CN206107574U - But gas filled cluster is expanded fast in low latitude - Google Patents
But gas filled cluster is expanded fast in low latitude Download PDFInfo
- Publication number
- CN206107574U CN206107574U CN201621019633.8U CN201621019633U CN206107574U CN 206107574 U CN206107574 U CN 206107574U CN 201621019633 U CN201621019633 U CN 201621019633U CN 206107574 U CN206107574 U CN 206107574U
- Authority
- CN
- China
- Prior art keywords
- parachute
- low latitude
- pack
- inflation
- recorery
- 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
Links
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a but gas filled cluster is expanded fast in low latitude, including rocket, guide pack and a plurality of landing recovery pack, the guide pack installs inside has the retarding parachute, and the outside cover of retarding parachute has long parachute sleeve, all is equipped with the whereabouts recorery parachute in a plurality of landings recovery pack, the top of the long parachute sleeve of rocket end -to -end connection, the bottom of long parachute sleeve is passed through tear -strip and is connected with the umbrella top of retarding parachute, the retarding parachute lower extreme is connected with the umbrella top of a plurality of landing recorery parachutes. The utility model discloses can aerify quick expansion the in low latitude, can make the quick parachute -opening of landing recorery parachute, stabilize the speed reduction to the air -drop system rapidly.
Description
Technical field
This utility model is related to parachute, more particularly to it is a kind of can low latitude rapid deployment inflation cluster.
Background technology
During refitting air-drop, aerial delivery system is completed after assigned tasks, should discharge large area landing recorery parachute for stable
Slow down to land and reclaim.Generally in such cases, landing recorery parachute is faced with that weight is big, highly low unfavorable conditions, needs it to have
There is the performance of low latitude rapid deployment inflation.
Utility model content
The purpose of this utility model, is to propose to return can landing in the cluster of low latitude rapid deployment inflation
Close one's umbrella quick parachute-opening, fast aeration, carries out stable deceleration to aerial delivery system rapidly.
This utility model is that the technical scheme adopted up to above-mentioned purpose is：
There is provided it is a kind of can the inflation of low latitude rapid deployment cluster, including rocket, guiding pack and multiple landings reclaim
Pack, guiding pack is cased with long parachute sleeve built with extractor parachute outside extractor parachute, multiple landings are reclaimed in pack and are respectively arranged with land
Recorery parachute；
Rocket end connects the top of long parachute sleeve, and the bottom of long parachute sleeve is connected by tear-strap with the umbrella top of extractor parachute
Connect；Extractor parachute lower end is connected with the umbrella top of multiple landing recorery parachutes.
It is described in the utility model can be in the cluster of low latitude rapid deployment inflation, guiding pack and multiple landings are reclaimed
Pack is each attached in the load bed of aerial delivery system.
It is described in the utility model can be in the cluster of low latitude rapid deployment inflation, the bottom of multiple landing recorery parachutes is equal
The load bed of aerial delivery system is fixedly connected.
It is described in the utility model can be in the cluster of low latitude rapid deployment inflation, the bottom of multiple landing recorery parachutes leads to
Cross U-loop to be fixedly connected with the load bed of aerial delivery system.
It is described in the utility model can be in the cluster of low latitude rapid deployment inflation, tear-strap is to be existed by zigzag stitched
Two belts together, two free ends of belt connect respectively long parachute sleeve top and extractor parachute top.
It is described in the utility model can be in the cluster of low latitude rapid deployment inflation, before parachute-opening, landing recorery parachute is in
"the" shape is folded and is placed in landing recovery pack.
It is described in the utility model can be in the cluster of low latitude rapid deployment inflation, rocket end is connected with steel wire rope,
Steel wire rope is connected by connection ring with the top of long parachute sleeve.
It is described in the utility model can be in the cluster of low latitude rapid deployment inflation, the lower end of extractor parachute is provided with becket bridle,
The connect band that becket bridle is arranged with the umbrella top of multiple landing recorery parachutes 7 is connected.
It is described in the utility model can be in the cluster of low latitude rapid deployment inflation, connect band is by each landing recorery parachute
Umbrella top links together, and converges at a bit.
This utility model produce beneficial effect be：This utility model can the inflation of low latitude rapid deployment cluster knot
Structure causes parachute-opening program clear, and canopy inflation is rapid, and low latitude opening speed is fast, reliably can carry out stable deceleration to aerial delivery system
Land and reclaim.
Description of the drawings
Below in conjunction with drawings and Examples, the utility model is described in further detail, in accompanying drawing：
Fig. 1 be this utility model embodiment can the inflation of low latitude rapid deployment cluster structural representation.
