FR3061134B1 - ACTUATOR FOR AIRCRAFT ELEMENT - Google Patents

ACTUATOR FOR AIRCRAFT ELEMENT 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
French (fr)
Other versions
FR3061134A1 (en
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/en
Application granted granted Critical
Publication of FR3061134B1 publication Critical patent/FR3061134B1/en
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)
  • Transmission Devices (AREA)
  • Retarders (AREA)

Abstract

L'invention concerne un actionneur pour actionner un dispositif d'un aéronef, en particulier un avion, avec au moins un capteur fonctionnant sans contact, dans lequel le capteur est agencé dans le chemin de charge de l'actionneur et au moins deux capteurs sans contact sont prévus, dont l'un est agencé en dehors du chemin de charge de l'actionneur. L'invention concerne en outre un aéronef configuré avec un actionneur correspondant.The invention relates to an actuator for actuating a device of an aircraft, in particular an airplane, with at least one sensor operating without contact, in which the sensor is arranged in the load path of the actuator and at least two sensors without contact. contact are provided, one of which is arranged outside the actuator charging path. The invention further relates to an aircraft configured with a corresponding actuator.

FR1763225A 2016-12-22 2017-12-26 ACTUATOR FOR AIRCRAFT ELEMENT Active FR3061134B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102016015382.2 2016-12-22
DE102016015382.2A DE102016015382A1 (en) 2016-12-22 2016-12-22 Actuator for actuating a device of an aircraft

Publications (2)

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

Family

ID=62509766

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1763225A Active FR3061134B1 (en) 2016-12-22 2017-12-26 ACTUATOR FOR AIRCRAFT ELEMENT

Country Status (4)

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

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 (en) 2022-04-13 2023-10-19 Liebherr-Aerospace Lindenberg Gmbh Measuring system, linear motion element and aircraft

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 (en) * 2001-01-23 2002-07-31 Sumitomo Metal Mining Co Ltd Noncontact magnetic measuring instrument
FR2920744B1 (en) * 2007-09-07 2010-04-09 Eurocopter France COMPENSATION JACK FOR FLIGHT CONTROL
CA2732671C (en) * 2008-08-04 2015-07-14 Bell Helicopter Textron, Inc. Force gradient using a non-contact proximity sensor
DE102008052754A1 (en) * 2008-10-22 2010-05-06 Airbus Deutschland Gmbh Adjustment device for coupling to an adjustment flap of an aircraft, fault-tolerant positioning system and method for reconfiguring a positioning system
DE102009009189B4 (en) * 2009-02-16 2011-06-16 Airbus Operations Gmbh Sensor and sensor network for an aircraft
RU2426079C1 (en) * 2009-11-27 2011-08-10 Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) Method of pressure measurement
EP2385353A1 (en) * 2010-05-04 2011-11-09 Wachendorff Automation GmbH & Co. KG Magnetic encoder, in particular for use in a measurement system for measuring the absolute position of a body which can be pushed or rotated relative to a reference body and measurement system
FR2970387B1 (en) * 2011-01-10 2013-12-13 Messier Bugatti ELECTROMECHANICAL ACTUATOR WITH DOUBLE EXCITATION.
EP2878938B1 (en) * 2013-11-27 2018-07-04 Ncte Ag Magnetostrictive sensor for actuators in aircraft
DE102014003157A1 (en) * 2014-03-03 2015-09-03 Liebherr-Aerospace Lindenberg Gmbh Electromechanical rotary actuator with unlocking
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
DE102016015382A1 (en) 2018-06-28
FR3061134A1 (en) 2018-06-29
CN108216592A (en) 2018-06-29
RU2757103C2 (en) 2021-10-11
RU2017145080A (en) 2019-06-21
CN108216592B (en) 2023-04-14
RU2017145080A3 (en) 2021-03-15

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