JP4820366B2 - コンパクトアクチュエータ - Google Patents
コンパクトアクチュエータ Download PDFInfo
- Publication number
- JP4820366B2 JP4820366B2 JP2007527672A JP2007527672A JP4820366B2 JP 4820366 B2 JP4820366 B2 JP 4820366B2 JP 2007527672 A JP2007527672 A JP 2007527672A JP 2007527672 A JP2007527672 A JP 2007527672A JP 4820366 B2 JP4820366 B2 JP 4820366B2
- Authority
- JP
- Japan
- Prior art keywords
- pinion
- gear
- compact actuator
- reduction gear
- ring gear
- 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.)
- Expired - Fee Related
Links
Images
Classifications
-
- 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
- F16H1/2809—Toothed gearings for conveying rotary motion with gears having orbital motion with means for equalising the distribution of load on the planet gears
- F16H1/2836—Toothed gearings for conveying rotary motion with gears having orbital motion with means for equalising the distribution of load on the planet gears by allowing limited movement of the planet gears relative to the planet carrier or by using free floating planet gears
-
- 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
-
- 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)
- Transmission Devices (AREA)
- Retarders (AREA)
- Gears, Cams (AREA)
- General Details Of Gearings (AREA)
- Gear Transmission (AREA)
Description
Claims (6)
- 支持体(21)に装着され、長手方向軸(x−x)の周りに回転するリングギア(25)とサンギア(29)と該サンギアに噛み合う少なくとも一つの遊星ギア(30)とを有する減速ギアユニット(24)と、
前記リングギアに装着されたピニオン(26)と、
を有し、前記ピニオンは追加のベアリングを必要とせず、前記リングギア用のベアリングの全てが前記減速ギアユニット内に収められ、前記ピニオンは、その回転により翼面(27)を前記支持体に対して相対的に移動させるようにラックに動作結合されており、前記翼面(27)上に設けられたラック(23)を前記支持体に対して相対的に適宜移動させるコンパクトアクチュエータ(20)。 - 前記ピニオン(26)は、脱着可能に前記リングギアに装着された請求項1に記載のコンパクトアクチュエータ。
- 前記減速ギアユニット(24)の横断方向中心線(y−y)が、前記ピニオン(26)の横断方向中心線とほぼ整合している請求項1に記載のコンパクトアクチュエータ。
- 前記翼面(27)は、フラップあるいはスラットである請求項1に記載のコンパクトアクチュエータ。
- さらに前記サンギアを回転させる手段を有する請求項1に記載のコンパクトアクチュエータ。
- 前記減速ギアユニット内に動作的にモータが設けられ、該モータにより前記リングギアを適宜回転させるようなっている請求項1に記載のコンパクトアクチュエータ。
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/865,102 | 2004-06-10 | ||
| US10/865,102 US7101297B2 (en) | 2004-06-10 | 2004-06-10 | Compact actuator |
| PCT/US2005/020054 WO2005124192A2 (en) | 2004-06-10 | 2005-06-07 | Compact actuator |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JP2008502866A JP2008502866A (ja) | 2008-01-31 |
| JP4820366B2 true JP4820366B2 (ja) | 2011-11-24 |
Family
ID=35461233
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2007527672A Expired - Fee Related JP4820366B2 (ja) | 2004-06-10 | 2005-06-07 | コンパクトアクチュエータ |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US7101297B2 (ja) |
| EP (1) | EP1753979B1 (ja) |
| JP (1) | JP4820366B2 (ja) |
| CN (1) | CN100441920C (ja) |
| DE (1) | DE602005015844D1 (ja) |
| ES (1) | ES2329261T3 (ja) |
| WO (1) | WO2005124192A2 (ja) |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR100748656B1 (ko) * | 2005-12-01 | 2007-08-10 | 현대자동차주식회사 | 하이브리드 차량의 동력 전달 시스템 |
| FR2901591B1 (fr) * | 2006-05-24 | 2009-01-16 | Valeo Embrayages | Dispositif de reduction du type a trains epicycloidaux imbriques |
| US10400818B2 (en) | 2007-12-06 | 2019-09-03 | Roller Bearing Company Of America, Inc. | Track roller bearings with rolling elements or liners |
| GB0816022D0 (en) * | 2008-09-03 | 2008-10-08 | Airbus Uk Ltd | Slat support assembly |
| CN101988570B (zh) * | 2009-07-31 | 2014-08-20 | 中国商用飞机有限责任公司 | 用于飞机缝翼作动器的齿轮齿条的设计方法 |
| FR2952348B1 (fr) * | 2009-11-10 | 2012-03-09 | Airbus Operations Sas | Gouverne aerodynamique crocodile pour aeronef |
| KR101009742B1 (ko) | 2010-10-29 | 2011-01-19 | 주식회사 세진아이지비 | 동력전달장치 |
| GB201111922D0 (en) | 2011-07-12 | 2011-08-24 | Airbus Operations Ltd | Leading edge rib assembly |
