GB1216732A - Retractable undercarriage for an aircraft - Google Patents
Retractable undercarriage for an aircraftInfo
- Publication number
- GB1216732A GB1216732A GB2531968A GB2531968A GB1216732A GB 1216732 A GB1216732 A GB 1216732A GB 2531968 A GB2531968 A GB 2531968A GB 2531968 A GB2531968 A GB 2531968A GB 1216732 A GB1216732 A GB 1216732A
- Authority
- GB
- United Kingdom
- Prior art keywords
- undercarriage
- housing
- brace
- retractable
- retraction
- 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
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
- B64C25/14—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like fore-and-aft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/001—Devices not provided for in the groups B64C25/02 - B64C25/68
- B64C2025/008—Comprising means for modifying their length, e.g. for kneeling, for jumping, or for leveling the aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
- Transmission Devices (AREA)
- Fluid-Damping Devices (AREA)
Abstract
1,216,732. Retractable undercarriages. MESSIER. 27 May, 1968 [29 May, 1967], No. 25319/68. Heading B7G. A retractable undercarriage has the mounting linkage designed so that on retraction the length of the undercarriage leg is first shortened and then lengthened. The undercarriage comprises a housing, 6, Fig. 1, a tube, 5, rotatable in the housing, but not axially movable with respect thereto, a shock absorber, 7, connected at one end to a wheel, 1, and at the other to a slider, 26, a bell-crank lever, 10, connected via a link, 28, to said slider and abutting the housing at 31 when the undercarriage is lowered, a rod, 20, articulated to the other limb of the bell-crank lever and at its other end by a cardan joint, 21, to a brace formed from two arms, 14, 15, and an hydraulic ram, 23. In the " lowered " position, Fig. 1, the ram, 23, contains the whole linkage via the brace and ensures that abutments 30 and 31 remain in contact and provides the means to break the brace at pivot, 19, upon retraction. (For Figures see next page.)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR108288A FR92984E (en) | 1965-07-22 | 1967-05-29 | Adjustable retractable landing gear. |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1216732A true GB1216732A (en) | 1970-12-23 |
Family
ID=8631859
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2531968A Expired GB1216732A (en) | 1967-05-29 | 1968-05-27 | Retractable undercarriage for an aircraft |
Country Status (3)
Country | Link |
---|---|
JP (1) | JPS5422679B1 (en) |
DE (2) | DE1756287B2 (en) |
GB (1) | GB1216732A (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2237781A (en) * | 1989-09-07 | 1991-05-15 | Dowty Rotol Ltd | Aircraft landing gear |
EP1279591A1 (en) * | 2001-07-24 | 2003-01-29 | Messier-Dowty S.A. | Vertically retractable landing gear for transport aircraft |
WO2010063893A1 (en) * | 2008-12-05 | 2010-06-10 | Messier-Dowty Sa | Device for retracting aircraft landing gear |
EP3409582A1 (en) * | 2017-06-02 | 2018-12-05 | The Boeing Company | Semi-levered shrink landing gear |
US20190077499A1 (en) * | 2017-09-13 | 2019-03-14 | General Atomics Aeronautical Systems, Inc. | Folding trailing arm landing gear |
EP3498601A1 (en) * | 2017-12-15 | 2019-06-19 | Goodrich Corporation | Latch assembly for shock strut |
US10384767B2 (en) | 2017-01-25 | 2019-08-20 | The Boeing Company | Single axle, semi-levered landing gear with shortening mechanism |
EP3611093A1 (en) * | 2018-07-30 | 2020-02-19 | The Boeing Company | Landing gear shrink link mechanism |
US10625849B2 (en) | 2017-04-11 | 2020-04-21 | The Boeing Company | Levered landing gear with inner shock strut |
US11161599B2 (en) | 2018-01-26 | 2021-11-02 | The Boeing Company | Landing gear strut assembly and method therefor |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1120987B (en) * | 1960-01-11 | 1961-12-28 | Wilhelm Tacke | Self-starting synchronous clock with simplified backstop for wrong direction of rotation of the motor |
CA1076090A (en) * | 1977-03-08 | 1980-04-22 | Societe Anonyme Dite: Messier-Hispano-Bugatti | Retractable fuselage mounted undercarriage |
FR2493265A1 (en) * | 1980-11-05 | 1982-05-07 | Messier Hispano Sa | LANDING TRAIN FOR AIRCRAFT |
DE3406359A1 (en) * | 1983-03-25 | 1984-09-27 | Messier-Hispano-Bugatti (S.A.), Montrouge | FRONT CHASSIS FOR AIRCRAFT |
