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FR2964737B1 - Procede de mesure d'efforts dans des jonctions en environnement haute temperature et axe instrumente de mise en oeuvre, en particulier pour attache arriere de turboreacteur d'aeronef - Google Patents

Procede de mesure d'efforts dans des jonctions en environnement haute temperature et axe instrumente de mise en oeuvre, en particulier pour attache arriere de turboreacteur d'aeronef

Info

Publication number
FR2964737B1
FR2964737B1 FR1057305A FR1057305A FR2964737B1 FR 2964737 B1 FR2964737 B1 FR 2964737B1 FR 1057305 A FR1057305 A FR 1057305A FR 1057305 A FR1057305 A FR 1057305A FR 2964737 B1 FR2964737 B1 FR 2964737B1
Authority
FR
France
Prior art keywords
loadings
tabs
turboelector
instrumental
junctions
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.)
Active
Application number
FR1057305A
Other languages
English (en)
Other versions
FR2964737A1 (fr
Inventor
Herve Magnin
Geraldine Hache
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 Operations SAS
Original Assignee
Airbus Operations SAS
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 SAS filed Critical Airbus Operations SAS
Priority to FR1057305A priority Critical patent/FR2964737B1/fr
Priority to PCT/FR2011/052081 priority patent/WO2012035245A1/fr
Priority to CN2011800547361A priority patent/CN103328945A/zh
Priority to US13/822,682 priority patent/US9151697B2/en
Publication of FR2964737A1 publication Critical patent/FR2964737A1/fr
Application granted granted Critical
Publication of FR2964737B1 publication Critical patent/FR2964737B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • G01L5/16—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes for measuring several components of force
    • G01L5/161—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes for measuring several components of force using variations in ohmic resistance
    • G01L5/1627—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes for measuring several components of force using variations in ohmic resistance of strain gauges
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • 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
    • G01L1/20—Measuring force or stress, in general by measuring variations in ohmic resistance of solid materials or of electrically-conductive fluids; by making use of electrokinetic cells, i.e. liquid-containing cells wherein an electrical potential is produced or varied upon the application of stress
    • G01L1/22—Measuring force or stress, in general by measuring variations in ohmic resistance of solid materials or of electrically-conductive fluids; by making use of electrokinetic cells, i.e. liquid-containing cells wherein an electrical potential is produced or varied upon the application of stress using resistance strain gauges
    • 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
    • G01L1/20—Measuring force or stress, in general by measuring variations in ohmic resistance of solid materials or of electrically-conductive fluids; by making use of electrokinetic cells, i.e. liquid-containing cells wherein an electrical potential is produced or varied upon the application of stress
    • G01L1/22—Measuring force or stress, in general by measuring variations in ohmic resistance of solid materials or of electrically-conductive fluids; by making use of electrokinetic cells, i.e. liquid-containing cells wherein an electrical potential is produced or varied upon the application of stress using resistance strain gauges
    • G01L1/2206—Special supports with preselected places to mount the resistance strain gauges; Mounting of supports
    • G01L1/2218—Special supports with preselected places to mount the resistance strain gauges; Mounting of supports the supports being of the column type, e.g. cylindric, adapted for measuring a force along a single direction
    • 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
    • G01L1/20—Measuring force or stress, in general by measuring variations in ohmic resistance of solid materials or of electrically-conductive fluids; by making use of electrokinetic cells, i.e. liquid-containing cells wherein an electrical potential is produced or varied upon the application of stress
    • G01L1/22—Measuring force or stress, in general by measuring variations in ohmic resistance of solid materials or of electrically-conductive fluids; by making use of electrokinetic cells, i.e. liquid-containing cells wherein an electrical potential is produced or varied upon the application of stress using resistance strain gauges
    • G01L1/2206—Special supports with preselected places to mount the resistance strain gauges; Mounting of supports
    • G01L1/2218—Special supports with preselected places to mount the resistance strain gauges; Mounting of supports the supports being of the column type, e.g. cylindric, adapted for measuring a force along a single direction
    • G01L1/2225—Special supports with preselected places to mount the resistance strain gauges; Mounting of supports the supports being of the column type, e.g. cylindric, adapted for measuring a force along a single direction the direction being perpendicular to the central axis
    • 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
    • G01L5/0004—Force transducers adapted for mounting in a bore of the force receiving structure
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M17/00—Testing of vehicles
    • G01M17/007—Wheeled or endless-tracked vehicles
    • G01M17/04—Suspension or damping
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D2045/0085—Devices for aircraft health monitoring, e.g. monitoring flutter or vibration

