CN106275363A - A kind of microminiature captive balloon system - Google Patents
A kind of microminiature captive balloon system Download PDFInfo
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- CN106275363A CN106275363A CN201610879143.3A CN201610879143A CN106275363A CN 106275363 A CN106275363 A CN 106275363A CN 201610879143 A CN201610879143 A CN 201610879143A CN 106275363 A CN106275363 A CN 106275363A
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- spheroid
- captive balloon
- capstan
- captive
- balloon
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/40—Balloons
- B64B1/50—Captive balloons
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/40—Balloons
- B64B1/42—Construction or attachment of stabilising surfaces
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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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- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
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Abstract
The invention discloses a kind of microminiature captive balloon, relate to captive balloon field, it includes that microsphere system, capstan system, gas charging system, ground control and reception system, cable system, load system and storage AIR CONVECTOR TECH.Wherein in microsphere system, spheroid is oblate revolution spheroid, and not only wind resistance is effective, good stability, and folding and unfolding is convenient, takes up space little.Wherein capstan system medium power system is folding and unfolding hand crank or retracting motor, easy to carry.The microminiature captive balloon that the present invention proposes is easy and simple to handle, and action required personnel are few, can rapid deployment, flexible；Low to site requirements, can in city, rural area or remote districts launch and provide.
Description
Technical field
The present invention relates to captive balloon field, particularly relate to a kind of small-sized captive balloon system.
Background technology
Load is observed, communication, the task such as take photo by plane are widely used for a long time to utilize aerial platform to carry,
Aerial platform provides observation visual angle and the covering power that a ground surface platform does not possesses, and have more preferable survival ability and
Ability to communicate.Its platform that can carry includes captive balloon, unmanned plane, dirigible etc., and different platform cuts both ways, and is respectively applied to
Matched occasion.Unmanned plane cruising time is short, load is little, poor stability, it is adaptable to take photo by plane in short-term；Weigh-off is good, fly
Line stabilization, can be used for taking photo by plane in short-term, observation etc.；Although captive balloon can not arbitrarily move in being fixed on certain area, but can
Long-time mooring in the air, aerial observation lasting when being suitable for long, communication relaying etc..
Captive balloon has long history, is developed so far the design having defined comparative maturity.Captive balloon divides greatly
Medium-sized and mini-system, is respectively suitable for different occasion, and big-and-middle-sized system load is big, lift-off is the highest, but system complex, occupation of land
Greatly, action required personnel are many；Although small-sized even microminiature captive balloon system load is little but action required personnel are few, operation letter
Single.The generally composition of captive balloon specifically includes that spheroid, heaving pile, ground tackle three parts.
Generally spheroid includes that streamlined spheroid air bag adds empennage, and tab thereon, rigging, charging valve, air bleeding valve
The devices such as door, bigger captive balloon also has the balloonet of independent control.Existing captive balloon ball-type is the most streamlined, specially
Door, for mooring operating mode, therefore has bigger round end and gradually receives thin afterbody, the thinnest thin before and after being different from dirigible
Long streamlined.Spheroid air bag is usually consistent with the material of empennage, for medium-and-large-sized captive balloon, and ball material generally height
The fibrous composite of intensity, the also use high score subclass thin-film material that small-sized captive balloon has is to reduce weight.
Heaving pile includes hawser, attachment means etc., and hawser can be high intensity stay cord, it is also possible to be to add power supply or signal
Compound mooring rope, attachment means can be common slip ring or photoelectricity is combined slip ring.
The key component of ground tackle is mooring capstan and extension and retraction system, is used for making the lift-off of captive balloon spheroid and returning
Receive.Additionally include spheroid anchoring fixing device, for power distribution equipment, control device etc..The ground tackle of medium-and-large-sized captive balloon
Typically there is an anchoring tower that can erect and fall, for the about bundled ball body nose cone when anchoring.Anchoring tower and a whole set of anchoring system
System freely can turn round along base, thus makes spheroid box haul adjust to spheroid just to direction of the wind comes from when anchoring, now spheroid
The windage being subject to is minimum, and system stressing conditions is best, bad by windage loss when being possible to prevent spheroid to anchor.Ground tackle is according to system
Scale is different with use occasion, it is also possible to be roughly divided into portable and fixed two classes.Portable ground tackle is usually to be installed
Above motor vehicles or torr trailer, can receive folded and launch, receiving and can move with vehicle under overlapping state, need anchoring or mooring
Time then launch use；It is main that fixed ground tackle typically only includes capstan winch and extension and retraction system and spheroid anchoring fixed system etc.
