CN106043659A - Field air inflation and unfolding method for aerostat - Google Patents
Field air inflation and unfolding method for aerostat Download PDFInfo
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- CN106043659A CN106043659A CN201610425300.3A CN201610425300A CN106043659A CN 106043659 A CN106043659 A CN 106043659A CN 201610425300 A CN201610425300 A CN 201610425300A CN 106043659 A CN106043659 A CN 106043659A
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- aerostatics
- utricule
- anchoring
- mooring system
- aerostat
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/66—Mooring attachments
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- Aviation & Aerospace Engineering (AREA)
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Abstract
The invention relates to the technical field of aerostats, in particular to a field air inflation and unfolding method for an aerostat. The field air inflation and unfolding method comprises the following steps that S1, a nose tower of anchoring equipment is connected with a nose cone of a bag body of the aerostat, ground auxiliary launching vehicles are connected with the side surface of the bag body of the aerostat through side lanyards, and helium storage equipment is connected with the bag body of the aerostat; S2, the bag body of the aerostat is continuously filled with helium through the helium storage equipment, the nose tower of the anchoring equipment is gradually raised to pull the bag body of the aerostat to rise, and the side lanyards are loosened along with rising of the bag body in a matched mode; S3, after the bag body of the aerostat rises and leaves the ground, an equipment pod is installed on the lower portion of the bag body of the aerostat, and an aerostat draught fan is connected with the equipment pod; S4, a ballonet of the aerostat is filled with air through the aerostat draught fan; S5, the side lanyards are pulled into a side arm of the anchoring equipment and are tightened, and the ground auxiliary launching vehicles are removed; and S6, the length of the side lanyards of the aerostat is adjusted so that the unfolding state of the aerostat can reach the anchoring posture.
Description
Technical field
The present invention relates to aerostatics technical field, particularly relate to a kind of inflating expanded method in aerostatics field.
Background technology
Aerostatics refers to internal filling light gas (being lighter than air), relies on or rely primarily on the realization of air net buoyancy at present
The airborne vehicle of lift-off, type is divided into free balloon, captive balloon and dirigible.Free balloon not drive, the most freely wafts；System
Stay balloon not drive, reside in aerial precalculated position by connecting the hawser of ground installation；Dirigible is then that one is carried dynamic
The aerostatics of power, relies on self power to realize controllable maneuvering flight.
Generally aerostatics due to structure huge, system composition complexity, it is therefore desirable to bigger boathouse provide before capsule
Body inflation and equipment install etc. preliminary preparation.The releasing mode being usually taken both at home and abroad at present is: first providing field
The boathouse that ground construction scale is huge, then at the internally installed equipment of boathouse, is inflated utricule structure, and is allowed to set with granting
Standby connected；Inflate complete after by delivery apparatus by aerostatics traction to provide place let fly away.Its advantage is owing to having
Boathouse, preliminary preparation can be carried out inside boathouse, free from the influence of the external environment.Its shortcoming is then to need letting field fly away
Boathouse is built on ground, or lets place fly away and must select the place of boathouse, and these demands then significantly increase aerostatics and let fly away
Cost, and limit the selection letting region fly away, it is impossible to embody that its survival ability is strong, motility is high, use cost is low
Feature.
Summary of the invention
(1) to solve the technical problem that
The technical problem to be solved in the present invention be solve existing aerostatics provide before inflating expanded time need at personal boat
Carrying out in storehouse, boathouse construction is limited by place, and therefore also limit aerostatics lets region fly away, and the motility to aerostatics is made
Become harmful effect, the problem that the construction of boathouse too increases the cost that aerostatics field trial is let fly away simultaneously.
(2) technical scheme
In order to solve above-mentioned technical problem, the invention provides a kind of inflating expanded method in aerostatics field, including following
Step:
S1, is connected the nose cone of the nose tower and the utricule of aerostatics that are in level of anchoring and mooring system, is assisted on ground
Distributing vehicle is connected by side lashing with the fixing tab of the utricule side of aerostatics, helium storage device and the utricule of aerostatics
Bottom inflatable mouth connect；
S2, continues to be filled with helium inside the utricule of aerostatics by helium storage device, and the nose tower of anchoring and mooring system is gradually
The utricule raising traction aerostatics raises, and side lashing coordinates utricule to raise and loosen；
S3, after the utricule of aerostatics lifts off ground, installs equipment pod in the utricule bottom of aerostatics, and will be floating
Pocket blower fan is connected with equipment pod；
S4, will be full of air by aerostatics blower fan in the balloonet of aerostatics；
S5, draws side lashing into the side arm of anchoring and mooring system and tightens up, and removes ground auxiliary distributing vehicle；
S6, adjusts the length of the side lashing of aerostatics so that the deployed condition of aerostatics reaches the attitude that anchors.
