CN105015758A - Body-variable airbag and aerostat - Google Patents
Body-variable airbag and aerostat Download PDFInfo
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- CN105015758A CN105015758A CN201510360187.0A CN201510360187A CN105015758A CN 105015758 A CN105015758 A CN 105015758A CN 201510360187 A CN201510360187 A CN 201510360187A CN 105015758 A CN105015758 A CN 105015758A
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- messenger wire
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Abstract
The invention belongs to the field of aerostats, in particular, relates to an airship or a balloon, and provides a body-variable airbag and an aerostat capable of gradually adjusting the size of the airbag to adapt to the air pressure in high altitude and low altitude in the ascending process of the aerostat and capable of adjusting the shape of the aerostat as needed. The body-variable airbag and the aerostat comprise an airbag of an airship and a balloon, wherein a cord fabric and a lifting wire are arranged in the airbag; the lifting wire is linked with a pulley or a hanging ring at the tip end of the triangular cord fabric; the cord fabric is arranged above and below the airbag; the lifting wire is continuous; the continuous lifting wire penetrates through the pulley or the hanging ring of the upper cord fabric and the lower cord fabric in sequence, and is finally connected with a tension power device; and the elasticity of the lifting wire is adjusted by the tension power device. The shape of the airship or the balloon can be adjusted; the internal and external pressure difference of the airship can be adjusted through adjusting the shape; and the pressure difference and the shape of the airbag can be adjusted without using an air valve.
Description
Technical field
The invention belongs to aerostatics field, be specifically related to a kind of dirigible or balloon.
Background technology
Dirigible of the prior art generally all comprises air bag, gondola, empennage, gondola is hung in the below of air bag, in order to keep the shape of dirigible not because gravity distortion, usually cord and messenger wire are set at inside air bag, messenger wire is connected between cord, be used for fixing the shape of air bag during inflation, strengthen equipment load hanging ability.
In prior art, because low latitude is different with the air pressure in high-altitude and gas with various temperature traverse expansion rate different, aerostatics air bag can change by inside and outside differential pressure, pressure reduction is crossed conference and to be risen relieving stagnant Qi capsule, the too small meeting of pressure causes air bag be out of shape and lose rigid support, usually be all that balloonet and pressure regulating system are set in air bag, at inside and outside differential pressure hour, air is poured to balloonet, along with rising or the temperature rising of dirigible, in dirigible, pressure reduction increase pressure regulating system open auxiliary air bag deflation valve is exhausted decompression to air bag, so that adjustment keeps inside and outside differential pressure at a constant range automatically, for stratospheric airship or balloon, because the above upper atmosphere of myriametre is thin, air pressure is small, temperature is extremely low, prior art once occurred in high-altitude that valve is frozen in, the thin inflation difficulty of air, abundant electric power is not had to pour enough air to balloonet, the bottleneck formed Deng technical barrier to such an extent as to China and even slow to the Recent Progresses In The Development entering advection layer aerostatics in the world, and the disclosed utricule patented technology that becomes adopts hardmetal structure at present, own wt, manufacturing cost can increase manyfold, to such an extent as at all unpractical, although adopt balloonet and pressure regulating system to be substantially tending towards ripe for low-altitude airship or balloon, but still there is the power consumption increase that up and down inflation/deflation frequently causes dirigible limited, to such an extent as to often affect airship flight safety because of short of electricity, or to climb fast or the air-charging and air-discharging system that declines does not catch up with and occurs safety misadventure, so it is extremely urgent to find a kind of practicable solution.
Summary of the invention
In order to solve the problems referred to above that current aerostatics exists, the invention provides in a kind of process that can rise at aerostatics, adjust the size of air bag gradually, thus adapt to the aerostatics of the air pressure in high-altitude and low latitude, and change utricule air bag and the aerostatics of the shape of aerostatics can be adjusted as required, concrete technical scheme is as follows:
A kind of change utricule air bag, cord and messenger wire are set in air bag, pulley or the link at messenger wire and triangle cord tip link, it is characterized in that: above and below air bag, all cord is set, messenger wire is set to link up, coherent messenger wire passes pulley or the link of upper cord and lower cord successively, is finally connected the elasticity being adjusted messenger wire by tensioning engine installation with tensioning engine installation.
Optimally, tensioning engine installation is set to winch.
Optimally, messenger wire is set to two-stage, and one-level is fixing messenger wire, and one-level is adjustment messenger wire, and fix messenger wire and be connected with upper cord, below arranges pulley, and adjustment messenger wire is connected with pulley or link and is then connected with tensioning engine installation.
