DE69739923D1 - Versetztes wechselgetriebe mit nicht rückwärtsgang - Google Patents
Versetztes wechselgetriebe mit nicht rückwärtsgangInfo
- Publication number
- DE69739923D1 DE69739923D1 DE69739923T DE69739923T DE69739923D1 DE 69739923 D1 DE69739923 D1 DE 69739923D1 DE 69739923 T DE69739923 T DE 69739923T DE 69739923 T DE69739923 T DE 69739923T DE 69739923 D1 DE69739923 D1 DE 69739923D1
- Authority
- DE
- Germany
- Prior art keywords
- reverse gear
- moved
- gear
- reverse
- moved reverse
- 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 - Lifetime
Links
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
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D9/00—Couplings with safety member for disconnecting, e.g. breaking or melting member
- F16D9/06—Couplings with safety member for disconnecting, e.g. breaking or melting member by breaking due to shear stress
- F16D9/08—Couplings with safety member for disconnecting, e.g. breaking or melting member by breaking due to shear stress over a single area encircling the axis of rotation, e.g. shear necks on shafts
-
- 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
- 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
-
- 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
- F16H35/00—Gearings or mechanisms with other special functional features
-
- 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
- B64D2045/001—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear for indicating symmetry of flaps deflection
-
- 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
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B2200/00—Constructional details of connections not covered for in other groups of this subclass
- F16B2200/63—Frangible connections
-
- 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
- F16H35/00—Gearings or mechanisms with other special functional features
- F16H2035/005—Gearings or mechanisms preventing back-driving
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- General Details Of Gearings (AREA)
- Retarders (AREA)
- Braking Arrangements (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US1792396P | 1996-05-15 | 1996-05-15 | |
PCT/US1997/008255 WO1997043557A1 (en) | 1996-05-15 | 1997-05-14 | No-back/offset gear box |
Publications (1)
Publication Number | Publication Date |
---|---|
DE69739923D1 true DE69739923D1 (de) | 2010-08-19 |
Family
ID=21785293
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69739923T Expired - Lifetime DE69739923D1 (de) | 1996-05-15 | 1997-05-14 | Versetztes wechselgetriebe mit nicht rückwärtsgang |
Country Status (4)
Country | Link |
---|---|
US (1) | US6231012B1 (de) |
EP (1) | EP0898661B1 (de) |
DE (1) | DE69739923D1 (de) |
WO (1) | WO1997043557A1 (de) |
Families Citing this family (33)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19724117A1 (de) * | 1997-06-09 | 1998-12-10 | Zf Luftfahrttechnik Gmbh | Bremse für einen Auftriebsklappenverstellmechanismus |
DE19754260A1 (de) * | 1997-12-06 | 1999-06-10 | Bosch Gmbh Robert | Sicherheitseinrichtung für ein Getriebe |
US5944148A (en) * | 1998-08-31 | 1999-08-31 | The Boeing Company | No-back brake |
US6659398B2 (en) * | 2000-09-08 | 2003-12-09 | Smiths Aerospace, Inc. | Two-brake torque limiting device |
US6672540B1 (en) | 2002-12-03 | 2004-01-06 | Rockwell Collins, Inc. | Actuator for aircraft stabilizers with a failure responsive lock control mechanism |
US6705570B1 (en) * | 2003-04-14 | 2004-03-16 | Curtiss-Wright Controls, Inc. | Arrangement and associated system having an actuator and a tubular flap-drive member about the actuator |
US7100870B2 (en) * | 2003-10-15 | 2006-09-05 | Parker-Hannifin Corporation | Jam tolerant electromechanical actuation systems and methods of operation |
DE102004047008A1 (de) * | 2004-09-28 | 2006-03-30 | Liebherr-Aerospace Lindenberg Gmbh | Vorrichtung zur Einstellung von Flugzeughöhenflossen |
US7603844B2 (en) * | 2005-10-19 | 2009-10-20 | General Electric Company | Gas turbine engine assembly and methods of assembling same |
GB0616730D0 (en) * | 2006-08-23 | 2006-10-04 | Airbus Uk Ltd | Jam-tolerant actuator |
US8230750B2 (en) * | 2006-09-01 | 2012-07-31 | Parker-Hannifin Corporation | Electromechanical actuating assembly |
US8136418B2 (en) * | 2007-02-07 | 2012-03-20 | Parker-Hannifin Corporation | Electromechanical actuating assembly |
US8312783B2 (en) * | 2007-02-16 | 2012-11-20 | Parker-Hannifin Corporation | Aircraft flight control actuation system with direct acting, force limiting, actuator |
JP2009024858A (ja) * | 2007-07-24 | 2009-02-05 | Yamaha Motor Co Ltd | 自動変速制御装置、自動変速制御装置を備えたパワーユニット、および、鞍乗型車両 |
