CN101417705A - Shape preserving high-altitude balloon - Google Patents
Shape preserving high-altitude balloon Download PDFInfo
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- CN101417705A CN101417705A CNA2008101373441A CN200810137344A CN101417705A CN 101417705 A CN101417705 A CN 101417705A CN A2008101373441 A CNA2008101373441 A CN A2008101373441A CN 200810137344 A CN200810137344 A CN 200810137344A CN 101417705 A CN101417705 A CN 101417705A
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- inflatable
- altitude balloon
- spheroid
- skeletons
- covering
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Abstract
A form-preserving high-altitude balloon relates to a high-altitude balloon and aims at solving the defects of the existing high-altitude balloon that the rigid under the low internal-pressure is low; and the form alters along the changing of wind and then the form-preserving capability is poor so that the located floating of the high-altitude balloon cannot be realized. An air intake (6) is arranged on a first charging framework (2) of the form-preserving high-altitude balloon and the upper borders and the lower borders of a plurality of first charging frameworks (2) are communicated respectively through a communicator (5); the first charging framework is communicated with the border of a second charging framework (3) through a four-way (4); a skin (1) is fixed on to a network surface formed by the first charging framework (2) and the second charging framework (3); and one end of a suspension cable (10) is fixedly connected with the skin (1) and the other end of the suspension cable (10) is fixedly connected with an effective load (11). The form-preserving high-altitude balloon is provided with the better rigid and can resist the distortion caused by wind; and the form-preserving capability is better and the located floating of the high-altitude balloon can be realized. The form-preserving high-altitude balloon reduces the requirement on the skin materials so as to reduce the cost and the balloon can bear the heavier effective load.
Description
Technical field
The present invention relates to a kind of aerostat, belong to the aerological ascent technical field of tools.
Background technology
Modern aerostat is a kind of aerological ascent instrument that grows up along with improving of space science.(the advection layer height is 30-40km) unpowered vehicle to aerostat, and aerostat has the flying height height, cost is low, the preparatory period is short and be easy to the not available characteristics of other aircraft such as flexible enforcement at the advection layer height as flight.Some developed countries develop the aerostat technology in succession on a large scale since the 60 to 70's in the world, make balloon become a kind of prospecting tools that carries out the atmosphere and space scientific research of running neck and neck with aircraft such as rocket and artificial satellites.The skin material of existing aerostat is the ultrathin flexible material, and the air pressure inside of aerostat is low, rigidity is poor, the shape of aerostat can change with the variation of wind-force, aerostat conformal ability, causes realizing that fixed point suspends.If improve the wind resistance deformability by the interior pressure that increases aerostat, i.e. the conformal ability of aerostat is along with the increase of the interior pressure of aerostat, the covering tension force of aerostat increases, certainly will need high-intensity skin material, then the weight of covering increases, and causes the efficient of aerostat to reduce.
Summary of the invention
To the objective of the invention is that the rigidity that existing aerostat depresses is poor, shape can change with the variation of wind-force, the conformal ability in order solving in low, cause aerostat can't realize the problem of fixing a point to suspend, and then a kind of shape preserving high-altitude balloon is provided.
Technical scheme of the present invention is: shape preserving high-altitude balloon comprises spheroid, suspension cable and capacity weight, described spheroid comprises covering, a plurality of first inflatable skeletons, a plurality of second inflatable skeletons, a plurality of four-ways, two connectednesses and a plurality of attaching parts, every warp of described spheroid is provided with a plurality of second inflatable skeletons, every parallel of spheroid is provided with a plurality of first inflatable skeletons, have induction opening on described first inflatable skeleton, the upper end intersection and the lower end intersection of a plurality of first inflatable skeletons are communicated with by connectedness respectively, the intersection of described first inflatable skeleton and second inflatable skeleton is communicated with by four-way, described covering is fixed on the outside face of the grid that first inflatable skeleton and second inflatable skeleton form by attaching parts, one end of described suspension cable is fixed on the covering, and the other end and the capacity weight of suspension cable are affixed.
The present invention compared with prior art has following beneficial effect: the present invention depresses in low has good stiffness, can resist the distortion that wind-force causes, and the conformal ability is good, and aerostat can realize that fixed point suspends.The present invention introduces the inflatable skeleton load causes interior pressure of balloon to reduce, thereby has reduced the requirement to skin material, and then has reduced the weight of aerostat, has reduced cost, and skin material has been realized production domesticization, and the present invention can be carried bigger capacity weight.
Description of drawings
Fig. 1 is an integral structure scheme drawing of the present invention, and Fig. 2 is the structural representation of four-way, and to be covering be fixed in structural representation on the outside face of the grid that first inflatable skeleton and second inflatable skeleton form by attaching parts to Fig. 3, and Fig. 4 is the left view of Fig. 3.