Optimally, upper cord at least arranges one.
Optimally, lower cord at least arranges one.
Optimally, cord is connected by pulley or link with messenger wire.
Optimally, messenger wire is arranged spring or clockwork spring.
Optimally, in air bag, balloonet is set.
A kind of change utricule aerostatics, comprise the air bag of dirigible and balloon, cord and messenger wire are set in air bag, pulley or the link at messenger wire and triangle cord tip link, above and below air bag, all cord is set, messenger wire is set to link up, and coherent messenger wire, successively through pulley or the link of upper cord and lower cord, to be finally connected with tensioning engine installation by the elasticity of tensioning engine installation adjustment messenger wire.
Optimally, tensioning engine installation is set to winch.
Optimally, messenger wire is set to two-stage, and one-level is fixing messenger wire, and one-level is adjustment messenger wire, and fix messenger wire and be connected with upper cord, below arranges pulley, and adjustment messenger wire is connected with pulley or link and is then connected with tensioning engine installation.
Optimally, upper cord at least arranges one.
Optimally, lower cord at least arranges one.
Optimally, cord is connected by pulley or link with messenger wire.
Optimally, messenger wire is arranged spring or clockwork spring.
Optimally, the balloon of non-transformer supply arranges solar cell and storage battery is powered to winch.
Optimally, in air bag, balloonet is set.
One provided by the present invention becomes utricule aerostatics, has the following advantages:
One, the dirigible of the technical program it comprise air bag, cord and messenger wire are set in air bag, messenger wire is arranged on shape cord being used for fixing dirigible, above and below air bag, all cord is set, messenger wire is set to link up, coherent messenger wire is successively through upper cord and lower cord, the elasticity being adjusted messenger wire by tensioning engine installation is finally connected with tensioning engine installation, because messenger wire is coherent, so can be strained by tensioning engine installation, messenger wire just can be strained when low latitude by such dirigible, then along with the rising of dirigible, loose messenger wire gradually, so just can adjust the pressure reduction inside and outside air bag, make it remain on a constant range not need to be adjusted by air valve, effectively prevent air valve to freeze or because of excessive the occurred safety misadventure of power consumption.If fine day, cloudy day change appear in the dirigible of this structure during in high-altitude, the shape of air bag can also be adjusted thus the air pressure of adjustment inside air bag by the elasticity of adjustment messenger wire, keep dirigible inside and outside differential pressure in suitable scope and rigidity; And can allow dirigible changes shape, add aesthetics.
Two, tensioning engine installation is set to winch, and winch cost compare is low, and the power source consumption of needs is also smaller, is relatively applicable to the application of this environment.
Three, messenger wire is set to two-stage, and one-level is fixing messenger wire, and one-level is adjustment messenger wire, and fixing messenger wire is connected with upper cord, is in fact equivalent to extend cord length, adopt fixing messenger wire replacement part cord can expendable weight, reduce costs; Below arranges pulley, movable messenger wire is connected with link and is then connected with tensioning engine installation, this is one of them embodiment, and cord and the messenger wire on this structural balloon top are fixing, and tensioning engine installation only just can adjust the shape of air bag by the messenger wire of adjustment bottom.
Four, upper cord at least arranges one, and lower cord at least arranges one, and cord and messenger wire can need the shape of adjustment to decide according to air bag.
Five, cord is connected by pulley or link with messenger wire, is connected by pulley or link, like this when adjustment, reduces friction force during adjustment, and adjustment is got up than smoothly.
Six, messenger wire is arranged spring or clockwork spring, spring and clockwork spring can be used for finely tuning.
Seven, in air bag, balloonet is set, both can increases setting range, can have complementary advantages again, keep full profile; And spring regulate can not power consumption, automatically regulating under situation of change without electricity or by a small margin.
Dirigible of the present invention or balloon can adjust, and can by the pressure reduction inside and outside adjustment Adjusting Shape dirigible, just can adjust pressure reduction and the shape of air bag by obstructed air valve.
Accompanying drawing explanation
Fig. 1 is the structural representation of the embodiment 1 of aerostatics of the present invention;
Fig. 2 is the structural representation of the embodiment 2 of aerostatics of the present invention;
Fig. 3 is the structural representation of the embodiment 4 of aerostatics of the present invention.
Number in the figure:
1: air bag; 2: upper cord; 3: pulley; 4: tensioning engine installation; 5: lower cord; 6: messenger wire; 7: fixing messenger wire; 8: spring; 9: adjustment messenger wire; 10: balloonet.
