CA2883179A1 - Control surface actuation assembly - Google Patents
Control surface actuation assembly Download PDFInfo
- Publication number
- CA2883179A1 CA2883179A1 CA2883179A CA2883179A CA2883179A1 CA 2883179 A1 CA2883179 A1 CA 2883179A1 CA 2883179 A CA2883179 A CA 2883179A CA 2883179 A CA2883179 A CA 2883179A CA 2883179 A1 CA2883179 A1 CA 2883179A1
- Authority
- CA
- Canada
- Prior art keywords
- control surface
- actuator
- aircraft
- assembly
- mode
- 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.)
- Abandoned
Links
- 238000013016 damping Methods 0.000 claims abstract description 43
- 230000033001 locomotion Effects 0.000 claims description 29
- 230000000694 effects Effects 0.000 claims description 7
- 230000015572 biosynthetic process Effects 0.000 claims description 6
- 238000010998 test method Methods 0.000 claims description 4
- 230000001419 dependent effect Effects 0.000 claims description 3
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 11
- 230000000712 assembly Effects 0.000 description 6
- 238000000429 assembly Methods 0.000 description 6
- 150000001875 compounds Chemical class 0.000 description 6
- 238000005755 formation reaction Methods 0.000 description 5
- 238000012360 testing method Methods 0.000 description 4
- 238000012545 processing Methods 0.000 description 3
- 230000003068 static effect Effects 0.000 description 3
- 238000013459 approach Methods 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 230000007257 malfunction Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 125000006850 spacer group Chemical group 0.000 description 2
- 238000004804 winding Methods 0.000 description 2
- 230000004323 axial length Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000356 contaminant Substances 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000010006 flight Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000004806 packaging method and process Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 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
- B64C13/38—Transmitting means with power amplification
- B64C13/50—Transmitting means with power amplification using electrical energy
- B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
-
- 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
- B64C13/34—Transmitting means without power amplification or where power amplification is irrelevant mechanical using toothed gearing
-
- 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
- B64C13/38—Transmitting means with power amplification
- B64C13/50—Transmitting means with power amplification using electrical energy
-
- 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
- F16H1/00—Toothed gearings for conveying rotary motion
- F16H1/28—Toothed gearings for conveying rotary motion with gears having orbital motion
- F16H1/46—Systems consisting of a plurality of gear trains each with orbital gears, i.e. systems having three or more central gears
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M17/00—Testing of vehicles
- G01M17/007—Wheeled or endless-tracked vehicles
- G01M17/04—Suspension or damping
-
- 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
- F16H1/00—Toothed gearings for conveying rotary motion
- F16H1/28—Toothed gearings for conveying rotary motion with gears having orbital motion
- F16H2001/2872—Toothed gearings for conveying rotary motion with gears having orbital motion comprising three central gears, i.e. ring or sun gear, engaged by at least one common orbital gear mounted on an idling carrier
-
- 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
- F16H1/00—Toothed gearings for conveying rotary motion
- F16H1/28—Toothed gearings for conveying rotary motion with gears having orbital motion
- F16H2001/2881—Toothed gearings for conveying rotary motion with gears having orbital motion comprising two axially spaced central gears, i.e. ring or sun gear, engaged by at least one common orbital gear wherein one of the central gears is forming the output
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Retarders (AREA)
