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FR3102756B1 - INTERACTIVE FAILURE FINDING IN AN AIRCRAFT - Google Patents

INTERACTIVE FAILURE FINDING IN AN AIRCRAFT Download PDF

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Publication number
FR3102756B1
FR3102756B1 FR1912464A FR1912464A FR3102756B1 FR 3102756 B1 FR3102756 B1 FR 3102756B1 FR 1912464 A FR1912464 A FR 1912464A FR 1912464 A FR1912464 A FR 1912464A FR 3102756 B1 FR3102756 B1 FR 3102756B1
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France
Prior art keywords
finding
fault
aircraft
procedure objects
functional
Prior art date
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Active
Application number
FR1912464A
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French (fr)
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FR3102756A1 (en
Inventor
Christian Gulli
Patrick Roussel
Jean-Paul Lacampagne
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
Airbus SAS
Original Assignee
Airbus Operations SAS
Airbus SAS
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Application filed by Airbus Operations SAS, Airbus SAS filed Critical Airbus Operations SAS
Priority to FR1912464A priority Critical patent/FR3102756B1/en
Publication of FR3102756A1 publication Critical patent/FR3102756A1/en
Application granted granted Critical
Publication of FR3102756B1 publication Critical patent/FR3102756B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND 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
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/60Testing or inspecting aircraft components or systems
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06QINFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
    • G06Q10/00Administration; Management
    • G06Q10/06Resources, workflows, human or project management; Enterprise or organisation planning; Enterprise or organisation modelling
    • G06Q10/063Operations research, analysis or management
    • G06Q10/0631Resource planning, allocation, distributing or scheduling for enterprises or organisations
    • G06Q10/06316Sequencing of tasks or work

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  • Business, Economics & Management (AREA)
  • Human Resources & Organizations (AREA)
  • Engineering & Computer Science (AREA)
  • Entrepreneurship & Innovation (AREA)
  • Economics (AREA)
  • Strategic Management (AREA)
  • Operations Research (AREA)
  • Physics & Mathematics (AREA)
  • Educational Administration (AREA)
  • Marketing (AREA)
  • Development Economics (AREA)
  • Quality & Reliability (AREA)
  • Tourism & Hospitality (AREA)
  • Game Theory and Decision Science (AREA)
  • General Business, Economics & Management (AREA)
  • General Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Debugging And Monitoring (AREA)
  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)

Abstract

L’invention concerne un système de recherche de pannes dans un aéronef, comportant:- des unités de stockages (7) configurées pour stocker une base de données contextuelle (13) modélisant des objets de procédure de recherche de pannes, ladite base de données contextuelle (13) étant une dématérialisation d’un manuel de recherche de pannes générée par une technique d’ingénierie de modélisation de systèmes complexes,- un microprocesseur (5) configuré pour implémenter lesdits objets de procédure de recherche de pannes en les structurant selon une représentation fonctionnelle et logique, et- une interface de sortie (9) configurée pour afficher ladite structure fonctionnelle et logique des objets de procédure de recherche de pannes. Fig. 1The invention relates to a fault-finding system in an aircraft, comprising:- storage units (7) configured to store a contextual database (13) modeling fault-finding procedure objects, said contextual database (13) being a dematerialization of a fault-finding manual generated by a complex systems modeling engineering technique,- a microprocessor (5) configured to implement said fault-finding procedure objects by structuring them according to a representation functional and logical, and- an output interface (9) configured to display said functional and logical structure of the troubleshooting procedure objects. Fig. 1

FR1912464A 2019-11-06 2019-11-06 INTERACTIVE FAILURE FINDING IN AN AIRCRAFT Active FR3102756B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1912464A FR3102756B1 (en) 2019-11-06 2019-11-06 INTERACTIVE FAILURE FINDING IN AN AIRCRAFT

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1912464 2019-11-06
FR1912464A FR3102756B1 (en) 2019-11-06 2019-11-06 INTERACTIVE FAILURE FINDING IN AN AIRCRAFT

Publications (2)

Publication Number Publication Date
FR3102756A1 FR3102756A1 (en) 2021-05-07
FR3102756B1 true FR3102756B1 (en) 2023-01-13

Family

ID=70613829

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1912464A Active FR3102756B1 (en) 2019-11-06 2019-11-06 INTERACTIVE FAILURE FINDING IN AN AIRCRAFT

Country Status (1)

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FR (1) FR3102756B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3129008A1 (en) * 2021-11-10 2023-05-12 Antidot User terminal control method

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6574537B2 (en) * 2001-02-05 2003-06-03 The Boeing Company Diagnostic system and method
JP2003002298A (en) * 2001-06-22 2003-01-08 Nec Aerospace Syst Ltd Aircraft maintenance information support system
US9123189B2 (en) * 2007-02-12 2015-09-01 The Boeing Company System and method for point-of-use instruction
FR3011105B1 (en) * 2013-09-20 2017-01-27 Airbus Operations Sas METHOD FOR IDENTIFYING FAILURE EQUIPMENT IN AN AIRCRAFT
FR3013140B1 (en) * 2013-11-13 2017-04-14 Flightwatching SYSTEM AND METHOD FOR DIAGNOSING AIRCRAFT FAILURE

Also Published As

Publication number Publication date
FR3102756A1 (en) 2021-05-07

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