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Force Measurement Appropriate To Specific Purposes (AREA)
  • Measurement Of Force In General (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
  • Measurement Of Length, Angles, Or The Like Using Electric Or Magnetic Means (AREA)
FR1057305A 2010-09-14 2010-09-14 Procede de mesure d'efforts dans des jonctions en environnement haute temperature et axe instrumente de mise en oeuvre, en particulier pour attache arriere de turboreacteur d'aeronef Active FR2964737B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1057305A FR2964737B1 (fr) 2010-09-14 2010-09-14 Procede de mesure d'efforts dans des jonctions en environnement haute temperature et axe instrumente de mise en oeuvre, en particulier pour attache arriere de turboreacteur d'aeronef
PCT/FR2011/052081 WO2012035245A1 (fr) 2010-09-14 2011-09-13 Procédé de mesure d'efforts dans des jonctions en environnement haute température et axe instrumenté de mise en oeuvre, en particulier pour attache arrière de turboréacteur d'aéronef
CN2011800547361A CN103328945A (zh) 2010-09-14 2011-09-13 尤其用于飞机涡轮喷气机的后部附件的测量高温环境下连接部内的载荷的方法及用于实施的配备仪器的轴
US13/822,682 US9151697B2 (en) 2010-09-14 2011-09-13 Method of measuring loadings in joins in a high-temperature environment and instrumented shaft for implementation, in particular for rear attachment of aircraft turbojet

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1057305A FR2964737B1 (fr) 2010-09-14 2010-09-14 Procede de mesure d'efforts dans des jonctions en environnement haute temperature et axe instrumente de mise en oeuvre, en particulier pour attache arriere de turboreacteur d'aeronef

Publications (2)

Publication Number Publication Date
FR2964737A1 FR2964737A1 (fr) 2012-03-16
FR2964737B1 true FR2964737B1 (fr) 2013-05-31

Family

ID=43836577

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1057305A Active FR2964737B1 (fr) 2010-09-14 2010-09-14 Procede de mesure d'efforts dans des jonctions en environnement haute temperature et axe instrumente de mise en oeuvre, en particulier pour attache arriere de turboreacteur d'aeronef

Country Status (4)

Country Link
US (1) US9151697B2 (fr)
CN (1) CN103328945A (fr)
FR (1) FR2964737B1 (fr)
WO (1) WO2012035245A1 (fr)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9016134B2 (en) * 2012-12-11 2015-04-28 Goodrich Corporation Circular load cell strain sensor configuration
GB201411715D0 (en) * 2014-07-01 2014-08-13 Ftl Subsea Ltd Sensing device
GB2527782B (en) * 2014-07-01 2017-01-18 Flintstone Tech Ltd A connector having an inductive transmission
CN105403335B (zh) * 2014-09-03 2018-05-18 北京强度环境研究所 一种测试火箭连杆装置载荷变化的力传感器
FR3026137B1 (fr) * 2014-09-22 2019-03-15 Safran Aircraft Engines Element pour une turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur d'avion
KR102544041B1 (ko) * 2015-03-31 2023-06-15 가부시키가이샤 네지로 통전로 부부재 및 통전로의 패터닝 방법, 부재 변화 계측 방법
DE102015106933A1 (de) * 2015-05-04 2016-11-10 Technische Universität Darmstadt Maschinenelement mit einer Sensoreinrichtung und Verfahren zur Herstellung eines Maschinenelements
US10351224B2 (en) * 2015-09-23 2019-07-16 The Boeing Company External structure mounting system for use with an aircraft
FR3058986B1 (fr) * 2016-11-21 2021-04-16 Airbus Operations Sas Attache arriere d'un moteur d'aeronef comportant des temoins de rupture
JP7416598B2 (ja) 2019-10-21 2024-01-17 ミネベアミツミ株式会社 荷重検出機構、及びピン型ロードセル
FR3102976B1 (fr) * 2019-11-13 2023-11-24 Safran Aircraft Engines Avion à suspension instrumentée
DE102020119655B4 (de) 2020-07-24 2022-11-03 Core Sensing Gmbh Hohlkörper mit einem zylinderförmigen Innenraumabschnitt und einer Messeinrichtung zur Anordnung in dem Hohlkörper
GB2623353A (en) * 2022-10-13 2024-04-17 Airbus Operations Ltd Landing gear load sensing apparatus and methods
FR3159591A1 (fr) * 2024-02-26 2025-08-29 Airbus Attache instrumentee de moteur d’aeronef et aeronef comprenant une telle attache.

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL6414342A (fr) * 1964-12-10 1966-06-13
FR2315690A1 (fr) * 1976-01-12 1977-01-21 Poclain Sa Dispositif de mesure d'un couple de basculement et procede de mesure du couple de basculement
DE3475001D1 (en) * 1984-03-13 1988-12-08 Yotaro Hatamura Load detector
EP0738882B1 (fr) * 1991-12-27 2001-10-24 ISHIDA CO., Ltd. Capteur de pesage avec une plaque à ouverture et un capteur de dilatation recouvrant
FR2793767B1 (fr) * 1999-05-17 2001-09-21 Aerospatiale Airbus Dispositif d'accrochage d'un moteur d'aeronef
GB0603243D0 (en) * 2006-02-17 2006-03-29 Dage Prec Ind Ltd Shear test device
DE102007012157A1 (de) * 2007-03-12 2008-09-18 Brosa Ag Modular aufgebaute Messachse
CN101206148B (zh) * 2007-12-17 2010-08-18 南昌航空大学 一种能准确测量高温应力应变的方法

Also Published As

Publication number Publication date
FR2964737A1 (fr) 2012-03-16
CN103328945A (zh) 2013-09-25
US20130305817A1 (en) 2013-11-21
US9151697B2 (en) 2015-10-06
WO2012035245A1 (fr) 2012-03-22

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