GB1018296A - Improvements in or relating to shock absorbing devices for loads descending in the atmosphere - Google Patents
Improvements in or relating to shock absorbing devices for loads descending in the atmosphereInfo
- Publication number
- GB1018296A GB1018296A GB1853562A GB1853562A GB1018296A GB 1018296 A GB1018296 A GB 1018296A GB 1853562 A GB1853562 A GB 1853562A GB 1853562 A GB1853562 A GB 1853562A GB 1018296 A GB1018296 A GB 1018296A
- Authority
- GB
- United Kingdom
- Prior art keywords
- load
- fluid
- ground
- atmosphere
- nozzles
- 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
- 230000035939 shock Effects 0.000 title abstract 2
- 239000012530 fluid Substances 0.000 abstract 6
- 239000012080 ambient air Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWERÂ PLANTSÂ OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
- B64D1/14—Absorbing landing shocks
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fluid-Damping Devices (AREA)
Abstract
1,018,296. Parachute apparatus. A. POURCHET. July 14, 1962, No. 18535/62. Heading B7G. A device to slow the descent of a load in the atmosphere comprises a load support 1, a container to hold fluid connected to the support, and means for causing the fluid to be released from the container into the atmosphere when the load is near the ground to form a layer of fluid at superatmospheric pressure between the load and the ground. The device may permit the load to settle on the ground without shock. Fig. 1 shows a parachute load platform 4. A pilot weight 14, on striking the ground, initiates flow of fluid from telescopically extendable nozzles 6, to brake the load, thus enabling the major part of the descent to be at a faster speed. The nozzles are supplied from a source of fluid under pressure, and contacting of the ground by the pilot weight may make an electrical circuit to detonate a cartridge which results in removal of an obstruction between the source and the nozzles (Fig. 4, not shown). In Fig. 2 (not shown) the fluid flow from line 11 is used to entrain ambient air in ejector ducts 10. An ejection seat may be fitted with similar .braking means.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1853562A GB1018296A (en) | 1962-07-14 | 1962-07-14 | Improvements in or relating to shock absorbing devices for loads descending in the atmosphere |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1853562A GB1018296A (en) | 1962-07-14 | 1962-07-14 | Improvements in or relating to shock absorbing devices for loads descending in the atmosphere |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1018296A true GB1018296A (en) | 1966-01-26 |
Family
ID=10114084
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1853562A Expired GB1018296A (en) | 1962-07-14 | 1962-07-14 | Improvements in or relating to shock absorbing devices for loads descending in the atmosphere |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1018296A (en) |
-
1962
- 1962-07-14 GB GB1853562A patent/GB1018296A/en not_active Expired
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3303807A (en) | Helicopter rapid securing device | |
GB969716A (en) | Ballistic actuated device for reeling in an elongated flexible element | |
GB1018296A (en) | Improvements in or relating to shock absorbing devices for loads descending in the atmosphere | |
FR1272957A (en) | Automatic righting device for airplanes landing vertically on the tail | |
US2492501A (en) | Means for arresting descent of a parachute supported load | |
US2783005A (en) | Aircraft launching and landing device | |
GB559763A (en) | Improvements in or relating to aircraft for conveying airborne troops | |
FR1292361A (en) | Automatic transition control device for vertical take-off and landing planes | |
IT1278596B1 (en) | PNEUMATIC LAUNCHING DEVICE FOR EMERGENCY PARACHUTE FOR PARAGLIDING OR HANG-GLIDING OR OTHER TYPES OF AERODINE AND BALLOONS | |
GB1094843A (en) | Improvements in and relating to devices for landing parachuted loads | |
GB673550A (en) | Improvements in means for launching aeroplanes and other flying bodies | |
GB1323585A (en) | Parachutes | |
GB1063652A (en) | Ground handling equipment for vertical take off and landing aircraft | |
GB581726A (en) | Improvements in or relating to parachutes | |
GB928409A (en) | Aircraft ground handling equipment | |
FR1255749A (en) | Airplane with jet propulsion and with a device for vertical take-off and landing | |
GB924971A (en) | Improved motor vehicle for the transfer of passengers to and from aircraft and the like | |
CRANE et al. | Use of a large jet transport as an inflight dynamic simulator(Modified jet transport used as inflight dynamic simulator for supersonic transport low speed approach and landing characteristics) | |
DE68920791D1 (en) | Device for launching heavy payloads from aircraft. | |
US3202386A (en) | Aerial cargo delivery device | |
GB931251A (en) | Improvements in or relating to jet-propelled aircraft | |
GB925415A (en) | Improvements in parachute apparatus | |
GB863686A (en) | Improvements relating to helicopters | |
WILLIAMSON | Variable-thrust propulsion for soft landing vehicles | |
ES213981A3 (en) | A parachute system for elevated dimensions (Machine-translation by Google Translate, not legally binding) |