Device, typically can not arbitrarily move after being placed in the three unities.
Although current existing captive balloon Technical comparing is ripe, but along with the development in epoch, people are to captive balloon
Require also in change.Than if any occasion common vehicle cannot arrive, can only single enter, this just requires aerial observation and communication
System accomplishes microminiature and flexible.The general sphere size of traditional captive balloon is the biggest, at present can band load work
Captive balloon minimum dimension general also more than 10 meters, and need the ground anchoring facility of Medium Truck rank, mooring gas
The personnel of the operation such as ball folding and unfolding the most at least need more than 4～6 people, and large balloon even needs tens of people to operate, and goes up to the air and reclaims
Time-consuming the most long, the most traditional captive balloon is suitable for open area and monitors the most in the air, and is not suitable for extreme terrain or city
City.On civilian, the increasing of large-scale activity, the increase of accident is required for tackling in time, the need to aerial monitor supervision platform in short-term
Ask increase, i.e. require that captive balloon takes up an area little, and can rapid deployment, quickly lift-off, quickly reclaim.
Meet above-mentioned application demand, first have to drop to the system scale of captive balloon, operation easier, personnel demand
Low, and require Portable power-driven, and be not primary to the precision of load, the requirement of detection quality.Therefore can protect
On the basis of staying most basic loading functionality, whole system is simplified and miniaturization, retain most basic system composition and function.
Captive balloon system, under the principle the simplest in line with system, is simplified to minimizing by the present invention, devises a kind of little
Type, quick, safe, easy-to-use captive balloon, can quickly reclaim by rapid deployment, is suitable for single or operated by two people and carries, both fitting
The area that cannot arrive for vehicle, be also applied for large-scale activity, accident in short-term, Quick air monitors and manages commander
Deng.
Summary of the invention
(1) to solve the technical problem that
The present invention proposes a kind of captive balloon, is used for solving existing captive balloon and takes up an area that space is big, go up to the air and regain time-consuming
Problem long, that operation is difficult, labor intensive material resources are big.For release conventional captive balloon cannot miniaturization, fastization, urbanization should
Limitation.
(2) technical scheme
Based on problem above, the present invention proposes a kind of captive balloon, including microsphere system and capstan system, wherein:
Microsphere system includes spheroid, and it is oblate revolution spheroid；
Capstan system includes dynamical system, and it is for providing the power of capstan system so that capstan system can be described in folding and unfolding
Microsphere system.
The depth-width ratio of above-mentioned oblate revolution spheroid is 0.5-0.9, and point film number of oblate revolution spheroid is not less than 12.
Above-mentioned microsphere system also includes stable sail, stablizes sail and is positioned at the back lower place of above-mentioned oblate revolution spheroid, uses
In making captive balloon stable equilibrium in wind.
Above-mentioned dynamical system is manual folding and unfolding crank or retracting motor.
Above-mentioned capstan system also includes capstan winch and fixing device.
Wherein the fixing device of capstan system can be earth anchor, for capstan winch is fixed on ground；The fixing dress of capstan system
Put and can also be used for connecting capstan winch and load for hook.
Above-mentioned captive balloon also includes load system, and load system includes load, payload platform and connects fixing device.
Above-mentioned captive balloon also includes that ground controls and reception system, and described ground controls to include receiving sky with reception system
Line, data display equipment, controlling equipment.
Above-mentioned captive balloon also includes that gas charging system, described gas charging system include helium tank, gas tube and spheroid protection set.
Above-mentioned spheroid protection set profile is monoblock cloth, and liner is smooth, and material is light-high-strength fiber composite cloth.
Above-mentioned helium tank can fall placement, it carries anti-roll rotation structure, and has the structure being connected with capstan winch.
Above-mentioned captive balloon also includes receiving AIR CONVECTOR TECH, and described storage AIR CONVECTOR TECH includes receiving knapsack and protection lining
Pad.
Above-mentioned storage AIR CONVECTOR TECH also includes receiving knapsack, and what described knapsack was furnished with pressure-reducing cushioning material bears double-shoulder belt.
