Nothing Special   »   [go: up one dir, main page]

FR2970358B1 - Pronostic de duree avant maintenance par fusion entre modelisation et simulation, pour equipements electroniques embarques dans un aeronef - Google Patents

Pronostic de duree avant maintenance par fusion entre modelisation et simulation, pour equipements electroniques embarques dans un aeronef Download PDF

Info

Publication number
FR2970358B1
FR2970358B1 FR1100030A FR1100030A FR2970358B1 FR 2970358 B1 FR2970358 B1 FR 2970358B1 FR 1100030 A FR1100030 A FR 1100030A FR 1100030 A FR1100030 A FR 1100030A FR 2970358 B1 FR2970358 B1 FR 2970358B1
Authority
FR
France
Prior art keywords
aircraft
modeling
simulation
prognostic
fusion
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
FR1100030A
Other languages
English (en)
Other versions
FR2970358A1 (fr
Inventor
Samir Ghelam
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.)
Airbus Helicopters SAS
Original Assignee
Airbus Helicopters SAS
Eurocopter France SA
Eurocopter SA
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 Airbus Helicopters SAS, Eurocopter France SA, Eurocopter SA filed Critical Airbus Helicopters SAS
Priority to FR1100030A priority Critical patent/FR2970358B1/fr
Priority to US13/343,031 priority patent/US8478479B2/en
Publication of FR2970358A1 publication Critical patent/FR2970358A1/fr
Application granted granted Critical
Publication of FR2970358B1 publication Critical patent/FR2970358B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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]
    • 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
    • G05B17/00—Systems involving the use of models or simulators of said systems
    • G05B17/02—Systems involving the use of models or simulators of said systems electric
    • 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
    • G05B23/0218—Electric 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
    • G05B23/0243—Electric 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 model based detection method, e.g. first-principles knowledge model
    • G05B23/0245—Electric 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 model based detection method, e.g. first-principles knowledge model based on a qualitative model, e.g. rule based; if-then decisions
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00—Error detection; Error correction; Monitoring
    • G06F11/008—Reliability or availability analysis
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00—Error detection; Error correction; Monitoring
    • G06F11/22—Detection or location of defective computer hardware by testing during standby operation or during idle time, e.g. start-up testing
    • G06F11/26—Functional testing
    • G06F11/27—Built-in tests
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00—Error detection; Error correction; Monitoring
    • G06F11/30—Monitoring
    • G06F11/3003—Monitoring arrangements specially adapted to the computing system or computing system component being monitored
    • G06F11/3013—Monitoring arrangements specially adapted to the computing system or computing system component being monitored where the computing system is an embedded system, i.e. a combination of hardware and software dedicated to perform a certain function in mobile devices, printers, automotive or aircraft systems
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00—Error detection; Error correction; Monitoring
    • G06F11/30—Monitoring
    • G06F11/3058—Monitoring arrangements for monitoring environmental properties or parameters of the computing system or of the computing system component, e.g. monitoring of power, currents, temperature, humidity, position, vibrations
    • G—PHYSICS
    • G07—CHECKING-DEVICES
    • G07C—TIME 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
    • G07C5/00—Registering or indicating the working of vehicles
    • G07C5/08—Registering or indicating performance data other than driving, working, idle, or waiting time, with or without registering driving, working, idle or waiting time
    • G07C5/0841—Registering performance data
    • G07C5/085—Registering performance data using electronic data carriers

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Quality & Reliability (AREA)
  • General Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Computing Systems (AREA)
  • Mathematical Physics (AREA)
  • Computer Hardware Design (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)

Abstract

L'invention concerne la maintenance prédictive d'équipements électroniques embarqués dans un aéronef (1). Pour produire un pronostic, on prévoit : une étape de modélisation (48) de l'équipement (3) avec un modèle d'endommagement (53) par une agression externe ; une étape de simulation (49) d'endommagement jusqu'à défaillance ; une étape d'apprentissage (64) ; une étape de classification (65) de valeurs calculées et normalisées ; et une étape de fusion (61) donnant le pronostic réel de durée de vie en unité de temps avant maintenance. L'invention s'applique notamment à un aéronef (1) à voilure tournante, par exemple un drone d'hélicoptère.
FR1100030A 2011-01-06 2011-01-06 Pronostic de duree avant maintenance par fusion entre modelisation et simulation, pour equipements electroniques embarques dans un aeronef Active FR2970358B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1100030A FR2970358B1 (fr) 2011-01-06 2011-01-06 Pronostic de duree avant maintenance par fusion entre modelisation et simulation, pour equipements electroniques embarques dans un aeronef
US13/343,031 US8478479B2 (en) 2011-01-06 2012-01-04 Predicting time to maintenance by fusion between modeling and simulation for electronic equipment on board an aircraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1100030A FR2970358B1 (fr) 2011-01-06 2011-01-06 Pronostic de duree avant maintenance par fusion entre modelisation et simulation, pour equipements electroniques embarques dans un aeronef
FR1100030 2011-01-06