Detailed description of the invention
Below in conjunction with drawings and Examples, dirigible of the present invention is described in further detail.
Embodiment 1:
With reference to Fig. 1, the change utricule aerostatics of the present embodiment, it comprises air bag 1, cord and messenger wire 6 are set in air bag 1, messenger wire 6 is arranged on shape cord being used for fixing dirigible, all arranges cord above and below air bag 1, and messenger wire 6 is set to link up, coherent messenger wire 6 through upper cord 2 and lower cord 5, is finally connected with tensioning engine installation 4 elasticity being adjusted messenger wire 6 by tensioning engine installation 4 successively.Tensioning engine installation 4 is set to winch.Upper cord 2 arranges one.Lower cord 5 arranges one.Cord is connected by pulley 3 with messenger wire 6.Dirigible is arranged solar storage battery to power to dirigible.
Embodiment 2:
As shown in Figure 2, the difference of the present embodiment and embodiment 1 is, messenger wire is set to two-stage, one-level is fixing messenger wire 7, one-level is adjustment messenger wire 9, and fix messenger wire 7 and be connected with upper cord 2, below arranges pulley 3, adjustment messenger wire 9 is connected with pulley 3 and is then connected with tensioning engine installation 4, messenger wire is arranged spring 8.
Embodiment 3:
The difference of the present embodiment and embodiment 1 is, the messenger wire of the present embodiment is set to multiple, and upper cord and lower cord are also set to two, and the cross section of such dirigible can be drawn as multiple shape.
Embodiment 4:
As shown in Figure 3, the difference of the present embodiment and embodiment 1 is, the present embodiment arranges balloonet 10 at inside air bag, and the present invention can be combined with existing balloonet, both can increase setting range, can have complementary advantages again, keeps full profile; And spring regulate can not power consumption, automatically regulating under situation of change without electricity or by a small margin.
Embodiment 5:
The present embodiment is a kind of change utricule air bag, it comprises air bag 1, cord and messenger wire 6 are set in air bag 1, messenger wire 6 is arranged on shape cord being used for fixing dirigible, above and below air bag 1, all cord is set, messenger wire 6 is set to link up, and coherent messenger wire 6 through upper cord 2 and lower cord 5, is finally connected with tensioning engine installation 4 elasticity being adjusted messenger wire 6 by tensioning engine installation 4 successively.Tensioning engine installation 4 is set to winch.Upper cord 2 arranges one.Lower cord 5 arranges one.Cord is connected by pulley 3 with messenger wire 6.This air bag user can be applied in the field of needs as required.
The above is only to preferred embodiment of the present invention, and be not do other forms of restriction to the present invention, any those skilled in the art may utilize the technology contents of above-mentioned announcement to be changed or be modified as the Equivalent embodiments of equivalent variations.But, everyly do not depart from the present invention program's content, according to technical spirit of the present invention to any simple modification made for any of the above embodiments, equivalent variations and remodeling, still belong to protection scope of the present invention.
Claims (10)
1. one kind becomes utricule air bag, cord and messenger wire are set in air bag, pulley or the link at messenger wire and triangle cord tip link, it is characterized in that: above and below air bag, all cord is set, messenger wire is set to link up, coherent messenger wire passes pulley or the link of upper cord and lower cord successively, is finally connected the elasticity being adjusted messenger wire by tensioning engine installation with tensioning engine installation.
2. change utricule air bag according to claim 1, is characterized in that: tensioning engine installation is set to winch.
3. change utricule air bag according to claim 1, is characterized in that: messenger wire is set to two-stage, and one-level is fixing messenger wire, one-level is adjustment messenger wire, fixing messenger wire is connected with upper cord, and below arranges pulley, and adjustment messenger wire is connected with pulley or link and is then connected with tensioning engine installation.
4. change utricule air bag according to claim 1, is characterized in that: upper cord and lower cord at least arrange one.
5. change utricule air bag according to claim 1, is characterized in that: cord is connected by pulley with messenger wire, messenger wire is arranged spring or clockwork spring, arrange balloonet in air bag.
6. an aerostatics, it comprises dirigible and air bag, cord and messenger wire are set in air bag, pulley or the link at messenger wire and triangle cord tip link, it is characterized in that: above and below air bag, all cord is set, messenger wire is set to link up, and coherent messenger wire, successively through pulley or the link of upper cord and lower cord, to be finally connected with tensioning engine installation by the elasticity of tensioning engine installation adjustment messenger wire.
7. change utricule aerostatics according to claim 1, is characterized in that: tensioning engine installation is set to winch.
8. change utricule aerostatics according to claim 1, is characterized in that: messenger wire is set to two-stage, and one-level is fixing messenger wire, one-level is adjustment messenger wire, fixing messenger wire is connected with upper cord, and below arranges pulley, and adjustment messenger wire is connected with pulley or link and is then connected with tensioning engine installation.
9. change utricule aerostatics according to claim 1, is characterized in that: upper cord and lower cord at least arrange one.
10. change utricule aerostatics according to claim 1, it is characterized in that: cord is connected by pulley with messenger wire, messenger wire is arranged spring or clockwork spring, the balloon of non-transformer supply arranges solar cell and storage battery is powered to winch, in air bag, balloonet is set.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510360187.0A CN105015758A (en) | 2015-06-26 | 2015-06-26 | Body-variable airbag and aerostat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510360187.0A CN105015758A (en) | 2015-06-26 | 2015-06-26 | Body-variable airbag and aerostat |
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| Publication Number | Publication Date |
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| CN105015758A true CN105015758A (en) | 2015-11-04 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201510360187.0A Pending CN105015758A (en) | 2015-06-26 | 2015-06-26 | Body-variable airbag and aerostat |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108206668A (en) * | 2017-12-06 | 2018-06-26 | 苏州绿豆豆智能装备科技有限公司 | A kind of suspension column system available for Photospot solar equipment |
| CN108216552A (en) * | 2017-12-14 | 2018-06-29 | 中国特种飞行器研究所 | A kind of middle-size and small-size unmanned airship gondola connection structure |
| CN109455288A (en) * | 2017-09-06 | 2019-03-12 | 东莞前沿技术研究院 | Unload buckle structure and aerostatics |
| CN109649627A (en) * | 2019-01-28 | 2019-04-19 | 上海交通大学 | The super cold superthermal control method of high altitude airship |
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| RU2264343C1 (en) * | 2004-07-05 | 2005-11-20 | Майсов Иван Александрович | Complex for use of associated gas |
| WO2013113866A1 (en) * | 2012-02-02 | 2013-08-08 | European Aeronautic Defence And Space Company Eads France | Closed structural assembly with improved resistance to compression |
| CN203681861U (en) * | 2014-01-24 | 2014-07-02 | 湖南航天机电设备与特种材料研究所 | Flow control device capable of reducing aerodynamic resistance of airship and improving attitude stability |
| CN104554698A (en) * | 2013-10-10 | 2015-04-29 | 陈德荣 | Capsule telescopic airship |
| 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 |
| CN205738037U (en) * | 2015-06-26 | 2016-11-30 | 青岛中航浮空器研究所 | Become utricule air bag and aerostatics |
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2015
- 2015-06-26 CN CN201510360187.0A patent/CN105015758A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2264343C1 (en) * | 2004-07-05 | 2005-11-20 | Майсов Иван Александрович | Complex for use of associated gas |
| WO2013113866A1 (en) * | 2012-02-02 | 2013-08-08 | European Aeronautic Defence And Space Company Eads France | Closed structural assembly with improved resistance to compression |
| CN104554698A (en) * | 2013-10-10 | 2015-04-29 | 陈德荣 | Capsule telescopic airship |
| CN203681861U (en) * | 2014-01-24 | 2014-07-02 | 湖南航天机电设备与特种材料研究所 | Flow control device capable of reducing aerodynamic resistance of airship and improving attitude stability |
| 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 |
| CN205738037U (en) * | 2015-06-26 | 2016-11-30 | 青岛中航浮空器研究所 | Become utricule air bag and aerostatics |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109455288A (en) * | 2017-09-06 | 2019-03-12 | 东莞前沿技术研究院 | Unload buckle structure and aerostatics |
| CN109455288B (en) * | 2017-09-06 | 2024-06-25 | 深圳光启空间技术有限公司 | Shackle structure and aerostat |
| CN108206668A (en) * | 2017-12-06 | 2018-06-26 | 苏州绿豆豆智能装备科技有限公司 | A kind of suspension column system available for Photospot solar equipment |
| CN108216552A (en) * | 2017-12-14 | 2018-06-29 | 中国特种飞行器研究所 | A kind of middle-size and small-size unmanned airship gondola connection structure |
| CN109649627A (en) * | 2019-01-28 | 2019-04-19 | 上海交通大学 | The super cold superthermal control method of high altitude airship |
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Application publication date: 20151104 |
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| RJ01 | Rejection of invention patent application after publication |