- Transmission Devices (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GBGB1214952.2A GB201214952D0 (en) | 2012-08-22 | 2012-08-22 | Control surface actuation assembly |
| GB1214952.2 | 2012-08-22 | ||
| PCT/GB2013/052144 WO2014029972A1 (en) | 2012-08-22 | 2013-08-12 | Control surface actuation assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA2883179A1 true CA2883179A1 (en) | 2014-02-27 |
Family
ID=47017137
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2883179A Abandoned CA2883179A1 (en) | 2012-08-22 | 2013-08-12 | Control surface actuation assembly |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US20150217855A1 (enExample) |
| EP (2) | EP3144220B1 (enExample) |
| JP (1) | JP2015527247A (enExample) |
| CN (2) | CN106394872B (enExample) |
| BR (1) | BR112015002453A2 (enExample) |
| CA (1) | CA2883179A1 (enExample) |
| GB (1) | GB201214952D0 (enExample) |
| WO (1) | WO2014029972A1 (enExample) |
Families Citing this family (28)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9593696B2 (en) | 2013-02-27 | 2017-03-14 | Woodward, Inc. | Rotary piston type actuator with hydraulic supply |
| US9163648B2 (en) | 2013-02-27 | 2015-10-20 | Woodward, Inc. | Rotary piston type actuator with a central actuation assembly |
| US8955425B2 (en) | 2013-02-27 | 2015-02-17 | Woodward, Inc. | Rotary piston type actuator with pin retention features |
| US9631645B2 (en) | 2013-02-27 | 2017-04-25 | Woodward, Inc. | Rotary piston actuator anti-rotation configurations |
| US9816537B2 (en) | 2013-02-27 | 2017-11-14 | Woodward, Inc. | Rotary piston type actuator with a central actuation assembly |
| US9476434B2 (en) | 2013-02-27 | 2016-10-25 | Woodward, Inc. | Rotary piston type actuator with modular housing |
| US9234535B2 (en) | 2013-02-27 | 2016-01-12 | Woodward, Inc. | Rotary piston type actuator |
| US10174818B2 (en) * | 2014-01-30 | 2019-01-08 | Genesis Advanced Technology Inc. | Roller drive |
| US9643716B2 (en) * | 2014-04-01 | 2017-05-09 | The Boeing Company | Air vehicle, actuator assembly and associated method of manufacture |
| US10759515B2 (en) | 2014-09-10 | 2020-09-01 | Hamilton Sunstrand Corporation | Electromechanical hinge-line rotary actuator |
| US20160229525A1 (en) * | 2014-09-10 | 2016-08-11 | Hamilton Sundstrand Corporation | Electromechanical rotary actuator |
| US9751617B2 (en) * | 2014-12-02 | 2017-09-05 | Hamilton Sundstrand Corporation | Multi-slice rotary electromechanical actuator |
| CN105775163B (zh) * | 2016-05-06 | 2017-10-13 | 江西昌河航空工业有限公司 | 一种飞机襟翼运动的测试模拟装置 |
| US10088006B2 (en) * | 2016-05-19 | 2018-10-02 | The Boeing Company | Rotational inerter and method for damping an actuator |
| FR3061135B1 (fr) * | 2016-12-23 | 2019-05-24 | Safran Electronics & Defense | Surface mobile de vol ayant au moins un actionneur integre |
| FR3067155B1 (fr) * | 2017-06-01 | 2022-01-28 | Thales Sa | Dispositif de securisation des mouvements electriques de plateformes mobiles pour simulateurs |
| CA3016400A1 (en) * | 2017-09-08 | 2019-03-08 | Hamilton Sundstrand Corporation | Electromechanical hinge-line rotary actuator |
| JP6706235B2 (ja) | 2017-11-02 | 2020-06-03 | 株式会社Ｓｕｂａｒｕ | 航空機の制御システム、航空機の制御方法及び航空機 |
| WO2019139654A1 (en) * | 2018-01-11 | 2019-07-18 | The Boeing Company | Dual rack and pinion rotational inerter system and method for damping movement of a flight control surface of an aircraft |
| CN109018303B (zh) * | 2018-08-14 | 2020-05-19 | 晨龙飞机（荆门）有限公司 | 一种可快速上仰和下俯的飞机平尾翼 |
| CN109018305B (zh) * | 2018-08-15 | 2020-08-11 | 晨龙飞机（荆门）有限公司 | 一种迅速调转飞机飞行方向的方向舵 |
| EP3653494A1 (en) * | 2018-11-16 | 2020-05-20 | Bombardier Inc. | High-lift actuation system having independent actuation control |
| KR101989161B1 (ko) * | 2019-03-28 | 2019-06-14 | 주식회사 컨트로맥스 | 오작동을 방지하는 다중센서가 구비된 항공기용 전기식 구동장치 |
| GB201904972D0 (en) * | 2019-04-08 | 2019-05-22 | Involution Tech Limited | Rotary actuator |
| US11199248B2 (en) | 2019-04-30 | 2021-12-14 | Woodward, Inc. | Compact linear to rotary actuator |
| US12151803B2 (en) | 2019-05-22 | 2024-11-26 | Moog Inc. | Preloaded torque shaft and the flight control driveline made therewith |
