GB595369A - Improvements in or relating to parachute assemblies - Google Patents
Improvements in or relating to parachute assembliesInfo
- Publication number
- GB595369A GB595369A GB260/45A GB26045A GB595369A GB 595369 A GB595369 A GB 595369A GB 260/45 A GB260/45 A GB 260/45A GB 26045 A GB26045 A GB 26045A GB 595369 A GB595369 A GB 595369A
- Authority
- GB
- United Kingdom
- Prior art keywords
- canopy
- skirt
- peak
- parachute
- lines
- 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
- 230000000712 assembly Effects 0.000 title 1
- 238000000429 assembly Methods 0.000 title 1
- 241000237503 Pectinidae Species 0.000 abstract 1
- 230000003247 decreasing effect Effects 0.000 abstract 1
- 230000000630 rising effect Effects 0.000 abstract 1
- 235000020637 scallop Nutrition 0.000 abstract 1
- 239000000725 suspension 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
- B64D17/00—Parachutes
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Emergency Lowering Means (AREA)
Abstract
595,369. Parachutes. SWITLIK, S. Jan. 3, 1945, No. 260. [Class 4] A parachute canopy is formed from a plurality of substantially triangular panels 1 seamed together along their longitudinal edges 2, the distance on the canopy between diametrically opposite points on the edge of the skirt being greater than the diameter of the skirt when the canopy is extended to its fullest extent but uninflated as shown in Fig. 2, load suspension lines 6 being attached at the skirt and along the seams. and terminating short of the canopy peak, whereby when the canopy is inflated in use its outline consists of rising curves which intersect to form a pointed peak 11, and scallops 14 are formed along the skirt decreasing in depth towards the peak, the region 15 surrounding the latter being smooth. Some of the lines 6 may extend loosely across the vent 3 for the attachment of a pilot parachute, or the latter may be connected to separate lines attached to the edge of the vent.
Publications (1)
Publication Number | Publication Date |
---|---|
GB595369A true GB595369A (en) | 1947-12-03 |
Family
ID=1593305
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB260/45A Expired GB595369A (en) | 1945-01-03 | Improvements in or relating to parachute assemblies |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB595369A (en) |
-
1945
- 1945-01-03 GB GB260/45A patent/GB595369A/en not_active Expired
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