Above-mentioned captive balloon also includes cable system, and cable system includes principal series cable, point heaving pile, load system, rigging and attachment means,
Cable system is for connecting described other system.
Above-mentioned point of heaving pile fixes meridian to position by the big envelope on oblate revolution spheroid top, and point heaving pile is at spheroid top
Connect.
The principal series cable of above-mentioned cable system and a point heaving pile are that photoelectricity is combined load cable.
(3) beneficial effect
1, the present invention proposes a kind of microminiature captive balloon system, and captive balloon is simplified to by this captive balloon system
Littleization, is suitable for single or operated by two people and carries；Easy and simple to handle, action required personnel are few, can rapid deployment, flexible；Right
Site requirements is low, can in city, rural area or remote districts launch and provide.
2, above-mentioned microminiature captive balloon system can within ten a few minutes rapid deployment, go up to the air and reclaim, fast reserve,
And wind loading rating is strong, stablizes sail by afterbody time resident in wind and realize stable equilibrium, provide stable aerial work for load
Make platform.
3, above-mentioned microminiature captive balloon system can be used for aerial observation, communication etc., can be deployed in what vehicle cannot arrive
Area；Can be used for security, communication etc., be particularly suited for large-scale activity or accident in short-term, Quick air monitors, security and
Management commander, and the communication relay of remote districts and signal covering etc..
Accompanying drawing explanation
Fig. 1 is system composition and the layout of microminiature captive balloon in one embodiment of the invention；
Fig. 2 is the system layout figure of spheroid inflated condition in Fig. 1；
Fig. 3 is the top view of microminiature captive balloon in Fig. 1；
Fig. 4 is the upward view of microminiature captive balloon in Fig. 1；
Fig. 5 is the first storage knapsack receiving state schematic layout pattern in one embodiment of the invention；
Fig. 6 is the second storage knapsack receiving state schematic layout pattern in one embodiment of the invention.
[description of reference numerals]
100-microsphere system；101-spheroid；
102-stablizes sail；200-capstan system；
201-capstan winch；202-fixing device；
203-dynamical system；300-load system；
301-load；302-payload platform；
303-connects fixing device；400-cable system；
401-principal series cable；Point heaving pile on rear side of 402-；
Point heaving pile on front side of 403-；404-attachment means；
500-ground controls and the system of reception；501-controlling equipment；
502-data display equipment；503-reception antenna；
600-gas charging system；601-helium tank；
602-gas tube；603-spheroid protection cloth；
700-receives AIR CONVECTOR TECH；701-first receives knapsack；
702-second receives knapsack.
Detailed description of the invention
For making the object, technical solutions and advantages of the present invention clearer, below in conjunction with specific embodiment, and reference
Accompanying drawing, the present invention is described in further detail.
The whole system subminiaturization of microsphere system, close to mooring aerostatics can the floating limit, by density of material and floating
Rising the restriction of gas, smaller aerostatics cannot take up own wt substantially.Sphere body is oblate spheroid revolving body, manufactures
Simply, it is suitable for small-sized utricule.Owing to oblate spheroid is compared, the most spherical when for mooring aerostatics, windward side is less, wind resistance effect
More preferably, more stable.But the most flat spherical meeting causes the dignity of spheroid than reducing, and the balloon surface of same volume is long-pending can be increased, from
And cause the increase of weight, so need to find equilibrium point between weight efficiency and wind loading rating.It is computed and tests, comparing
Suitably depth-width ratio, typically about 0.6, is adjusted according to using and depositing the requirement of occasion, typically takes 0.5～0.9 left
Right.In order to ensure more preferable circularity and reduce machining period, for about 3 meters spheroids, take 15 after submodular is optimized and divide film
Number minimum is typically no less than 12, to ensure the excess smoothness of diaphragm junction, reduces stress and concentrates.Spheroid without Stress control,
Simplified system complexity, reduces weight and power consumption, and balloon itself can need not electric energy, and manually folding and unfolding crank type capstan winch can
Realize single manual operation.Sphere size is less, and surface curvature radius is little, and bearing capacity is strong, can bear after rising to 100 meters of height
The pressure reduction change that day and night temperature causes.Spheroid this as revolving body, confirm position for convenience, it is stipulated that equipped with stable sail (or wind
The wing, Feng Qi, air duct) side be rear portion, and stablize sail and be positioned at the position that spheroid rear portion is on the lower side, may be used in wind stable
Spheroid orientation and attitude.