Wherein, further comprising the steps of before step S1:
S01, the stand of selected anchoring and mooring system；
S02, by the utricule lay of aerostatics at the lower wind direction of anchoring and mooring system；
S03, by the top rotation platform locking of anchoring and mooring system；
S04, is positioned over level by the nose tower of anchoring and mooring system.
Wherein, the nose cone of the utricule of described aerostatics is connected with the nose tower cylinder of described anchoring and mooring system by nose lashing, institute
State helium storage device to be connected by gas tube with the bottom inflatable mouth of the utricule of described aerostatics.
Wherein, further comprising the steps of between step S4 and step S5:
S41, after the nose tower of anchoring and mooring system is raised to vertical state, is persistently filled with helium to the utricule of aerostatics until floating
The entirely pneumatic molding of utricule of pocket；
S42, is disconnected gas tube by the bottom inflatable mouth of the utricule of aerostatics, and seals bottom inflatable mouth；
S43, tightens up nose lashing and makes the nose cone of utricule of aerostatics completely into the horn mouth of the nose tower of anchoring and mooring system and lock
Tightly；
S44, is connected gas tube with the head inflating mouth of the utricule of aerostatics, continues to be filled with inside the utricule of aerostatics
Helium；
S45, opens the air bleeding valve of the balloonet of aerostatics, discharges partial air therein until helium aeration quantity reaches pre-
If value；
S46, stops filling helium, is disconnected by the head inflating mouth of the utricule of aerostatics by gas tube, close aerostatics
The air bleeding valve of balloonet；
Wherein, further comprising the steps of between step S5 and step S6:
S51, opens the top rotation platform of anchoring and mooring system.
Wherein, described ground auxiliary distributing vehicle includes cylinder, car body and auxiliary lashing, and described cylinder is arranged at described car body
On, described auxiliary lashing one end is connected with described cylinder, and the other end is connected with described side lashing.
Wherein, described anchoring and mooring system is anchoring car.
(3) beneficial effect
The technique scheme of the present invention has the advantage that the inflating expanded method in aerostatics field of the present invention makes whole
The inflating expanded process of aerostatics is carried out the most in the wild, it is not necessary to the guarantee of boathouse, reduces the requirement providing place, pole
The big cost reducing aerostatics field trial, adds the flexibility ratio of place election simultaneously；The installation process of equipment pod
It is interspersed in the gas replenishment process to utricule and carries out, decrease the operating time, reduce the risk of field inflation；Auxiliary provides vehicle
For wheeled construction, can freely walk providing place, add the motility that aerostatics is inflating expanded；Inflating expanded at aerostatics
During, the nose tower of anchoring and mooring system is along with the slowly rising that increases of amount of helium, ground auxiliary distributing vehicle and the utricule side of aerostatics
Face connects fixing, it is to avoid equipment the waving and vibrating during inflating expanded such as the utricule of aerostatics and gondola, are a kind of
Stable inflating expanded method；The equipment that the present invention relates to is simple, and to providing, site requirements is the highest, it is adaptable to most floating
Pocket inflating expanded.
Except the technical characteristic of technical scheme that described above present invention solves the technical problem that, constitute and there is this
Outside the advantage that the technical characteristic of a little technical schemes is brought, the other technologies feature of the present invention and these technical characteristics bring
Advantage, will further illustrate in conjunction with accompanying drawing.