US8336817B2 (en) | 2007-10-30 | 2012-12-25 | Parker-Hannifin Corporation | Jam tolerant electromechanical actuation systems and methods of operation |
US8336818B2 (en) * | 2007-10-30 | 2012-12-25 | Parker-Hannifin Corporation | Jam tolerant electromechanical actuation systems and methods of operation |
DE102007055669A1 (de) * | 2007-11-21 | 2009-06-04 | Airbus Deutschland Gmbh | Landeklappenkinematik angetrieben über Ritzelantrieb |
FR2953266B1 (fr) * | 2009-11-27 | 2011-11-11 | Airbus Operations Sas | Procede de surveillance d'un dispositif d'irreversibilite d'actionneur de plan horizontal reglable, systeme et aeronef correspondants |
US8262531B2 (en) * | 2009-12-17 | 2012-09-11 | Hamilton Sundstrand Corporation | Actuator with differential and brake |
DE102010047512A1 (de) * | 2010-10-05 | 2012-04-05 | Airbus Operations Gmbh | Hochauftriebssystem für ein Flugzeug mit zwei getrennten Antriebseinheiten |
GB201111922D0 (en) | 2011-07-12 | 2011-08-24 | Airbus Operations Ltd | Leading edge rib assembly |
US9261149B2 (en) * | 2012-03-07 | 2016-02-16 | Hamilton Sundstrand Corporation | No-back check device |
TW201405032A (zh) * | 2012-07-24 | 2014-02-01 | huang-xi Xu | 能使烤肉架間歇轉動的動力模組 |
DE102013000544A1 (de) * | 2013-01-15 | 2014-07-17 | Liebherr-Aerospace Lindenberg Gmbh | Rücklaufsperre |
WO2015166525A1 (ja) | 2014-04-28 | 2015-11-05 | 株式会社島津製作所 | トルク伝達機構 |
US9416832B1 (en) | 2015-02-02 | 2016-08-16 | The Boeing Company | Half system torque brakes |
US10072582B2 (en) | 2016-04-28 | 2018-09-11 | General Electric Company | Integral offset oil tank for inline accessory gearbox |
US10765575B2 (en) * | 2016-06-29 | 2020-09-08 | Stryker Corporation | Patient support systems with rotary actuators comprising rotation limiting devices |
US10813807B2 (en) * | 2016-06-29 | 2020-10-27 | Stryker Corporation | Patient support systems with hollow rotary actuators |
US10610429B2 (en) | 2016-06-29 | 2020-04-07 | Stryker Corporation | Rotary actuator having clutch assembly for use with patient support apparatus |
US10864128B2 (en) | 2016-06-29 | 2020-12-15 | Stryker Corporation | Patient support systems with rotary actuators having cycloidal drives |
DE102017129235A1 (de) * | 2017-12-08 | 2019-06-13 | Liebherr-Aerospace Lindenberg Gmbh | Dynamische Rücklaufbremse mit Dämpfungselement |
US11440640B2 (en) * | 2018-12-18 | 2022-09-13 | The Boeing Company | Bi-directional no-back brake progressive modulation spring systems and methods |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3090258A (en) | 1958-01-31 | 1963-05-21 | Renk Ag Zahnraeder | Epicyclic gear transmission with herringbone teeth |
US2892329A (en) | 1958-09-26 | 1959-06-30 | Gaetano T Trigilio | Drive mechanism |
US3185413A (en) | 1963-03-25 | 1965-05-25 | Dale W Walker | Integral tension bar retainer |
FR1373805A (fr) | 1963-08-20 | 1964-10-02 | Renault | Dispositif de transmission élastique anti-vibratoire |
US3667214A (en) | 1970-03-11 | 1972-06-06 | Gen Motors Corp | Engine turbosupercharger with vibration reducing drive |
US4411635A (en) * | 1980-11-20 | 1983-10-25 | Ingersoll-Rand Company | Shear overload release coupling |
DE3151399A1 (de) * | 1981-12-24 | 1983-07-07 | Gewerkschaft Eisenhütte Westfalia, 4670 Lünen | Vorrichtung zum auswechseln des sollbruchbolzens bei brechern, insbesondere bei als walzenbrecher ausgebildeten durchlaufbrechern |
US4411546A (en) | 1982-09-20 | 1983-10-25 | Technicraft, Inc. | Oil well sucker rod shear tool |
US4669999A (en) | 1984-08-22 | 1987-06-02 | Sundstrand Corporation | Lubricant delivering and containment overload shearable coupling |
US4971267A (en) | 1989-02-13 | 1990-11-20 | Allied-Signal Inc. | Multi-fuseable shaft |
DE4005235A1 (de) * | 1989-02-23 | 1990-09-06 | Zahnradfabrik Friedrichshafen | Antriebseinrichtung mit variablem drehmoment-begrenzungssystem |
US5141084A (en) * | 1990-09-28 | 1992-08-25 | Sundstrand Corporation | Brake stop |
US5474408A (en) | 1993-11-04 | 1995-12-12 | Transpo Industries, Inc. | Break-away coupling with spaced weakened sections |
US5553960A (en) | 1995-04-13 | 1996-09-10 | Turer; Eric S. | Field serviceable derailleur device |
-
1996
- 1996-05-14 US US09/180,778 patent/US6231012B1/en not_active Expired - Lifetime
-
1997
- 1997-05-14 EP EP97927643A patent/EP0898661B1/de not_active Expired - Lifetime
- 1997-05-14 DE DE69739923T patent/DE69739923D1/de not_active Expired - Lifetime
- 1997-05-14 WO PCT/US1997/008255 patent/WO1997043557A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO1997043557A1 (en) | 1997-11-20 |
US6231012B1 (en) | 2001-05-15 |
EP0898661B1 (de) | 2010-07-07 |
EP0898661A1 (de) | 1999-03-03 |
EP0898661A4 (de) | 2001-01-17 |
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