FR2598676B1 (en) * | 1986-05-13 | 1988-07-29 | Messier Hispano Sa | AIRCRAFT LANDER WITH TIPPING BEAM AND REDUCED SIZE |
US4907760A (en) * | 1988-05-18 | 1990-03-13 | The Boeing Company | Contracting landing gear shock strut |
FR2688467B1 (en) * | 1992-03-11 | 1994-05-13 | Messier Bugatti | LIFT LEVER WITH LEG SHORTENING. |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB689114A (en) * | 1950-08-14 | 1953-03-18 | British Messier Ltd | Improvements in or relating to retractable undercarriage for aircraft |
US2772060A (en) * | 1953-09-03 | 1956-11-27 | Lockheed Aircraft Corp | Actuating and locking mechanism |
-
1968
- 1968-04-17 JP JP2612968A patent/JPS5422679B1/ja active Pending
- 1968-05-02 DE DE19681756287 patent/DE1756287B2/en active Granted
- 1968-05-22 DE DE19681756450 patent/DE1756450B1/en not_active Withdrawn
- 1968-05-27 GB GB2531968A patent/GB1216732A/en not_active Expired
Cited By (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2237781B (en) * | 1989-09-07 | 1993-06-09 | Dowty Rotol Ltd | A landing gear arrangement |
GB2237781A (en) * | 1989-09-07 | 1991-05-15 | Dowty Rotol Ltd | Aircraft landing gear |
EP1279591A1 (en) * | 2001-07-24 | 2003-01-29 | Messier-Dowty S.A. | Vertically retractable landing gear for transport aircraft |
FR2827834A1 (en) * | 2001-07-24 | 2003-01-31 | Messier Dowty Sa | LIFT GEAR FOR LARGE CARRIER AIRCRAFT, VERTICAL LIFT TYPE |
WO2010063893A1 (en) * | 2008-12-05 | 2010-06-10 | Messier-Dowty Sa | Device for retracting aircraft landing gear |
FR2939407A1 (en) * | 2008-12-05 | 2010-06-11 | Messier Dowty Sa | DEVICE FOR SHORTENING AN AIRCRAFT AIRCRAFT |
RU2488523C2 (en) * | 2008-12-05 | 2013-07-27 | Мессье-Бюгатти-Довти | Device to decrease aircraft undercarriage length |
US8505849B2 (en) | 2008-12-05 | 2013-08-13 | Messier-Bugatti-Dowty | Device for retracting aircraft landing gear |
US10384767B2 (en) | 2017-01-25 | 2019-08-20 | The Boeing Company | Single axle, semi-levered landing gear with shortening mechanism |
US11136113B2 (en) | 2017-01-25 | 2021-10-05 | The Boeing Company | Single axle, semi-levered landing gear with shortening mechanism |
US10625849B2 (en) | 2017-04-11 | 2020-04-21 | The Boeing Company | Levered landing gear with inner shock strut |
US11352129B2 (en) | 2017-04-11 | 2022-06-07 | The Boeing Company | Levered landing gear with inner shock strut |
US11873079B2 (en) | 2017-04-11 | 2024-01-16 | The Boeing Company | Levered landing gear with inner shock strut |
EP3409582A1 (en) * | 2017-06-02 | 2018-12-05 | The Boeing Company | Semi-levered shrink landing gear |
US10800516B2 (en) | 2017-06-02 | 2020-10-13 | The Boeing Company | Semi-levered shrink landing gear |
CN108974331A (en) * | 2017-06-02 | 2018-12-11 | 波音公司 | Half rocking arm formula shrinks undercarriage |
US11827342B2 (en) | 2017-06-02 | 2023-11-28 | The Boeing Company | Semi-levered shrink landing gear |
US11572158B2 (en) | 2017-06-02 | 2023-02-07 | The Boeing Company | Semi-levered shrink landing gear |
US11530031B2 (en) | 2017-09-13 | 2022-12-20 | General Atomics Aeronautical Systems, Inc. | Folding trailing arm landing gear |
US10967959B2 (en) * | 2017-09-13 | 2021-04-06 | General Atomics Aeronautical Systems, Inc. | Folding trailing arm landing gear |
US11932379B2 (en) | 2017-09-13 | 2024-03-19 | General Atomics Aeronautical Systems, Inc. | Folding trailing arm landing gear |
US20190077499A1 (en) * | 2017-09-13 | 2019-03-14 | General Atomics Aeronautical Systems, Inc. | Folding trailing arm landing gear |
US10974819B2 (en) | 2017-12-15 | 2021-04-13 | Goodrich Corporation | Latch assembly for shock strut |
EP3498601A1 (en) * | 2017-12-15 | 2019-06-19 | Goodrich Corporation | Latch assembly for shock strut |
US11161599B2 (en) | 2018-01-26 | 2021-11-02 | The Boeing Company | Landing gear strut assembly and method therefor |
EP3611093A1 (en) * | 2018-07-30 | 2020-02-19 | The Boeing Company | Landing gear shrink link mechanism |
US11708151B2 (en) | 2018-07-30 | 2023-07-25 | The Boeing Company | Landing gear shrink link mechanism |
US10981646B2 (en) | 2018-07-30 | 2021-04-20 | The Boeing Company | Landing gear shrink link mechanism |
Also Published As
Publication number | Publication date |
---|---|
DE1756287B2 (en) | 1979-05-31 |
DE1756450B1 (en) | 1970-09-24 |
JPS5422679B1 (en) | 1979-08-08 |
DE1756287A1 (en) | 1970-04-09 |
DE1756287C3 (en) | 1980-01-24 |
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