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 PDFInfo
- 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
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).
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)
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)
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)
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 |
-
2007
- 2007-12-03 DE DE102007058102.7A patent/DE102007058102B4/en not_active Expired - Fee Related
-
2008
- 2008-12-03 WO PCT/EP2008/066741 patent/WO2009071602A2/en active Application Filing
Patent Citations (6)
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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