Publications (2)

Publication Number Publication Date
FR2970358A1 FR2970358A1 (fr) 2012-07-13
FR2970358B1 true FR2970358B1 (fr) 2019-04-12

Family

ID=44119602

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1100030A Active FR2970358B1 (fr) 2011-01-06 2011-01-06 Pronostic de duree avant maintenance par fusion entre modelisation et simulation, pour equipements electroniques embarques dans un aeronef

Country Status (2)

Country Link
US (1) US8478479B2 (fr)
FR (1) FR2970358B1 (fr)

Families Citing this family (52)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130066924A1 (en) * 2008-12-23 2013-03-14 Honeywell International Inc. Method and apparatus for utilizing matlab functionality in java-enabled environment
US8744651B2 (en) * 2010-04-21 2014-06-03 Sikorsky Aircraft Corporation Method of determining a maneuver performed by an aircraft
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
US10023305B2 (en) * 2012-05-10 2018-07-17 Sikorsky Aircraft Corporation System and method of determining rotor loads and motion
US9274854B2 (en) * 2012-07-27 2016-03-01 International Business Machines Corporation Contamination based workload management
CN102886637B (zh) * 2012-10-24 2017-05-10 哈尔滨东安发动机（集团）有限公司 国外直升机减速器的翻修方法
US20140188405A1 (en) 2012-12-28 2014-07-03 International Business Machines Corporation Predicting a time of failure of a device
US10055537B2 (en) * 2013-03-14 2018-08-21 Honeywell International Inc. Simulation methods and systems for an aircraft
BR112015031914B1 (pt) * 2013-06-19 2021-02-17 Volvo Truck Corporation método para identificar falhas em um veículo
US9646114B2 (en) * 2013-07-10 2017-05-09 The Boeing Company Electrical power system stability
CN103699112B (zh) * 2013-11-29 2016-01-20 中国航空无线电电子研究所 基于io信号故障仿真的航电自检测验证设备及其验证方法
FR3014952B1 (fr) 2013-12-13 2016-01-22 Snecma Prevision d'operations de maintenance a appliquer sur un moteur
CN103699118B (zh) * 2013-12-18 2016-08-31 北京航天测控技术有限公司 一种航天器运行异常状态的分析方法及装置
EP3035140B1 (fr) * 2014-12-19 2018-09-12 Rolls-Royce Deutschland Ltd & Co KG Procédé et système de surveillance de l'état d'un équipement
US9796479B2 (en) 2015-02-13 2017-10-24 Bell Helicopter Textron Inc. Self-referencing sensors for aircraft monitoring
US11042128B2 (en) * 2015-03-18 2021-06-22 Accenture Global Services Limited Method and system for predicting equipment failure
WO2016200467A1 (fr) 2015-06-11 2016-12-15 Sikorsky Aircraft Corporation Procédé de prédiction de potentiel de corrosion, de surveillance d'une charge de contaminant et d'optimisation d'une maintenance contre la corrosion
US9568912B2 (en) * 2015-06-15 2017-02-14 Honeywell International Inc. Aircraft prognostic systems and methods for determining adaptive time between overhaul for line replaceable units
FR3042294B1 (fr) * 2015-10-12 2018-06-01 Airbus Operations Procede de prediction des temperatures supportees par un composant, un equipement ou une structure d'un vehicule
FR3046268B1 (fr) * 2015-12-23 2019-05-10 Safran Aircraft Engines Systeme d'exploitation de donnees de vol d'un aeronef
US9898875B2 (en) * 2016-07-06 2018-02-20 Honeywell International Inc. Maintenance systems and methods for ECS elements
ES2783623T3 (es) * 2016-07-18 2020-09-17 Airbus Operations Sl Método y dispositivo para la inspección del daño en el revestimiento de un avión después del impacto de un rayo
FR3057971B1 (fr) * 2016-10-25 2018-10-26 Safran Procede et systeme de surveillance de la sante d'helicopteres
JP6720101B2 (ja) * 2017-02-27 2020-07-08 三菱重工業株式会社 航空機管理装置及び方法並びにプログラム
US11193387B2 (en) 2017-07-11 2021-12-07 General Electric Company Performance and life optimizing control system for a turbine engine
US10902387B2 (en) * 2017-08-25 2021-01-26 The Boeing Company Aircraft digital event ledger
US11169045B2 (en) * 2017-12-19 2021-11-09 Knappco, LLC Methods and systems for determining residual life of a swivel
KR102364585B1 (ko) * 2018-01-26 2022-02-17 휴렛-팩커드 디벨롭먼트 컴퍼니, 엘.피. 메인터넌스 개입 예측
US10909781B2 (en) 2018-03-09 2021-02-02 Honeywell International Inc. System and method of using mechanical systems prognostic indicators for aircraft maintenance
FR3078791B1 (fr) * 2018-03-09 2020-02-28 Safran Helicopter Engines Outil de diagnostic calculateur
EP3598256B1 (fr) 2018-07-16 2023-11-29 ABB Schweiz AG Appareil permettant de prédire la durée de vie résiduelle d'un système électrique
US11061066B1 (en) * 2018-07-31 2021-07-13 Rockwell Collins, Inc. Predictive maintenance system for aviation power supplies
EP3611588A1 (fr) * 2018-08-14 2020-02-19 Siemens Aktiengesellschaft Dispositif et procédé de prévision d'une durée de vie d'une machine
US11016117B2 (en) 2018-08-31 2021-05-25 Honeywell International Inc. Air data probe replacement determination system
CN109143231B (zh) * 2018-10-29 2023-03-28 河海大学 基于循环对消的数字电视无源双基地雷达目标检测方法
MX2021008371A (es) * 2019-01-09 2021-10-26 Westrock Packaging Systems Llc Herramienta de mantenimiento predictivo basada en modelo digital.
US11335131B2 (en) 2019-11-19 2022-05-17 International Business Machines Corporation Unmanned aerial vehicle maintenance and utility plan
US11422153B2 (en) 2020-01-24 2022-08-23 Honeywell International Inc. Air data probe replacement determination system
US20220187819A1 (en) * 2020-12-10 2022-06-16 Hitachi, Ltd. Method for event-based failure prediction and remaining useful life estimation
CN112817295B (zh) * 2020-12-29 2023-01-13 中国航空工业集团公司西安飞机设计研究所 一种飞机管理系统的试验系统及方法
CN112905429B (zh) * 2021-02-20 2024-07-05 北京物芯科技有限责任公司 一种系统仿真的监控方法及装置
KR20230162044A (ko) 2021-03-26 2023-11-28 에이이에스 글로벌 홀딩스 피티이 리미티드 시스템 컴포넌트들의 잔여 수명 추정
CN112948163B (zh) * 2021-03-26 2023-09-19 中国航空无线电电子研究所 基于bp神经网络的评估设备对功能故障影响的方法
US20220382272A1 (en) * 2021-05-28 2022-12-01 Skygrid, Llc Predictive maintenance of an unmanned aerial vehicle
CN114580705B (zh) * 2022-01-12 2023-07-25 中国电子科技集团公司第十研究所 航电产品剩余寿命预测方法
US20230251283A1 (en) * 2022-02-07 2023-08-10 Rosemount Aerospace Inc. Dynamic multi-stage air data probe prognostics health monitoring system
FR3136066B1 (fr) * 2022-05-31 2024-06-07 Airbus Helicopters Procédé et système de gestion continue en vol d'un générateur de faisceaux embarqué
FR3142574A1 (fr) * 2022-11-24 2024-05-31 Safran Helicopter Engines Procédé apte à fournir une information à un opérateur pour la gestion d’au moins un vieillissement cumulatif
CN116027673B (zh) * 2023-03-29 2023-06-06 中国电子科技集团公司第二十九研究所 一种基于模糊神经网络的装备控制自主决策方法
CN118226835A (zh) * 2024-02-05 2024-06-21 北京蓝天航空科技股份有限公司 飞行汽车仿真实验的综合管理方法及装置
CN118278921B (zh) * 2024-05-31 2024-10-11 中国电子产品可靠性与环境试验研究所（（工业和信息化部电子第五研究所）（中国赛宝实验室）） 设备维修性能检测方法、装置、计算机设备和存储介质
CN118428741B (zh) * 2024-07-02 2024-09-06 合肥优晟电力科技有限公司 一种适应于特殊操作和应急操作的智能防误处理方法

