FR2989500B1 - 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 - Google Patents

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

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Publication number
FR2989500B1
FR2989500B1 FR1253384A FR1253384A FR2989500B1 FR 2989500 B1 FR2989500 B1 FR 2989500B1 FR 1253384 A FR1253384 A FR 1253384A FR 1253384 A FR1253384 A FR 1253384A FR 2989500 B1 FR2989500 B1 FR 2989500B1
Authority
FR
France
Prior art keywords
aiding
trouble
devices
computer program
aircraft system
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
FR1253384A
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English (en)
Other versions
FR2989500A1 (fr
Inventor
Vincent Cheriere
Jeremy Roger
Estrada Laia Vilalta
Ioana Geanta
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 Operations SAS
Original Assignee
Airbus Operations 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 Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1253384A priority Critical patent/FR2989500B1/fr
Priority to US13/860,952 priority patent/US9266626B2/en
Priority to CN201310277294.8A priority patent/CN103425817B/zh
Publication of FR2989500A1 publication Critical patent/FR2989500A1/fr
Application granted granted Critical
Publication of FR2989500B1 publication Critical patent/FR2989500B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/40—Maintaining or repairing aircraft
    • 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
    • G06F11/07—Responding to the occurrence of a fault, e.g. fault tolerance
    • G06F11/0703—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation
    • G06F11/0706—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation the processing taking place on a specific hardware platform or in a specific software environment
    • G06F11/0736—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation the processing taking place on a specific hardware platform or in a specific software environment in functional embedded systems, i.e. in a data processing system designed as a combination of hardware and software dedicated to performing a certain function
    • G06F11/0739—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation the processing taking place on a specific hardware platform or in a specific software environment in functional embedded systems, i.e. in a data processing system designed as a combination of hardware and software dedicated to performing a certain function in a data processing system embedded in automotive or aircraft systems
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00—Error detection; Error correction; Monitoring
    • G06F11/07—Responding to the occurrence of a fault, e.g. fault tolerance
    • G06F11/0703—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation
    • G06F11/079—Root cause analysis, i.e. error or fault diagnosis
    • 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
    • G05B23/0248—Causal models, e.g. fault tree; digraphs; qualitative physics

Landscapes

  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Quality & Reliability (AREA)
  • Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Health & Medical Sciences (AREA)
  • Biomedical Technology (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Testing And Monitoring For Control Systems (AREA)
FR1253384A 2012-04-12 2012-04-12 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 Active FR2989500B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1253384A FR2989500B1 (fr) 2012-04-12 2012-04-12 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
US13/860,952 US9266626B2 (en) 2012-04-12 2013-04-11 Method, devices and program for computer-aided analysis of the failure tolerance of an aircraft system, using critical event charts
CN201310277294.8A CN103425817B (zh) 2012-04-12 2013-04-12 用担忧状况图辅助分析飞行器系统故障容差的方法、设备

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1253384A FR2989500B1 (fr) 2012-04-12 2012-04-12 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

Publications (2)

Publication Number Publication Date
FR2989500A1 FR2989500A1 (fr) 2013-10-18
FR2989500B1 true FR2989500B1 (fr) 2014-05-23

Family

ID=46650651

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1253384A Active FR2989500B1 (fr) 2012-04-12 2012-04-12 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

Country Status (3)

Country Link
US (1) US9266626B2 (fr)
CN (1) CN103425817B (fr)
FR (1) FR2989500B1 (fr)

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Also Published As

Publication number Publication date
CN103425817A (zh) 2013-12-04
US20130274991A1 (en) 2013-10-17
US9266626B2 (en) 2016-02-23
FR2989500A1 (fr) 2013-10-18
CN103425817B (zh) 2017-08-15

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