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WO2009071602A3 - Réseaux de capteurs et dispositif de surveillance d'état pour un aéronef, ainsi que procédé de surveillance d'état - Google Patents

Réseaux de capteurs et dispositif de surveillance d'état pour un aéronef, ainsi que procédé de surveillance d'état Download PDF

Info

Publication number
WO2009071602A3
WO2009071602A3 PCT/EP2008/066741 EP2008066741W WO2009071602A3 WO 2009071602 A3 WO2009071602 A3 WO 2009071602A3 EP 2008066741 W EP2008066741 W EP 2008066741W WO 2009071602 A3 WO2009071602 A3 WO 2009071602A3
Authority
WO
WIPO (PCT)
Prior art keywords
state monitoring
aircraft
sensor network
monitoring device
monitoring method
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.)
Ceased
Application number
PCT/EP2008/066741
Other languages
German (de)
English (en)
Other versions
WO2009071602A2 (fr
Inventor
Thomas Becker
Jordi Sabater
Peter Sollberger
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 Defence and Space GmbH
Original Assignee
EADS Deutschland GmbH
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 EADS Deutschland GmbH filed Critical EADS Deutschland GmbH
Publication of WO2009071602A2 publication Critical patent/WO2009071602A2/fr
Publication of WO2009071602A3 publication Critical patent/WO2009071602A3/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L5/00—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0016—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings of aircraft wings or blades
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0041—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by determining deflection or stress
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0066—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by exciting or detecting vibration or acceleration
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04Q—SELECTING
    • H04Q9/00—Arrangements in telecontrol or telemetry systems for selectively calling a substation from a main station, in which substation desired apparatus is selected for applying a control signal thereto or for obtaining measured values therefrom

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Arrangements For Transmission Of Measured Signals (AREA)
  • Testing Or Calibration Of Command Recording Devices (AREA)

Abstract

Réseaux de capteurs permettant de mesurer des paramètres environnementaux sur la structure d'un aéronef. A cet effet, une pluralité de dispositifs capteurs (12) est fixée sur la structure de l'aéronef, une identification étant associée à chacun de ces dispositifs capteurs (12) en vue de leur localisation.
PCT/EP2008/066741 2007-12-03 2008-12-03 Réseaux de capteurs et dispositif de surveillance d'état pour un aéronef, ainsi que procédé de surveillance d'état Ceased WO2009071602A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102007058102.7 2007-12-03
DE102007058102.7A DE102007058102B4 (de) 2007-12-03 2007-12-03 Zustandsüberwachungssystem für ein Luftfahrzeug

Publications (2)

Publication Number Publication Date
WO2009071602A2 WO2009071602A2 (fr) 2009-06-11
WO2009071602A3 true WO2009071602A3 (fr) 2009-08-06

Family

ID=40638069

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2008/066741 Ceased WO2009071602A2 (fr) 2007-12-03 2008-12-03 Réseaux de capteurs et dispositif de surveillance d'état pour un aéronef, ainsi que procédé de surveillance d'état

Country Status (2)

Country Link
DE (1) DE102007058102B4 (fr)
WO (1) WO2009071602A2 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009039431B4 (de) 2009-08-31 2014-05-22 Eads Deutschland Gmbh Kollisionsverringerungsverfahren sowie Verwendung desselben
US20110313614A1 (en) * 2010-06-21 2011-12-22 Hinnant Jr Harris O Integrated aeroelasticity measurement for vehicle health management
DE102010049909A1 (de) 2010-10-28 2012-05-03 Eads Deutschland Gmbh Instandhaltungsinformationsvorrichtung, Zustandssensor zur Verwendung darin sowie damit durchführbares Verfahren zur Entscheidungsfindung für oder gegen eine Instandhaltung
DE102013021066A1 (de) 2013-12-18 2015-06-18 Airbus Defence and Space GmbH Herstellverfahren zum Herstellen eines tragenden Rumpfpaneels sowie damit herstellbares Rumpfpaneel
AT519490B1 (de) * 2016-12-30 2020-01-15 Avl List Gmbh Kommunikation eines Netzwerkknotens in einem Datennetz
JP7272785B2 (ja) 2018-12-05 2023-05-12 ナブテスコ株式会社 疲労度算出装置、疲労度算出方法、アクチュエータ、アクチュエータ制御装置および航空機
US11753187B2 (en) * 2020-09-01 2023-09-12 Ge Aviation Systems Llc System and method for performing enhanced maintenance of aircraft
DE102021109700A1 (de) 2021-04-16 2022-10-20 Airbus Operations Gmbh Flugzustandsermittlungsvorrichtung und verfahren zum ermitteln eines flugzustandes eines flugzeugs