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8915406D0 (en) 1989-07-05 1989-08-23 Bristow Helicopters Aircraft health and usage monitoring system
US5239468A (en) 1990-12-07 1993-08-24 United Technologies Corporation Automated helicopter maintenance monitoring
FR2676556B1 (fr) 1991-05-15 1993-07-23 Europ Gas Turbines Sa Systeme de surveillance predictive d'un processus.
US5719675A (en) 1992-06-16 1998-02-17 Honeywell Inc. Laser gyro life prediction
FR2778766B1 (fr) 1998-05-18 2001-09-07 Eurocopter France Procede et dispositif d'aide a la maintenance d'un aeronef, notamment d'un helicoptere
WO2002018879A1 (fr) 2000-08-25 2002-03-07 Battelle Memorial Institute Procede et appareil de prediction de la duree de vie restante d'un systeme operationnel
DE10048826B4 (de) 2000-09-29 2012-03-01 Robert Bosch Gmbh Verfahren und Vorrichtung zur Erfassung alterungsbedingter Veränderungen von technischen Systemen wie Elektromotoren
DE10153151A1 (de) 2001-10-27 2003-05-15 Airbus Gmbh Diagnosesystem sowie Diagnoseverfahren zur Unterstützung der Flugzeugwartung
FR2841352B1 (fr) 2002-06-19 2004-08-06 Eurocopter France Dispositif et systeme de maintenance d'un systeme complexe, en particulier d'un aeronef
US20040176887A1 (en) 2003-03-04 2004-09-09 Arinc Incorporated Aircraft condition analysis and management system
US7474989B1 (en) 2005-03-17 2009-01-06 Rockwell Collins, Inc. Method and apparatus for failure prediction of an electronic assembly using life consumption and environmental monitoring
KR101322434B1 (ko) 2005-07-11 2013-10-28 브룩스 오토메이션 인코퍼레이티드 지능형 상태 감시 및 결함 진단 시스템
FR2896875B1 (fr) 2006-01-30 2008-04-25 Eads Europ Aeronautic Defence Dispositif et procede de surveillance d'une grandeur environnementale en temps reel
US7912669B2 (en) * 2007-03-27 2011-03-22 Honeywell International Inc. Prognosis of faults in electronic circuits
US7684936B2 (en) * 2008-05-07 2010-03-23 Simmonds Precision Products, Inc. Method, apparatus and computer program product for determining a future time of a component
US8521443B2 (en) * 2008-10-16 2013-08-27 Oxfordian Method to extract parameters from in-situ monitored signals for prognostics

