FR2436074A1 - Dispositif d'asservissement de gouvernes d'un aeronef et procede de detection de defaillances dans le circuit de charge principal de ce dispositif - Google Patents

Dispositif d'asservissement de gouvernes d'un aeronef et procede de detection de defaillances dans le circuit de charge principal de ce dispositif

Info

Publication number
FR2436074A1
FR2436074A1 FR7919275A FR7919275A FR2436074A1 FR 2436074 A1 FR2436074 A1 FR 2436074A1 FR 7919275 A FR7919275 A FR 7919275A FR 7919275 A FR7919275 A FR 7919275A FR 2436074 A1 FR2436074 A1 FR 2436074A1
Authority
FR
France
Prior art keywords
aircraft
main load
governes
controlling
load circuit
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.)
Granted
Application number
FR7919275A
Other languages
English (en)
Other versions
FR2436074B1 (fr
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.)
Sundstrand Corp
Original Assignee
Sundstrand Corp
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 Sundstrand Corp filed Critical Sundstrand Corp
Publication of FR2436074A1 publication Critical patent/FR2436074A1/fr
Application granted granted Critical
Publication of FR2436074B1 publication Critical patent/FR2436074B1/fr
Granted legal-status Critical Current

Links

Classifications

    • 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
    • B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
    • 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
    • B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
    • B64D2045/001—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear for indicating symmetry of flaps deflection
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00—Machine element or mechanism
    • Y10T74/19—Gearing
    • Y10T74/19023—Plural power paths to and/or from gearing
    • Y10T74/19074—Single drive plural driven

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
  • Braking Arrangements (AREA)
  • Force Measurement Appropriate To Specific Purposes (AREA)

Abstract

L'invention concerne un dispositif d'asservissement des gouvernes d'un aéronef, destiné à maintenir la symétrie des gouvernes disposées sur les côtés opposés d'un aéronef. Ce dispositif comporte un arbre de sécurité relié par ses extrémités aux extrémités correspondantes d'un circuit principal de charge ou de transmission de force. Cet arbre ne transmet normalement aucun couple ou qu'un couple très faible. En cas de défaillance du circuit principal, il est soumis à un couple plus important provoquant une déformation par torsion qui est détectée par des capteurs montés sur les extrémités opposées de cet arbre. Domaine d'application : commande des gouvernes d'aéronefs, etc.
FR7919275A 1978-09-12 1979-07-26 Dispositif d'asservissement de gouvernes d'un aeronef et procede de detection de defaillances dans le circuit de charge principal de ce dispositif Granted FR2436074A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/941,695 US4256277A (en) 1978-09-12 1978-09-12 Actuator system for aircraft control surfaces

Publications (2)

Publication Number Publication Date
FR2436074A1 true FR2436074A1 (fr) 1980-04-11
FR2436074B1 FR2436074B1 (fr) 1983-04-15

Family

ID=25476913

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7919275A Granted FR2436074A1 (fr) 1978-09-12 1979-07-26 Dispositif d'asservissement de gouvernes d'un aeronef et procede de detection de defaillances dans le circuit de charge principal de ce dispositif

Country Status (4)

Country Link
US (1) US4256277A (fr)
JP (1) JPS5539895A (fr)
FR (1) FR2436074A1 (fr)
GB (1) GB2031356B (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0818387A1 (fr) * 1995-05-15 1998-01-14 The Boeing Company Système de détection de désalignement et de perte d'une surface hypersustentatrice individuelle

