GB767631A - High speed low opening shock stabilized parachutes - Google Patents
High speed low opening shock stabilized parachutesInfo
- Publication number
- GB767631A GB767631A GB36180/54A GB3618054A GB767631A GB 767631 A GB767631 A GB 767631A GB 36180/54 A GB36180/54 A GB 36180/54A GB 3618054 A GB3618054 A GB 3618054A GB 767631 A GB767631 A GB 767631A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gores
- panels
- parachutes
- outer end
- parachute
- 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 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
- B64D17/18—Vent arrangement or construction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Emergency Lowering Means (AREA)
Abstract
767,631. Parachutes. PIONEER PARACHUTE CO., Inc. Dec. 14, 1954 [Dec. 30, 1953], No. 36180/54. Class 4. A parachute comprises a number of gores 6 secured to each other at their lateral edges 7 to form a canopy and downwardly convergent shroud lines 3 connected to the said edges, wherein the outer end portions of the gores are so shaped that when the parachute is inflated, the outer end edges 10 of the gores slope downwardly and inwardly towards the descent axis at a material angle, being an angle greater than that assumed by the shroud lines, and wherein a number of circumferentially spaced spoiler panels 13 are each connected between a pair of shroud lines below the canopy. As shown, the panels 13 are placed below alternate gores, and adjacent corners of successive panels are joined by tapes 16. Panels 9 are stitched to the outer end edges 10 of the gores, so as to leave vents 11. A crown vent is provided. Reference has been directed by the Comptroller to Specification 703,026.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US767631XA | 1953-12-30 | 1953-12-30 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB767631A true GB767631A (en) | 1957-02-06 |
Family
ID=22134029
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB36180/54A Expired GB767631A (en) | 1953-12-30 | 1954-12-14 | High speed low opening shock stabilized parachutes |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB767631A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107651198A (en) * | 2017-09-08 | 2018-02-02 | 襄阳宏伟航空器有限责任公司 | A kind of spherical parachute |
-
1954
- 1954-12-14 GB GB36180/54A patent/GB767631A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107651198A (en) * | 2017-09-08 | 2018-02-02 | 襄阳宏伟航空器有限责任公司 | A kind of spherical parachute |
| CN107651198B (en) * | 2017-09-08 | 2024-04-12 | 襄阳宏伟航空器有限责任公司 | Spherical parachute |
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