Also Published As

Publication number Publication date
FR2970358A1 (fr) 2012-07-13
US8478479B2 (en) 2013-07-02
US20120179326A1 (en) 2012-07-12

Similar Documents

Publication Publication Date Title
FR2970358B1 (fr) Pronostic de duree avant maintenance par fusion entre modelisation et simulation, pour equipements electroniques embarques dans un aeronef
ES2523701R1 (es) Sistema y procedimiento de determinación de los parámetros operacionales de una aeronave y mejora de la operación de la aeronave
WO2018005891A3 (fr) Système et procédés utilisant une modélisation à éléments finis d'œil 3d virtuelle prédictive en temps réel pour la simulation de biomécanique de structure oculaire
MX2016008890A (es) Sistema y metodo de evaluacion de estructura de aeronave no tripulada.
WO2013140401A3 (fr) Planification et surveillance de mission autonome
WO2011130474A3 (fr) Modélisation et simulation d'environnements d'alimentation
MX2016004679A (es) Elemento de cierre a prueba de manipulacion y estructura receptora.
EP2876519A3 (fr) Analyse de sécurité d'un système complexe à l'aide d'arbres de défaillances des composants
CL2014003641A1 (es) Una caja que comprende un alojamiento, una unidad de sellado que posee una disposicion de sellado que define una pluralidad de puertos de cables, incluyendo ademas la unidad de sellado una disposicion de accionamiento que incluye estructuras de presurizacion interna y externa en las que se situa la disposicion de sellado; y metodo.
WO2014107511A3 (fr) Système et procédé de développement, de déploiement et d'implémentation d'applications informatiques de système d'alimentation
WO2013177353A3 (fr) Appareil et procédés d'évaluation de systèmes associés à des têtes de puits
WO2014130703A3 (fr) Système de surveillance d'un bloc obturateur de puits et son procédé d'utilisation
GB2527009A (en) Simulation of production systems
GB201000878D0 (en) Sandwich panel
GB2546645A (en) Predicting temperature-cycling-induced downhole tool failure
FR2995422B1 (fr) Procede de modification d'un plan de vol d'un aeronef sur un ecran tactile
WO2015071632A3 (fr) Système de protection de pipeline intégré
WO2014078030A3 (fr) Procédé de gestion de notifications dans un dispositif de communication
GB201212616D0 (en) Performance of a system
FR2985069B1 (fr) Systeme de gestion des systemes d'un aeronef
JP2013196698A5 (fr)
WO2013095415A3 (fr) Système et procédé d'attribution de machines virtuelles sur la base d'informations physiques
BR112013000806A2 (pt) identificação precoce de um estado de anel de vórtice
SG10201807209VA (en) Method and system for designing aircraft
CN106483976A (zh) 用于无人机的飞行安全控制方法、系统及电子设备

Legal Events

Date Code Title Description
CD Change of name or company name

Owner name: AIRBUS HELICOPTERS, FR

Effective date: 20140602

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 8

PLFP Fee payment

Year of fee payment: 10

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13

PLFP Fee payment

Year of fee payment: 14