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4317681A (en) * 1980-11-07 1982-03-02 Johnson & Johnson Modifiers for ion-leachable cement compositions
NL8200197A (nl) * 1982-01-20 1983-08-16 Fokker Bv Vleugelklepconstructie en vliegtuig, voorzien van zulk een constructie.
US4441675A (en) * 1982-06-25 1984-04-10 Mcdonnell Douglas Corporation High lift surface actuation system
US4688744A (en) * 1982-09-03 1987-08-25 Sundstrand Corporation Jam tolerant rotary actuation system
US4575027A (en) * 1983-05-16 1986-03-11 Lockheed Corporation Electromechanical actuator system with anti-jamming features
JPS61502882A (ja) * 1984-08-01 1986-12-11 サンドストランド・コ−ポレ−ション 多段機関飛行機に対するスラスト操作装置
US4779822A (en) * 1986-05-23 1988-10-25 Sundstrand Corporation Actuator system
US4762205A (en) * 1987-05-20 1988-08-09 Simmonds Precision Flight control surface actuator for aircraft including remote braking failure detection
US4779820A (en) * 1987-11-02 1988-10-25 The Boeing Company Flexible control surface drive for folding wing aircraft
US4971267A (en) * 1989-02-13 1990-11-20 Allied-Signal Inc. Multi-fuseable shaft
US5351004A (en) * 1991-10-15 1994-09-27 Eldec Corporation Saturable core proximity sensor including a flux director and a magnetic target element
US5285154A (en) * 1991-10-15 1994-02-08 Eldec Corporation Saturable core proximity sensor aligned perpendicular to a magnet target having a plate and a non-magnetic metal housing
US5414878A (en) * 1993-11-03 1995-05-16 Sanijet Corporation Sanitary whirlpool jet apparatus
US5628477A (en) * 1995-02-13 1997-05-13 The Boeing Company Auxiliary airfoil lost motion detector and actuator
US5680124A (en) * 1995-05-15 1997-10-21 The Boeing Company Skew and loss detection system for adjacent high lift devices
US5743490A (en) * 1996-02-16 1998-04-28 Sundstrand Corporation Flap/slat actuation system for an aircraft
US6299108B1 (en) 1997-12-12 2001-10-09 Jeffrey V. Lindstrom Method and apparatus for detecting skew and asymmetry of an airplane flap
US6382566B1 (en) 1998-12-29 2002-05-07 The Boeing Company Method and apparatus for detecting skew and asymmetry of an airplane flap
US6483436B1 (en) * 2001-05-21 2002-11-19 Hamilton Sundstrand Corporation Method and apparatus for sensing skews and disconnects of adjacent movable components
US6923206B2 (en) * 2002-10-28 2005-08-02 Brass Craft Manufacturing Company Excess flow valve with magnet
DE10326799B3 (de) * 2003-06-13 2004-12-16 Airbus Deutschland Gmbh Vorrichtung zur Betätigung von Klappenelementen an den Tragflächen eines Flugzeuges
DE10361891A1 (de) * 2003-12-23 2005-08-04 Airbus Deutschland Gmbh Vorrichtung zur Ansteuerung und Verstellung von Klappen an Flugzeugtragflächen
FR2872483B1 (fr) * 2004-06-30 2007-10-12 Ratier Figeac Soc Dispositif de detection de defaillance de la voie principale de transmission d'effort pour actionneurs de commande de vol a double voie de transmission d'effort
FR2872783B1 (fr) * 2004-07-09 2007-11-30 Mbda France Sa Dispositif de gouverne aerodynamique a moteur deporte
FR2874982B1 (fr) * 2004-09-09 2008-02-01 Goodrich Actuation Systems Soc Dispositif de freinage anti-retour a detection de defaillance
US7574756B2 (en) * 2004-09-24 2009-08-18 Vu Tran Re-circulating multiple directional whirlpool jet
DE102005059369B4 (de) * 2005-12-13 2012-06-14 Airbus Operations Gmbh Verfahren und Einrichtung zur automatischen Entlastung eines Hochauftriebsflächensystems, insbesondere eines Landeklappensystems, eines Flugzeugs
DE102008018362A1 (de) * 2008-04-11 2009-10-15 Liebherr-Aerospace Lindenberg Gmbh Drehmomentsensor
US8281678B2 (en) 2008-12-30 2012-10-09 Eaton Corporation Ballscrew assembly with detection feature
DE102009020840A1 (de) * 2009-05-12 2010-11-25 Liebherr-Aerospace Lindenberg Gmbh Flugzeughochauftriebssystem sowie Verfahren zur Ermittlung eines Betriebszustandes eines Flugzeughochauftriebssystems
US10065728B2 (en) 2011-06-30 2018-09-04 Parker-Hannifin Corporation Horizontal stabilizer trim actuator failure detection system and method using position sensors
FR3016607B1 (fr) * 2014-01-20 2016-01-22 Sagem Defense Securite Actionneur de commande d'un plan horizontal de stabilisation d'un aeronef
CN105270606B (zh) * 2015-10-10 2017-06-06 中航飞机股份有限公司西安飞机分公司 一种飞机双套硬式操纵系统
US10933978B2 (en) 2017-01-10 2021-03-02 Parker-Hannifin Corporation Moving end electronic detection of secondary load path engagement of aircraft flight control actuator
EP3613666B1 (fr) 2018-08-20 2021-06-30 Goodrich Actuation Systems Limited Système actionneur

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2253665A1 (fr) * 1973-12-11 1975-07-04 Lucas Industries Ltd
US3935754A (en) * 1974-06-14 1976-02-03 The Boeing Company Failure detector and indicator for aircraft flap actuation system
US3986689A (en) * 1973-12-11 1976-10-19 Lucas Industries Limited Drive arrangements for aircraft control surfaces

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL254347A (fr) * 1959-09-23
GB1400449A (en) * 1971-09-23 1975-07-16 Lucas Industries Ltd Actuating arrangements for aircraft control surfaces
JPS5240276A (en) * 1975-09-26 1977-03-29 Mitsubishi Heavy Ind Ltd Fluid pressure type actuator
US4040272A (en) * 1976-01-26 1977-08-09 Eaton Corporation Flexible drive for rotating a fan

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2253665A1 (fr) * 1973-12-11 1975-07-04 Lucas Industries Ltd
US3986689A (en) * 1973-12-11 1976-10-19 Lucas Industries Limited Drive arrangements for aircraft control surfaces
US3935754A (en) * 1974-06-14 1976-02-03 The Boeing Company Failure detector and indicator for aircraft flap actuation system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0818387A1 (fr) * 1995-05-15 1998-01-14 The Boeing Company Système de détection de désalignement et de perte d'une surface hypersustentatrice individuelle

Also Published As

Publication number Publication date
JPH0146359B2 (fr) 1989-10-06
GB2031356B (en) 1982-08-11
US4256277A (en) 1981-03-17
JPS5539895A (en) 1980-03-21
FR2436074B1 (fr) 1983-04-15
GB2031356A (en) 1980-04-23

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