CN2598864Y - Manned powerless balloon parachute device - Google Patents
Manned powerless balloon parachute device Download PDFInfo
- Publication number
- CN2598864Y CN2598864Y CNU032365799U CN03236579U CN2598864Y CN 2598864 Y CN2598864 Y CN 2598864Y CN U032365799 U CNU032365799 U CN U032365799U CN 03236579 U CN03236579 U CN 03236579U CN 2598864 Y CN2598864 Y CN 2598864Y
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- CN
- China
- Prior art keywords
- cabin
- parachute
- captive balloon
- manned
- jumping
- 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 - Fee Related
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Abstract
The utility model discloses a manned powerless balloon parachute device, which comprises a moorage balloon, a parachute cabin, a traction cable, a traction cable winching mechanism, a traction cable ground pulley guiding device and a control device. The whole parachute cabin is shaped like a ring and is hung beneath the moorage balloon. The annular cabin chamber is provided with a driver cabin, a couch cabin, an inner cabin and a parachute preparation cabin in sequence. A safety door is arranged between the inner cabin and the parachute preparation cabin. A guiding parachute suspension link traction device is arranged inside the parachute preparation cabin. One end of the traction cable crosses an empty cavity in the middle of the parachute cabin and is fixed on the moorage balloon, while the other end rounds the traction cable ground pulley guiding device and is connected with the traction cable winching mechanism on the ground. The control device is arranged inside the driver cabin and the couch cabin. Compared with the prior parachute device, the device has the advantages of low running cost, little affection by environment and easy control of the parachute height, which is favorable for the development of parachute jump sports.
Description
Technical field
The utility model relates to a kind of parachute device, and especially a kind of cabin of will parachuting is suspended on a kind of manned unpowered captive balloon parachute device on the unpowered captive balloon.
Background technology
Parachute jumping is liked by increasing people that as a useful able-bodied sports events its form is also more and more abundanter, and the high altitude bailout of jumping off from aircraft is arranged, and the parapenting that jumps off is from the hilltop arranged, and the traction parachute jumping that utilizes motorboat, automobile to carry out is arranged, or the like.High altitude bailout need be employed aircraft, parapenting needs specific landform, and the traction parachute jumping needs specific place and special-purpose accessory appliances, therefore, all there are problems such as expense costliness, limiting factor (s) are many in above-mentioned various parachute jumping form, and these problems have hindered the development of parachuting.
The utility model content
Problem at the prior art existence, the purpose of this utility model provides a kind of new parachute device, this device utilizes constant relatively, the additive decrementation energy not when suspending article in midair aloft of captive balloon lift, and can adjust advantages such as its aerial delay height easily by pull-cord, with it as the high-altitude carrying tool, be used for hanging the parachute jumping cabin, thereby provide a kind of cost parachute jumping instrument low, easy to use for the parachute jumping fan.
For realizing the purpose of this utility model, this manned unpowered captive balloon parachute device comprises: captive balloon, parachute jumping cabin, pull-cord, pull-cord hoisting mechanism, pull-cord ground block guide piece, control setup; Parachute jumping cabin integral body is the ring-type that is surrounded by the cabin, the cabin is by framework, shrouding and safety net constitute, its section is an enclosed construction, shrouding is positioned at the sidewall below, shrouding joins with safety net after the cabin base plate extends upward suitable height, the parachute jumping cabin is suspended on the captive balloon below by rope centering, be disposed with chaufeur and trainer cabin in the ring-type cabin, the cabin is prepared in interior cabin and parachute jumping, interior cabin and parachute jumping prepare to be provided with safety door between the cabin, parachute jumping is prepared the place, cabin and is provided with the hatch door of stepping on cabin and parachute jumping usefulness for personnel in the cabin, parachute jumping prepares also to be provided with pilot-parachute draw ring draw gear in the cabin, and chaufeur and two ends, trainer cabin are provided with safe isolating door; Pull-cord one end passes parachute jumping cabin middle cavity and is fixed on the captive balloon, and its other end is connected on the ground pull-cord hoisting mechanism after walking around pull-cord ground block guide piece; Control setup is arranged in chaufeur and the trainer cabin.
Further, be provided with control setup standby control setup arranged side by side in a cover and chaufeur and the trainer cabin on the ground simultaneously.
Further, described chaufeur and two ends, trainer cabin are provided with two parachute jumpings altogether and prepare the cabin, and the safe isolating door at described chaufeur and two ends, trainer cabin is made of hatch door from the place, cabin to the parachute jumping of inward opening that prepare.