Specific embodiment
In order that the purpose of this utility model, technical scheme and advantage become more apparent, below in conjunction with accompanying drawing and enforcement
Example, is further elaborated to this utility model.It should be appreciated that specific embodiment described herein is only to explain this
Utility model, is not used to limit this utility model.
This utility model can the cluster of low latitude rapid deployment inflation can inflate in low latitude rapid deployment, landing can be made
The quick parachute-opening of recorery parachute, fast aeration, carry out stable deceleration to aerial delivery system rapidly.
As shown in figure 1, this utility model embodiment can the cluster of low latitude rapid deployment inflation include rocket 1, draw
Pilot chute bag 2 and multiple landing reclaim pack 8, and guiding pack 2 is cased with long parachute sleeve 3 built with extractor parachute 5 outside extractor parachute 5, many
Land recorery parachute 7 is respectively arranged with the individual recovery pack 8 that lands.Landing recorery parachute 7 is used for the stable deceleration of aerial delivery system and steady
Land.The recovery pack 8 that lands is mainly used in packing landing recorery parachute 7, in binding yarn set of the umbrella rope uniform restraint on the outside of pack, to protect
Card landing recorery parachute can in an orderly manner pull out pack.
The end of rocket 1 connects the top of long parachute sleeve 3, and the bottom of long parachute sleeve 3 is by tear-strap 4 and the umbrella of extractor parachute 5
Top connection；The lower end of extractor parachute 5 is connected with the umbrella top of multiple landing recorery parachutes 7.Extractor parachute 5 is quickly pulled out using the power of rocket 1.
Extractor parachute 5 can produce enough pulling force and will have landing recorery parachute 7 more and pull out respective pack after opening.
Preferably, rocket 1 can be linked together with long parachute sleeve 3 by connection ring.Guiding pack 2 is mainly used in packaging length
Parachute sleeve 3 and extractor parachute 5, and ensure that the long parachute sleeve 3 equipped with extractor parachute 5 pulls out in an orderly manner extractor parachute 5.The umbrella rope of extractor parachute 5
In lasso of the uniform restraint outside long parachute sleeve 3, it is ensured that guiding 5 is being pulled out to from total length in guiding parachute sleeve 3 from pack
All the time can be by established procedure constraint relief in an orderly manner during stretching.
Before parachute-opening, extractor parachute 5 is folded in the long parachute sleeve 3 of neat rear threading, and umbrella rope is constrained in order on the outside of long parachute sleeve
In lasso, by the lasso package on umbrella rope and long parachute sleeve；Long parachute sleeve 3 in outer cover, is then placed in after the folding of extractor parachute 5
In guiding pack 2；The lower end of extractor parachute 5 is connected by connection ring with many umbrella top connect bands 6；Each free end of umbrella top connect band 6
It is connected with the umbrella top of a tool landing recorery parachute 7 by way of socket；After landing recorery parachute 7 of often having is folded neatly, canopy is put into and is landed
Pack 8 is reclaimed, canopy withstands on landing and reclaims the oral area of pack 8, and parachute skirt is in recovery pack 8 bottom of landing, form of zigzag folding
Folded, the cotton cord form of zigzag of umbrella top connect band 6 constrains in pack oral area, and umbrella rope constrains in order landing and reclaims outside pack 8
In the binding yarn set of side, landing is sealed by the latch connected in umbrella top connect band 6 and reclaims pack 8.Many lower ends of tool landing recorery parachute 7
It is connected with the load bed suspender belt of aerial delivery system by U-loop.
Preferably, tear-strap 7 is the two belts by zigzag stitched together, and two free ends of belt connect respectively
The top of long parachute sleeve 3 and the top of extractor parachute 5.Tear-strap 4 can ensure that extractor parachute 5 is equal all the time before long parachute sleeve 3 is not drawn out
It is even to be distributed in long parachute sleeve 3；When extractor parachute 5 is drawn out long parachute sleeve 3, by the sawtooth of tear-strap 4 progressively tear order from
Open long parachute sleeve 3.Can prevent extractor parachute from piling up in parachute sleeve in this way, produce minusg, cause long parachute sleeve 3 to carry
Before untie package.
Preferably, rocket end is provided with steel wire rope, and steel wire rope can be connected by connection ring with the top of long parachute sleeve.
The lower end of extractor parachute 5 can be provided with becket bridle, and the one end for the connect band that becket bridle is arranged with the umbrella top of multiple landing recorery parachutes 7 connects
Connect；The other end of each umbrella top connect band is connected with a tool landing recorery parachute 7.Before air-drop, extractor parachute 5 is packaged in long parachute sleeve
Load in 3 and then in the lump and be fixed in the guiding pack 2 in aerial delivery system load bed, landing recorery parachute 7 is fixed on aerial delivery system goods
Landing on platform is reclaimed in pack 8.Landing recorery parachute 7 be mounted in land reclaim pack 8 bag mouth at, be easy to landing recorery parachute 7 with
First go out canopy and go out the suitable traction therapy of umbrella rope again to stretch.Contribute to the fast aeration of canopy along traction therapy.
