GB593381A - Apparatus for testing parachutes - Google Patents
Apparatus for testing parachutesInfo
- Publication number
- GB593381A GB593381A GB1348445A GB1348445A GB593381A GB 593381 A GB593381 A GB 593381A GB 1348445 A GB1348445 A GB 1348445A GB 1348445 A GB1348445 A GB 1348445A GB 593381 A GB593381 A GB 593381A
- Authority
- GB
- United Kingdom
- Prior art keywords
- parachute
- pack
- plate
- wires
- arm
- 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
- 238000012360 testing method Methods 0.000 title abstract 4
- KAATUXNTWXVJKI-UHFFFAOYSA-N cypermethrin Chemical compound CC1(C)C(C=C(Cl)Cl)C1C(=O)OC(C#N)C1=CC=CC(OC=2C=CC=CC=2)=C1 KAATUXNTWXVJKI-UHFFFAOYSA-N 0.000 abstract 2
- 230000004048 modification Effects 0.000 abstract 1
- 238000012986 modification Methods 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 POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D21/00—Testing of parachutes
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
593,381. Testing parachutes. CLEVELAND, F. J. (Pioneer Parachute Co., Inc.). May 29, 1945. No. 13484. [Class 4] Apparatus for testing parachutes comprises means. whereby the parachute can be swung in a circular path at high velocity to simulate operating conditions. A vertical shaft 6 is mounted at the top of a tower 2 and is driven through gearing 8, shaft 10 and clutch 14 by an engine 12 on the ground. An arm 16 is hinged to the shaft 6 and its outer end is connected by a cable 26 to a slidable counterweight 30. The parachute pack 36 to be tested is supported by a plate 34 connected by wires 18, 20 to the end of the arm 16. The weight and characteristics of plate 34 are arranged to correspond with those of the load to be supported by the parachute when in use. The rip cord of the parachute is attached to a control line 44 passing through the centre of shaft 6 and extending to a point near the engine 12 so that it may be pulled by the operator. The line 44 is normally maintained inoperative by a spring attached to the wire 18. A motion picture camera 43 is resiliently mounted on the wire 18 and is focused on the pack 36. The mounting includes a rod 46 pivoted to the wire 18 and slidable in a collar fixed to the wire 20 so that relative movement. of the wires may take place without affecting the focusing of the camera. The operating lever of the camera is connected to the line 44 by an elastic cable. When at rest, the wires and parachute pack hang downwardly in the dotted line position and the arm 16 is held in a raised position by the weight 30 to prevent the pack dragging on the ground. To test the parachute, the the operator engages the clutch 14 by means of a lever 64 and the arm and wires then extend to the full line position under the action of centrifugal force acting on the plate 34 and pack 36. When the desired velocity is attained, the control line 44 is pulled to first operate camera 43 and then release the parachute. At the same time the clutch 14 is disengaged so that the apparatus slows down under the action of the open parachute. In a modification, Fig. 5 (not shown), the supporting plate for the pack is detachably connected to suspension wires 118, 120 and may be. released by pulling a control line 144 to allow the pack and plate to fly off at a tangent. The release of the plate operates the rip cord of the parachute.
Publications (1)
Publication Number | Publication Date |
---|---|
GB593381A true GB593381A (en) | 1947-10-15 |
Family
ID=1728181
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1348445A Expired GB593381A (en) | 1945-05-29 | Apparatus for testing parachutes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB593381A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104608931A (en) * | 2015-03-05 | 2015-05-13 | 襄阳宏伟航空器有限责任公司 | Parachute with pretensioning device |
CN112224422A (en) * | 2020-10-14 | 2021-01-15 | 航宇救生装备有限公司 | Launch type parachute dynamic test device |
CN117087890A (en) * | 2023-10-16 | 2023-11-21 | 山西省城乡规划设计研究院有限公司 | Territorial space planning topography measuring equipment based on unmanned aerial vehicle platform |
-
1945
- 1945-05-29 GB GB1348445A patent/GB593381A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104608931A (en) * | 2015-03-05 | 2015-05-13 | 襄阳宏伟航空器有限责任公司 | Parachute with pretensioning device |
CN112224422A (en) * | 2020-10-14 | 2021-01-15 | 航宇救生装备有限公司 | Launch type parachute dynamic test device |
CN112224422B (en) * | 2020-10-14 | 2023-05-12 | 航宇救生装备有限公司 | Dynamic test device for transmitting parachute |
CN117087890A (en) * | 2023-10-16 | 2023-11-21 | 山西省城乡规划设计研究院有限公司 | Territorial space planning topography measuring equipment based on unmanned aerial vehicle platform |
CN117087890B (en) * | 2023-10-16 | 2023-12-22 | 山西省城乡规划设计研究院有限公司 | Territorial space planning topography measuring equipment based on unmanned aerial vehicle platform |
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