GB787656A - Improvements in aircraft casterable nosewheel or tailwheel mountings - Google Patents
Improvements in aircraft casterable nosewheel or tailwheel mountingsInfo
- Publication number
- GB787656A GB787656A GB388355A GB388355A GB787656A GB 787656 A GB787656 A GB 787656A GB 388355 A GB388355 A GB 388355A GB 388355 A GB388355 A GB 388355A GB 787656 A GB787656 A GB 787656A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- pivots
- undercarriage
- extension
- 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)
- Fluid-Damping Devices (AREA)
Abstract
787,656. Aircraft undercarriages. DOWTY EQUIPMENT, Ltd. Feb. 7, 1956 [Feb. 9, 1955], No. 3883/55. Class 4. In a levered-suspension nose or tail wheel undercarriage for aircraft wherein an outer casing 5 mounted for retraction about a pivot 39 carries a rotatable element 15 supporting the landing wheel, the piston rod 28 of shock absorber 27 has a universal mounting 29 with a cylindrical member 32 which is mounted for axial movement within a cylindrical extension 17 of element 15. The member 32 has a pivotal connection 34 with a link 35 which is connected at 36 to a bell-crank 38 mounted bn pivot 39 and secured rigidly at 43 to the aircraft structure. The member 32 has opposed cam faces 46 which merge into a parallel-sided slot 47 for co-operation with a roller 48 pivotally mounted on extension 17. With the undercarriage lowered as shown in full lines in Fig. 2, pivots 39, 36, link 35 and pivots 34 and 29 are aligned, thereby resisting upward movement of piston rod 28. During retraction this linkage is " broken and due to the offset between pivots 36 and 39 member 32 will be drawn upwardly within extension 17 to the position shown by dotted lines in Fig. 2, thereby shortening the undercarriage. During such shortening movement roller 48 will be brought into contact with one or the other of cam faces 46 until it lies within slot 47, thereby ensuring that the wheel is correctly centred before final retraction.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB388355A GB787656A (en) | 1955-02-09 | 1955-02-09 | Improvements in aircraft casterable nosewheel or tailwheel mountings |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB388355A GB787656A (en) | 1955-02-09 | 1955-02-09 | Improvements in aircraft casterable nosewheel or tailwheel mountings |
Publications (1)
Publication Number | Publication Date |
---|---|
GB787656A true GB787656A (en) | 1957-12-11 |
Family
ID=9766667
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB388355A Expired GB787656A (en) | 1955-02-09 | 1955-02-09 | Improvements in aircraft casterable nosewheel or tailwheel mountings |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB787656A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4540142A (en) * | 1983-03-25 | 1985-09-10 | Messier-Hispnao-Bugatti (S.A.) | Nose-wheel type landing gear for aircraft |
EP1279591A1 (en) * | 2001-07-24 | 2003-01-29 | Messier-Dowty S.A. | Vertically retractable landing gear for transport aircraft |
WO2022056623A1 (en) * | 2020-09-15 | 2022-03-24 | Robert Kyle Schmidt | Landing gear with shortening motion |
-
1955
- 1955-02-09 GB GB388355A patent/GB787656A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4540142A (en) * | 1983-03-25 | 1985-09-10 | Messier-Hispnao-Bugatti (S.A.) | Nose-wheel type landing gear for aircraft |
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 |
WO2022056623A1 (en) * | 2020-09-15 | 2022-03-24 | Robert Kyle Schmidt | Landing gear with shortening motion |
EP4214119A4 (en) * | 2020-09-15 | 2024-09-04 | Safran Landing Systems Canada Inc | Landing gear with shortening motion |
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