GB630183A - Improvements in aircraft landing elements - Google Patents
Improvements in aircraft landing elementsInfo
- Publication number
- GB630183A GB630183A GB3304247A GB3304247A GB630183A GB 630183 A GB630183 A GB 630183A GB 3304247 A GB3304247 A GB 3304247A GB 3304247 A GB3304247 A GB 3304247A GB 630183 A GB630183 A GB 630183A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wheels
- aircraft
- leg
- aircraft landing
- axle
- 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
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/34—Alighting gear characterised by elements which contact the ground or similar surface wheeled type, e.g. multi-wheeled bogies
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/34—Alighting gear characterised by elements which contact the ground or similar surface wheeled type, e.g. multi-wheeled bogies
- B64C2025/345—Multi-wheel bogies having one or more steering axes
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vehicle Body Suspensions (AREA)
Abstract
630,183. Aircraft undercarriages. DOWTY EQUIPMENT, Ltd., and BOUND, R. H. Dec. 15, 1947, No. 33042. [Class 4] An aircraft undercarriage comprises a fourwheeled bogie, of which two of the wheels 16, 17 are independently rotatable and are mounted on a common transverse axle 15 at the lower end of the undercarriage leg 13, the other two wheels 21, 24 being mounted in tandem in a fore-andaft plane extending between and parallel to the wheels 16, 17, and being castorable and/or steerable. The wheels 21, 24 are carried by brackets 18, 19 mounted on the axle 15 and provided with supplementary shock-absorbers 26, 27 connected to a cross-head 28 on the leg 13. Anti-shimmy devices may be provided for the castoring wheels, together with means for aligning them when the aircraft is airborne.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3304247A GB630183A (en) | 1947-12-15 | 1947-12-15 | Improvements in aircraft landing elements |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3304247A GB630183A (en) | 1947-12-15 | 1947-12-15 | Improvements in aircraft landing elements |
Publications (1)
Publication Number | Publication Date |
---|---|
GB630183A true GB630183A (en) | 1949-10-06 |
Family
ID=10347735
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3304247A Expired GB630183A (en) | 1947-12-15 | 1947-12-15 | Improvements in aircraft landing elements |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB630183A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1118018B (en) * | 1958-07-07 | 1961-11-23 | Cleveland Pneumatic Ind Inc | Landing gear for aircraft |
US5207398A (en) * | 1990-11-30 | 1993-05-04 | Messier-Bugatti | Device for locking a support for steerable wheels |
US5242131A (en) * | 1992-04-08 | 1993-09-07 | The Boeing Company | Steerable landing gear |
-
1947
- 1947-12-15 GB GB3304247A patent/GB630183A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1118018B (en) * | 1958-07-07 | 1961-11-23 | Cleveland Pneumatic Ind Inc | Landing gear for aircraft |
US5207398A (en) * | 1990-11-30 | 1993-05-04 | Messier-Bugatti | Device for locking a support for steerable wheels |
US5242131A (en) * | 1992-04-08 | 1993-09-07 | The Boeing Company | Steerable landing gear |
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