BR112015024038A2 - sensor de carga de alta sensibilidade para alívio de carga e aplicação em estruturas - Google Patents

sensor de carga de alta sensibilidade para alívio de carga e aplicação em estruturas

Info

Publication number
BR112015024038A2
BR112015024038A2 BR112015024038A BR112015024038A BR112015024038A2 BR 112015024038 A2 BR112015024038 A2 BR 112015024038A2 BR 112015024038 A BR112015024038 A BR 112015024038A BR 112015024038 A BR112015024038 A BR 112015024038A BR 112015024038 A2 BR112015024038 A2 BR 112015024038A2
Authority
BR
Brazil
Prior art keywords
load
high sensitivity
relief
sensor
structural application
Prior art date
Application number
BR112015024038A
Other languages
English (en)
Other versions
BR112015024038B1 (pt
Inventor
pedersen Derek
Randall Kohuth Kerry
Original Assignee
Moog Inc
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 Moog Inc filed Critical Moog Inc
Publication of BR112015024038A2 publication Critical patent/BR112015024038A2/pt
Publication of BR112015024038B1 publication Critical patent/BR112015024038B1/pt

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
    • G01L5/22—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes for measuring the force applied to control members, e.g. control members of vehicles, triggers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B64C9/20—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by multiple flaps
    • 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
    • G01L5/0028—Force sensors associated with force applying means
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
    • G01N3/08—Investigating strength properties of solid materials by application of mechanical stress by applying steady tensile or compressive forces
    • 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

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Automation & Control Theory (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Biochemistry (AREA)
  • General Health & Medical Sciences (AREA)
  • Immunology (AREA)
  • Pathology (AREA)
  • Health & Medical Sciences (AREA)
  • Force Measurement Appropriate To Specific Purposes (AREA)
  • Mechanical Engineering (AREA)
  • Measurement Of Force In General (AREA)

Abstract

1/1 resumo “sensor de carga de alta sensibilidade para alívio de carga e aplicação em estruturas” a presente invenção refere-se a uma estrutura de detecção de carga que tem um corpo principal (26) tendo um eixo de carregamento longitudinal (a) ao longo do qual uma carga aplicada é transmitida, e um elemento de detecção de carga (38) disposto para transportar pelo menos uma parte da carga aplicada quando a carga está dentro de uma faixa predeterminada, onde o elemento de detecção de carga (38) inclui pelo menos um sensor de carga (46) gerando um sinal de carga.
BR112015024038-0A 2013-03-22 2014-03-21 Estrutura de detecção de carga BR112015024038B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201361804559P 2013-03-22 2013-03-22
US61/804,559 2013-03-22
PCT/US2014/031467 WO2014153518A1 (en) 2013-03-22 2014-03-21 High sensitivity, load alleviating load sensor for strut application

Publications (2)

Publication Number Publication Date
BR112015024038A2 true BR112015024038A2 (pt) 2017-07-18
BR112015024038B1 BR112015024038B1 (pt) 2022-07-26

Family

ID=51581526

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015024038-0A BR112015024038B1 (pt) 2013-03-22 2014-03-21 Estrutura de detecção de carga

Country Status (6)