Accompanying drawing explanation
Fig. 1 is the process schematic of step S1 of the inflating expanded method in embodiment of the present invention aerostatics field；
Fig. 2 is step S2 and the process schematic of step S3 of the inflating expanded method in embodiment of the present invention aerostatics field；
Fig. 3 is the process schematic of step S5 of the inflating expanded method in embodiment of the present invention aerostatics field；
Fig. 4 is the process schematic of step S44 of the inflating expanded method in embodiment of the present invention aerostatics field；
Fig. 5 is the process schematic of step S6 of the inflating expanded method in embodiment of the present invention aerostatics field.
In figure: 1: utricule；2: anchoring and mooring system；3: ground auxiliary distributing vehicle；4: helium storage device；5: gas tube；6: set
Standby gondola；7: balloonet；8: side-line rope；9: nose lashing；21: nose tower；22: side arm；31: auxiliary lashing；32: cylinder；33: car
Body.
Detailed description of the invention
For making the purpose of the embodiment of the present invention, technical scheme and advantage clearer, below in conjunction with the embodiment of the present invention
In accompanying drawing, the technical scheme in the embodiment of the present invention is clearly and completely described, it is clear that described embodiment is
A part of embodiment of the present invention rather than whole embodiments.Based on the embodiment in the present invention, ordinary skill people
The every other embodiment that member is obtained on the premise of not making creative work, broadly falls into the scope of protection of the invention.
In describing the invention, it should be noted that unless otherwise clearly defined and limited, term " is installed ", " phase
Even ", " connection " should be interpreted broadly, for example, it may be fixing connection, it is also possible to be to removably connect, or be integrally connected；Can
To be mechanical connection, it is also possible to be electrical connection；Can be to be joined directly together, it is also possible to be indirectly connected to by intermediary, Ke Yishi
The connection of two element internals.For the ordinary skill in the art, can understand that above-mentioned term is at this with concrete condition
Concrete meaning in invention.
Additionally, in describing the invention, except as otherwise noted, " multiple ", " many ", " many groups " be meant that two or
Two or more, " several ", " some ", " some groups " are meant that one or more.
The inflating expanded method in aerostatics field that the embodiment of the present invention provides, comprises the following steps:
S1, as it is shown in figure 1, connect the nose cone of the nose tower 21 being in level of anchoring and mooring system 2 with the utricule 1 of aerostatics
Connecing, ground is assisted distributing vehicle 3 be connected by side lashing 8 with the fixing tab of utricule 1 side of aerostatics, helium storage sets
Standby 4 are connected with the bottom inflatable mouth of the utricule 1 of aerostatics；
S2, as in figure 2 it is shown, be filled with helium by lasting utricule 1 inside to aerostatics of helium storage device 4, anchoring sets
The nose tower 21 of standby 2 is gradually raised the utricule 1 of traction aerostatics and is raised, and side lashing 8 coordinates utricule 1 to raise and loosen；
S3, as in figure 2 it is shown, after the utricule 1 of aerostatics lifts off ground, install in utricule 1 bottom of aerostatics and set
Standby gondola 6, and aerostatics blower fan is connected with equipment pod 6；
S4, will be full of air by aerostatics blower fan in the balloonet 7 of aerostatics；
S5, as it is shown on figure 3, drawn by side lashing 8 into the side arm 22 of anchoring and mooring system 2 and tighten up, removes ground auxiliary and sends out
Put car 3；
S6, as it is shown in figure 5, adjust the length of the side lashing 8 of aerostatics so that the deployed condition of aerostatics reaches anchoring
Attitude.
The inflating expanded method in aerostatics field of the present invention makes the inflating expanded process of whole aerostatics enter the most in the wild
OK, it is not necessary to the guarantee of boathouse, reduce the requirement providing place, greatly reduce the cost of aerostatics field trial,
Add the flexibility ratio of place election simultaneously；The installation process of equipment pod is interspersed in the gas replenishment process to utricule and carries out, and subtracts
Lack the operating time, reduce the risk of field inflation；It is wheeled construction that auxiliary provides vehicle, can provide place free walker
Walk, add the motility that aerostatics is inflating expanded；During aerostatics is inflating expanded, helium storage device continues to utricule
Inside being filled with helium, the nose tower of anchoring and mooring system is along with the slowly rising that increases of amount of helium, ground auxiliary distributing vehicle and the capsule of aerostatics
Body side surface connects fixing, it is to avoid equipment the waving and vibrating during inflating expanded such as the utricule of aerostatics and gondola, is
A kind of stable inflating expanded method；The equipment that the present invention relates to is simple, and to providing, site requirements is the highest, it is adaptable to the most most
Count the inflating expanded of aerostatics.
