GB461144A - Improvements in resilient struts for use more especially in connection with the landing wheels of aeroplanes - Google Patents
Improvements in resilient struts for use more especially in connection with the landing wheels of aeroplanesInfo
- Publication number
- GB461144A GB461144A GB22936/35A GB2293635A GB461144A GB 461144 A GB461144 A GB 461144A GB 22936/35 A GB22936/35 A GB 22936/35A GB 2293635 A GB2293635 A GB 2293635A GB 461144 A GB461144 A GB 461144A
- Authority
- GB
- United Kingdom
- Prior art keywords
- plunger
- plug
- valve
- tube
- apertures
- 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
- B64C25/60—Oleo legs
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fluid-Damping Devices (AREA)
Abstract
461,144. Shock-absorbers. RIBBESFORD CO., Ltd., and ONIONS, J. H. Aug. 15, 1935, No. 22936. [Class 108 (iii)] In a resilient strut particularly for aircraft comprising telescopic, tubular, plunger-andcylinder members 14, 10, relative movement of which is resisted by flow of liquid through one or more restricted passages, a floating piston 38 separates the liquid from compressed gas or air which supports the normal axial load. As shown in Fig. 1, the plunger-head 15 contains a series of large apertures 19 and a small central opening 20, flow of liquid through which is regulated by a centrally-apertured flutter-valve 17 such that, on compression of the strut, liquid flows relatively freely through the apertures 19 and valve-aperture 21 while on extension the valve 17 is pressed downwardly, the flow of liquid being restricted by the opening 20, the apertures 19 being closed by the valve. The lower end of the cylinder 10 is closed by a plug 22 secured by three diametral pins &c. 23 and provided with an oil-filling passage 25. Compression of the strut is arrested by an annular buffer 27 resting on the plug 22 and extension by a resilient ring 28 surrounding the plunger 14 and resting on a spacing tube 30. A preferably resilient sleeve 43 acts as a stop for the floating piston 38, the sleeve bearing against another plug 32 which closes the outer end of the plunger 14, and is fitted with an air or gas inlet valve 37. The relative disposition of the parts may be reversed as in the construction shown in Fig. 2. In this case the upper plug 45 supports a central rod or tube 46 carrying at its lower end a piston 47 having small apertures 48, the piston and tube working with clearance in the body and head respectively of the plunger tube 14. The valve 17 is normally spring-pressed to close the apertures 19 in the plunger-head 15. The floating-piston 38 may have an axial guidestem 53 slidable in the tube 46. The plug 45 comprises portions having bevelled edges 54, 56 adapted to force outwardly into contact with the cylinder 10 a packing ring 58 when the two portions are clamped axially by a nut 57. A plug 59 closing the lower end of the plunger tube 14 is sealed by an L-section packing-ring 63 preferably of rubber.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB22936/35A GB461144A (en) | 1935-08-15 | 1935-08-15 | Improvements in resilient struts for use more especially in connection with the landing wheels of aeroplanes |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB22936/35A GB461144A (en) | 1935-08-15 | 1935-08-15 | Improvements in resilient struts for use more especially in connection with the landing wheels of aeroplanes |
Publications (1)
Publication Number | Publication Date |
---|---|
GB461144A true GB461144A (en) | 1937-02-11 |
Family
ID=10187461
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB22936/35A Expired GB461144A (en) | 1935-08-15 | 1935-08-15 | Improvements in resilient struts for use more especially in connection with the landing wheels of aeroplanes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB461144A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2951558A (en) * | 1957-05-02 | 1960-09-06 | Allis Chalmers Mfg Co | Shock absorbing device |
DE1248480B (en) * | 1964-08-24 | 1967-08-24 | Hughes Tool Co | Strut for aircraft landing gear |
US5094407A (en) * | 1989-05-18 | 1992-03-10 | Aerospatiale Societe Nationale Industrielle S.A. | Device for reducing the flexibility of an oleo-pneumatic shock absorber for an undercarriage, and shock absorber and undercarriage including it |
-
1935
- 1935-08-15 GB GB22936/35A patent/GB461144A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2951558A (en) * | 1957-05-02 | 1960-09-06 | Allis Chalmers Mfg Co | Shock absorbing device |
DE1248480B (en) * | 1964-08-24 | 1967-08-24 | Hughes Tool Co | Strut for aircraft landing gear |
US5094407A (en) * | 1989-05-18 | 1992-03-10 | Aerospatiale Societe Nationale Industrielle S.A. | Device for reducing the flexibility of an oleo-pneumatic shock absorber for an undercarriage, and shock absorber and undercarriage including it |
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