GB117119A - Improvements in or relating to Pneumatic Cushioning-devices. - Google Patents
Improvements in or relating to Pneumatic Cushioning-devices.Info
- Publication number
- GB117119A GB117119A GB9542/17A GB954217A GB117119A GB 117119 A GB117119 A GB 117119A GB 9542/17 A GB9542/17 A GB 9542/17A GB 954217 A GB954217 A GB 954217A GB 117119 A GB117119 A GB 117119A
- Authority
- GB
- United Kingdom
- Prior art keywords
- chambers
- helix
- cushioning
- pneumatic
- bolts
- 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
117,119. Sloper, T. July 3, 1917. Pneumatic springs.-A cushioning-device for aircraft comprises a number of flexible, elongated pneumatic chambers placed side by side and secured along longitudinal lines near to each other so that the chambers are crowded together and against the part to be cushioned. Fig. 1 shows in cross-section a cushioning-device comprising four chambers B of rubbered canvas having wired edges B<1> with eyelet holes through which a helix C is wound. The helix is secured to the keel of a gondola by a wire D passed through eye bolts E<1>, or the helix may be itself threaded through the eyes in the bolts. The chambers B may be airtight or provided with separate inner tubes F, and are preferably of stream-line form. Should one chamber collapse, the remaining chambers expand laterally and remain operative.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9542/17A GB117119A (en) | 1917-07-03 | 1917-07-03 | Improvements in or relating to Pneumatic Cushioning-devices. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9542/17A GB117119A (en) | 1917-07-03 | 1917-07-03 | Improvements in or relating to Pneumatic Cushioning-devices. |
Publications (1)
Publication Number | Publication Date |
---|---|
GB117119A true GB117119A (en) | 1918-07-03 |
Family
ID=32247267
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9542/17A Expired GB117119A (en) | 1917-07-03 | 1917-07-03 | Improvements in or relating to Pneumatic Cushioning-devices. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB117119A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2433238A (en) * | 1944-10-13 | 1947-12-23 | Ramirez Humberto Villarreal | Landing device for aircraft |
US2887055A (en) * | 1956-08-07 | 1959-05-19 | Harvey Machine Co Inc | Training and test missile |
US4165059A (en) * | 1976-04-30 | 1979-08-21 | American Safety Equipment Corporation | Float assembly for a helicopter or the like |
-
1917
- 1917-07-03 GB GB9542/17A patent/GB117119A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2433238A (en) * | 1944-10-13 | 1947-12-23 | Ramirez Humberto Villarreal | Landing device for aircraft |
US2887055A (en) * | 1956-08-07 | 1959-05-19 | Harvey Machine Co Inc | Training and test missile |
US4165059A (en) * | 1976-04-30 | 1979-08-21 | American Safety Equipment Corporation | Float assembly for a helicopter or the like |
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