GB976582A - Helicopter landing gear - Google Patents
Helicopter landing gearInfo
- Publication number
- GB976582A GB976582A GB2856262A GB2856262A GB976582A GB 976582 A GB976582 A GB 976582A GB 2856262 A GB2856262 A GB 2856262A GB 2856262 A GB2856262 A GB 2856262A GB 976582 A GB976582 A GB 976582A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wheels
- centre
- helicopter
- axis
- castoring
- 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
- B64C25/50—Steerable undercarriages; Shimmy-damping
-
- 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
- B64C2025/325—Alighting gear characterised by elements which contact the ground or similar surface specially adapted for helicopters
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Vehicles With Linear Motors And Vehicles That Are Magnetically Levitated (AREA)
Abstract
976,582. Helicopter undercarriages. MINISTER OF AVIATION. Oct. 9, 1963 [July 25, 1962], No. 28562/62. Heading B7G. A helicopter undercarriage has four wheels arranged in diamond formation, two diagonally opposed wheels 15, 16 being on the fore and aft axis and fully castoring, and the other two 11, 12, which are the primary load-carrying wheels, being on a common transverse axis. As shown, the axis of the wheels 11, 12 passes directly under the centre of gravity CG. The wheels 15, 16 are steerable, their common turning centre lying under the centre of gravity, and are connected to each other and to a control wheel 16 by a chain 25. The front wheel may be connected to a towbar (Fig. 3, not shown) for ground manoeuvring, the steering control being disconnected. Alternatively, only one of the wheels 15, 16 is steerable, the other castoring freely.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2856262A GB976582A (en) | 1962-07-25 | 1962-07-25 | Helicopter landing gear |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2856262A GB976582A (en) | 1962-07-25 | 1962-07-25 | Helicopter landing gear |
Publications (1)
Publication Number | Publication Date |
---|---|
GB976582A true GB976582A (en) | 1964-11-25 |
Family
ID=10277594
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2856262A Expired GB976582A (en) | 1962-07-25 | 1962-07-25 | Helicopter landing gear |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB976582A (en) |
-
1962
- 1962-07-25 GB GB2856262A patent/GB976582A/en not_active Expired
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