GB1024337A - Oleo strut - Google Patents
Oleo strutInfo
- Publication number
- GB1024337A GB1024337A GB34539/64A GB3453964A GB1024337A GB 1024337 A GB1024337 A GB 1024337A GB 34539/64 A GB34539/64 A GB 34539/64A GB 3453964 A GB3453964 A GB 3453964A GB 1024337 A GB1024337 A GB 1024337A
- Authority
- GB
- United Kingdom
- Prior art keywords
- plunger
- strut
- floating piston
- cylinder
- piston
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
- F16F9/06—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium using both gas and liquid
- F16F9/063—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium using both gas and liquid comprising a hollow piston rod
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Fluid-Damping Devices (AREA)
Abstract
1,024,337. Telescopic shock absorbers. HUGHES TOOL CO. Aug. 24, 1964, No. 34539/64. Heading F2S. A landing-gear telescopic oleo strut for an aircraft comprises a plunger 10 sliding within a cylinder 20, and end wall 12 of the plunger 10 being provided with an opening 14. A floating piston 30 co-operates with the interior of the plunger 10 to separate pressurized gas in a compartment 31 from a liquid filling the cylinder 20 and that part of the interior of the plunger 10 below the piston 30, these liquid filled compartments being connected by the opening 14. In the extended position of the strut a shoulder 13 of the plunger 10 normally abuts a shoulder 23 of the cylinder 20. The floating piston 30 is pre-loaded against the gas pressure by a spring 34 acting between the end wall 12 of the plunger 10 and the floating piston. The floating piston 30 is acted on by the spring 34 only in the initial stages of contraction or in the final stages of extension, the latter to absorb energy from the piston 30 in its return movement so as to minimize the transmission of shock to the aircraft especially if the return movement is caused by rapid unloading of the strut. In the contracted position of the strut the end wall 12 of the plunger abuts the end cap 21 of the cylinder 20 and the floating piston abuts the closure plug 11 of the plunger 10.
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US268414A US3162432A (en) | 1963-03-27 | 1963-03-27 | Oleo strut |
GB34539/64A GB1024337A (en) | 1964-08-24 | 1964-08-24 | Oleo strut |
FR986655A FR1413974A (en) | 1964-08-24 | 1964-08-31 | Hydraulic landing gear strut for airplanes |
DEH53715A DE1248480B (en) | 1964-08-24 | 1964-09-05 | Strut for aircraft landing gear |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB34539/64A GB1024337A (en) | 1964-08-24 | 1964-08-24 | Oleo strut |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1024337A true GB1024337A (en) | 1966-03-30 |
Family
ID=10366884
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB34539/64A Expired GB1024337A (en) | 1963-03-27 | 1964-08-24 | Oleo strut |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1024337A (en) |
-
1964
- 1964-08-24 GB GB34539/64A patent/GB1024337A/en not_active Expired
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