The specific embodiment
The specific embodiment one: present embodiment is described in conjunction with Fig. 1～Fig. 4, present embodiment comprises spheroid, suspension cable 10 and capacity weight 11, described spheroid comprises covering 1, a plurality of first inflatable skeletons 2, a plurality of second inflatable skeletons 3, a plurality of four-ways 4, two connectednesses 5 and a plurality of attaching parts 7, every warp of described spheroid is provided with a plurality of second inflatable skeletons 3, every parallel of spheroid is provided with a plurality of first inflatable skeletons 2, have induction opening 6 on described first inflatable skeleton 2, the upper end intersection of a plurality of first inflatable skeletons 2 and lower end intersection are communicated with by connectedness 5 respectively, the intersection of described first inflatable skeleton 2 and second inflatable skeleton 3 is communicated with by four-way 4, described covering 1 is fixed on the outside face of the grid that first inflatable skeleton 2 and second inflatable skeleton 3 form by attaching parts 7, one end of described suspension cable 10 is fixed on the covering 1, the other end of suspension cable 10 and capacity weight 11 are affixed, and capacity weight 11 can be cabin body capacity weight, detector capacity weight and power capacity weight etc.
The specific embodiment two: present embodiment is described in conjunction with Fig. 3 and Fig. 4, the attaching parts 7 of present embodiment is made up of first adhesive linkage 12 and second adhesive linkage 13, described first adhesive linkage, 12 medial surfaces 14 are mutually bonding with the lateral surface 16 of second adhesive linkage 13, the lateral surface 15 of described first adhesive linkage 12 is mutually bonding with covering 1, and the medial surface 17 of described second adhesive linkage 13 is mutually bonding with the outside face of a plurality of first inflatable skeletons 2 and a plurality of second inflatable skeletons 3.So be provided with, the conformal ability is better.Other composition is identical with the specific embodiment one with annexation.
The specific embodiment three: in conjunction with Fig. 1 present embodiment is described, the difference of the present embodiment and the specific embodiment one is that described spheroid also increases the paster 9 of enhancing, and described enhancing paster 9 sticks on the junction of suspension cable 10 and covering 1.So be provided with, avoided the destruction of covering, increased capacity weight.Other composition is identical with the specific embodiment one with annexation.
The specific embodiment four: present embodiment is described in conjunction with Fig. 1, the difference of the present embodiment and the specific embodiment one is, described spheroid also increases has many to strengthen outstanding backguy 8, the outstanding backguy 8 of described enhancing is connected between per two first relative inflatable skeletons 2, and is evenly distributed on the inboard that is positioned at second inflatable skeleton 3 on the spheroid axis.So be provided with, make to strengthen outstanding backguy 8 and first inflatable skeleton, 2 collaborative stands under load, the conformal ability is better.Other composition is identical with the specific embodiment one with annexation.
Claims (4)
1, a kind of shape preserving high-altitude balloon, it comprises spheroid, suspension cable (10) and capacity weight (11), it is characterized in that: described spheroid comprises covering (1), a plurality of first inflatable skeletons (2), a plurality of second inflatable skeletons (3), a plurality of four-ways (4), two connectednesses (5) and a plurality of attaching parts (7), every warp of described spheroid is provided with a plurality of second inflatable skeletons (3), every parallel of spheroid is provided with a plurality of first inflatable skeletons (2), have induction opening (6) on described first inflatable skeleton (2), the upper end intersection of a plurality of first inflatable skeletons (2) and lower end intersection are communicated with by connectedness (5) respectively, the intersection of described first inflatable skeleton (2) and second inflatable skeleton (3) is communicated with by four-way (4), described covering (1) is fixed on the outside face of the grid that first inflatable skeleton (2) and second inflatable skeleton (3) form by attaching parts (7), one end of described suspension cable (10) is fixed on the covering (1), and the other end of suspension cable (10) and capacity weight (11) are affixed.
2, according to the described shape preserving high-altitude balloon of claim 1, it is characterized in that: described attaching parts (7) is made up of first adhesive linkage (12) and second adhesive linkage (13), described first adhesive linkage (12) medial surface (14) is mutually bonding with the lateral surface (16) of second adhesive linkage (13), the lateral surface (15) of described first adhesive linkage (12) is mutually bonding with covering (1), and the medial surface (17) of described second adhesive linkage (13) is mutually bonding with the outside face of a plurality of first inflatable skeletons (2) and a plurality of second inflatable skeleton (3).