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4240600C1 (de) * 1992-12-03 1994-06-09 Deutsche Aerospace Verfahren zum Erkennen von Strukturschwächen von Flugzeugen
US6415242B1 (en) * 1999-07-23 2002-07-02 Abnaki Information Systems, Inc. System for weighing fixed wing and rotary wing aircraft by the measurement of cross-axis forces
US20030063585A1 (en) * 2001-08-03 2003-04-03 Honeywell International Inc. Energy aware network management
US20050242943A1 (en) * 2004-04-28 2005-11-03 Kazuhiko Matsumoto Method for inspecting and monitoring building, structure, or facilities accompanying them
US20070096979A1 (en) * 2005-11-01 2007-05-03 The Boeing Company Integrated aeroelasticity measurement system
US20070265790A1 (en) * 2006-05-09 2007-11-15 Lockheed Martin Corporation System to monitor the health of a structure, program product and related methods

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5001638A (en) * 1989-04-18 1991-03-19 The Boeing Company Integrated aircraft air data system
US6013108A (en) * 1997-03-18 2000-01-11 Endevco Corporation Intelligent sensor system with network bus
US6131119A (en) * 1997-04-01 2000-10-10 Sony Corporation Automatic configuration system for mapping node addresses within a bus structure to their physical location
FI20000325A0 (fi) * 2000-02-15 2000-02-15 Koivisto Marja Liisa Menetelmä rakenteen rasituksen määrittämiseksi
DE102004025319A1 (de) * 2004-05-19 2005-12-22 Airbus Deutschland Gmbh Sitzstatus-Anzeigesystem für Passagierräume von Flugzeugen und Fahrzeugen, Sitz für Passagiere von Flugzeugen und Fahrzeugen, sowie Bedien- und Anzeigeeinheit
DE102006020341A1 (de) * 2006-04-28 2007-10-31 Endress + Hauser Conducta Gesellschaft für Mess- und Regeltechnik mbH + Co. KG Sensor für eine Messstelle und Verfahren zur Überprüfung eines Sensors für eine Messstelle

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4240600C1 (de) * 1992-12-03 1994-06-09 Deutsche Aerospace Verfahren zum Erkennen von Strukturschwächen von Flugzeugen
US6415242B1 (en) * 1999-07-23 2002-07-02 Abnaki Information Systems, Inc. System for weighing fixed wing and rotary wing aircraft by the measurement of cross-axis forces
US20030063585A1 (en) * 2001-08-03 2003-04-03 Honeywell International Inc. Energy aware network management
US20050242943A1 (en) * 2004-04-28 2005-11-03 Kazuhiko Matsumoto Method for inspecting and monitoring building, structure, or facilities accompanying them
US20070096979A1 (en) * 2005-11-01 2007-05-03 The Boeing Company Integrated aeroelasticity measurement system
US20070265790A1 (en) * 2006-05-09 2007-11-15 Lockheed Martin Corporation System to monitor the health of a structure, program product and related methods

Also Published As

Publication number Publication date
DE102007058102B4 (de) 2016-02-04
WO2009071602A2 (fr) 2009-06-11
DE102007058102A1 (de) 2009-07-09

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