WO2009071602A3 - Sensor network and state monitoring device for an aircraft and state monitoring method - Google Patents

Sensor network and state monitoring device for an aircraft and state monitoring method Download PDF

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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
Application number
PCT/EP2008/066741
Other languages
German (de)
French (fr)
Other versions
WO2009071602A2 (en
Inventor
Thomas Becker
Jordi Sabater
Peter Sollberger
Original Assignee
Eads Deutschland Gmbh
Hochschule Fuer Technik Und Ar
Thomas Becker
Jordi Sabater
Peter Sollberger
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, Hochschule Fuer Technik Und Ar, Thomas Becker, Jordi Sabater, Peter Sollberger filed Critical Eads Deutschland Gmbh
Publication of WO2009071602A2 publication Critical patent/WO2009071602A2/en
Publication of WO2009071602A3 publication Critical patent/WO2009071602A3/en

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

Abstract

The invention relates to a sensor network for measuring environmental parameters on the structure of an aircraft. For this purpose, a plurality of sensor units (12) is fastened on the structure of an aircraft, with which identifiers are associated for localization of the sensor units (12).
PCT/EP2008/066741 2007-12-03 2008-12-03 Sensor network and state monitoring device for an aircraft and state monitoring method WO2009071602A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102007058102.7 2007-12-03
DE102007058102.7A DE102007058102B4 (en) 2007-12-03 2007-12-03 Condition monitoring system for an aircraft

Publications (2)

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

Family

ID=40638069

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2008/066741 WO2009071602A2 (en) 2007-12-03 2008-12-03 Sensor network and state monitoring device for an aircraft and state monitoring method

Country Status (2)

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

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009039431B4 (en) 2009-08-31 2014-05-22 Eads Deutschland Gmbh Collision reduction method and use thereof
US20110313614A1 (en) * 2010-06-21 2011-12-22 Hinnant Jr Harris O Integrated aeroelasticity measurement for vehicle health management
DE102010049909A1 (en) 2010-10-28 2012-05-03 Eads Deutschland Gmbh Maintenance information device, condition sensor for use therein, and method of decision making for or against maintenance that can be performed thereby
DE102013021066A1 (en) 2013-12-18 2015-06-18 Airbus Defence and Space GmbH Manufacturing method for producing a load-bearing fuselage panel and fuselage panel manufacturable therewith
AT519490B1 (en) 2016-12-30 2020-01-15 Avl List Gmbh Communication of a network node in a data network
JP7272785B2 (en) 2018-12-05 2023-05-12 ナブテスコ株式会社 FATIGUE CALCULATION DEVICE, FATIGUE CALCULATION METHOD, ACTUATOR, ACTUATOR CONTROL DEVICE, AND AIRCRAFT
US11753187B2 (en) * 2020-09-01 2023-09-12 Ge Aviation Systems Llc System and method for performing enhanced maintenance of aircraft
DE102021109700A1 (en) 2021-04-16 2022-10-20 Airbus Operations Gmbh FLIGHT CONDITION DETERMINING DEVICE AND METHOD FOR DETERMINING A FLIGHT CONDITION OF AN AIRCRAFT

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4240600C1 (en) * 1992-12-03 1994-06-09 Deutsche Aerospace Structural defect detection system for aircraft - uses modal analysis via detected oscillation of aircraft structure and comparison with aircraft model
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 (en) * 2000-02-15 2000-02-15 Koivisto Marja Liisa Method for determination of structural stress
DE102004025319A1 (en) * 2004-05-19 2005-12-22 Airbus Deutschland Gmbh Seat condition indication system for e.g. aircraft, has sensor arrangements with seat-occupancy and belt sensors to detect occupancy and closed condition of safety belt of seats, respectively
DE102006020341A1 (en) * 2006-04-28 2007-10-31 Endress + Hauser Conducta Gesellschaft für Mess- und Regeltechnik mbH + Co. KG Point measuring sensor, has sensor head and sensor head counterpiece, which are detachably connected to each other, and sensor head counterpiece connected with control system, to which processed measuring value is transmitted

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4240600C1 (en) * 1992-12-03 1994-06-09 Deutsche Aerospace Structural defect detection system for aircraft - uses modal analysis via detected oscillation of aircraft structure and comparison with aircraft model
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 (en) 2016-02-04
DE102007058102A1 (en) 2009-07-09
WO2009071602A2 (en) 2009-06-11

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