GB568513A - Improvements relating to parachute packs - Google Patents
Improvements relating to parachute packsInfo
- Publication number
- GB568513A GB568513A GB5163/43A GB516343A GB568513A GB 568513 A GB568513 A GB 568513A GB 5163/43 A GB5163/43 A GB 5163/43A GB 516343 A GB516343 A GB 516343A GB 568513 A GB568513 A GB 568513A
- Authority
- GB
- United Kingdom
- Prior art keywords
- parachute
- retained
- pack
- loop
- bolt
- 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 4
- 230000003068 static effect Effects 0.000 abstract 2
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
- B64D17/40—Packs
- B64D17/52—Opening, e.g. manual
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Emergency Lowering Means (AREA)
- Jib Cranes (AREA)
Abstract
568,513. Parachute packs. QUILTER, J. R. C. March 31, 1943. No. 5163. [Class 4] The static line controlling the pack-retaining means of a container dropped from aircraft is guided by a fairlead 36, carried by a flexible member'secured to the load and detachably secured to the pack, so that a straight pull is exerted on the retaining means. The cover flaps 18 of the parachute pack are overlapped at the centre and retained by a flexible wire loop 19 passed through the eyelet 20 of the uppermost flap and through loops 23, 24 attached to the lowermost flap and threaded through the eyelet 20. The loop 19 is connected to a member 21 having a rigid guide loop 22, and elastic cables 41 connect the member 21 to a webbing 38 which carries the fairlead 36. The webbing 38 passes through a hole 15 inthe upper open end 12 of the rigid container and has a wire frame 39 threaded over one of the lift webs 14 of the parachute. The loop 19 is retained by a pin connected to an extension 35 of the static line, or, as shown in Fig. 5, it is retained by a bolt 29 of a delay action device 28, the bolt having a series of holes 33 engageable by a pin 34 connected to the extension 35. The hole selected determines the time interval between the withdrawal of the pin and the retraction of the bolt to release the parachute. The device 28 is retained in position on the pack by a web 48 looped over the opposite lift web and adjustable to tighten the base-plate 27 against the loops 23, 24 which pass through a hole 26 in the base-plate.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB5163/43A GB568513A (en) | 1943-03-31 | 1943-03-31 | Improvements relating to parachute packs |
| ES173896A ES173896A1 (en) | 1943-03-31 | 1946-07-07 | A PARACHUTE PACKAGE |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB5163/43A GB568513A (en) | 1943-03-31 | 1943-03-31 | Improvements relating to parachute packs |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB568513A true GB568513A (en) | 1945-04-09 |
Family
ID=9790864
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB5163/43A Expired GB568513A (en) | 1943-03-31 | 1943-03-31 | Improvements relating to parachute packs |
Country Status (2)
| Country | Link |
|---|---|
| ES (1) | ES173896A1 (en) |
| GB (1) | GB568513A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3158103A (en) * | 1959-02-09 | 1964-11-24 | Eickmann Karl | Vane assembly in rotary fluid machines |
| CN117141734A (en) * | 2023-11-01 | 2023-12-01 | 四川腾盾科技有限公司 | Unmanned aerial vehicle emergency parachute opening lower body strength design and verification method |
-
1943
- 1943-03-31 GB GB5163/43A patent/GB568513A/en not_active Expired
-
1946
- 1946-07-07 ES ES173896A patent/ES173896A1/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3158103A (en) * | 1959-02-09 | 1964-11-24 | Eickmann Karl | Vane assembly in rotary fluid machines |
| CN117141734A (en) * | 2023-11-01 | 2023-12-01 | 四川腾盾科技有限公司 | Unmanned aerial vehicle emergency parachute opening lower body strength design and verification method |
| CN117141734B (en) * | 2023-11-01 | 2024-01-23 | 四川腾盾科技有限公司 | Unmanned aerial vehicle emergency parachute opening lower body strength design and verification method |
Also Published As
| Publication number | Publication date |
|---|---|
| ES173896A1 (en) | 1946-07-16 |
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