Capstan winch aspect, without the revolution anchoring structure such as tower, by the slip ring of principal series cable with point heaving pile junction make principal series cable and
The rotation decoupling of spheroid.Capstan winch includes mooring capstan body, retracting motor/manual folding and unfolding crank, capstan winch fixing device.Capstan winch is solid
Determining device can be earth anchor, for capstan winch is fixed on ground；Can also be hook, for capstan winch is connected to weight.
Directly power supply, load data and the control signal of typically battery and load being put together is passed through to be wirelessly transferred.As carried
The bigger power cable that need to connect of lotus power consumption to ground, then can use electric slip ring or photoelectricity shaft coupling.Use surface power supply mode
Time, no requirement (NR) basic to battery size and weight, load continuous working period can be longer, and data transfer bandwidth can also be more
Greatly.This system can supporting load categories include: visible ray, the optics load such as infrared, multispectral, communication forward load, environment
Monitors load etc..Load corollary system also includes that The Cloud Terrace, Slung-Load platform, hanging connect rope etc..The Cloud Terrace can be used for controlling
Load attitude and orientation.Video monitoring class load uses the The Cloud Terrace with self-stabilization function, can shake at balloon platform
Or during a small amount of inclination, make the visual angle of monitoring camera keep fixing.
Spheroid is connected with principal series cable by many point heaving piles, and a point heaving pile fixes broadwise position by the big envelope on spheroid top,
Many points of heaving pile tops connect, and spheroid are not required to arrange tab, decrease stress concentration, machining period length and difficulty of processing, carry
High robustness and wind loading rating.Connecting hanging cable can rotate by single shaft, spheroid will not drive principal series cable to twist when rotating.Principal series cable
Use current supply cable or optoelectronic composite cable, be used for powering and transmitting data.
For having the captive balloon of three pieces points of heaving piles, under original state, in three pieces points of heaving piles of spheroid, a piece point below
Heaving pile is longer than two pieces points of heaving piles above, makes spheroid have certain natural gradient forward, according to calculating and test knot
Really, in conjunction with load operation requirement, the natural gradient of spheroid take about 10～30 ° proper.Spheroid midpoint in the case of calm
Directly over capstan winch, having spheroid wind direction skew under edge under wind-force effect in the case of wind, principal series cable tilts therewith, and spheroid is three
Root divides and has certain sweptback angle under the effect of heaving pile, and this angle can the natural gradient of part and spheroid be supported
Disappear.When load installation site requires level as far as possible, it would however also be possible to employ in the following manner: point heaving pile of rear side coordinates also
A stretch cord installed by connection, and when stretch cord shrinks, rear side heaving pile relaxes, and length is consistent with two outer two bond cable lengths, and spheroid is protected
Water holding is put down.When having wind, stretch cord elongates, and in certain angle of inclination, spheroid still keeps level.
Ground controls/receives terminal and can be used for controlling capstan winch motor folding and unfolding, control load The Cloud Terrace, control load work, connecing
Record lotus return data information.
In gas charging system, helium tank can use one or two gas cylinder according to helium usage amount.Helium tank can fall
Place, it carries the structure of anti-rolling, and with the structure being connected with capstan winch, capstan winch can be connected on helium tank, utilize
It is as weight.If wind-force is bigger, it is also possible to capstan winch is connected on other heavier objects.Spheroid protection set uses
Light-high-strength fiber composite cloth is made, wear-resisting, scratch resistant, anti-cutting, anti-puncture, and profile is monoblock cloth, and liner is smooth, will not damage
Hinder spheroid.After under receiving state, the spheroid folded received by parcel, it is positioned among knapsack.It is wrapped in outside spheroid during spheroid storage
Portion, makes spheroid be completely in spheroid protection set, is used for protecting spheroid to avoid damage under receiving state；When spheroid launches inflation
This protection set is launched and is layed in ground, spheroid is placed thereon, it is used for protecting spheroid to avoid by ground sharp object
Damage, and the place that offer spheroid spreads out in gas replenishment process.