3, according to the described shape preserving high-altitude balloon of claim 1, it is characterized in that: described spheroid also comprises enhancing paster (9), and described enhancing paster (9) sticks on the junction of suspension cable (10) and covering (1).
4, according to the described shape preserving high-altitude balloon of claim 1, it is characterized in that: described spheroid comprises that also many strengthen outstanding backguy (8), described enhancing is hanged backguy (8) and is connected between per two relative first inflatable skeletons (2), and is evenly distributed on the inboard of second inflatable skeleton (3) that is positioned on the spheroid axis.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2008101373441A CN101417705B (en) | 2008-10-17 | 2008-10-17 | Shape preserving high-altitude balloon |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2008101373441A CN101417705B (en) | 2008-10-17 | 2008-10-17 | Shape preserving high-altitude balloon |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN101417705A true CN101417705A (en) | 2009-04-29 |
| CN101417705B CN101417705B (en) | 2011-01-26 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2008101373441A Expired - Fee Related CN101417705B (en) | 2008-10-17 | 2008-10-17 | Shape preserving high-altitude balloon |
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| CN (1) | CN101417705B (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103600831A (en) * | 2013-12-04 | 2014-02-26 | 新誉集团有限公司 | Capsule self-forming anti-damage inflation auxiliary mechanism for non-rigid airship and inflation method thereof |
| CN104590539A (en) * | 2014-08-19 | 2015-05-06 | 中国特种飞行器研究所 | Overpressure and deformation control device for umbrella opening type airship gasbag |
| ES2538595A1 (en) * | 2013-12-20 | 2015-06-22 | Universitat Politècnica De Catalunya | Pneumatic structure of stiffening the tarpaulin of a balloon and aerostats in general and pressurized operation of said structure (Machine-translation by Google Translate, not legally binding) |
| CN105261818A (en) * | 2015-11-06 | 2016-01-20 | 哈尔滨工业大学 | Air inflation support ring for space-borne radial rib inflation expansion antenna |
| CN107054611A (en) * | 2017-04-05 | 2017-08-18 | 杭州东沣科技有限公司 | A kind of dirigible utricule fast aeration system and method |
| CN110525627A (en) * | 2019-09-18 | 2019-12-03 | 哈尔滨工业大学 | A kind of dirigible support construction based on carbon fiber skeleton |
| CN114506440A (en) * | 2020-11-16 | 2022-05-17 | 株式会社岩谷技研 | Balloon with a detachable cover |
-
2008
- 2008-10-17 CN CN2008101373441A patent/CN101417705B/en not_active Expired - Fee Related
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103600831A (en) * | 2013-12-04 | 2014-02-26 | 新誉集团有限公司 | Capsule self-forming anti-damage inflation auxiliary mechanism for non-rigid airship and inflation method thereof |
| ES2538595A1 (en) * | 2013-12-20 | 2015-06-22 | Universitat Politècnica De Catalunya | Pneumatic structure of stiffening the tarpaulin of a balloon and aerostats in general and pressurized operation of said structure (Machine-translation by Google Translate, not legally binding) |
| CN104590539A (en) * | 2014-08-19 | 2015-05-06 | 中国特种飞行器研究所 | Overpressure and deformation control device for umbrella opening type airship gasbag |
| CN104590539B (en) * | 2014-08-19 | 2016-06-08 | 中国特种飞行器研究所 | Formula airship envelope superpressure and deformation controller in hole is opened for umbrella |
| CN105261818A (en) * | 2015-11-06 | 2016-01-20 | 哈尔滨工业大学 | Air inflation support ring for space-borne radial rib inflation expansion antenna |
| CN105261818B (en) * | 2015-11-06 | 2017-09-22 | 哈尔滨工业大学 | Inflated supporting ring for spaceborne radial rib inflatable space antenna |
| CN107054611A (en) * | 2017-04-05 | 2017-08-18 | 杭州东沣科技有限公司 | A kind of dirigible utricule fast aeration system and method |
| CN110525627A (en) * | 2019-09-18 | 2019-12-03 | 哈尔滨工业大学 | A kind of dirigible support construction based on carbon fiber skeleton |
| CN110525627B (en) * | 2019-09-18 | 2022-08-09 | 哈尔滨工业大学 | Airship supporting structure based on carbon fiber framework |
| CN114506440A (en) * | 2020-11-16 | 2022-05-17 | 株式会社岩谷技研 | Balloon with a detachable cover |
| CN114506440B (en) * | 2020-11-16 | 2023-12-12 | 株式会社岩谷技研 | balloon |
Also Published As
| Publication number | Publication date |
|---|---|
| CN101417705B (en) | 2011-01-26 |
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Granted publication date: 20110126 Termination date: 20201017 |