Country Link
US (1) US9459168B2 (pt)
EP (1) EP2976224B1 (pt)
CN (1) CN105228840B (pt)
BR (1) BR112015024038B1 (pt)
CA (1) CA2907732C (pt)
WO (1) WO2014153518A1 (pt)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014019134A1 (de) * 2014-12-18 2016-06-23 Liebherr-Aerospace Lindenberg Gmbh Auftriebsvorrichtung für ein Luftfahrzeug mit wenigstens einer bewegbaren Klappe
DE102015101336A1 (de) * 2015-01-29 2016-08-04 Airbus Operations Gmbh Verfahren zum Einstellen des Spiels in einem Hochauftriebssystem eines Flugzeugs
US10472046B1 (en) * 2016-02-03 2019-11-12 Lockheed Martin Corporation Internal wing control surface linkage system
US10386254B2 (en) * 2016-04-25 2019-08-20 The Boeing Company Fastener Status Detection System
EP3275789B1 (en) * 2016-07-27 2021-11-17 Ratier-Figeac SAS Actuator assembly
EP3336485B1 (en) 2016-12-15 2020-09-23 Safran Landing Systems UK Limited Aircraft assembly including deflection sensor
JP2018105806A (ja) * 2016-12-28 2018-07-05 Ntn株式会社 荷重センサおよび電動ブレーキ装置
DE102018114297A1 (de) * 2018-06-14 2019-12-19 Liebherr-Aerospace Lindenberg Gmbh Verfahren zur Detektion eines Bruchs in einem Hochauftriebssystem eines Fluggeräts
CN108760125B (zh) * 2018-07-17 2020-07-10 中国空气动力研究与发展中心超高速空气动力研究所 一种轴承滚动摩擦力矩测量方法
FR3092662B1 (fr) 2019-02-12 2021-03-05 Airbus Helicopters Système de détection et procédé pour détecter une usure d’un dispositif de liaison à rotule d’une bielle, ensemble rotor et aéronef
CN113291458A (zh) * 2021-06-25 2021-08-24 庆安集团有限公司 飞机高升力系统用内外襟翼交联装置
CN114426093B (zh) * 2022-01-19 2024-03-01 中电科芜湖通用航空产业技术研究院有限公司 一种无人机随动襟翼系统及无人机的机翼和无人机

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4103532A (en) * 1976-06-10 1978-08-01 Carlo Buzzi Device for measuring the damping effect of motor vehicle suspensions
JPS62286816A (ja) * 1986-06-03 1987-12-12 Nissan Motor Co Ltd サスペンシヨン荷重検出装置
FR2599793B1 (fr) * 1986-06-09 1988-10-21 Aerospatiale Systeme de bielle destine a resister a un seuil d'efforts longitudinaux
FR2653880B1 (fr) * 1989-10-31 1992-01-17 Bendix France Capteur de charge instantanee d'un vehicule automobile.
JPH0754830Y2 (ja) 1990-01-24 1995-12-18 株式会社ユニシアジェックス 荷重センサ取付構造
US5152547A (en) * 1990-11-02 1992-10-06 Davis Leo W Dual piston strut
JP2548907Y2 (ja) * 1991-02-21 1997-09-24 株式会社ユニシアジェックス 荷重センサの取付構造
JP2003504566A (ja) * 1997-09-26 2003-02-04 ビステック， インコーポレイテッド 微細振動隔離装置
JP4444046B2 (ja) * 2004-09-09 2010-03-31 東海ゴム工業株式会社 サブフレーム機構
JP5116147B2 (ja) 2007-11-13 2013-01-09 パラマウントベッド株式会社 荷重センサ内蔵アクチュエータ
US8267383B2 (en) * 2008-07-28 2012-09-18 Honda Motor Company, Ltd. Mount devices and methods for measuring force
DE102010044678A1 (de) * 2010-09-08 2012-03-08 Airbus Operations Gmbh Überwachungsvorrichtung für ein Stellsystem eines Flugzeugs, Stellsystem und Verfahren zur Rekonfiguration des Stellsystems

Also Published As

Publication number Publication date
EP2976224B1 (en) 2018-04-18
CN105228840A (zh) 2016-01-06
CA2907732C (en) 2017-07-11
CN105228840B (zh) 2017-06-23
US20150346043A1 (en) 2015-12-03
EP2976224A4 (en) 2016-11-30
BR112015024038B1 (pt) 2022-07-26
CA2907732A1 (en) 2014-09-25
US9459168B2 (en) 2016-10-04
WO2014153518A1 (en) 2014-09-25
EP2976224A1 (en) 2016-01-27

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 21/03/2014, OBSERVADAS AS CONDICOES LEGAIS