Storage AIR CONVECTOR TECH profile is large-scale knapsack, is furnished with bearing double-shoulder belt and being placed in knapsack dorsal part of pressure-reducing cushioning material
Bear pressure drop materials.Knapsack can be two, two people bear respectively, and one of them includes one (or two) big separation, uses
In depositing helium tank；Another includes multiple compartments, is used for depositing spheroid, capstan winch (containing the principal series cable that dish is good), load are put down
Other equipment in addition to helium tank such as platform, ground control terminal.Knapsack is alternatively a knapsack, for depositing the institute of captive balloon
There is part.
For more massive system, vehicle-mounted mode can be used, be equipped with vehicle-mounted containing box or trailer, wherein containing gas cylinder, ball
The devices such as body storage；Additionally including the circular anchoring bracket at casing top, bracket is the soft padded coaming of annulus outer cover, uses
Use during spheroid does not rises unprecedented or anchoring after falling, main push-towing rope rope by the middle part of bracket annulus with containing box bottom capstan winch
Connect, spheroid can be fixed, effectively prevent spheroid to be contained case and damage, and increase the wind loading rating under its anchored condition.
Here a specific embodiment is lifted, for parameter determination and the system composition portion of this captive balloon system are described
Point:
Captive balloon in the present embodiment is suitable for two people and bears operation, has three points of heaving piles.
As shown in figures 1 to 6, a kind of microminiature captive balloon includes microsphere system 100, capstan system 200, load system
300, cable system 400, ground control and receive system 500, gas charging system 600, storage AIR CONVECTOR TECH 700.
Microsphere system 100 includes spheroid 101, stablizes the dependency structures such as sail 102 (wing, flag) and inflation inlet；
Capstan system 200 includes capstan winch 201, fixing device 202 and dynamical system 203；
Load system 300 includes load 301, payload platform 302 and connects fixing device 303；
Cable system 400 includes principal series cable 401, point heaving pile 402-403 and attachment means 404；
Ground controls to include reception antenna 503, data display equipment 502 and controlling equipment 501 etc. with reception system 500；
Gas charging system 600 includes helium tank 601, gas tube 602 and spheroid protection cloth 603；
Storage AIR CONVECTOR TECH 700 includes receiving knapsack 701-702, protection liner etc..
Spheroid 101 is oblate revolution spheroid, and spheroid depth-width ratio is 0.6, and spheroid divides film number to be 15, stablizes sail 102 and is
Circular hood is connected to spheroid and is positioned at position, the spheroid back lower place.Dynamical system 203 in capstan system 200 is manual folding and unfolding crank,
Fixing device 202 is hook form.Divide heaving pile to have three, be positioned at point heaving pile 402 at spheroid rear than being positioned at dividing of spheroid front
Heaving pile 403 is long, the free inclination degree of spheroid about 15 °；In gas charging system, helium tank 601 is two bottles；Storage knapsack has two, is the
One storage knapsack 701 and the second storage knapsack 702, the second storage knapsack 702 has a big separation, is used for depositing nitrogen cylinder
601, the first storage knapsack 701 includes multiple compartments, is used for depositing microsphere system 100, capstan system 200, load system
300, cable system 400, ground control and reception system 500 etc. are except the other system in addition to helium tank, when depositing, and microsphere system
100 are placed in spheroid protection cloth 603, to prevent microsphere system from sustaining damage in storage knapsack.It addition, give ball in captive balloon
During body inflation, should be placed on spheroid protection cloth 603, as in figure 2 it is shown, be used for protecting spheroid to avoid damage.Last captive balloon
Each performance parameter is:
Maximum gauge: about 3.5 meters；
Maximum lift-off height: about 100 meters；
Lifting capacity: about 1kg；
Free buoyancy: about 1kgf, the freest buoyancy is that the gross buoyancy of captive balloon deducts gross weight and (includes that hawser rises dead band
Weight) the most remaining buoyancy value；
Gross buoyancy: be about 12kgf；
Airlift ability: for the gross weight of deadweight, load and instrument bag, about 11kg；
Mooring wind-force: be 3～4 grades；
Terrestrial operation wind-force: less than 3 grades.
