ATE511086T1 - Vorrichtung mit beschädigungsanzeigemerkmal - Google Patents

Vorrichtung mit beschädigungsanzeigemerkmal

Info

Publication number
ATE511086T1
ATE511086T1 AT08806695T AT08806695T ATE511086T1 AT E511086 T1 ATE511086 T1 AT E511086T1 AT 08806695 T AT08806695 T AT 08806695T AT 08806695 T AT08806695 T AT 08806695T AT E511086 T1 ATE511086 T1 AT E511086T1
Authority
AT
Austria
Prior art keywords
design space
load
stress
load path
primary structure
Prior art date
Application number
AT08806695T
Other languages
English (en)
Inventor
Goncalves De Oliveira Andre Rossi
Original Assignee
Airbus Operations Ltd
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 Airbus Operations Ltd filed Critical Airbus Operations Ltd
Application granted granted Critical
Publication of ATE511086T1 publication Critical patent/ATE511086T1/de

Links

Classifications

    • 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
    • G01M5/0033—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by determining damage, crack or wear
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L1/00—Measuring force or stress, in general
    • G01L1/06—Measuring force or stress, in general by measuring the permanent deformation of gauges, e.g. of compressed bodies
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B33—ADDITIVE MANUFACTURING TECHNOLOGY
    • B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y80/00—Products made by additive manufacturing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B2200/00—Constructional details of connections not covered for in other groups of this subclass
    • F16B2200/63—Frangible connections

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Vibration Dampers (AREA)
  • Buildings Adapted To Withstand Abnormal External Influences (AREA)
  • Transplanting Machines (AREA)
  • Prostheses (AREA)
  • Investigating Or Analyzing Materials By The Use Of Ultrasonic Waves (AREA)
  • Powder Metallurgy (AREA)
  • Bridges Or Land Bridges (AREA)
AT08806695T 2007-10-04 2008-09-29 Vorrichtung mit beschädigungsanzeigemerkmal ATE511086T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB0719272.7A GB0719272D0 (en) 2007-10-04 2007-10-04 Apparatus with damage indication feature
PCT/GB2008/050879 WO2009044191A2 (en) 2007-10-04 2008-09-29 Apparatus with damage indication feature

Publications (1)

Publication Number Publication Date
ATE511086T1 true ATE511086T1 (de) 2011-06-15

Family

ID=38787818

Family Applications (1)

Application Number Title Priority Date Filing Date
AT08806695T ATE511086T1 (de) 2007-10-04 2008-09-29 Vorrichtung mit beschädigungsanzeigemerkmal

Country Status (5)

Country Link
US (1) US8366045B2 (de)
EP (1) EP2195630B1 (de)
AT (1) ATE511086T1 (de)
GB (1) GB0719272D0 (de)
WO (1) WO2009044191A2 (de)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0715303D0 (en) * 2007-08-08 2007-09-19 Airbus Uk Ltd Composite laminate structure
US8401827B2 (en) * 2008-04-14 2013-03-19 Daa Draexlmaier Automotive Of America Llc Processing device and method for structure data representing a physical structure
GB2485803B (en) 2010-11-24 2013-02-06 Messier Dowty Ltd Mechanical position indicator
EP2634446B1 (de) * 2012-02-28 2020-04-08 Meritor Heavy Vehicle Braking Systems (UK) Limited Gegossene oder geschmiedete Komponente mit Angabe der Lebensdauer
FR3016554B1 (fr) * 2014-01-20 2016-01-01 Renault Sas Chape de liaison fusible entre le bras de suspension et le berceau moteur
US9638588B2 (en) * 2014-03-07 2017-05-02 Sikorsky Aircraft Corporation Multifunctional load and damage sensor
US9500249B2 (en) * 2015-03-09 2016-11-22 The Boeing Company Energy absorbing link
JP6750860B2 (ja) * 2016-07-06 2020-09-02 公立大学法人秋田県立大学 リミット型変位検出装置および構造物等の健全性モニタリングシステム
EP3803315B1 (de) * 2018-06-04 2026-02-18 Conseil et Technique Verfahren zur warnnung vor der bruch- oder verformungsgefahr eines teils aus einem verbundwerkstoff und hergestelltes teil
FR3081993B1 (fr) * 2018-06-04 2020-12-04 Conseil & Technique Procede d'avertissement d'un risque de rupture ou de deformation d'une piece en materiau composite, et piece composite obtenue
FR3081992B1 (fr) * 2018-06-04 2021-07-02 Conseil & Technique Procede d'avertissement d'un risque de rupture ou de deformation d'une piece en materiau composite, et piece obtenue
US11169062B2 (en) * 2018-09-08 2021-11-09 The Boeing Company Methods and systems for identifying an internal flaw in a part produced using additive manufacturing

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4322981A (en) * 1980-07-10 1982-04-06 Amsted Industries Incorporated Railway car truck fatigue detector
US4392623A (en) * 1980-12-22 1983-07-12 The Boeing Company Fused connection adapted to fail under different overloads acting in different directions
DE4338850A1 (de) * 1993-11-13 1995-05-18 Dornier Gmbh Einrichtung zum Überwachen der Zeitfestigkeit von Strukturen
US5599129A (en) * 1995-01-17 1997-02-04 Dcd Design & Manufacturing Ltd. Load limited connector
GB2312532B (en) 1995-04-19 1998-04-22 Honda Motor Co Ltd Method of generating die structure data and producing a die structure
EP0850170B1 (de) * 1995-09-14 1999-03-17 Sikorsky Aircraft Corporation Energie absorbierende fahrgestell/heckstütze mit anordnung zum anzeigen der kraft einer schlagartigen belastung
US5895892A (en) * 1997-08-29 1999-04-20 Interpool Limited Overload detection system
WO2001048884A1 (fr) 1999-12-23 2001-07-05 Hydro-Quebec Detendeurs-deglaceurs pour cables aeriens
US6488434B1 (en) * 2000-08-30 2002-12-03 Westinghouse Electric Company Llc Overload indicator
FR2829546B1 (fr) * 2001-09-11 2004-02-20 Eurocopter France Barre de liaison a absorption d'energie, et son application comme barre de suspension de boite de transmission pour giravion
US7121780B2 (en) * 2004-10-21 2006-10-17 The Boeing Company Multiple load path fastener systems
DE102007011618B4 (de) * 2007-01-22 2012-04-26 Airbus Operations Gmbh Crashpaddel zur Verstärkung einer primären Rumpfstruktur eines Flugzeugs

Also Published As

Publication number Publication date
US20100308163A1 (en) 2010-12-09
GB0719272D0 (en) 2007-11-21
WO2009044191A2 (en) 2009-04-09
EP2195630B1 (de) 2011-05-25
US8366045B2 (en) 2013-02-05
EP2195630A2 (de) 2010-06-16
WO2009044191A3 (en) 2009-06-11

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