Wherein, further comprising the steps of before step S1:
S01, the stand of selected anchoring and mooring system 2；
S02, by utricule 1 lay of aerostatics at the lower wind direction of anchoring and mooring system 2；
S03, by the top rotation platform locking of anchoring and mooring system 2；
S04, places 21 in level by the nose tower of anchoring and mooring system 2.
Owing to inflating in the wild, before aerostatics is inflated, therefore need fully to understand inflation weather condition on the same day and follow-up
Change, typically requires that wind speed is not more than 5m/s.The placement location of selected anchoring and mooring system, the utricule lay of aerostatics is in anchoring and mooring system
Lower wind direction at, by the top rotation platform locking of anchoring and mooring system, it is ensured that aerating position firm, not by the shadow of field wind-force
Ring.
Wherein, as depicted in figs. 1 and 2, the nose cone of the utricule 1 of aerostatics is by the nose tower 21 of nose lashing 9 with anchoring and mooring system 2
Cylinder connects, and helium storage device 4 is connected by gas tube 5 with the bottom inflatable mouth of the utricule 1 of aerostatics.Nose tower is tilted to
Level, the nose cone of utricule enters the nose tower cylinder of anchoring and mooring system by nose lashing and fixes, the utricule side of aerostatics with
Ground auxiliary distributing vehicle connects fastening, it is ensured that utricule will not swing in gas replenishment process with the wind.Helium storage device first passes through fills
Trachea is connected with bottom inflatable mouth as standby inflation inlet on utricule, is filled with helium, makes gas inside utricule in utricule
The most gradually accumulate, it is ensured that the stability of utricule molding in gas replenishment process.
Wherein, as shown in Fig. 3, Fig. 4 and Fig. 5, further comprising the steps of between step S4 and step S5:
S41, after the nose tower 21 of anchoring and mooring system 2 is raised to vertical state, persistently to be filled with helium straight for the utricule 1 to aerostatics
The entirely pneumatic molding of utricule 1 to aerostatics；
S42, is disconnected gas tube 5 by the bottom inflatable mouth of the utricule 1 of aerostatics, and carries out close to bottom inflatable mouth
Envelope；
S43, tightens up nose lashing 9 and makes the nose cone of utricule 1 of aerostatics completely into the horn mouth of the nose tower 21 of anchoring and mooring system 2
And lock；
S44, is connected the head inflating mouth of gas tube 5 with the utricule 1 of aerostatics, continues to the utricule 1 of aerostatics internal
It is filled with helium；
S45, opens the air bleeding valve of the balloonet 7 of aerostatics, discharges partial air therein until helium aeration quantity reaches
Preset value；
S46, stops filling helium, is disconnected by the head inflating mouth of the utricule 1 of aerostatics by gas tube 5, close aerostatics
The air bleeding valve of balloonet 7；
During utricule fills helium, helium storage device continues the utricule inner inflatable to aerostatics, along with amount of helium
Increasing, utricule gradually expands rising, now adjusts anchoring car nose tower angle so that it is along with utricule raises progressively lifting, adjust simultaneously
The length of the side lashing that whole utricule is connected with ground auxiliary distributing vehicle, until equipment pod installation site is lifted away from ground on utricule
Face, now installs equipment pod, is connected with actuators such as utricule blower fan, valves by equipment pod, and utricule gradually floats rising
The nose tower of anchoring and mooring system also with traction lifting, when nose tower be raised to by level completely erected after, until being persistently filled with helium
To the complete molding of utricule, now disconnect gas tube and to bottom inflation inlet seal, then tighten up nose lashing make nose cone completely into
Nose tower horn mouth is also locked.Now gas tube moved to as the head inflating mouth of utricule main gas charge mouth and connect, continuing to capsule
Internal portion is filled with helium, opens balloonet air bleeding valve simultaneously, will be full of the sky of the balloonet of aerostatics before this by aerostatics blower fan
Gas is discharged, until amount of helium reaches predetermined value.After amount of helium in aerostatics reaches predetermined value, by helium storage device and secondary gas
The air bleeding valve of capsule is turned off, and unloads gas tube.