Further, the hatch door at place, described parachute jumping preparation cabin is the push-pull type hatch door.
Further, described pilot-parachute draw ring draw gear is the trailing cable litter, and this trailing cable litter is horizontal suitably highly to be located above the cabin.
Further, but described pilot-parachute draw ring draw gear is the spring reel formula trailing cable of traction hook automatic drawing back.
Further, described parachute jumping cabin is that anistree annular or annulus are capable.
This manned unpowered captive balloon parachute device adopts the aerial carrying tool of captive balloon as the parachute jumping cabin, hoisting mechanism is controlled the height in parachute jumping cabin by the folding and unfolding pull-cord, and the reliably anchoring on the ground of hoisting mechanism and pull-cord ground block guide piece, need not other auxiliary facilities, thereby this device is compared with existing various parachute jumping forms, have over-the-road expense low, be subjected to that such environmental effects is little, jumping altitude is convenient to advantages such as control, help carrying out of parachuting.
Description of drawings
Fig. 1 is the utility model running condition scheme drawing;
Fig. 2 is parachute jumping cabin enlarged diagram;
Fig. 3 is an A-A view among Fig. 2.
The specific embodiment
As shown in Figure 1, the utility model comprises captive balloon 1, parachute jumping cabin 3, pull-cord 8, hoisting mechanism 6, hang below captive balloon 1 by rope 2 centerings in parachute jumping cabin 3, middle cavity and captive balloon 1 that one end of pull-cord 8 passes parachute jumping cabin 3 fix, the other end of pull-cord 8 is walked around pulley guide piece 5 backs that are provided with on the ground 7 and is linked to each other with hoisting mechanism 6, and hoisting mechanism 6 is anchored on the ground 7.Mark 4 is depicted as the parachutist and jumps off the cabin 3 from parachute jumping among the figure.
Shown in Fig. 2,3, parachute jumping cabin 3 integral body are anistree and go in ring, the cabin in parachute jumping cabin is made of framework 31, shrouding 32 and safety net 33, its section is a closed, shrouding 32 joins with safety net 33 after the cabin base plate extends upward suitable height, thereby form the inwall 36 and the outer wall 35 in cabin, safety net 33 seals the top in cabin simultaneously.The cabin is divided into interior cabin, cabin 42 and chaufeur and trainer cabin 43 are prepared in parachute jumping, interior cabin 41 and parachute jumping prepare to be provided with between the cabin 42 by safety door 37, the both sides that cabin 42 lays respectively at chaufeur and trainer cabin 43 are prepared in two parachute jumpings, one of them parachute jumping prepares to be provided with pilot-parachute draw ring trailing cable litter 39 in the cabin 42, these litter two ends are separately fixed on the framework 31 in parachute jumping cabin, another parachute jumping is prepared to be provided with in cabin 42 38, two parachute jumpings of pilot-parachute draw ring spring reel formula trailing cable and is prepared 42 places, cabin and be provided with and step on hatch door 34.In chaufeur and the trainer cabin 43 control setup is installed.
This device in use, at first hoisting mechanism 6 is anchored on the ground 7, apart from hoisting mechanism 6 suitable distances pull-cord pulley guide piece 5 is set, the captive balloon 1 that will install parachute jumping cabin 3 is then fixed with an end of pull-cord 8, handle hoisting mechanism 6 recovery hawsers 8 and make 3 landing of parachute jumping cabin on the ground, treat chaufeur, after trainer and parachutist step on the cabin, control setup in the pilot control operator's compartment makes hoisting mechanism 6 discharge pull-cord 8, parachute jumping cabin 3 is along with captive balloon 1 goes up to the air together, after parachute jumping cabin 3 is elevated to predetermined altitude, hoisting mechanism 6 stops to discharge hawser, and parachute jumping cabin 3 is hovered in the air, for parachutist's parachute jumping is got ready.The parachutist of standby for bailout opens safety door 37 successively and enters parachute jumping preparation cabin 42 from interior cabin, the parachutist who enters parachute jumping preparation cabin 42 closes safety door 37, perform and open hatch door 34 after parachute jumping is prepared, lock the safety barrier that hatch door 34 makes it to become chaufeur and two ends, trainer cabin simultaneously, after parachutist when formerly jumps off, the trainer opens as the hatch door 34 of guardrail and with it and reliably closes, for next parachutist's parachute jumping is got ready.When the landing of needs parachute jumping cabin, chaufeur is handled hoisting mechanism 6 by control setup and is reclaimed pull-cord 8, and captive balloon 1 is landing downwards under the traction of hawser 8, drops on the ground until the parachute jumping cabin.So circulation.
