GB2192723A - Operational-load monitoring system for aircraft - Google Patents

Operational-load monitoring system for aircraft Download PDF

Info

Publication number
GB2192723A
GB2192723A GB08714601A GB8714601A GB2192723A GB 2192723 A GB2192723 A GB 2192723A GB 08714601 A GB08714601 A GB 08714601A GB 8714601 A GB8714601 A GB 8714601A GB 2192723 A GB2192723 A GB 2192723A
Authority
GB
United Kingdom
Prior art keywords
aircraft
load
data
quantities
structural components
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.)
Withdrawn
Application number
GB08714601A
Other languages
English (en)
Other versions
GB8714601D0 (en
Inventor
Hans Jorg Meyer
Meinhard Schmucker
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
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB8714601D0 publication Critical patent/GB8714601D0/en
Publication of GB2192723A publication Critical patent/GB2192723A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G07—CHECKING-DEVICES
    • G07C—TIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
    • G07C3/00—Registering or indicating the condition or the working of machines or other apparatus, other than vehicles

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Testing Or Calibration Of Command Recording Devices (AREA)
GB08714601A 1986-06-21 1987-06-22 Operational-load monitoring system for aircraft Withdrawn GB2192723A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19863620888 DE3620888A1 (de) 1986-06-21 1986-06-21 Betriebslastenueberwachungseinrichtung fuer luftfahrzeuge

Publications (2)

Publication Number Publication Date
GB8714601D0 GB8714601D0 (en) 1987-07-29
GB2192723A true GB2192723A (en) 1988-01-20

Family

ID=6303455

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08714601A Withdrawn GB2192723A (en) 1986-06-21 1987-06-22 Operational-load monitoring system for aircraft

Country Status (4)

Country Link
AU (1) AU7453887A (fr)
DE (1) DE3620888A1 (fr)
FR (1) FR2600419A1 (fr)
GB (1) GB2192723A (fr)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0407179A1 (fr) * 1989-07-05 1991-01-09 Bristow Helicopters Limited Système pour la surveillance du bon état et de l'usure d'un aéronef
GB2234353A (en) * 1989-07-28 1991-01-30 James Ormond Beaumont Incipient failure detector
FR2871440A1 (fr) * 2004-06-15 2005-12-16 Airbus France Sas Procede et dispositif pour detecter un depassement de charges de dimensionnement de la derive d'un avion
FR2871439A1 (fr) * 2004-06-15 2005-12-16 Airbus France Sas Procede et dispositif pour detecter un depassement de charges de dimensionnement de l'empennage horizontal arriere d'un avion
GB2481488A (en) * 2010-06-21 2011-12-28 Boeing Co Integrated aeroelasticity measurement for vehicle health management
RU2599108C1 (ru) * 2015-07-07 2016-10-10 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Способ мониторинга нагрузок и накопленной усталостной повреждаемости в условиях эксплуатации самолета

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3803015A1 (de) * 1988-02-02 1989-08-10 Pfister Gmbh Verfahren und system zum betrieb eines luftfahrzeugs
DE4036241A1 (de) * 1990-11-14 1992-05-21 Joerg Golombek Verfahren und vorrichtung zur ermittlung und verwertung der physikalischen daten eines im betrieb befindlichen fahrzeugmodells
GB9211719D0 (en) * 1992-06-03 1992-07-15 Westland Helicopters Method & apparatus for in-flight shake testing of an aircraft fuselage
DE4336588C2 (de) * 1993-10-27 1999-07-15 Eurocopter Deutschland Verfahren zur Ermittlung der individuellen Lebensdauer eines Fluggerätes
FR2713193B1 (fr) * 1993-12-06 1996-01-26 Aerospatiale Procédé et dispositif pour détecter un dépassement des charges de dimensionnement d'un aéronef.

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4336595A (en) * 1977-08-22 1982-06-22 Lockheed Corporation Structural life computer
GB2020432B (en) * 1978-05-06 1982-07-28 Arcubos Ltd Strain detecting devices
NZ190374A (en) * 1978-05-10 1982-08-17 Res Analysis & Dev Aircraft structure deflection measurement and detection
DE3024914A1 (de) * 1980-07-01 1982-02-11 Hans-Jürgen Dipl.-Phys. 8057 Eching Langer Vorrichtung zur messung kleiner biegewinkel
US4409842A (en) * 1981-05-18 1983-10-18 Scott Science & Technology, Inc. Structural information detector

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0407179A1 (fr) * 1989-07-05 1991-01-09 Bristow Helicopters Limited Système pour la surveillance du bon état et de l'usure d'un aéronef
GB2234353A (en) * 1989-07-28 1991-01-30 James Ormond Beaumont Incipient failure detector
GB2234353B (en) * 1989-07-28 1994-06-01 James Ormond Beaumont Incipient failure detector
FR2871440A1 (fr) * 2004-06-15 2005-12-16 Airbus France Sas Procede et dispositif pour detecter un depassement de charges de dimensionnement de la derive d'un avion
FR2871439A1 (fr) * 2004-06-15 2005-12-16 Airbus France Sas Procede et dispositif pour detecter un depassement de charges de dimensionnement de l'empennage horizontal arriere d'un avion
EP1607815A1 (fr) * 2004-06-15 2005-12-21 Airbus France Procédé et dispositif pour détecter un dépassement de charges de dimensionnement de la dérive d'un avion
EP1607814A1 (fr) * 2004-06-15 2005-12-21 AIRBUS France Procédé et dispositif pour détecter un dépassement de charges de dimensionnement de l'empennage horizontal arrière d'un avion
US7271741B2 (en) 2004-06-15 2007-09-18 Airbus France Method and device for detecting an overstepping of design loads of the fin of an aircraft
US7382283B2 (en) 2004-06-15 2008-06-03 Airbus France Method and device for detecting an overstepping of design loads of the tailplane of an aircraft
GB2481488A (en) * 2010-06-21 2011-12-28 Boeing Co Integrated aeroelasticity measurement for vehicle health management
RU2599108C1 (ru) * 2015-07-07 2016-10-10 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Способ мониторинга нагрузок и накопленной усталостной повреждаемости в условиях эксплуатации самолета

Also Published As

Publication number Publication date
GB8714601D0 (en) 1987-07-29
DE3620888A1 (de) 1988-01-14
FR2600419A1 (fr) 1987-12-24
AU7453887A (en) 1987-12-24

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)