As shown in figure 1, the lower end of extractor parachute 5 is provided with becket bridle, the connect band that becket bridle is arranged with the umbrella top of multiple landing recorery parachutes 7
6 connections.
Connect band 6 links together on the umbrella top of each landing recorery parachute 7, converges at a bit, is easy to control between each umbrella
Mutual distance, plays the maximum effect of air-drop influence area.
This utility model can the structure of cluster of low latitude rapid deployment inflation cause parachute-opening program clear, low latitude parachute-opening
Speed is fast, and canopy inflation is rapid, stable landing of slowing down reliably can be carried out to aerial delivery system and is reclaimed.
It should be appreciated that for those of ordinary skills, can according to the above description be improved or be converted,
And all these modifications and variations should all belong to the protection domain of this utility model claims.
Claims (9)
1. it is a kind of can the inflation of low latitude rapid deployment cluster, it is characterised in that including rocket, guiding pack and multiple landings
Pack is reclaimed, guiding pack is cased with long parachute sleeve built with extractor parachute outside extractor parachute, multiple landings are reclaimed and are respectively arranged with pack
Land recorery parachute；
Rocket end connects the top of long parachute sleeve, and the bottom of long parachute sleeve is connected by tear-strap with the umbrella top of extractor parachute；Draw
Pilot chute lower end is connected with the umbrella top of multiple landing recorery parachutes.
2. it is according to claim 1 can the inflation of low latitude rapid deployment cluster, it is characterised in that guiding pack and many
The individual recovery pack that lands is each attached in the load bed of aerial delivery system.
3. it is according to claim 1 can the inflation of low latitude rapid deployment cluster, it is characterised in that multiple landings are reclaimed
The load bed of the equal aerial delivery system in bottom of umbrella is fixedly connected.
4. it is according to claim 3 can the inflation of low latitude rapid deployment cluster, it is characterised in that multiple landings are reclaimed
The bottom of umbrella is fixedly connected by U-loop with the load bed of aerial delivery system.
5. it is according to claim 1 can the inflation of low latitude rapid deployment cluster, it is characterised in that tear-strap is to pass through
Zigzag stitched two belts together, two free ends of belt connect respectively long parachute sleeve top and extractor parachute top.
6. it is according to claim 1 can the inflation of low latitude rapid deployment cluster, it is characterised in that before parachute-opening, land
Recorery parachute form of zigzag is folded and is placed in landing recovery pack.
7. it is according to claim 1 can the inflation of low latitude rapid deployment cluster, it is characterised in that rocket end connects
There is steel wire rope, steel wire rope is connected by connection ring with the top of long parachute sleeve.
8. it is according to claim 1 can the inflation of low latitude rapid deployment cluster, it is characterised in that the lower end of extractor parachute
Becket bridle is provided with, the connect band that becket bridle is arranged with the umbrella top of multiple landing recorery parachutes 7 is connected.
9. it is according to claim 8 can the inflation of low latitude rapid deployment cluster, it is characterised in that connect band will be each
The umbrella top of land recorery parachute links together, and converges at a bit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621019633.8U CN206107574U (en) | 2016-08-31 | 2016-08-31 | But gas filled cluster is expanded fast in low latitude |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621019633.8U CN206107574U (en) | 2016-08-31 | 2016-08-31 | But gas filled cluster is expanded fast in low latitude |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206107574U true CN206107574U (en) | 2017-04-19 |
Family
ID=58515292
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621019633.8U Expired - Fee Related CN206107574U (en) | 2016-08-31 | 2016-08-31 | But gas filled cluster is expanded fast in low latitude |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206107574U (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107745814A (en) * | 2017-11-15 | 2018-03-02 | 航宇救生装备有限公司 | A kind of active landed for aerial delivery system is anti-to turn over controlling organization |
| CN107757924A (en) * | 2017-10-27 | 2018-03-06 | 航宇救生装备有限公司 | The parachute deployment means of large area group's umbrella system |
