GB274167A - Improvements in under-carriages or landing gear for aircraft - Google Patents
Improvements in under-carriages or landing gear for aircraftInfo
- Publication number
- GB274167A GB274167A GB9222/26A GB922226A GB274167A GB 274167 A GB274167 A GB 274167A GB 9222/26 A GB9222/26 A GB 9222/26A GB 922226 A GB922226 A GB 922226A GB 274167 A GB274167 A GB 274167A
- Authority
- GB
- United Kingdom
- Prior art keywords
- machine
- skids
- wheels
- aircraft
- centre
- 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
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/02—Gyroplanes
-
- 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
- B64C25/52—Skis or runners
-
- 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
- B64C25/54—Floats
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tires In General (AREA)
Abstract
274,167. La Cierva, J. de. April 7, 1926. Wheels, runners, and skids; floats, arrangement and disposition of.-The landing elements of an aircraft of the type having freely-rotative wings or positively driven lifting screws are so arranged with relation to the centre of gravity of the machine that the machine may assume either of two positions of equilibrium, one for use when the aircraft is at rest or just about to land, in which the longitudinal axis of the machine is horizontal and the angle of incidence of the wings zero, and the other for use when taking off in which the tail-skid contacts with the ground and the incidence of the wings is positive. The invention is described as applied to aircraft with rotary wing-systems of the kind described in Specification 196,594. The axles D' of the main landing wheels D are disposed to the rear of the centre of gravity x when the longitudinal axis BB of the machine is horizontal and the wing incidence is zero, the aircraft being maintained in this position by one or more front wheels F. The machine may be displaced to rest on the wheels D and a tail-skid J, in which position the centre of gravity x is to the rear of the axles D<1> and the wing incidence is positive, by depressing the elevator to cause the propeller slip stream to tilt the fuselage. The front wheels F may be replaced by skids. In amphibian aircraft the main wheels and the front wheels or skids may be mounted upon floats or on the hull. In a modification, each skid H, Fig. 4, together with its main wheel D, is mounted to permit a restricted pivotal movement about a vertical axis M in advance of the centre of friction in order that the landing elements may set themselves parallel to the resultant line of advance when the aircraft lands with a lateral as well as a forward speed. Centralizing springs may be provided to maintain the skids normally parallel to the fuselage. An arrangement is described in the Provisional Specification in which skids are provided with small wheels or rollers at their rear ends, the skids being sufficiently long by themselves to support the machine with its longitudinal axis horizontal, whilst when the machine is tilted backwards the machine is supported partly by the skids and partly by the wheels or rollers.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9222/26A GB274167A (en) | 1926-04-07 | 1926-04-07 | Improvements in under-carriages or landing gear for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9222/26A GB274167A (en) | 1926-04-07 | 1926-04-07 | Improvements in under-carriages or landing gear for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB274167A true GB274167A (en) | 1927-07-07 |
Family
ID=9867765
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9222/26A Expired GB274167A (en) | 1926-04-07 | 1926-04-07 | Improvements in under-carriages or landing gear for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB274167A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2641423A (en) * | 1951-09-27 | 1953-06-09 | Bell Aircraft Corp | Aircraft undercarriage |
CN102602532A (en) * | 2011-12-19 | 2012-07-25 | 天津全华时代航天科技发展有限公司 | Sledge and wheel integrated landing gear for unmanned aircraft |
WO2018090810A1 (en) * | 2016-11-17 | 2018-05-24 | 深圳光启空间技术有限公司 | Landing gear and aircraft |
CN110682751B (en) * | 2019-10-17 | 2022-07-15 | 哈尔滨工程大学 | A mechanism for assisting aircraft gliding on water and land based on the principle of water-drifting |
-
1926
- 1926-04-07 GB GB9222/26A patent/GB274167A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2641423A (en) * | 1951-09-27 | 1953-06-09 | Bell Aircraft Corp | Aircraft undercarriage |
CN102602532A (en) * | 2011-12-19 | 2012-07-25 | 天津全华时代航天科技发展有限公司 | Sledge and wheel integrated landing gear for unmanned aircraft |
WO2018090810A1 (en) * | 2016-11-17 | 2018-05-24 | 深圳光启空间技术有限公司 | Landing gear and aircraft |
CN110682751B (en) * | 2019-10-17 | 2022-07-15 | 哈尔滨工程大学 | A mechanism for assisting aircraft gliding on water and land based on the principle of water-drifting |
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