GB516292A - Improvements in or relating to parachutes - Google Patents
Improvements in or relating to parachutesInfo
- Publication number
- GB516292A GB516292A GB19125/38A GB1912538A GB516292A GB 516292 A GB516292 A GB 516292A GB 19125/38 A GB19125/38 A GB 19125/38A GB 1912538 A GB1912538 A GB 1912538A GB 516292 A GB516292 A GB 516292A
- Authority
- GB
- United Kingdom
- Prior art keywords
- parachute
- lines
- main
- cable
- spring
- 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
- 230000000717 retained effect Effects 0.000 abstract 2
- 239000000725 suspension Substances 0.000 abstract 2
- 238000007689 inspection Methods 0.000 abstract 1
- 230000004048 modification Effects 0.000 abstract 1
- 238000012986 modification Methods 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 POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/02—Canopy arrangement or construction
- B64D17/04—Canopy arrangement or construction formed with two or more canopies arranged about a common axis
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
516,292. Parachutes. THORNBLAD, A. R. June 28, 1938, No. 19125. Convention date, June 29, 1937. [Class 4] A parachute is composed of at least two component parachutes, a main parachute, and an auxiliary parachute adapted to open first and pull the main parachute from its container into an elongated and only partly spread condition, the top of the main parachute being freely movable with respect to the suspension lines of the auxiliary parachute so that it can spread independently of the tension of the suspension lines of the auxiliary parachute when the latter has sufficiently retarded the descent. An auxiliary parachute 2 is connected by lines 5 to a load-supporting cable 6, and lines 12 connected to a large vent of the main parachute 3 pass through rings 10, secured to the cable 6, and are anchored to a slide 11 acted upon by a spring 9 surrounding the cable. Before the lines 7 of the main parachute are withdrawn from their pockets the parachute 2 raises the rings 10 and the lines 12 draw the upper edge of the main parachute from its pack, at the same time compressing ,the spring 9. As the lines 7 are pulled out the main parachute rises with respect to auxiliary parachute but it remains elongated with the spring 9 compressed until the speed and therefore the pressure is sufficiently reduced to allow the spring 9 to expand and draw down the top of the main parachute to permit it to spread. A smaller pilot parachute 1 which forms the cover of the parachute pack is connected to the vent of the parachute 2 by draw-strings 4 which slacken as the speed is reduced. When folded, the main parachute rests upon a rigid base 8 and is retained thereon by two straps 24, Fig. 3, secured together by a clip 25 adapted to be released by the pull of the cable 6 and lines 12.' The parachute 2 rests upon the main parachute where it is retained by two strips 22 looped together and secured by inserting a loop of the lines 4 and is covered by the parachute 1 which has eyelets secured over pins 17 on flaps 18 on the base by wires 19 connected to a release cable 21. Spring hinged flaps 15 ensure the spreading of the parachute 1. Numerous modifications are described. The lines 12 may themselves be made elastic and the spring 9 dispensed with, and the lines 4, 5 also may be elastic to draw the three parachutes closer together as the speed falls. For the same purpose the lines 5 and' 7 may be continuous and be passed through rings, adjacent to the load, limit stops being provided on the lines. The various lines may be secured to separate points on the main cable 6, or lines from the top edges of the parachutes 2, 3 may be connected to the main supporting lines of the next higher parachute. The top edge of the. main parachute may have rings which slide on the lines of the auxiliary parachute, stops on the lines ensuring the initial withdrawal of the main parachute. Breakable connections or releasable clips may be employed to ensure the initial restrictions of the openings. The three parachutes may lie one within the other at the same level instead of being superposed. A drift vane may be provided in the rigging. In the Specification as open to inspection under Sect. 91, other arrangements of springs acting on the lines 12 are described. This subject-matter does not appear in the Specification as accepted.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE516292X | 1937-06-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB516292A true GB516292A (en) | 1939-12-29 |
Family
ID=20311088
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB19125/38A Expired GB516292A (en) | 1937-06-29 | 1938-06-28 | Improvements in or relating to parachutes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB516292A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2509496A (en) * | 1945-10-11 | 1950-05-30 | Hart Russell | Means for landing aircraft and other objects by parachute |
US4623109A (en) * | 1985-06-28 | 1986-11-18 | The United States Of America As Represented By The Secretary Of The Army | Low altitude parachute system |
CN105644799A (en) * | 2016-04-11 | 2016-06-08 | 长光卫星技术有限公司 | Separated type parachute ejection capsule for an unmanned aerial vehicle |
CN107238330A (en) * | 2017-07-13 | 2017-10-10 | 襄阳宏伟航空器有限责任公司 | A kind of rotating parachute |
WO2017176200A1 (en) * | 2016-04-06 | 2017-10-12 | Bae Systems Bofors Ab | Parachute device for a divisible shell |
-
1938
- 1938-06-28 GB GB19125/38A patent/GB516292A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2509496A (en) * | 1945-10-11 | 1950-05-30 | Hart Russell | Means for landing aircraft and other objects by parachute |
US4623109A (en) * | 1985-06-28 | 1986-11-18 | The United States Of America As Represented By The Secretary Of The Army | Low altitude parachute system |
WO2017176200A1 (en) * | 2016-04-06 | 2017-10-12 | Bae Systems Bofors Ab | Parachute device for a divisible shell |
US20190137246A1 (en) * | 2016-04-06 | 2019-05-09 | Bae Systems Bofors Ab | Parachute device for a divisible shell |
US10458765B2 (en) | 2016-04-06 | 2019-10-29 | Bae Systems Bofors Ab | Parachute device for divisible shell |
CN105644799A (en) * | 2016-04-11 | 2016-06-08 | 长光卫星技术有限公司 | Separated type parachute ejection capsule for an unmanned aerial vehicle |
CN107238330A (en) * | 2017-07-13 | 2017-10-10 | 襄阳宏伟航空器有限责任公司 | A kind of rotating parachute |
CN107238330B (en) * | 2017-07-13 | 2023-11-17 | 襄阳宏伟航空器有限责任公司 | Rotary umbrella |
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