Wherein, ground auxiliary distributing vehicle 3 includes cylinder 32, car body 33 and auxiliary lashing 31, and cylinder 32 is arranged at car body 33
On, auxiliary lashing 31 one end is connected with cylinder 32, and auxiliary lashing 31 other end is connected with side lashing 8.Ground auxiliary distributing vehicle
Car body carry cylinder, auxiliary lashing be connected with cylinder and side lashing connection, cylinder can be passed through in aerostatics gas replenishment process
Rotate and adjust its tightness being connected with side lashing, in order to adjust according to the inflation float state of aerostatics and stablize aerostatics
Degree of stability, car body form is moved easily, be conducive to be adjusted according to the position of actual aerostatics.
Wherein, further comprising the steps of between step S5 and step S6:
S51, opens the top rotation platform of anchoring and mooring system 2.
Utricule fill helium complete after, disconnect gas tube, then tighten up side-line rope, until auxiliary distributing vehicle be connected with side-line rope
Auxiliary lashing fully relaxed, now remove ground auxiliary distributing vehicle, and open anchoring and mooring system top rotation platform so that it is can
Rotating with the wind, aerostatics proceeds to anchored condition, completes the inflating expanded operation in aerostatics field.
Wherein, anchoring and mooring system 2 is anchoring car.Anchoring and mooring system is the anchoring car of wheeled construction, can provide place free walker
Walk, add aerostatics inflating expanded motility.
In sum, the inflating expanded method in aerostatics field of the present invention makes the inflating expanded process of whole aerostatics complete
Carry out in the wild, it is not necessary to the guarantee of boathouse, reduce the requirement providing place, greatly reduce aerostatics field trial
Cost, add the flexibility ratio of place election simultaneously；The installation process of equipment pod is interspersed in the gas replenishment process to utricule
Carry out, decrease the operating time, reduce the risk of field inflation；It is wheeled construction that auxiliary provides vehicle, can provide place
Freely walk, add the motility that aerostatics is inflating expanded；During aerostatics is inflating expanded, helium storage device continues
Being filled with helium in utricule, the nose tower of anchoring and mooring system is along with the slowly rising that increases of amount of helium, ground auxiliary distributing vehicle and floating
The utricule side of device connects fixing, it is to avoid equipment the waving and shaking during inflating expanded such as the utricule of aerostatics and gondola
Dynamic, it is a kind of stable inflating expanded method；The equipment that the present invention relates to is simple, and to providing, site requirements is the highest, it is adaptable to
Most aerostatics inflating expanded.
Last it is noted that above example is only in order to illustrate technical scheme, it is not intended to limit；Although
With reference to previous embodiment, the present invention is described in detail, it will be understood by those within the art that: it still may be used
So that the technical scheme described in foregoing embodiments to be modified, or wherein portion of techniques feature is carried out equivalent；
And these amendment or replace, do not make appropriate technical solution essence depart from various embodiments of the present invention technical scheme spirit and
Scope.
Claims (7)
1. the inflating expanded method in aerostatics field, it is characterised in that: comprise the following steps:
S1, is connected the nose cone of the nose tower and the utricule of aerostatics that are in level of anchoring and mooring system, ground auxiliary is provided
Car is connected by side lashing with the fixing tab of the utricule side of aerostatics, the end of the utricule of helium storage device and aerostatics
Portion's inflation inlet connects；
S2, continues to be filled with helium inside the utricule of aerostatics by helium storage device, and the nose tower of anchoring and mooring system is gradually raised
The utricule of traction aerostatics raises, and side lashing coordinates utricule to raise and loosen；
S3, after the utricule of aerostatics lifts off ground, installs equipment pod in the utricule bottom of aerostatics, and by aerostatics
Blower fan is connected with equipment pod；
S4, will be full of air by aerostatics blower fan in the balloonet of aerostatics；
S5, draws side lashing into the side arm of anchoring and mooring system and tightens up, and removes ground auxiliary distributing vehicle；
S6, adjusts the length of the side lashing of aerostatics so that the deployed condition of aerostatics reaches the attitude that anchors.
