FR3061134B1 - Actionneur pour element d'aeronef - Google Patents

Actionneur pour element d'aeronef Download PDF

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Publication number
FR3061134B1
FR3061134B1 FR1763225A FR1763225A FR3061134B1 FR 3061134 B1 FR3061134 B1 FR 3061134B1 FR 1763225 A FR1763225 A FR 1763225A FR 1763225 A FR1763225 A FR 1763225A FR 3061134 B1 FR3061134 B1 FR 3061134B1
Authority
FR
France
Prior art keywords
actuator
contact
aircraft
aircraft element
sensor
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
FR1763225A
Other languages
English (en)
French (fr)
Other versions
FR3061134A1 (fr
Inventor
Andre Dorkel
Nikolaus Dreyer
Thomas Schlegel
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.)
Liebherr Aerospace Lindenberg GmbH
Original Assignee
Liebherr Aerospace Lindenberg GmbH
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 Liebherr Aerospace Lindenberg GmbH filed Critical Liebherr Aerospace Lindenberg GmbH
Publication of FR3061134A1 publication Critical patent/FR3061134A1/fr
Application granted granted Critical
Publication of FR3061134B1 publication Critical patent/FR3061134B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/18—Operating mechanisms
    • B64C25/26—Control or locking systems therefor
    • 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
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/18—Operating mechanisms
    • 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
    • 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
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/60—Testing or inspecting aircraft components or systems
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D3/00—Indicating or recording apparatus with provision for the special purposes referred to in the subgroups
    • G01D3/028—Indicating or recording apparatus with provision for the special purposes referred to in the subgroups mitigating undesired influences, e.g. temperature, pressure
    • G01D3/036—Indicating or recording apparatus with provision for the special purposes referred to in the subgroups mitigating undesired influences, e.g. temperature, pressure on measuring arrangements themselves
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D5/00—Mechanical means for transferring the output of a sensing member; Means for converting the output of a sensing member to another variable where the form or nature of the sensing member does not constrain the means for converting; Transducers not specially adapted for a specific variable
    • G01D5/12—Mechanical means for transferring the output of a sensing member; Means for converting the output of a sensing member to another variable where the form or nature of the sensing member does not constrain the means for converting; Transducers not specially adapted for a specific variable using electric or magnetic means
    • 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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L3/00—Measuring torque, work, mechanical power, or mechanical efficiency, in general

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Force Measurement Appropriate To Specific Purposes (AREA)
  • Actuator (AREA)
  • Retarders (AREA)
  • Transmission Devices (AREA)
FR1763225A 2016-12-22 2017-12-26 Actionneur pour element d'aeronef Active FR3061134B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102016015382.2A DE102016015382A1 (de) 2016-12-22 2016-12-22 Aktuator zum Betätigen einer Einrichtung eines Fluggeräts
DE102016015382.2 2016-12-22

Publications (2)

Publication Number Publication Date
FR3061134A1 FR3061134A1 (fr) 2018-06-29
FR3061134B1 true FR3061134B1 (fr) 2021-09-24

Family

ID=62509766

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1763225A Active FR3061134B1 (fr) 2016-12-22 2017-12-26 Actionneur pour element d'aeronef

Country Status (4)

Country Link
CN (1) CN108216592B (zh)
DE (1) DE102016015382A1 (zh)
FR (1) FR3061134B1 (zh)
RU (1) RU2757103C2 (zh)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11485476B2 (en) 2019-10-25 2022-11-01 Hamilton Sundstrand Corporation Driveline torque monitoring for long-term health assessment
DE102022109015A1 (de) 2022-04-13 2023-10-19 Liebherr-Aerospace Lindenberg Gmbh Messsystem, Linearbewegungselement und Luftfahrzeug

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4474060A (en) * 1982-07-12 1984-10-02 Goodyear Aerospace Corporation Torque readout sensor
JP2002213992A (ja) * 2001-01-23 2002-07-31 Sumitomo Metal Mining Co Ltd 非接触磁気式計測装置
FR2920744B1 (fr) * 2007-09-07 2010-04-09 Eurocopter France Verin de compensation pour commande de vol de giravion
CA2732671C (en) * 2008-08-04 2015-07-14 Bell Helicopter Textron, Inc. Force gradient using a non-contact proximity sensor
DE102008052754A1 (de) * 2008-10-22 2010-05-06 Airbus Deutschland Gmbh Verstellvorrichtung zur Ankopplung an eine Verstellklappe eines Flugzeugs, fehlertolerantes Stellsystem und Verfahren zur Rekonfiguration eines Stellsystems
DE102009009189B4 (de) * 2009-02-16 2011-06-16 Airbus Operations Gmbh Sensor und Sensornetzwerk für ein Luftfahrzeug
RU2426079C1 (ru) * 2009-11-27 2011-08-10 Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) Способ измерения давления
EP2385353A1 (de) * 2010-05-04 2011-11-09 Wachendorff Automation GmbH & Co. KG Magnetischer Encoder, insbesondere zur Verwendung in einem Messsystem zur Messung der Absolut-Position eines gegenüber einem Referenzkörper verschiebbaren oder verdrehbaren Körpers, und Messsystem
FR2970387B1 (fr) * 2011-01-10 2013-12-13 Messier Bugatti Actionneur electromecanique a double excitation.
EP2878938B1 (de) * 2013-11-27 2018-07-04 Ncte Ag Magnetostriktiver Sensor für Aktuatoren in Flugzeugen
DE102014003157A1 (de) * 2014-03-03 2015-09-03 Liebherr-Aerospace Lindenberg Gmbh Elektromechanischer Rotationsaktuator mit Entriegelung
US10093435B2 (en) * 2015-05-19 2018-10-09 Embraer S.A. Integrated system and methods for management and monitoring of vehicles

Also Published As

Publication number Publication date
CN108216592B (zh) 2023-04-14
DE102016015382A1 (de) 2018-06-28
CN108216592A (zh) 2018-06-29
RU2017145080A (ru) 2019-06-21
FR3061134A1 (fr) 2018-06-29
RU2017145080A3 (zh) 2021-03-15
RU2757103C2 (ru) 2021-10-11

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