| TR201913068A2 (tr) * | 2019-08-28 | 2021-03-22 | Tusas Tuerk Havacilik Ve Uzay Sanayii Anonim Sirketi | Bir hareketlendirici sistem. |
| EP4133186B1 (en) | 2020-04-08 | 2025-10-01 | Woodward, Inc. | Rotary piston type actuator with a central actuation assembly |
Family Cites Families (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6441498A (en) * | 1987-08-07 | 1989-02-13 | Teijin Seiki Co Ltd | Controller for rudder surface |
| US5120285A (en) * | 1990-10-01 | 1992-06-09 | Sundstrand Corporation | Jam tolerant geared rotary actuator for multiple actuator systems with a single prime mover |
| FR2778164B1 (fr) * | 1998-04-29 | 2000-06-23 | Aerospatiale | Systeme de commande mixte pour surface aerodynamique d'aeronef |
| WO2000029286A1 (en) * | 1998-11-12 | 2000-05-25 | Coventry University | Geared rotary actuator |
| US7431676B2 (en) * | 2002-11-25 | 2008-10-07 | Delbert Tesar | Self-contained rotary actuator |
| US20040200928A1 (en) * | 2003-04-14 | 2004-10-14 | Arthur Degenholtz | Actuator and flap arrangement with actuator interconnection |
| US7100870B2 (en) * | 2003-10-15 | 2006-09-05 | Parker-Hannifin Corporation | Jam tolerant electromechanical actuation systems and methods of operation |
| WO2008112363A2 (en) * | 2007-02-07 | 2008-09-18 | Parker Hannifin Corporation | Electromechanical actuating assembly |
| DE102007023394A1 (de) * | 2007-05-18 | 2008-11-20 | Airbus Deutschland Gmbh | Verfahren und Einrichtung zur Fehlerdetektierung im Lastpfad eines Spindelaktuators |
| US20090031488A1 (en) * | 2007-07-31 | 2009-02-05 | Tsai-Hui Hsieh | Flush valve assembly |
| DE102008022092A1 (de) * | 2008-05-05 | 2009-11-19 | Airbus Deutschland Gmbh | Fehlertolerantes Stellsystem zur Verstellung von Klappen eines Flugzeugs mit einer Verstell-Kinematik mit feststehender Drehachse |
| DE102010021576A1 (de) * | 2010-05-26 | 2011-12-01 | Airbus Operations Gmbh | Vorrichtung für eine Stellklappe eines Tragflügels |
| DE102010025475A1 (de) * | 2010-06-29 | 2011-12-29 | Airbus Operations Gmbh | Stellsystem eines Flugzeugs mit einer Stellklappe |
| US9190942B2 (en) * | 2010-07-22 | 2015-11-17 | Parker-Hannifin Corporation | Near synchronous controlled induction motor drive actuation system |
| CN202140375U (zh) * | 2011-06-29 | 2012-02-08 | 南京王行航空附件维修工程有限公司 | 飞机伺服阀、舵机、刹车活门综合试验台 |
| KR101842235B1 (ko) * | 2012-02-09 | 2018-03-27 | 무그 인코포레이티드 | 액츄에이터 시스템 및 방법 |
| DE102013013340B4 (de) * | 2013-08-09 | 2023-08-10 | Liebherr-Aerospace Lindenberg Gmbh | Klappensystem für ein Flugzeughochauftriebsystem oder eine Triebwerksaktuation und Verfahren zur Überwachung eines Klappensystems |
| US9193440B2 (en) * | 2013-09-24 | 2015-11-24 | The Boeing Company | Variable camber flap system and method |
-
2012
- 2012-08-22 GB GBGB1214952.2A patent/GB201214952D0/en not_active Ceased
-
2013
- 2013-08-12 EP EP16187065.4A patent/EP3144220B1/en active Active
- 2013-08-12 JP JP2015527963A patent/JP2015527247A/ja not_active Ceased
- 2013-08-12 CN CN201610864433.0A patent/CN106394872B/zh not_active Expired - Fee Related
- 2013-08-12 CN CN201380043679.6A patent/CN104619590B/zh not_active Expired - Fee Related
- 2013-08-12 BR BR112015002453A patent/BR112015002453A2/pt not_active Application Discontinuation
- 2013-08-12 US US14/420,366 patent/US20150217855A1/en not_active Abandoned
- 2013-08-12 WO PCT/GB2013/052144 patent/WO2014029972A1/en not_active Ceased
- 2013-08-12 CA CA2883179A patent/CA2883179A1/en not_active Abandoned
- 2013-08-12 EP EP13750123.5A patent/EP2888163B1/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| US20150217855A1 (en) | 2015-08-06 |
| BR112015002453A2 (pt) | 2017-12-12 |
| CN106394872A (zh) | 2017-02-15 |
| CN106394872B (zh) | 2018-11-09 |
| EP2888163B1 (en) | 2017-11-08 |
| CN104619590B (zh) | 2017-03-15 |
| JP2015527247A (ja) | 2015-09-17 |
| GB201214952D0 (en) | 2012-10-03 |
| EP2888163A1 (en) | 2015-07-01 |
| WO2014029972A1 (en) | 2014-02-27 |
| EP3144220A1 (en) | 2017-03-22 |
| EP3144220B1 (en) | 2019-11-27 |
| CN104619590A (zh) | 2015-05-13 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request |
Effective date: 20180323 |
|
| FZDE | Discontinued |
Effective date: 20200831 |