GB357476A - Improvements in or relating to landing gear for aeroplanes - Google Patents
Improvements in or relating to landing gear for aeroplanesInfo
- Publication number
- GB357476A GB357476A GB6473/31A GB647331A GB357476A GB 357476 A GB357476 A GB 357476A GB 6473/31 A GB6473/31 A GB 6473/31A GB 647331 A GB647331 A GB 647331A GB 357476 A GB357476 A GB 357476A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ski
- strut
- adjustable
- march
- landing gear
- 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
- B64C25/52—Skis or runners
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
- Display Devices Of Pinball Game Machines (AREA)
Abstract
357,476. Aeroplane landing gear. FIAT SOC. ANON., 250, Via Nizza, Turin, Italy. March 2, 1931, No. 6473. Convention date, March 6, 1930. [Class 4.] To enable an aeroplane to alight on snow-covered ground the wheels are removed from spring- supported axles and replaced by skis that are adjustable in inclination, a rear ski being applied to the usual rear skid. The front skis are mounted on triangular tubular frames 5 and are held at the correct angle by elastic members 7, 8 preadjusted or adjustable in tension and provided with cables to limit their extension. The rear ski has a flanged plate 14, Fig. 5, slidably engaging the spring skid 15 and is connected to the fuselage by a double strut 16 having adjustable ends 16a and an elastic member 17 similar to the members 7, 8. The strut 16 is pivoted to a plate 18 on the ski and the angle of the ski is adjusted by screws 19 engaging projections on the lower end of the strut. Hooks 20 may be provided for braking the machine on frozen snow.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| IT357476X | 1930-03-06 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB357476A true GB357476A (en) | 1931-09-24 |
Family
ID=11242781
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB6473/31A Expired GB357476A (en) | 1930-03-06 | 1931-03-02 | Improvements in or relating to landing gear for aeroplanes |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB357476A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2918234A (en) * | 1956-01-13 | 1959-12-22 | Iii Thomas H Mcconica | Ski rigging apparatus |
| EP2332831A1 (en) | 2009-11-30 | 2011-06-15 | Eurocopter | Tail skid for an aircraft, aircraft and method to avoid the tipping of the aircraft by the use of said tail skid |
| CN106477031A (en) * | 2016-11-30 | 2017-03-08 | 江西洪都航空工业集团有限责任公司 | A kind of SUAV landing buffer system |
| CN113734428A (en) * | 2021-08-30 | 2021-12-03 | 北京航空航天大学 | A simple and easy skid formula rear landing gear for solar energy unmanned aerial vehicle |
-
1931
- 1931-03-02 GB GB6473/31A patent/GB357476A/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2918234A (en) * | 1956-01-13 | 1959-12-22 | Iii Thomas H Mcconica | Ski rigging apparatus |
| EP2332831A1 (en) | 2009-11-30 | 2011-06-15 | Eurocopter | Tail skid for an aircraft, aircraft and method to avoid the tipping of the aircraft by the use of said tail skid |
| US8430357B2 (en) | 2009-11-30 | 2013-04-30 | Eurocopter | Tail skid for protecting a structural element of an aircraft, an aircraft provided with such a tail skid, and an anti-overturning method implemented by said tail skid |
| CN106477031A (en) * | 2016-11-30 | 2017-03-08 | 江西洪都航空工业集团有限责任公司 | A kind of SUAV landing buffer system |
| CN113734428A (en) * | 2021-08-30 | 2021-12-03 | 北京航空航天大学 | A simple and easy skid formula rear landing gear for solar energy unmanned aerial vehicle |
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