FR3016607B1 - Actionneur de commande d'un plan horizontal de stabilisation d'un aeronef - Google Patents
Actionneur de commande d'un plan horizontal de stabilisation d'un aeronefInfo
- Publication number
- FR3016607B1 FR3016607B1 FR1450421A FR1450421A FR3016607B1 FR 3016607 B1 FR3016607 B1 FR 3016607B1 FR 1450421 A FR1450421 A FR 1450421A FR 1450421 A FR1450421 A FR 1450421A FR 3016607 B1 FR3016607 B1 FR 3016607B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- actuator
- controlling
- horizontal stabilization
- stabilization plan
- 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
Links
- 230000006641 stabilisation Effects 0.000 title 1
- 238000011105 stabilization Methods 0.000 title 1
Classifications
-
- 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
- B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
- B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
- B64C13/341—Transmitting means without power amplification or where power amplification is irrelevant mechanical having duplication or stand-by provisions
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/10—Stabilising surfaces adjustable
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H25/00—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
- F16H25/18—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
- F16H25/20—Screw mechanisms
- F16H25/205—Screw mechanisms comprising alternate power paths, e.g. for fail safe back-up
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H25/00—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
- F16H25/18—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
- F16H25/20—Screw mechanisms
- F16H25/24—Elements essential to such mechanisms, e.g. screws, nuts
- F16H25/2472—Safety nuts
-
- 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
- G01D5/14—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 influencing the magnitude of a current or voltage
- G01D5/142—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 influencing the magnitude of a current or voltage using Hall-effect devices
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Transmission Devices (AREA)
- Vehicle Body Suspensions (AREA)
- Fluid Mechanics (AREA)
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1450421A FR3016607B1 (fr) | 2014-01-20 | 2014-01-20 | Actionneur de commande d'un plan horizontal de stabilisation d'un aeronef |
| CN201580009903.9A CN106458315B (zh) | 2014-01-20 | 2015-01-20 | 用于对飞行器的水平稳定器进行控制的致动器 |
| PCT/EP2015/050945 WO2015107208A2 (fr) | 2014-01-20 | 2015-01-20 | Actionneur de commande d'un plan horizontal de stabilisation d'un aeronef |
| US15/112,668 US10040539B2 (en) | 2014-01-20 | 2015-01-20 | Actuator for controlling a horizontal stabilizer of an aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1450421A FR3016607B1 (fr) | 2014-01-20 | 2014-01-20 | Actionneur de commande d'un plan horizontal de stabilisation d'un aeronef |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR3016607A1 FR3016607A1 (fr) | 2015-07-24 |
| FR3016607B1 true FR3016607B1 (fr) | 2016-01-22 |
Family
ID=50489319
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR1450421A Active FR3016607B1 (fr) | 2014-01-20 | 2014-01-20 | Actionneur de commande d'un plan horizontal de stabilisation d'un aeronef |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US10040539B2 (fr) |
| CN (1) | CN106458315B (fr) |
| FR (1) | FR3016607B1 (fr) |
| WO (1) | WO2015107208A2 (fr) |
Families Citing this family (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3016607B1 (fr) * | 2014-01-20 | 2016-01-22 | Sagem Defense Securite | Actionneur de commande d'un plan horizontal de stabilisation d'un aeronef |
| EP3072808B1 (fr) * | 2015-03-26 | 2017-10-25 | Goodrich Actuation Systems SAS | Fixation supérieure pour actionneur de stabilisateur horizontal compensable |
| FR3044635B1 (fr) * | 2015-12-04 | 2018-08-17 | Ratier Figeac | Butee d'absorption d'energie de fin de course d'actionneur d'aeronef a portee destructible demontable, actionneur et aeronef |
| US10822074B2 (en) * | 2016-04-29 | 2020-11-03 | Parker-Hannifin Corporation | Aircraft actuator with no-back, load detent assembly |
| US10483880B2 (en) | 2016-10-10 | 2019-11-19 | The Boeing Company | Multiple electromechanical actuator control system |