The difficulty of the present invention is, this system is close to the dimension limit of mooring aerostatics, and mooring aerostatics is inherently
Lift-off weight just includes the weight such as spheroid, hawser, inherently needs certain buoyance lift gas to make it go up to the air, and on the other hand also needs
The weight of load to be added and certain free buoyancy, therefore the volume of spheroid can not be infinitely small.Through repeatedly calculating and trying
Test, in conjunction with actual liter of hollow testing of multiple microminiature captive balloons, obtain the volume of 5～20 cubic metres the most close to mooring gas
The limit of ball.
The helium tank commonly used at present discharges the capacity of helium in the case of normal atmosphere after being full of be 5 cubes
About meter, the spheroid of minimum 5 cubic metres the most given here is contemplated to adapt to the capacity of single bottle of helium.Certainly, if made
Higher by the height above sea level in place, then the spheroid volume using single bottle of helium corresponding is accomplished by increasing further.If volume
The least, it is still desirable to helium tank is its supply, and helium system needs the weight born maximum be exactly helium tank, this
Sample is difficult to improve further in whole efficiency.
Particular embodiments described above, has been carried out the purpose of the present invention, technical scheme and beneficial effect the most in detail
Describe in detail bright it should be understood that the foregoing is only the specific embodiment of the present invention, be not limited to the present invention, all
Within the spirit and principles in the present invention, any modification, equivalent substitution and improvement etc. done, should be included in the protection of the present invention
Within the scope of.
Claims (14)
1. a captive balloon system, including microsphere system and capstan system, wherein:
Described microsphere system includes spheroid, and it is oblate revolution spheroid；
Described capstan system includes dynamical system, and it is for providing the power of capstan system so that capstan system can be described in folding and unfolding
Microsphere system.
2. captive balloon as claimed in claim 1, it is characterised in that the depth-width ratio of described oblate revolution spheroid is 0.5-0.9.
3. captive balloon as claimed in claim 1, it is characterised in that described microsphere system also includes stable sail, described stable
Sail is positioned at the back lower place of described oblate revolution spheroid, is used for making described captive balloon stable equilibrium in wind.
4. captive balloon as claimed in claim 1, it is characterised in that described dynamical system is folding and unfolding crank or retracting motor.
5. captive balloon as claimed in claim 1, it is characterised in that described capstan system also includes capstan winch and fixing device.
6. captive balloon as claimed in claim 5, it is characterised in that the fixing device of described capstan system is earth anchor, is used for
Capstan winch is fixed on ground.
7. captive balloon as claimed in claim 5, it is characterised in that the fixing device of described capstan system is hook, is used for
Connect capstan winch and load.
8. captive balloon as claimed in claim 1, it is characterised in that also include that gas charging system, described gas charging system include helium
Gas cylinder, gas tube and spheroid protection set.
9. captive balloon as claimed in claim 8, it is characterised in that the material of described spheroid protection set is that light-high-strength is fine
Dimension Compound Fabric.
10. captive balloon as claimed in claim 8, it is characterised in that the liner of described spheroid protection set is smooth.
11. captive balloons as claimed in claim 8, it is characterised in that described helium tank can fall placement, it carries anti-roll
Rotation structure, and there is the structure being connected with capstan winch.
12. captive balloons as claimed in claim 1, it is characterised in that also including receiving AIR CONVECTOR TECH, described storage is born and is
System includes receiving knapsack and protection liner.
13. captive balloons as claimed in claim 12, it is characterised in that described storage knapsack is furnished with the back of the body of pressure-reducing cushioning material
Negative double-shoulder belt.
14. captive balloons as claimed in claim 1, it is characterised in that also include that cable system, the heaving pile of described cable system are
Photoelectricity is combined load cable.
