GB438165A - Shock-absorbing means for the under-carriages of aircraft - Google Patents
Shock-absorbing means for the under-carriages of aircraftInfo
- Publication number
- GB438165A GB438165A GB36068/34A GB3606834A GB438165A GB 438165 A GB438165 A GB 438165A GB 36068/34 A GB36068/34 A GB 36068/34A GB 3606834 A GB3606834 A GB 3606834A GB 438165 A GB438165 A GB 438165A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shock
- torsion
- tube
- lever
- arm
- 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
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vehicle Body Suspensions (AREA)
Abstract
438,165. Shock-absorbing arrangements. ELEKTRONMETALL GES., Bad-Canstatt, Stuttgart, Germany. Dec. 15, 1934, No. 36068. Convention date, Dec. 16, 1933. [Class 108 (iii)] [See also Group XXXIII] A shock - absorbing arrangement for float or wheel undercarriages of aircraft comprises a number of torsion elements which are brought into operation successively. In the arrangement shown in Figs. 7, 8, the shock is applied by a lever to an arm 14 connected to an innermost tube 17 rigidly held at one end. After a predetermined movement of the arm 14 a lever 15 places a second tube 18 in torsion and, in the case of a very severe shock, a lever 16 is engaged and places the outermost tube 19 in torsion. The arm 21 through which the shock is transmitted to the torsion tube arrangement shown in Fig. 10 as applied to a single torsion tube, carries a plate 22 pressed by a spring 23 against a fixed member 24. The torsion bars or tubes may be provided with a bearing support intermediate their ends.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE438165X | 1933-12-16 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB438165A true GB438165A (en) | 1935-11-12 |
Family
ID=6507127
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB36068/34A Expired GB438165A (en) | 1933-12-16 | 1934-12-15 | Shock-absorbing means for the under-carriages of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB438165A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2954188A (en) * | 1954-07-07 | 1960-09-27 | Lockheed Aircraft Corp | Landing gear for aircraft |
| US3128971A (en) * | 1964-04-14 | Aircraft landing gear | ||
| US3193221A (en) * | 1962-11-13 | 1965-07-06 | Hiller Aircraft Company Inc | Aircraft landing gear strut structure |
| US9555877B2 (en) | 2012-02-24 | 2017-01-31 | Safran Landing Systems Uk Ltd | Landing gear |
-
1934
- 1934-12-15 GB GB36068/34A patent/GB438165A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3128971A (en) * | 1964-04-14 | Aircraft landing gear | ||
| US2954188A (en) * | 1954-07-07 | 1960-09-27 | Lockheed Aircraft Corp | Landing gear for aircraft |
| US3193221A (en) * | 1962-11-13 | 1965-07-06 | Hiller Aircraft Company Inc | Aircraft landing gear strut structure |
| US9555877B2 (en) | 2012-02-24 | 2017-01-31 | Safran Landing Systems Uk Ltd | Landing gear |
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