| DE202016006848U1 (de) * | 2016-11-07 | 2018-02-21 | Liebherr-Aerospace Lindenberg Gmbh | Spindelmuttereinheit zum Antreiben eines Hochauftriebssystems eines Fluggeräts |
| EP3330144B1 (fr) * | 2016-12-02 | 2021-07-14 | Ratier-Figeac SAS | Pompe à vis |
| US10974846B2 (en) * | 2016-12-09 | 2021-04-13 | Parker-Hannifin Corporation | Fixed end electronic detection of secondary load path engagement of aircraft flight control actuator |
| US11175115B2 (en) * | 2017-01-05 | 2021-11-16 | Bae Systems Information And Electronic Systems Integration Inc. | Determination of guided-munition roll orientation |
| 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 |
| US10837531B2 (en) * | 2017-10-24 | 2020-11-17 | Eaton Intelligent Power Limited | Actuator |
| US11066152B2 (en) * | 2018-05-25 | 2021-07-20 | The Boeing Company | Slotted entry gimbal |
| TR201808777A2 (tr) * | 2018-06-20 | 2018-07-23 | Tirsan Kardan Sanayi Ve Ticaret Anonim Sirketi | Kardan mi̇lleri̇nde devi̇r tespi̇ti̇ i̇çi̇n bi̇r si̇stem, i̇lgi̇li̇ si̇steme hai̇z bi̇r kardan mi̇li̇ ve tespi̇t yöntemi̇ |
| US11628926B2 (en) | 2018-08-02 | 2023-04-18 | Parker-Hannifin Corporation | LVDT-based actuator output load limited |
| EP3751172B1 (fr) * | 2019-06-14 | 2023-03-01 | Goodrich Actuation Systems SAS | Actionneur vis écrou et méthode de fabrication correspondante |
| US11873092B2 (en) | 2020-12-16 | 2024-01-16 | The Boeing Company | Trim actuators for horizontal stabilizers and methods of controlling horizontal stabilizers |
| BR112023020792A2 (pt) | 2021-04-07 | 2023-12-12 | Skyryse Inc | Atuador eletromecânico com mecanismo de falha operacional integrado |
| US11454305B1 (en) * | 2021-06-11 | 2022-09-27 | Whippany Actuation Systems Llc | Jam free linear actuation system implementing a mechanical disengagement mechanism and process thereof |
| US12454966B2 (en) * | 2023-07-27 | 2025-10-28 | Goodrich Actuation Systems Limited | Hydraulic rotary gearless actuator |
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| EP2891827B1 (fr) * | 2013-08-12 | 2019-06-19 | Airbus Defence and Space GmbH | Dispositif de découplage à actionnement électromécanique pour actionneurs |
| JP6148961B2 (ja) * | 2013-10-08 | 2017-06-14 | ナブテスコ株式会社 | 電動アクチュエータ |
| EP3078101B1 (fr) * | 2013-12-05 | 2018-07-11 | Safran Electronics & Defense | Actionneur electrique a moyens manuels d'entrainement |
| FR3016607B1 (fr) * | 2014-01-20 | 2016-01-22 | Sagem Defense Securite | Actionneur de commande d'un plan horizontal de stabilisation d'un aeronef |
| EP2902314B1 (fr) * | 2014-01-29 | 2017-07-19 | Airbus Operations GmbH | Système hypersustentateur pour avion et avion muni d'un tel système hypersustentateur |
| WO2015138687A1 (fr) * | 2014-03-13 | 2015-09-17 | Moog Inc. | Mécanisme de retenue et de libération d'ailette |
| US9797490B2 (en) * | 2014-03-27 | 2017-10-24 | Lcdrives Corp. | High reliability actuator |
| US9765867B2 (en) * | 2014-04-23 | 2017-09-19 | Nabtesco Corporation | Electromechanical actuator |
| US20160025199A1 (en) * | 2014-07-25 | 2016-01-28 | Triumph Actuation Systems - Connecticut, LLC, d/b/a Triumph Aerospace Systems - Seattle | Ball screw actuator with internal locking |
| CA2919342C (fr) * | 2015-04-15 | 2023-08-15 | Goodrich Actuation Systems Sas | Dispositif de verification destine a un dispositif de detection de defaillance de chemin de charge primaire d'actionneur |
| US10041481B2 (en) * | 2016-01-22 | 2018-08-07 | Marotta Controls, Inc. | Actuation mechanism and associated methods |
-
2014
- 2014-01-20 FR FR1450421A patent/FR3016607B1/fr active Active
-
2015
- 2015-01-20 WO PCT/EP2015/050945 patent/WO2015107208A2/fr not_active Ceased
- 2015-01-20 US US15/112,668 patent/US10040539B2/en active Active
- 2015-01-20 CN CN201580009903.9A patent/CN106458315B/zh active Active
Also Published As
| Publication number | Publication date |
|---|---|
| WO2015107208A3 (fr) | 2015-09-11 |
| FR3016607A1 (fr) | 2015-07-24 |
| CN106458315B (zh) | 2018-02-02 |
| US10040539B2 (en) | 2018-08-07 |
| CN106458315A (zh) | 2017-02-22 |
| WO2015107208A2 (fr) | 2015-07-23 |
| US20160340026A1 (en) | 2016-11-24 |
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