The inflating expanded method in aerostatics field the most according to claim 1, it is characterised in that: also include following before step S1
Step:
S01, the stand of selected anchoring and mooring system；
S02, by the utricule lay of aerostatics at the lower wind direction of anchoring and mooring system；
S03, by the top rotation platform locking of anchoring and mooring system；
S04, is positioned over level by the nose tower of anchoring and mooring system.
The inflating expanded method in aerostatics field the most according to claim 1, it is characterised in that: the utricule of described aerostatics
Nose cone is connected with the nose tower cylinder of described anchoring and mooring system by nose lashing, described helium storage device and the utricule of described aerostatics
Bottom inflatable mouth connected by gas tube.
The inflating expanded method in aerostatics field the most according to claim 3, it is characterised in that: between step S4 and step S5
Further comprising the steps of:
S41, after the nose tower of anchoring and mooring system is raised to vertical state, is persistently filled with helium to the utricule of aerostatics until aerostatics
The entirely pneumatic molding of utricule；
S42, is disconnected gas tube by the bottom inflatable mouth of the utricule of aerostatics, and seals bottom inflatable mouth；
S43, tightens up nose lashing and makes the nose cone of utricule of aerostatics completely into the horn mouth of the nose tower of anchoring and mooring system and lock；
S44, is connected gas tube with the head inflating mouth of the utricule of aerostatics, continues to be filled with helium inside the utricule of aerostatics
Gas；
S45, opens the air bleeding valve of the balloonet of aerostatics, discharges partial air therein until helium aeration quantity reaches default
Value；
S46, stops filling helium, is disconnected by the head inflating mouth of the utricule of aerostatics by gas tube, close the secondary gas of aerostatics
The air bleeding valve of capsule.
The inflating expanded method in aerostatics field the most according to claim 2, it is characterised in that: between step S5 and step S6
Further comprising the steps of:
S51, opens the top rotation platform of anchoring and mooring system.
The inflating expanded method in aerostatics field the most according to claim 1, it is characterised in that: described ground auxiliary distributing vehicle
Including cylinder, car body and auxiliary lashing, described cylinder is arranged on described car body, and described auxiliary lashing one end is with described cylinder even
Connecing, the other end is connected with described side lashing.
The inflating expanded method in aerostatics field the most according to claim 1, it is characterised in that: described anchoring and mooring system is anchoring
Car.
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| CN107719624A (en) * | 2017-09-30 | 2018-02-23 | 山西铱格斯曼航空科技有限公司 | A kind of state of ground of stratosphere aerostatics is anti-vertical and inflates restoration methods |
| CN108263589A (en) * | 2016-12-30 | 2018-07-10 | 海口未来技术研究院 | Discharge the method for aerostatics |
| CN111055750A (en) * | 2019-12-13 | 2020-04-24 | 中国特种飞行器研究所 | Mooring balloon rapid deployment anchoring system |
| CN111547220A (en) * | 2020-04-15 | 2020-08-18 | 中国科学院空天信息创新研究院 | Forming and distributing method for stratospheric airship |
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| CN110065648A (en) * | 2019-04-19 | 2019-07-30 | 中国电子科技集团公司第三十八研究所 | A kind of anchoring semi-mounted chassis being tethered at for large-scale captive balloon with transition transport |
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| CN104890851A (en) * | 2015-05-25 | 2015-09-09 | 湖南航天机电设备与特种材料研究所 | Near space balloon system safety release method |
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| CN108263589A (en) * | 2016-12-30 | 2018-07-10 | 海口未来技术研究院 | Discharge the method for aerostatics |
| CN107719624A (en) * | 2017-09-30 | 2018-02-23 | 山西铱格斯曼航空科技有限公司 | A kind of state of ground of stratosphere aerostatics is anti-vertical and inflates restoration methods |
| CN107719624B (en) * | 2017-09-30 | 2020-04-07 | 山西铱格斯曼航空科技有限公司 | Ground state anti-sagging and inflation recovery method for stratospheric aerostat |
| CN111055750A (en) * | 2019-12-13 | 2020-04-24 | 中国特种飞行器研究所 | Mooring balloon rapid deployment anchoring system |
| CN111547220A (en) * | 2020-04-15 | 2020-08-18 | 中国科学院空天信息创新研究院 | Forming and distributing method for stratospheric airship |
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