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| CN108557051A (en) * | 2018-06-15 | 2018-09-21 | 湖南航天远望科技有限公司 | A kind of captive balloon sphere, shelter for guaranteeing and its captive balloon system |
| CN109018293A (en) * | 2018-07-18 | 2018-12-18 | 苏州开端机电科技有限公司 | A kind of captive balloon |
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| CN111806669A (en) * | 2020-07-20 | 2020-10-23 | 邓迪 | Captive balloon system suitable for small ship carries on |
| CN112703154A (en) * | 2018-07-23 | 2021-04-23 | Adf集团 | System and method for mooring an aircraft or airship balloon-type aerial vehicle |
| CN112706911A (en) * | 2021-03-15 | 2021-04-27 | 田志超 | Multifunctional portable aerostat |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102582818A (en) * | 2012-03-07 | 2012-07-18 | 北京航空航天大学 | Mooring ball mounted wind power generating device |
| CN204341385U (en) * | 2014-12-17 | 2015-05-20 | 中国电子科技集团公司第三十八研究所 | A kind of captive balloon band perforate cord fabric type empennage |
| WO2015170078A2 (en) * | 2014-05-05 | 2015-11-12 | Spillconsult Limited | Tethered aerial platform and aerial observation system |
| JP2016002973A (en) * | 2014-06-19 | 2016-01-12 | ソフトバンク株式会社 | Captive balloon |
| CN206155762U (en) * | 2016-10-08 | 2017-05-10 | 中国科学院光电研究院 | Subminiature captive balloon system |
-
2016
- 2016-10-08 CN CN201610879143.3A patent/CN106275363B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102582818A (en) * | 2012-03-07 | 2012-07-18 | 北京航空航天大学 | Mooring ball mounted wind power generating device |
| WO2015170078A2 (en) * | 2014-05-05 | 2015-11-12 | Spillconsult Limited | Tethered aerial platform and aerial observation system |
| JP2016002973A (en) * | 2014-06-19 | 2016-01-12 | ソフトバンク株式会社 | Captive balloon |
| CN204341385U (en) * | 2014-12-17 | 2015-05-20 | 中国电子科技集团公司第三十八研究所 | A kind of captive balloon band perforate cord fabric type empennage |
| CN206155762U (en) * | 2016-10-08 | 2017-05-10 | 中国科学院光电研究院 | Subminiature captive balloon system |
Non-Patent Citations (1)
| Title |
|---|
| PRESS: "《https://www.suasnews.com/2015/02/rt-lta-systems-introduces-its-new-mini-aerostat-system-the-skystar-100/》", 19 February 2015 * |
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|---|---|---|---|---|
| CN108284937A (en) * | 2017-01-10 | 2018-07-17 | 湖南航天远望科技有限公司 | One kind being tethered at floating balloon platform |
| CN110740932A (en) * | 2017-04-27 | 2020-01-31 | R·I·米勒 | Systems, methods, and apparatus to improve safety and functionality of aircraft having or more rotors |
| CN107128473A (en) * | 2017-06-23 | 2017-09-05 | 中国特种飞行器研究所 | Lift-off recovering mechanism, captive balloon system and its control method |
| CN107128473B (en) * | 2017-06-23 | 2023-11-21 | 中国特种飞行器研究所 | Lifting recovery mechanism, tethered balloon system and control method thereof |
| CN109788245A (en) * | 2017-11-13 | 2019-05-21 | 丰田自动车株式会社 | Animal rescue system, animal rescue mode and its used server |
| CN108557051B (en) * | 2018-06-15 | 2023-10-24 | 湖南航天远望科技有限公司 | Tethered balloon sphere, guaranteeing shelter and tethered balloon system thereof |
| CN108557051A (en) * | 2018-06-15 | 2018-09-21 | 湖南航天远望科技有限公司 | A kind of captive balloon sphere, shelter for guaranteeing and its captive balloon system |
| CN109018293A (en) * | 2018-07-18 | 2018-12-18 | 苏州开端机电科技有限公司 | A kind of captive balloon |
| CN112703154B (en) * | 2018-07-23 | 2023-12-05 | Adf集团 | System and method for mooring an aircraft or airship balloon-type aeronautical vehicle |
| CN112703154A (en) * | 2018-07-23 | 2021-04-23 | Adf集团 | System and method for mooring an aircraft or airship balloon-type aerial vehicle |
| CN111641769A (en) * | 2020-06-16 | 2020-09-08 | 中南大学 | Individual soldier mooring floating investigation communication system |
| CN111806669A (en) * | 2020-07-20 | 2020-10-23 | 邓迪 | Captive balloon system suitable for small ship carries on |
| CN112706911A (en) * | 2021-03-15 | 2021-04-27 | 田志超 | Multifunctional portable aerostat |
| CN113772074A (en) * | 2021-09-27 | 2021-12-10 | 上海交大重庆临近空间创新研发中心 | Mooring floating air ball system |
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