07-10 Siemens Power Generation, Inc. Engine component life monitoring system and method for determining remaining useful component life
US7280941B2 (en) * 2004-12-29 2007-10-09 General Electric Company Method and apparatus for in-situ detection and isolation of aircraft engine faults
RU2308069C2 (ru) * 2005-06-30 2007-10-10 Валентин Афанасьевич Сухолитко Способ интегрированной логистической поддержки эксплуатационного контроля летательных аппаратов
US7933754B2 (en) * 2006-12-07 2011-04-26 General Electric Company System and method for damage propagation estimation
US7930128B2 (en) * 2007-04-16 2011-04-19 Acellent Technologies, Inc. Robust damage detection
US8437904B2 (en) * 2007-06-12 2013-05-07 The Boeing Company Systems and methods for health monitoring of complex systems
US20090030752A1 (en) * 2007-07-27 2009-01-29 General Electric Company Fleet anomaly detection method
US20100030519A1 (en) * 2008-07-31 2010-02-04 Collier Jarrell D System for Real-Time Object Damage Detection and Evaluation
GB0818544D0 (en) * 2008-10-09 2008-11-19 Oxford Biosignals Ltd Improvements in or relating to multi-parameter monitoring
US8442702B2 (en) * 2008-10-22 2013-05-14 Airbus Operations Gmbh Fault diagnosis device and method for optimizing maintenance measures in technical systems
JP5025676B2 (ja) * 2009-03-25 2012-09-12 株式会社東芝 監視装置および監視方法
CN101963937B (zh) * 2010-09-29 2016-08-10 南京航空航天大学 飞控计算机系统剩余寿命预测方法
RU2431175C1 (ru) * 2010-10-18 2011-10-10 Федеральное государственное унитарное предприятие "Летно-исследовательский институт имени М.М. Громова" Система интегрированного контроля работы бортового оборудования летательного аппарата
CN102288412B (zh) * 2011-05-04 2013-05-01 哈尔滨工业大学 基于损伤基线的航空发动机硬件损伤分析与寿命预测方法
GB2491564A (en) * 2011-05-24 2012-12-12 Isis Innovation Method of system monitoring
FR2989500B1 (fr) * 2012-04-12 2014-05-23 Airbus Operations Sas Procede, dispositifs et programme d'ordinateur d'aide a l'analyse de la tolerance aux pannes d'un systeme d'un aeronef, utilisant des graphes d'evenements redoutes
FR2989499B1 (fr) * 2012-04-12 2014-05-16 Airbus Operations Sas Procede, dispositifs et programme d'ordinateur d'aide au diagnostic preventif d'un systeme d'un aeronef, utilisant des graphes d'evenements redoutes
FR2991485B1 (fr) * 2012-06-05 2015-08-14 Airbus Operations Sas Procede et dispositif d'estimation automatique d'une degradation en consommation et en trainee d'un aeronef.
GB201215649D0 (en) * 2012-09-03 2012-10-17 Isis Innovation System monitoring
US9014918B2 (en) * 2012-10-12 2015-04-21 Cummins Inc. Health monitoring systems and techniques for vehicle systems
US9251502B2 (en) * 2012-11-01 2016-02-02 Ge Aviation Systems Llc Maintenance system for aircraft fleet and method for planning maintenance
US20140257716A1 (en) * 2013-03-11 2014-09-11 Board Of Trustees Of Michigan State University Methods for estimating remaining life of a monitored structure

Also Published As

Publication number Publication date
EP2850499B1 (fr) 2016-11-23
BR112014028184B1 (pt) 2021-02-09
FR2990725B1 (fr) 2014-05-02
CA2873689A1 (fr) 2013-11-21
US20150134198A1 (en) 2015-05-14
US9346558B2 (en) 2016-05-24
BR112014028184B8 (pt) 2022-02-22
FR2990725A1 (fr) 2013-11-22
CN104303122A (zh) 2015-01-21
CA2873689C (fr) 2020-08-18
RU2629479C2 (ru) 2017-08-29
EP2850499A1 (fr) 2015-03-25
CN104303122B (zh) 2016-09-21
RU2014148343A (ru) 2016-07-10
WO2013171427A1 (fr) 2013-11-21

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B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 15/05/2013, OBSERVADAS AS CONDICOES LEGAIS.

B16C Correction of notification of the grant [chapter 16.3 patent gazette]

Free format text: REFERENTE AO DESPACHO 16.1 PUBLICADO NA RPI 2614 DE 09.02.2021, QUANTO AO TITULO E AOS NOMES DOS INVENTORES