| CN107902093A (en) * | 2017-12-18 | 2018-04-13 | 浙江工业职业技术学院 | Hand throwing type disaster search and rescue robot |
| CN107902092A (en) * | 2017-12-15 | 2018-04-13 | 浙江工业职业技术学院 | Hand throwing type robot |
| CN107953999A (en) * | 2017-12-25 | 2018-04-24 | 襄阳宏伟航空器有限责任公司 | It is a kind of to penetrate umbrella rocket means for the quick parachute-opening of parachute |
| CN108216693A (en) * | 2018-01-10 | 2018-06-29 | 邹文 | Based on the space netting for determining power tear-strap |
| CN109466777A (en) * | 2018-10-30 | 2019-03-15 | 航宇救生装备有限公司 | A kind of refitting air-drop equipment automatic-posture-adjustment system |
| CN110723299A (en) * | 2019-10-29 | 2020-01-24 | 航宇救生装备有限公司 | Method for improving parachute opening synchronism of multi-parachute system |
| CN112357014A (en) * | 2020-11-30 | 2021-02-12 | 航宇救生装备有限公司 | Life-saving boat automatic air charging device in air based on drag parachute |
-
2016
- 2016-08-31 CN CN201621019633.8U patent/CN206107574U/en not_active Expired - Fee Related
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107757924A (en) * | 2017-10-27 | 2018-03-06 | 航宇救生装备有限公司 | The parachute deployment means of large area group's umbrella system |
| CN107745814A (en) * | 2017-11-15 | 2018-03-02 | 航宇救生装备有限公司 | A kind of active landed for aerial delivery system is anti-to turn over controlling organization |
| CN107745814B (en) * | 2017-11-15 | 2023-12-22 | 航宇救生装备有限公司 | Active anti-overturning control mechanism for landing of air drop system |
| CN107902092A (en) * | 2017-12-15 | 2018-04-13 | 浙江工业职业技术学院 | Hand throwing type robot |
| CN107902093A (en) * | 2017-12-18 | 2018-04-13 | 浙江工业职业技术学院 | Hand throwing type disaster search and rescue robot |
| CN107953999A (en) * | 2017-12-25 | 2018-04-24 | 襄阳宏伟航空器有限责任公司 | It is a kind of to penetrate umbrella rocket means for the quick parachute-opening of parachute |
| CN108216693A (en) * | 2018-01-10 | 2018-06-29 | 邹文 | Based on the space netting for determining power tear-strap |
| CN108216693B (en) * | 2018-01-10 | 2020-07-07 | 邹文 | Space rope net based on fixed-force tearing belt |
| CN109466777A (en) * | 2018-10-30 | 2019-03-15 | 航宇救生装备有限公司 | A kind of refitting air-drop equipment automatic-posture-adjustment system |
| CN109466777B (en) * | 2018-10-30 | 2022-02-01 | 航宇救生装备有限公司 | Automatic posture adjusting system for reloading air-drop equipment |
| CN110723299A (en) * | 2019-10-29 | 2020-01-24 | 航宇救生装备有限公司 | Method for improving parachute opening synchronism of multi-parachute system |
| CN112357014A (en) * | 2020-11-30 | 2021-02-12 | 航宇救生装备有限公司 | Life-saving boat automatic air charging device in air based on drag parachute |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206107574U (en) | But gas filled cluster is expanded fast in low latitude | |
| CN104596361B (en) | The sub-level recovery method of a kind of carrier rocket | |
| CN107757924A (en) | The parachute deployment means of large area group's umbrella system | |
| CN107618669B (en) | A kind of parachute with apical pore lid | |
| CN106240823A (en) | It is capable of the aerial delivery system with attitude stabilization that slows down of disembarking | |
| US2389578A (en) | Parachute pack | |
| CN107826256B (en) | Method for reducing parachute opening impact of ram parafoil | |
| CN207433805U (en) | A kind of air-drop type gravity type air bag with buffering efficiency | |
| US4588149A (en) | Lowered opening shock parachute canopy | |
| US2583905A (en) | Parachute pack and container | |
| CN109250122B (en) | Inflatable ram parafoil for pulling parachute opening | |
| CN107600433B (en) | Parachute canopy protective sleeve by means of back-pull method and mounting method thereof | |
| CN209290702U (en) | One kind being used for large area parachute construction | |
| CN109466776B (en) | Control large tracts of land crowd umbrella structure of opening | |
| CN207374682U (en) | A kind of parachute canopy of falling daraf(reciprocal of farad) protective case | |
| CN110723296A (en) | Method for improving parachute opening reliability of large-scale stamping parafoil | |
| CN213008770U (en) | Air blowing pocket type secondary unfolding parachute | |
| US2439318A (en) | Parachute pack | |
| US2979294A (en) | Parachute combination and ejection device | |
| GB2220626A (en) | Parachutes | |
| CN209795839U (en) | Combined umbrella cover | |
| US3837604A (en) | Means for controlling the deployment and the development of a parachute canopy | |
| CN110723297A (en) | Control method for assisting parachute opening of ram parafoil | |
| CN110723299A (en) | Method for improving parachute opening synchronism of multi-parachute system | |
| CN112644715B (en) | Open parachute packaging container |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170419 Termination date: 20180831 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |