CN106553746A - Aerostatics and its utricule structure - Google Patents
Aerostatics and its utricule structure Download PDFInfo
- Publication number
- CN106553746A CN106553746A CN201510634041.0A CN201510634041A CN106553746A CN 106553746 A CN106553746 A CN 106553746A CN 201510634041 A CN201510634041 A CN 201510634041A CN 106553746 A CN106553746 A CN 106553746A
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- CN
- China
- Prior art keywords
- hydrogen
- balloonet
- aerostatics
- main gasbag
- utricule structure
- 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.)
- Pending
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- 239000001257 hydrogen Substances 0.000 claims abstract description 135
- 229910052739 hydrogen Inorganic materials 0.000 claims abstract description 135
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims abstract description 121
- 239000001307 helium Substances 0.000 claims abstract description 21
- 229910052734 helium Inorganic materials 0.000 claims abstract description 21
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims abstract description 21
- 239000007789 gas Substances 0.000 claims description 18
- 150000002431 hydrogen Chemical class 0.000 claims description 18
- 230000015572 biosynthetic process Effects 0.000 claims description 16
- 238000000746 purification Methods 0.000 claims description 9
- 210000000744 eyelid Anatomy 0.000 claims description 7
- 239000000843 powder Substances 0.000 claims description 6
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 4
- 239000003570 air Substances 0.000 description 43
- 239000002775 capsule Substances 0.000 description 6
- 238000005276 aerator Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000007667 floating Methods 0.000 description 3
- 150000004678 hydrides Chemical class 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 230000007062 hydrolysis Effects 0.000 description 2
- 238000006460 hydrolysis reaction Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- YZCKVEUIGOORGS-OUBTZVSYSA-N Deuterium Chemical compound [2H] YZCKVEUIGOORGS-OUBTZVSYSA-N 0.000 description 1
- 239000012080 ambient air Substances 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000000740 bleeding effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000011858 nanopowder Substances 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
Abstract
The invention provides a kind of aerostatics and its utricule structure.The utricule structure of the aerostatics that the present invention is provided, including for accommodating the main gasbag of helium, is also located at the air balloonet inside the main gasbag including at least one hydrogen balloonet being wrapped in inside main gasbag and at least one.Using technical scheme, while being conducive to the security performance and loading capacity for improving aerostatics, it is possible to reduce the cost of aerostatics.The aerostatics that the present invention is provided has the utricule structure of above-mentioned aerostatics.
Description
Technical field
The present invention relates to technical field of aerospace, more particularly, to a kind of aerostatics and its utricule knot
Structure.
Background technology
In prior art, for the aerostatics with closed main gasbag such as dirigible and captive balloon comes
Say, hydrogen aerostatics and helium aerostatics can be divided into according to the gas being filled with main gasbag.Its
In, the lift that rises of hydrogen aerostatics is provided by the hydrogen in main gasbag completely, hydrogen aerostatics
Cost is relatively low and deadweight is low, can provide larger loading capacity, once however, hydrogen aerostatics goes out
When existing main gasbag leaks the failure of hydrogen, fire and explosive risks is susceptible to, safety is relatively low, is also just limited
The extensive application of hydrogen aerostatics.The rising lift of helium aerostatics is then completely by main gasbag
Helium is provided, although helium aerostatics is with higher safety, helium is difficult acquisition, valency
Lattice are expensive, and helium, from anharmonic ratio hydrogen weight, the loading capacity of helium aerostatics will be less than same specification
The half of hydrogen aerostatics or so, cause the cost of helium aerostatics to be significantly larger than hydrogen aerostatics.
It is therefore proposed that a kind of not only improve the security performance and loading capacity for improving aerostatics, and can drop
The technical scheme of the cost of low aerostatics, is the technical problem of those skilled in the art's urgent need to resolve.
The content of the invention
It is an object of the present invention to provide a kind of utricule structure of aerostatics, to be conducive to improving
While the security performance and loading capacity of aerostatics, it is possible to reduce the cost of aerostatics.The present invention
Another purpose be that a kind of aerostatics is provided.
The utricule structure of the aerostatics that the present invention is provided, including for accommodating the main gasbag of helium, goes back
The hydrogen balloonet inside main gasbag and at least one is wrapped in positioned at main gasbag including at least one
Internal air balloonet.
Further, the utricule structure also includes hydrogen formation apparatus, the hydrogen of hydrogen formation apparatus
Outlet is connected with hydrogen balloonet.
Further, hydrogen formation apparatus are arranged in main gasbag.
Further, it is provided with hydrogen formation apparatus for generating the nanometer powder and water of hydrogen.
Further, the utricule structure also includes controller and the interior gas for detecting hydrogen balloonet
The sensor of pressure；Controller is electrically connected with hydrogen formation apparatus, and sensor is electrically connected with the controller.
Further, the utricule structure also includes：For detecting the hydrogen purity in hydrogen balloonet
Purity detecting device, and, the hydrogen purification apparatus being connected with hydrogen balloonet；Purity detecting
Device and hydrogen purification apparatus are electrically connected with the controller respectively.
Further, exhaust apparatus is installed on hydrogen balloonet.
Further, the eyelid covering of air balloonet has the part for sharing with the eyelid covering of main gasbag；Hydrogen
Gas balloonet is arranged near the top of main gasbag, and air balloonet is arranged on the bottom of main gasbag, empty
Gas balloonet is spaced apart at a predetermined distance from each other with hydrogen balloonet.
Present inventor is analysing in depth the basis of hydrogen aerostatics and helium aerostatics pluses and minuses
On, in order to take into account safety and the cost of aerostatics, it is proposed that the utricule structure of above-mentioned aerostatics.
In the utricule structure of the aerostatics, safe helium is accommodated in main gasbag, in main gasbag
At least one hydrogen balloonet and at least one air balloonet wrap up in portion, so that having the capsule
The aerostatics of body structure can be provided jointly by the hydrogen in the helium in main gasbag and hydrogen balloonet
Lift lift-off.Because hydrogen is readily available and low cost, conducts oneself with dignity low, it is thus advantageous to reduce floating
The cost of pocket simultaneously improves the loading capacity of aerostatics, it is even more important that using the utricule structure
Aerostatics, isolates hydrogen balloonet and air contact equivalent to by this non-combustible gas of helium,
Also the probability that hydrogen fires danger is just greatly reduced, so as to be conducive to improving the safety of aerostatics
Property.
In further technical scheme, the utricule structure also includes hydrogen formation apparatus, and hydrogen is sent out
The hydrogen outlet of generating apparatus is connected with hydrogen balloonet.So, when hydrogen balloonet is in the course of work
During middle generation leakage, hydrogen balloonet need not be opened, can be to hydrogen pair by hydrogen formation apparatus
Hydrogen is automatically replenished in air bag, the maintenance cost of aerostatics is advantageously reduced.
The aerostatics that the present invention is provided, the utricule structure with above-mentioned aerostatics.
Further, the aerostatics also includes：Keel shoe inside main gasbag；Positioned at main gas
The empennage of capsule afterbody；And, hang the gondola below main gasbag.
Description of the drawings
The accompanying drawing for constituting the part of the present invention is used for providing a further understanding of the present invention, this
Bright schematic description and description is used to explain the present invention, does not constitute to the improper of the present invention
Limit.In the accompanying drawings：
Fig. 1 diagrammatically illustrates the structure of aerostatics provided in an embodiment of the present invention.
Specific embodiment
It should be noted that in the case where not conflicting, in the embodiment and embodiment in the application
Feature can be mutually combined.Below with reference to the accompanying drawings and in conjunction with the embodiments describing the present invention in detail.
Fig. 1 shows the structure of aerostatics provided in an embodiment of the present invention, and wherein also show this
The structure of the utricule structure of the aerostatics that inventive embodiments are provided.Aerostatics in the present embodiment is with winged
As a example by ship, it is possible to understand that, although in the present embodiment aerostatics by taking dirigible as an example, but other enforcement
In example, aerostatics can also be captive balloon or other there is the aerostatics of closed main gasbag.
By utricule structure (the hereinafter referred to as utricule structure) bag that the aerostatics is can be seen that in Fig. 1
Include for accommodating the main gasbag 1 of helium, and at least one be wrapped in inside main gasbag 1 for holding
Receive the hydrogen balloonet 2 of hydrogen.By safe helium is accommodated in main gasbag 1, in hydrogen
Hydrogen is accommodated in gas balloonet 2 so that the aerostatics with the utricule structure can be by main gasbag 1
In helium and hydrogen balloonet 2 in the lift lift-off that jointly provides of hydrogen.Because hydrogen is easy
Obtain and low cost, conduct oneself with dignity it is low, be thus advantageous to reduce using the utricule structure aerostatics into
This simultaneously improves the loading capacity of aerostatics, it is even more important that using the aerostatics of the utricule structure,
Isolate hydrogen balloonet 2 and air contact equivalent to by this non-combustible gas of helium, also
The probability of combustion of hydrogen blast is greatly reduced, so as to be conducive to improving the safety of aerostatics.
Preferably also sent out including hydrogen by the utricule structure that the present embodiment offer is can be seen that in Fig. 1
Generating apparatus 3, the hydrogen outlet of hydrogen formation apparatus 3 are connected with hydrogen balloonet 2, for hydrogen
2 hydrogen make-up of gas balloonet.Hydrogen formation apparatus 3 can be internally provided with for generating hydrogen
Nanometer powder and water device, nanometer powder for example can adopt nanometer powder form hydride,
According to the hydrolysis principle of hydride, nanometer powder generates hydrogen with water reaction, and adopts nano powder
The hydride of last form is hydrolyzed and can substantially improve hydrolysis dynamics characteristic；Or, hydrogen is sent out
Generating apparatus 3 can also be suitably applied the device of aerostatics for other.So, when hydrogen balloonet
2 in the course of the work occur leakage when, hydrogen balloonet 2 need not be opened, by hydrogen formation apparatus
3 can be automatically replenished hydrogen into hydrogen balloonet 2, and then reduce the maintenance cost of aerostatics.
Preferably, hydrogen formation apparatus 3 are arranged in main gasbag 1, for example, can be fixed on main gasbag 1
On internal keel shoe so as to which hydrogen outlet is communicated with hydrogen balloonet by pipeline；Or, hydrogen
Gas generating meanss 3 can also be arranged in hydrogen balloonet 2, for example, can be fixed on and be installed on hydrogen
On the flange of 2 top eyelid covering of gas balloonet, so, hydrogen formation apparatus 3 are again by main gasbag
Helium and air insulated in 1, further increases the safety of aerostatics.
In addition, to realize hydrogen formation apparatus 3 to the automatic of 2 hydrogen make-up process of hydrogen balloonet
Control and promptness, it is preferable that the utricule structure also includes controller and for detecting hydrogen pair
The sensor of the interior air pressure of air bag 2, wherein, sensor is electrically connected with the controller, controller and hydrogen
Gas generating meanss 3 are electrically connected.When aerostatics works, sensor is by the interior gas of hydrogen balloonet 2
Pressure information transmission causes hydrogen balloonet 2 to controller if hydrogen balloonet 2 occurs leakage
Interior air pressure be less than preset value when, controller then to hydrogen formation apparatus 3 send startup generate hydrogen
Information, the hydrogen make of generation automatically supplement at any time hydrogen so as to reach in hydrogen balloonet 2
The purpose of gas.It is appreciated that when the interior air pressure of hydrogen balloonet 2 reaches preset value, can be with
Sent to hydrogen formation apparatus 3 by controller and stop the information for generating hydrogen, realize hydrogen pair gas
Capsule 2 hydrogen make-up process is automatically controlled.
Additionally, the utricule structure preferably also includes：It is pure for detecting the hydrogen in hydrogen balloonet
The purity detecting device of degree, and, the hydrogen purification apparatus being connected with hydrogen balloonet.Purity is examined
Device and hydrogen purification apparatus are surveyed, is respectively used to be electrically connected with the controller and installed in utricule structure
Correct position.So, when hydrogen balloonet because leakage or other reasonses are caused in hydrogen balloonet
Hydrogen when being contaminated, by purity detecting device by the hydrogen purity information in hydrogen balloonet
Controller is passed to, if the hydrogen purity in hydrogen balloonet is less than preset value, controller can
To control hydrogen purification apparatus startup work so that the gas in hydrogen balloonet is through hydrogen purification
It is back in hydrogen balloonet after device purification, to ensure that the hydrogen purity in hydrogen balloonet does not exist
In the range of its explosion limit, and then improve the operational security of aerostatics.
Preferably, it is also equipped with hydrogen balloonet for discharging gas in hydrogen balloonet
Exhaust apparatus (not shown), exhaust apparatus are, for example, the suitable structure such as hydrogen valve, to keep away
Exempt from because of the excessive destruction for causing hydrogen balloonet of the air pressure in hydrogen balloonet.
By in Fig. 1 it can also be seen that the utricule structure also including at least one be located at main gasbag 1 in
The air balloonet 4 in portion, air balloonet 4 are used to accommodate air, are commonly provided with exhaust apparatus 41,
Exhaust apparatus 41 for example includes exhaust fan, air bleeding valve etc..By arranging air balloonet 4, when floating
Pocket can keep rational pressure reduction inside and outside main bag body 1 in aloft work, prevent main gasbag 1 swollen
It is broken.The operation principle of air balloonet 4 is specific as follows：Before aerostatics goes up to the air, air pair gas
Air is charged in capsule 4；With the increase of aerostatics lifting height, external ambient air pressure is reduced, main
1 inside and outside differential pressure of air bag increases, and main gasbag 1 expands, and now opens the aerofluxuss dress of air balloonet 4
41 are put, air balloonet 4 is subject to the extruding of helium in main gasbag 1 to reduce, while so that main gasbag
1 interior air pressure reduces, it is ensured that main gasbag 1 is not burst, it is ensured that aerostatics is skyborne outer
Shape and buoyancy.It is appreciated that air balloonet except configure exhaust apparatus 41 in addition to, be also configured with into
(not shown in figure, such as aerator, aerator can be fixed on the outer surface of main gasbag to device of air
On, by pipeline communication air balloonet and free surrounding space；Or aerator can also be fixed on sky
The outside of gas balloonet), for air is supplemented into air balloonet, the air pressure of air balloonet is surveyed
Amount is controlled by corresponding control system with intake and exhaust operation, be will not be described here.
Preferably, the eyelid covering of air balloonet 4 has the part for sharing with the eyelid covering of main gasbag 1,
So contribute to further reducing the deadweight of aerostatics, and then the loading capacity of aerostatics can be improved.
Preferably, air balloonet 4 is spaced apart at a predetermined distance from each other with the hydrogen balloonet 2, in air
Balloonet 4 is non-interference with hydrogen balloonet 2 when being full of.Preferably, also illustrate that in the present embodiment
The preferred arrangement of hydrogen balloonet 2 and air balloonet 4, as illustrated, can be by hydrogen
Gas balloonet 2 is arranged near the top of main gasbag 1, and air balloonet 4 is arranged on main gasbag 1
Bottom.It is appreciated that the mounting means of hydrogen balloonet 2 and air balloonet 4 can be using current
The mounting means of all kinds of dirigible air balloonets is installed, i.e., directly weld corresponding skin material
In 1 corresponding site of main gasbag for designing forming each different independent air chamber.
Referring again to Fig. 1, aerostatics provided in an embodiment of the present invention has the capsule of above-mentioned aerostatics
Body structure.Because the utricule structure of aerostatics provided in an embodiment of the present invention can reach above-mentioned technology effect
Really, the aerostatics that application has the utricule structure should also possess corresponding technique effect, and here is no longer gone to live in the household of one's in-laws on getting married
State.
Preferably, the aerostatics also includes：Keel shoe inside main gasbag 1, positioned at main gas
The empennage 5 of 1 afterbody of capsule, and, hang the gondola 6 below main gasbag 1.Wherein, empennage 5
Play stability contorting effect；Gondola 6 can be by hanging rope and main gasbag 1 or air balloonet
4 connections.In addition, for the aerostatics of airship type, generally also including propulsion plant, use
In for the taking off of dirigible, land and hovering provides power.Propulsion plant can be propeller,
Air jet system or other power set, apply the needs in direction according to power, are arranged on floating
On the outer surfaces such as pocket, gondola.
Presently preferred embodiments of the present invention is these are only, it is not to limit the present invention, all at this
Within the spirit and principle of invention, any modification, equivalent substitution and improvements made etc. all should be wrapped
It is contained within protection scope of the present invention.
Claims (10)
1. the utricule structure of a kind of aerostatics, including for accommodating the main gasbag of helium, its feature exists
In the hydrogen balloonet and at least one being also wrapped in including at least one inside the main gasbag
Air balloonet inside the main gasbag.
2. utricule structure according to claim 1, it is characterised in that also occur including hydrogen
Device, the hydrogen outlet of the hydrogen formation apparatus are connected with the hydrogen balloonet.
3. utricule structure according to claim 2, it is characterised in that the hydrogen occurs dress
Put in the main gasbag.
4. utricule structure according to claim 2, it is characterised in that the hydrogen occurs dress
It is provided with putting for generating the nanometer powder and water of hydrogen.
5. utricule structure according to claim 2, it is characterised in that also including controller and
For detecting the sensor of the interior air pressure of the hydrogen balloonet；The controller is sent out with the hydrogen
Generating apparatus are electrically connected, and the sensor is electrically connected with the controller.
6. utricule structure according to claim 5, it is characterised in that also include：For examining
The purity detecting device of the hydrogen purity surveyed in the hydrogen balloonet, and, with the hydrogen pair
The hydrogen purification apparatus of air bag connection；The purity detecting device and hydrogen purification apparatus difference
Electrically connect with the controller.
7. utricule structure according to claim 2, it is characterised in that the hydrogen balloonet
On exhaust apparatus is installed.
8. utricule structure according to claim 1, it is characterised in that the air balloonet
The eyelid covering of eyelid covering and the main gasbag there is the part for sharing；The hydrogen balloonet is near described
The top of main gasbag is arranged, and the air balloonet is arranged on the bottom of the main gasbag, the sky
Gas balloonet is spaced apart at a predetermined distance from each other with the hydrogen balloonet.
9. a kind of aerostatics, it is characterised in that with any one of claim 1 to 8
The utricule structure of aerostatics.
10. aerostatics according to claim 9, it is characterised in that the aerostatics is also wrapped
Include：Keel shoe inside the main gasbag；Positioned at the empennage of the main gasbag afterbody；And,
Hang the gondola below the main gasbag.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510634041.0A CN106553746A (en) | 2015-09-28 | 2015-09-28 | Aerostatics and its utricule structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510634041.0A CN106553746A (en) | 2015-09-28 | 2015-09-28 | Aerostatics and its utricule structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106553746A true CN106553746A (en) | 2017-04-05 |
Family
ID=58415954
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510634041.0A Pending CN106553746A (en) | 2015-09-28 | 2015-09-28 | Aerostatics and its utricule structure |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108528674A (en) * | 2018-03-09 | 2018-09-14 | 中国电子科技集团公司第三十八研究所 | Near space dirigible and its surface flow field control method |
| WO2019157577A1 (en) * | 2018-02-19 | 2019-08-22 | Melo Andre Augusto Ceballos | Aerostat reinforcement system and method |
| CN112461051A (en) * | 2020-11-19 | 2021-03-09 | 中国人民解放军国防科技大学 | Long-endurance low-energy-consumption interception and capture system for non-cooperative cluster flying target |
| CN113060271A (en) * | 2021-03-03 | 2021-07-02 | 浙江热土航空发展有限公司 | Hydrogen energy airship with novel airbag layout and using method |
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| CN112461051A (en) * | 2020-11-19 | 2021-03-09 | 中国人民解放军国防科技大学 | Long-endurance low-energy-consumption interception and capture system for non-cooperative cluster flying target |
| CN113060271A (en) * | 2021-03-03 | 2021-07-02 | 浙江热土航空发展有限公司 | Hydrogen energy airship with novel airbag layout and using method |
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