| DE102014007266B4 (de) * | 2014-05-16 | 2024-08-01 | Liebherr-Aerospace Lindenberg Gmbh | Hochlast-Getriebe für einen Hochauftriebs-Träger, Hochauftriebs-Träger, sowie Klappeneinheit und Verfahren zur Montage von Klappen |
| FR3028836B1 (fr) * | 2014-11-20 | 2016-12-16 | Sagem Defense Securite | Actionneur de gouverne de commande de vol d'un aeronef |
| WO2015156705A2 (en) | 2015-05-06 | 2015-10-15 | Zakrytoe Aktsionernoe Obschestvo "Diakont" | Transmission gear, roller reducer comprising the transmission gear, and method of assembly thereof |
| CN112109878B (zh) * | 2020-08-23 | 2023-01-10 | 北京航空航天大学 | 一种适用于折叠变体机翼的折叠机构 |
Family Cites Families (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1586944A (en) * | 1922-05-23 | 1926-06-01 | Ruckstell Sales & Mfg Company | Planetary-gear mechanism |
| US1917428A (en) | 1927-12-17 | 1933-07-11 | Uppercu Burnelli Corp | Aircraft |
| GB718645A (en) * | 1951-05-16 | 1954-11-17 | Ciotat La | Improvements in or relating to transmission devices |
| US2959070A (en) * | 1959-01-09 | 1960-11-08 | Borg Warner | Accessory drive |
| US4043216A (en) * | 1974-10-11 | 1977-08-23 | Lucas Industries Limited | Compound pinions for use in epicyclic gear boxes |
| DE2847513A1 (de) * | 1978-11-02 | 1980-05-14 | Curtiss Wright Corp | Schwimmendes planetengetriebe |
| US4305488A (en) * | 1979-11-13 | 1981-12-15 | Borg-Warner Corporation | Accessory drive system |
| US4471928A (en) | 1980-08-13 | 1984-09-18 | The Boeing Company | Extendible airfoil track assembly |
| US4691584A (en) * | 1985-02-20 | 1987-09-08 | Ohi Seisakusho Co., Ltd. | Actuator for remote devices or the like |
| US4753402A (en) * | 1985-12-30 | 1988-06-28 | The Boeing Company | Biased leading edge slat apparatus |
| GB8711252D0 (en) * | 1987-05-13 | 1987-07-15 | British Aerospace | High lift device |
| US4995575A (en) | 1988-09-26 | 1991-02-26 | The Boeing Company | Wing trailing edge flap mechanism |
| DE4030489A1 (de) * | 1990-09-26 | 1992-04-02 | Man Ghh Logistics | Planetengetriebe |
| US5544847A (en) | 1993-11-10 | 1996-08-13 | The Boeing Company | Leading edge slat/wing combination |
| GB2304656B (en) | 1995-08-26 | 1999-10-13 | British Aerospace | Deployment mechanisms for aircraft auxiliary aerofoils |
| JPH11303977A (ja) * | 1998-04-22 | 1999-11-02 | Matex Kk | 遊星歯車装置のケーシング取付構造 |
| JP3888834B2 (ja) * | 2000-04-25 | 2007-03-07 | ダイハツ工業株式会社 | 車両用自動変速機 |
| JP2003166557A (ja) * | 2001-11-30 | 2003-06-13 | Exedy Corp | クラッチのアクチュエータ |
| ITPD20020223A1 (it) * | 2002-09-03 | 2004-03-04 | Carraro Spa | Riduttore epicloidale di tipo embricato. |
| US6783478B2 (en) * | 2002-09-13 | 2004-08-31 | Moog Inc. | Compound differential planetary gear assembly |
-
2004
- 2004-06-10 US US10/865,102 patent/US7101297B2/en not_active Expired - Lifetime
-
2005
- 2005-06-07 WO PCT/US2005/020054 patent/WO2005124192A2/en not_active Ceased
- 2005-06-07 ES ES05757487T patent/ES2329261T3/es not_active Expired - Lifetime
- 2005-06-07 EP EP05757487A patent/EP1753979B1/en not_active Expired - Lifetime
- 2005-06-07 CN CNB2005800188556A patent/CN100441920C/zh not_active Expired - Fee Related
- 2005-06-07 JP JP2007527672A patent/JP4820366B2/ja not_active Expired - Fee Related
- 2005-06-07 DE DE602005015844T patent/DE602005015844D1/de not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| ES2329261T3 (es) | 2009-11-24 |
| CN1965182A (zh) | 2007-05-16 |
| WO2005124192A2 (en) | 2005-12-29 |
| WO2005124192A3 (en) | 2006-06-01 |
| CN100441920C (zh) | 2008-12-10 |
| EP1753979B1 (en) | 2009-08-05 |
| WO2005124192B1 (en) | 2006-08-17 |
| US7101297B2 (en) | 2006-09-05 |
| US20050277513A1 (en) | 2005-12-15 |
| EP1753979A2 (en) | 2007-02-21 |
| EP1753979A4 (en) | 2007-12-26 |
| DE602005015844D1 (de) | 2009-09-17 |
| JP2008502866A (ja) | 2008-01-31 |
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