Claims (7)
1. a manned unpowered captive balloon parachute device comprises captive balloon, pull-cord, it is characterized in that, also comprises pull-cord hoisting mechanism, pull-cord ground block guide piece, control setup; Parachute jumping cabin integral body is the ring-type that is surrounded by the cabin, the cabin is by framework, shrouding and safety net constitute, its section is an enclosed construction, shrouding is positioned at the sidewall below, shrouding joins with safety net after the cabin base plate extends upward suitable height, the parachute jumping cabin is suspended on the captive balloon below by rope centering, be disposed with chaufeur and trainer cabin in the ring-type cabin, the cabin is prepared in interior cabin and parachute jumping, interior cabin and parachute jumping prepare to be provided with safety door between the cabin, parachute jumping is prepared the place, cabin and is provided with the hatch door of stepping on cabin and parachute jumping usefulness for personnel in the cabin, parachute jumping prepares also to be provided with pilot-parachute draw ring draw gear in the cabin, and chaufeur and two ends, trainer cabin are provided with safe isolating door; Pull-cord one end passes parachute jumping cabin middle cavity and is fixed on the captive balloon, and its other end is connected on the ground pull-cord hoisting mechanism after walking around pull-cord ground block guide piece; Control setup is arranged in chaufeur and the trainer cabin.
2. manned unpowered captive balloon parachute device as claimed in claim 1 is characterized in that, is provided with the control setup standby control setup arranged side by side in a cover and chaufeur and the trainer cabin on the ground simultaneously.
3. manned unpowered captive balloon parachute device as claimed in claim 1, it is characterized in that, described chaufeur and two ends, trainer cabin are provided with two parachute jumpings altogether and prepare the cabin, and the safe isolating door at described chaufeur and two ends, trainer cabin is made of hatch door from the place, cabin to the parachute jumping of inward opening that prepare.
4. as claim 1,2,3 described manned unpowered captive balloon parachute devices, it is characterized in that described pilot-parachute draw ring draw gear is the trailing cable litter, this trailing cable litter is horizontal suitably highly to be located above the cabin.
5. as claim 1,2,3 described manned unpowered captive balloon parachute devices, it is characterized in that, but described pilot-parachute draw ring draw gear is the spring reel formula trailing cable of traction hook automatic drawing back.
6. manned unpowered captive balloon parachute device as claimed in claim 1 is characterized in that described parachute jumping cabin is that anistree annular or annulus are capable.
7. manned unpowered captive balloon parachute device as claimed in claim 1 is characterized in that, the hatch door that the place, cabin is prepared in described parachute jumping is the push-pull type hatch door.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU032365799U CN2598864Y (en) | 2003-01-27 | 2003-01-27 | Manned powerless balloon parachute device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU032365799U CN2598864Y (en) | 2003-01-27 | 2003-01-27 | Manned powerless balloon parachute device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2598864Y true CN2598864Y (en) | 2004-01-14 |
Family
ID=34166855
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU032365799U Expired - Fee Related CN2598864Y (en) | 2003-01-27 | 2003-01-27 | Manned powerless balloon parachute device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2598864Y (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106983963A (en) * | 2016-04-12 | 2017-07-28 | 华移信通（北京）信息技术有限公司 | Low altitude safe jump wear system |
| CN111746774A (en) * | 2020-06-01 | 2020-10-09 | 中国科学院空天信息创新研究院 | High-altitude balloon issuing system and method |
| CN114353325A (en) * | 2021-12-30 | 2022-04-15 | 中国特种飞行器研究所 | Heating device for mooring rope |
-
2003
- 2003-01-27 CN CNU032365799U patent/CN2598864Y/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106983963A (en) * | 2016-04-12 | 2017-07-28 | 华移信通（北京）信息技术有限公司 | Low altitude safe jump wear system |
| CN111746774A (en) * | 2020-06-01 | 2020-10-09 | 中国科学院空天信息创新研究院 | High-altitude balloon issuing system and method |
| CN111746774B (en) * | 2020-06-01 | 2021-09-28 | 中国科学院空天信息创新研究院 | High-altitude balloon issuing system and method |
| CN114353325A (en) * | 2021-12-30 | 2022-04-15 | 中国特种飞行器研究所 | Heating device for mooring rope |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |