CN108557051A - A kind of captive balloon sphere, shelter for guaranteeing and its captive balloon system - Google Patents
A kind of captive balloon sphere, shelter for guaranteeing and its captive balloon system Download PDFInfo
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- CN108557051A CN108557051A CN201810619298.2A CN201810619298A CN108557051A CN 108557051 A CN108557051 A CN 108557051A CN 201810619298 A CN201810619298 A CN 201810619298A CN 108557051 A CN108557051 A CN 108557051A
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- utricule
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- 238000012544 monitoring process Methods 0.000 claims abstract description 13
- 238000009826 distribution Methods 0.000 claims abstract description 12
- 238000009530 blood pressure measurement Methods 0.000 claims abstract description 9
- 239000002131 composite material Substances 0.000 claims description 19
- 238000004873 anchoring Methods 0.000 claims description 12
- 239000000463 material Substances 0.000 claims description 7
- 238000005192 partition Methods 0.000 claims description 7
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- 230000005622 photoelectricity Effects 0.000 claims description 6
- 150000001875 compounds Chemical class 0.000 claims description 4
- 239000004744 fabric Substances 0.000 claims description 4
- 239000004677 Nylon Substances 0.000 claims description 3
- 229920004933 Terylene® Polymers 0.000 claims description 3
- 229920000508 Vectran Polymers 0.000 claims description 3
- 239000004979 Vectran Substances 0.000 claims description 3
- 229920006231 aramid fiber Polymers 0.000 claims description 3
- 229920002521 macromolecule Polymers 0.000 claims description 3
- 239000012528 membrane Substances 0.000 claims description 3
- 229920001778 nylon Polymers 0.000 claims description 3
- 230000005693 optoelectronics Effects 0.000 claims description 3
- -1 polyethylene Polymers 0.000 claims description 3
- 229920000573 polyethylene Polymers 0.000 claims description 3
- 239000005020 polyethylene terephthalate Substances 0.000 claims description 3
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 2
- 229920000642 polymer Polymers 0.000 claims 1
- 238000009738 saturating Methods 0.000 claims 1
- 238000009434 installation Methods 0.000 abstract description 5
- 238000004378 air conditioning Methods 0.000 abstract description 3
- 230000007613 environmental effect Effects 0.000 abstract description 3
- 230000001276 controlling effect Effects 0.000 description 9
- 238000000034 method Methods 0.000 description 8
- 238000010586 diagram Methods 0.000 description 7
- 239000002775 capsule Substances 0.000 description 6
- 239000000203 mixture Substances 0.000 description 5
- 238000004891 communication Methods 0.000 description 4
- 230000007812 deficiency Effects 0.000 description 4
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- 238000011161 development Methods 0.000 description 2
- 230000018109 developmental process Effects 0.000 description 2
- 238000005457 optimization Methods 0.000 description 2
- 238000001959 radiotherapy Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 208000025274 Lightning injury Diseases 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
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- 238000007667 floating Methods 0.000 description 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
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Classifications
-
- 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
-
- 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
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tents Or Canopies (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of captive balloon systems, are mainly made of four parts such as captive balloon sphere, tether cable, balloon borne equipment, shelter for guaranteeing.Captive balloon sphere is using single utricule structure, and charge valve, vent valve, warning lamp, pressure measurement interface and layback rope are installed on utricule etc., it is divided into equipment compartment and monitoring cabin inside shelter for guaranteeing, it is highly integrated to have the first capstan winch, power supply and distribution device, gas supply device and system report control platform, air-conditioning and seat etc., provide space for the installation and the manipulation of the comfort of storage and system of system equipment.The present invention has easy to operate, and deployment is quick, and wind resistance is good, and protection is good, and site requirements is low, the advantages of being suitable for disposing for a long time under remote districts or severe environmental conditions.
Description
Technical field
The invention belongs to be lighter than air aircraft field, and in particular to a kind of captive balloon sphere, shelter for guaranteeing and its be
Stay balloon system.
Background technology
Captive balloon system is that a kind of floating pinpointing work in sky by buoyancy lift-off, by tether cable realization is flat
Platform, as a kind of common aero vehicle, captive balloon system has the hang time long（The continuous hang time is from several days to one
Month）, weatherability is strong, disposes simple and flexible, the advantages that efficiency-cost ratio is high；Larger vision range over the ground can be provided for balloon borne equipment,
Stagnant outage degree is higher, and coverage area is bigger, can be used for atmosphere environment supervision, early warning, electronic countermeasure, remote sensing and monitoring, myriametric wave
The civil and militaries field such as communication and information relaying.
Captive balloon system can be divided into miniature according to its operational profile size（100m3 and following）, it is small-sized（100m
³-300m³）, it is medium-sized（300m³-3000 m³）, it is large-scale（3000m³-5000m³）, super-huge captive balloon（5000m3 or more）System
It unites, includes utricule, balloon borne equipment, tether cable, ground anchoring device and guarantee in the composition of usual captive balloon system
Equipment etc..
For medium-sized or above captive balloon system because its contour structure size is big, system structure is complex, ensures that equipment is numerous,
On the one hand durings the storage of system, transport and deployment are with receipts etc. are removed, it is desirable that operating personnel's quantity is more, and skills involved in the labour
It is required that high, on the other hand, it is more slow that receipts process is unfolded and is removed to system, thus to the requirement of the meteorological window considerations of the two processes
Harshness, also, the conveyance vehicle for largely loading secure equipment needs to stop in deployment place, and captive balloon system is to disposing field
Ground and road conditions also have higher requirement, and it is larger that these deficiencies cause captive balloon system to be received in practical implementation
Limitation.
For deficiency existing for previous medium-and-large-sized captive balloon system, to improve the flexible of captive balloon system deployment
Property and convenience, in recent years, with the development of technology, motor driven rapid deployment microminiature captive balloon system has obtained increasingly
Extensive concern.Wherein, American UAV and aerostatics manufacturer DRNE are based on U.S. army's information monitoring and emergency communication demand, develop
Going out miniature tactics aerostatics WASP platforms, the form which uses semitrailer realizes the Flexible deployment of miniature captive balloon,
By utricule, ground anchoring device and ensure integration of equipments on a motorless semitrailer, miniature system similar with WASP
Balloon platform is stayed to also have the Skystar series captive balloons of RT technology companies of Israel, AllsoppHelikites companies to be
Stay balloon and the TEA-45 etc. of SkySentry companies；This kind of miniature captive balloon system disclosure satisfy that weight 40kg, stay sky
Height 200m balloon borne device requirements below, it is flexible, it is fast to dispose and remove receipts speed.
The small-sized system of RAID captive balloons system and some domestic unit developments that LockeedMartin companies of the U.S. develop
Balloon system is stayed, weight can be met in 50kg or more, the 300m of degree in outage balloon borne device requirement below, these systems mostly use
Utricule, ground tackle and part are ensured that equipment is fixed on haulage vehicle, to a certain extent by conventional streamlined utricule configuration
The mobility of system deployment is improved, but these systems, since utricule appearance and size is larger, deployment operation is inconvenient, the time is long,
Deficiency more than operating personnel's quantity still has.
One disclosed in the individual soldier's portable type captive balloon and Chinese patent application CN201610879143.3 of RT technology companies
Kind microminiature captive balloon system, belongs to miniature captive balloon system, by the way of one or operated by two people and carrying, will be
Stay balloon system component by first disassemble transport after combination forming scheme rapid deployment to city, hamlet or remote districts, can
It is applied in the region that vehicle is unable to reach.It is balloon borne to set using battery powered however since the system is limited to system weight
Standby microminaturization, system lift-off height is small, and coverage area is small, and the time in sky is short, therefore its function and application effect are limited.
In addition, current microminiature captive balloon system is to promote mobility, system composition is utmostly simplified, has not been had
Ground control room is set, and the comfort that the system of reducing uses is micro- under conditions of other no auxiliary vehicles or facility are supported
Small-sized captive balloon system is also difficult to meet the application demand in deployment for a long time from far-off regions.
Invention content
In view of the above-mentioned problems, the present invention is intended to provide a kind of level of integrated system is high, deployment is quick flexibly, the time in sky is grown simultaneously
And it is suitable for the microminiature captive balloon system to map out the work for a long time and captive balloon sphere, shelter for guaranteeing, for solving
Normal miniature captive balloon system function and application effect is limited, Conventional compact captive balloon system deployment is inconvenient, time-consuming
The deficiencies of.
The technical solution that the present invention solves the problems, such as is：A kind of captive balloon sphere, including utricule, it is set to utricule lower part
Windward pocket, the charge valve for being set to utricule upper and lower part, vent valve and warning lamp, be set to utricule bottom pressure measurement interface,
The tether cable being connect with utricule, the layback rope being fixedly connected with outer surface, the utricule are lightweight flexible composite material system
At single utricule structure；All parts installed on utricule constitute a modularization entirety together with utricule, can be with utricule
Integrated folding storage.
The generally inside and outside double utricule structures of existing utricule, complicated, incidental various parts are also complicated, fill
Gas velocity degree is slow, and needs the various parts of in-site installation, wastes time.And existing single utricule balloon, structure are again too simple,
Often only there are one the utricule structures inflated, above not or rarely auxiliary function component, cannot meet long-time and stay
Empty demand.
Utricule is changed to single utricule structure by said program, and makes the parts installed on utricule that can integrally be rolled over utricule
It is folded, so utricule can integrally be stored, it is rapidly aerated when needing to let fly away to let fly away, eliminate the journey of in-site installation functional component
Sequence realizes rapid deployment.
Further, the vent valve is set at the top of utricule, and the warning lamp is set at the top of vent valve；
Also report includes the power cord and signal wire that can be electrically connected vent valve, warning lamp with balloon borne equipment, the power cord and signal
The epimere of line is embedded in utricule inner surface, hypomere is pierced by from utricule inner surface, in being pierced by position equipped with through walls for utricule surface
Electric connector；
The pressure measurement interface is connected with the pressure guiding pipe that can be connect with balloon borne equipment, and power cord and signal wire hypomere are together with pressure guiding pipe
It is packaged in sleeve and is pierced by from casing.
Power cord and the such design of signal wire are more conducive to fold with utricule.It can be in capsule using casing overall package
Body is inflating expanded or during removing receipts, realizes the observing and controlling case of balloon borne equipment and the rapid-assembling/disassembling of utricule.
Specifically, the utricule is the composite wood based on aramid fiber or ultra high molecular polyethylene or Vectran fabrics
Material is made；
Or, the utricule is made of the composite material based on nylon or terylene；
Or, the utricule is made of PU, PE macromolecule membrane material.
Material based on cited by above-mentioned is the matrix for making utricule, and common material is also added with when making utricule
Material forms the composite material of light flexible or has high-elongation light flexible composite material together.
Further, the tether cable includes main push-towing rope rope and divides hawser, and all points of hawser upper ends connect with utricule, lower end
It converges and is connected to main push-towing rope rope upper end；
Main push-towing rope rope is power supply compound mooring rope or optoelectronic composite cable rope, and main push-towing rope rope upper end is equipped with electric slip ring or photoelectricity slip ring, divides hawser
By link up with on main push-towing rope rope electric slip ring or photoelectricity slip ring connect.
Slip ring can play the role of that main push-towing rope rope and utricule and balloon borne equipment relative motion is isolated, and main push-towing rope rope is avoided to rotate
In be damaged.
Meanwhile a kind of shelter for guaranteeing of the application, including hollow box shell, housing cavity are separated into equipment compartment by partition wall
With monitoring cabin；
It is equipped with the utricule case for utricule after storing folding in equipment compartment inner top, storage is respectively provided in utricule case both sides
The gas tube storage bin of gas tube and balloon borne equipment box for storing balloon borne equipment；
Utricule case, gas tube storage bin, balloon borne equipment box three connection, and case lid is equipped on the shell at the top of three；
It is equipped with the gas supply device being connect with gas tube in equipment compartment, is connect with the tether cable in utricule bottom portion is passed through
First capstan winch, first capstan winch are fixed on Housing Base；
System report control platform is installed in monitoring cabin, the system report control platform includes controller, display unit, the control
Device is electrically connected with control panel, the gas supply device on the first capstan winch, the second capstan winch, balloon borne equipment, utricule；
Multiple folding horizontal mounting arms are equipped in housing bottom horizontal extension, being equipped on each horizontal mounting arm can correspond to and side
Second capstan winch of drag-line connection.
In traditional technology, ground installation is all scene placement at random, and the system of composition not enough optimizes, inconvenient, unfavorable
In rapid deployment.Be useful for utricule is let and is removed fly away the equipment during receiving is all integrated is arranged into a shelter by said program
In, and by structural layout optimization so that compacter, operation, transport are more convenient, it can be achieved that rapid deployment.
Preferably, transparent windows or the camera for observation device cabin are provided on partition wall.
It is equipped with guide wheel in utricule bottom portion, described tether cable one end is connect with utricule, the other end passes through guide wheel and first
Capstan winch connects.
Guide wheel avoids tether cable from interfering with utricule case for guiding tether cable in the folding and unfolding in utricule bottom portion.
Further, power supply and distribution device is equipped in equipment compartment, the power supply and distribution device includes generator and power distribution cabinet, generator
It is mounted on equipment compartment bottom by guide rail, corresponding to generator position on shell is provided with door dynamo.
Power supply and distribution device is for the system normal power supply in the case of no alternating current.To avoid generator noise and vibration to operation
The influence of personnel and other equipment can open door dynamo before starting generator, and generator is pulled out out of my cabin.
Preferably, the utricule case region of case top, by tether cable centered on, be laid with the capsule of foldable lodging
Body support frame, the utricule pedestal upper end are equipped with arc bracket identical with balloon shapes.To utricule when utricule holder is used to anchor
Support is carried out, to ensure that utricule is stablized.
Preferably, it is respectively equipped with liftable supporting leg in shell both sides.Supporting leg is the dumping device of shell, the supporting leg side of making
Bilge portion can leave ground and rise certain altitude, convenient in the case where lifting equipment lacks, can also realize with common fortune
Defeated vehicle loading and unloading.The lifting of supporting leg is electric or hand elevating mechanism.
Correspondingly, the present invention also provides a kind of captive balloon system, including balloon borne equipment, the balloon borne equipment includes load
Mounting platform, the observing and controlling case mounted on load mounting platform upper surface, the payload mounted on load mounting platform lower surface,
Further include above-mentioned captive balloon sphere and above-mentioned shelter for guaranteeing, the tether cable includes main push-towing rope rope and divides hawser, Suo Youfen
Hawser upper end is connect with utricule, lower end is converged and is connected to main push-towing rope rope upper end, and main push-towing rope rope is connect with the first capstan winch；
The load mounting platform is placed within the space that point hawser is surrounded, the edge of load mounting platform with divide hawser corresponding
Connection；
Layback rope correspondence is connect with each second capstan winch when anchoring.
Above-mentioned captive balloon system can also realize that system inflates exhibition under the support of shelter for guaranteeing on haulage vehicle
It opens, anchor and work in sky, to realize that the fast reserve of system is disposed.
Storage, transhipment, expansion and the anchoring of above-mentioned captive balloon system go up to the air, remove the application method of five processes of receipts such as
Under：
System is stored：Complete to remove the system components after receiving after maintenance, after the utricule support-folding of shelter for guaranteeing
It lodges and pushes up and fix in cabin, be stored in both sides in equipment compartment after horizontal mounting arm and the folding of the second capstan winch, generator is solid by guide rail
Due in equipment compartment, utricule（Including the functional components such as pocket windward, charge valve, vent valve, warning lamp, pressure measurement interface on utricule）
And be attached thereto layback rope, divide hawser orderly to fold after be stored in utricule case.Balloon borne equipment and the power cord being attached thereto
And signal wire hypomere, pressure guiding pipe etc. are deposited in balloon borne equipment box.
System is transported：In the case of having lifting equipment, can by lifting equipment by shelter for guaranteeing handling to haulage vehicle or
It hangs oneself from haulage vehicle to ground.
In the case of there is no lifting equipment, operating personnel's operation or control supporting leg lifting so that it is centainly high that shelter leaves ground
Degree, haulage vehicle enter shelter bottom and realize that the loading of shelter for guaranteeing or haulage vehicle leave shelter bottom and realize indemnifying party
The unloading in cabin.
System is unfolded and anchoring：It after shelter for guaranteeing is unloaded to system deployment place, props up found utricule holder first, expansion is horizontal
Support arm, and generator is opened, it then opens case lid, open gas supply device.Gas tube is found out from gas tube storage box and is incited somebody to action
It connect with the charge valve on utricule top, starts to be inflated utricule, will after utricule rises certain altitude out of utricule case
Gas tube is removed from the charge valve on utricule top, and is connect with the charge valve of utricule lower part and continued to inflate.In gas replenishment process, by capsule
Side drag-line is connect with the second capstan winch, and hawser is divided to be connect with balloon borne equipment, power cord and signal wire hypomere and pressure guiding pipe and utricule
Bottom connects.Also, system operatio platform powers on, and monitors utricule pressure and balloon borne equipment state；After the completion of utricule inflation, pass through
It controls the second capstan winch adjusting side guy cable length utricule anchoring is fixed on utricule holder.
System is gone up to the air：By system report control platform in monitoring cabin, the second capstan winch synchronous release layback rope, capsule are controlled first
Body leaves utricule holder and gradually goes up to the air, and increases with height, and the balloon borne equipment that operating personnel help in balloon borne equipment box leaves guarantee
Cabin top；Wait for that layback rope discharges completely, the first capstan winch of control discharges main push-towing rope rope, and utricule carries balloon borne equipment lift-off.
System removes receipts：Utricule is placed in anchored condition first, and balloon borne equipment is stored in balloon borne equipment box.Then,
Operating personnel send out the vent valve at the top of instruction unpack utricule by system report control platform, and utricule excludes buoyance lift gas.It was vented
Cheng Zhong, operating personnel dismantle the power cord that separation is connected with utricule and signal wire hypomere and pressure guiding pipe from utricule.Then beam holds together
Good utricule simultaneously folds into utricule case, until exhaust is completed.Then layback rope is removed into consolidation from the second capstan winch and is put into capsule well
In body case.Shelter for guaranteeing is finally restored to storage state.
The present invention remarkable result be：
（1）Utricule is changed to single utricule structure, and makes the parts installed on utricule that can integrally be folded with utricule, so
Utricule is integrally stored, it is rapidly aerated when needing to let fly away to let fly away, the program of in-site installation parts is eliminated, is realized quickly
Deployment.
（2）The microminiature captive balloon system altitude is integrated in standard-sized shelter for guaranteeing, and be useful for utricule is put
Fly and remove that equipment during receiving is all integrated to be arranged into a shelter, and by structural layout optimization so that compacter, operation
It is more convenient, crane lifting or shelter the body dumping mechanism loading or unloading from haulage vehicle can be used, it is easy to accomplish rapid deployment.
（3）In ground anchoring state, utricule is supported the microminiature captive balloon system by utricule holder, utricule layback
Rope is connect with the second capstan winch, relative to conventional captive balloon ground anchoring equipment be tethered at anchoring tower or single utricule bracket is solid
Fixed, system is easily operated, and wind resistance is good, and environmental adaptability is strong.
（4）The microminiature captive balloon system components use modularized design, use and operating process it is simple,
Fast, 2-3 operating personnel can be in the rapid deployment of the system of completion.
（5）The microminiature captive balloon system to deployment place site requirements it is low, can be completed on haulage vehicle be unfolded,
Anchoring and rapid deployment, can also be deployed on naval vessel.
（6）Monitoring cabin has been separately provided in shelter for guaranteeing, abundant intuitive manipulation circle is provided for system operators
Face and comfortable working environment so that system adapts to dispose for a long time under remote districts or severe environmental conditions.
（7）Microminiature captive balloon system load ability is strong, safe, protection is good for this, is especially suitable for balloon borne equipment
Weight 100kg or less, lift-off height 300m load application demands below, can be widely applied to atmosphere environment supervision, remote sensing with
The fields such as reconnaissance and surveillance and communication.
Description of the drawings
The invention will be further described below in conjunction with the accompanying drawings.
Fig. 1 is the captive balloon system structure composition schematic diagram of the present invention.
Fig. 2 is the captive balloon sphere structure schematic diagram of the present invention.
Fig. 3 is the balloon borne device structure schematic diagram of captive balloon of the present invention.
Fig. 4 is the captive balloon shelter for guaranteeing structure composition schematic diagram of the present invention.
Fig. 5 is the captive balloon system anchored condition front view of the present invention.
Fig. 6 is the captive balloon system anchored condition side view of the present invention.
Fig. 7 is the captive balloon system transfer status diagram of the present invention.
Fig. 8 schematic diagrames under vehicle-mounted anchored condition for captive balloon system of the invention.
Fig. 9 is the captive balloon system of the present invention in vehicle-mounted schematic diagram under staying dummy status.
In figure：100- captive balloon spheres, 101- utricules, 102- pockets windward, 103- charge valves, 104- vent valves, 105-
Warning lamp, 106- power cords and signal wire epimere, 107- power cords and signal wire hypomere, 108- pressure guiding pipes, 109- layback ropes；
The balloon borne equipment of 200-, 201- observing and controlling casees, 202- load mounting platforms, 203- payload；300- shelter for guaranteeing, 301- supporting legs,
302- shells, 303- guide wheels, 310- monitoring cabin, 311- partition walls, 312- system report control platforms, 313- horizontal mounting arms, 314- seats,
315- air-conditionings, 316- hanging rings, 320- equipment compartments, 321- utricule casees, 322- gas tube storage boxes, the balloon borne equipment boxs of 323-, 324-
Utricule holder, 325- gas tubes, 326- case lids, 327- load brackets, 328- gas supply devices, the first capstan winches of 329-, 330-
Power supply and distribution device；400- tether cables, 401- main push-towing rope ropes, 402- divide hawser；500- haulage vehicles.
Specific implementation mode
With reference to Fig. 2, a kind of captive balloon sphere, including utricule 101, be set to 101 lower part of utricule pocket windward 102, set
The charge valve 103, vent valve 104 and the warning lamp 105 that are placed in 101 upper and lower part of utricule, the pressure measurement for being set to 101 bottom of utricule
Interface, the tether cable 400 being connect with utricule 101, the layback rope 109 being fixedly connected with 101 outer surface of utricule.
The captive balloon sphere 100 of the present invention is using single utricule structure.It is oblate spheroid shape after 101 inflation of utricule,
Volume is in 30m3-300m3.For especially 101 volume of utricule in 100 m3 or more, technical scheme of the present invention is in quick and durable portion
Advantage in terms of administration, safety and protection is more obvious.
Using air-tightness, good, weather proof light flexible composite material makes molding to utricule 101.
Increase caused utricule pressure difference in order to resist difference variation and lift-off height and increase, the utricule 101 can be used
High-strength, light flexible composite material, such as composite material based on aramid fiber or ultra high molecular polyethylene or Vectran fabrics
It is made.Under normal circumstances, difference variation is bigger, lift-off height is higher, and the intensity requirement of flexible composite is higher.
On the other hand, utricule 101 can also high-elongation light flexible composite material, such as based on nylon or terylene
Composite material be made；Or, being made of PU, PE macromolecule membrane material.It in general, can also be big using this flexible composite
Width reduces the manufacturing cost of captive balloon sphere 100.
Tether cable 400 is including main push-towing rope rope 401 and divides hawser 402.For by captive balloon sphere 100, balloon borne equipment 200
And shelter for guaranteeing 300 connects, and constitutes a set of captive balloon system with complete function.
Described point of hawser 402 is three or four.All points of 402 upper ends of hawser are connect with utricule 101, lower end is converged simultaneously
It is connected to 401 upper end of main push-towing rope rope.Main push-towing rope rope 401 is power supply compound mooring rope or optoelectronic composite cable rope, and 401 upper end of main push-towing rope rope is equipped with electricity
Slip ring or photoelectricity slip ring, divide hawser 402 by link up with on main push-towing rope rope 401 electric slip ring or photoelectricity slip ring connect.In order to avoid
Balloon borne equipment 200 is influenced by lightning stroke, in general, being additionally provided with the gold for providing channel for lightning with entering inside main push-towing rope rope 401
Belong to shielded layer.
In order to constrain circumferential vibration range of point hawser 402 on utricule 101, it is provided on utricule 101 multiple for dividing
The limit sling that hawser 402 positions.
Pocket 102 is set to 101 lower part of utricule windward.It is made of light flexible cloth.Pocket 102 is in inverted triangle shape windward,
Its longer bottom edge is connect with utricule 101, and the wedge angle to hang down is connect by rope with a point of hawser 402.Pocket 102 also may be used windward
To be triangle and rectangle, trapezoidal compound shape, it is mainly used for the posture automatic adjustment of captive balloon sphere 100.It determines
The principal element of regulating effect is the effective dimensions area of pocket 102 windward.Under normal circumstances, 102 area of pocket is bigger windward, production
Raw aerodynamic force is bigger, and 100 posture self-regulation effect of captive balloon sphere is also more apparent, but captive balloon sphere 100 drifts about
Amount is also bigger, and height decline is bigger, affects system safety and payload application effect to a certain degree.Therefore, pocket 102 windward
Size need by comprehensive analysis calculate determine.
Two charge valves 103 are separately fixed at the upper and lower part of utricule 101, for filling buoyance lift gas to utricule 101.One
The setting of a vent valve 104 is at 101 top of utricule, and the setting of warning lamp 105 is at 104 top of vent valve.
DC power supply operated type flash lamp or solar powered formula flash lamp can be used in the warning lamp 105.
Vent valve 104,105 power cord of warning lamp and signal wire are divided into two sections, and power cord and signal wire epimere 106 are set to
101 inner surface of utricule.In utricule manufacturing process, power cord and signal wire epimere 106 are implanted into 101 inner surface of utricule, power supply
Line and signal wire hypomere 107 are set to outside utricule 101, by the way that electric connector through walls is arranged on 101 surface of utricule, make two sections
Power cord and signal wire are connected, and make the observing and controlling of the vent valve 104, warning lamp 105 and balloon borne equipment 200 at 101 top of utricule
Case 201 is connected to.
Pressure measurement interface is connect with the observing and controlling case 201 of balloon borne equipment 200 by pressure guiding pipe 108 and is being inflated with monitoring utricule 101
Pressure during use afterwards.In actual use, power cord and signal wire hypomere 107 are encapsulated with pressure guiding pipe by casing
Constitute an entirety together, utricule 101 is inflating expanded or during removing receipts, you can realize the fast of observing and controlling case 201 and utricule 101
Quick-mounting is torn open.
The bottom of 300 length direction both sides of shelter for guaranteeing is additionally provided with 3-4 folding horizontal mounting arms 313, and every
Second capstan winch is installed on a horizontal mounting arm 313.
Layback rope 109 is fixed on 101 outer surface of utricule.Three or four layback rope side drag-lines are set altogether on utricule 101.It adopts
It is made of high-strength light flexible rope or ribbon.When utricule 101 anchors, the level with 300 length direction both sides of shelter for guaranteeing
The second capstan winch connection on support arm 313 matches, and to improve the wind loading rating of utricule 101, ensures that utricule 101 anchors safety.
Power cord and signal wire epimere 106, pocket 102, charge valve 103, vent valve 104, warning lamp 105, pressure measurement connect windward
Mouth and layback rope 109 are respectively mounted in place during utricule 101, and captive balloon sphere 100 is made to constitute a modular entirety.
In removing receipts, storage process, above-mentioned functional structure is folded with utricule 101, stores captive balloon sphere 100, substantially carries
The convenience of the operation of captive balloon system is risen.
With reference to attached drawing 3, balloon borne equipment 200 includes mainly observing and controlling case 201, load mounting platform 202 and payload 203.
Observing and controlling case 201 use closed cabinet design, inside be equipped with control computer, power supply module, communication module, lightning-protection module and
Multiple sensors.
Load mounting platform 202 uses triangle or quadrangle truss structure, upper surface to install observing and controlling case 201, following table
Face is installed by payload 203.Load mounting platform 202 is placed within the space that point hawser 402 is surrounded.Load mounting platform
202 edge is correspondingly connected with hawser 402 is divided.
With reference to attached drawing 4, shelter for guaranteeing 300 includes hollow box shell 302, and 302 inner cavity of shell is divided by partition wall 311
Equipment compartment 320 and monitoring 310 two, cabin part.302 top quadrangle of shell is respectively arranged with hanging ring 316.By hanging ring 316, adopt
With lifting equipment and suspender belt（Rope）Shelter for guaranteeing 300 is hung into certain altitude, realizes shelter for guaranteeing 300 on vehicle or ship
Loading or unloading.
320 top of equipment compartment is provided with utricule case 321, gas tube storage box 322 and the balloon borne equipment box for the one that is connected
323.Utricule case 321, gas tube storage bin 322,323 three of balloon borne equipment box connection, and set on the shell 302 at the top of three
There is case lid 326.Gas supply device 328, the first capstan winch 329 and power supply and distribution device 330 are also equipped in equipment compartment 320.
Load bracket 327 is arranged in the inside of balloon borne equipment box 323, when system is not gone up to the air, balloon borne equipment 200 and is attached thereto
Power cord and signal cable hypomere 107, pressure guiding pipe 108 etc. are deposited on the load bracket 327 of balloon borne equipment box 323.
First capstan winch 329 is fixed on the bottom plate of equipment compartment 320, and in 101 lifting process of utricule, main push-towing rope rope 401 is first
The guide wheel 303 of 321 bottom of capstan winch 329 and utricule case enters under guiding and reaches 300 top of shelter for guaranteeing.
The power supply and distribution device 330 includes generator and power distribution cabinet, and generator is mounted on equipment compartment bottom by guide rail,
Generator position, which is corresponded to, on shell 302 is provided with door dynamo.
Gas supply device 328 is modular high pressure gas gas cylinders group, and gas cylinders group is deposited by high-pressure air pipe and gas tube
Utricule gas tube 325 in storage tank 322 connects.
In order to reduce system structure weight and save space in equipment compartment 320, it is super that pressure can be used in gas supply device 328
The composite high-pressure gas cylinders group for crossing 40MPa replaces routine 15MPa-20MPa steel high pressure gas gas cylinders groups.Also, it is
The supportability of the system of raising, it is desirable that volume of the buoyance lift gas volume that gas supply device 328 can be provided than utricule 101
Big 10%-20%.
Monitoring is equipped with system report control platform 312, seat 314 and air-conditioning 315 in cabin 310.It is provided on partition wall 311 transparent
Observation window or camera, operating personnel can watch equipment working state in equipment compartment 320 in monitoring cabin 310.
The system report control platform 312 includes controller, display unit, and the controller and the first capstan winch 329, second twist
Control panels, the gas supply devices 328 such as disk, balloon borne equipment 200, the charge valve 103 on utricule 101 and vent valve 104 are electrically connected
It connects.
321 region of utricule case at the top of shell 302, by main push-towing rope rope 401 centered on, be laid with the capsule of foldable lodging
Body support frame 324.324 upper end of utricule holder is equipped with arc bracket identical with balloon shapes.
300 side wall of shelter for guaranteeing is equipped with reception hole, and when transport, horizontal mounting arm 313 can be collected in indemnifying party after folding
In reception hole on 300 side wall of cabin.
300 front and rear sides of shelter for guaranteeing are also respectively provided with supporting leg 301.Supporting leg 301 is the dumping device of shell 302, branch
Leg 301 enables shelter bottom to leave ground and rises certain altitude, is convenient in the case where lifting equipment lacks, also can be real
Current common haulage vehicle loads and unloading.The lifting of supporting leg 301 is electric or hand hydraulicefficiency elevation structure.
Referring to Fig.1, Fig. 5,6, above structure constitutes a kind of microminiature captive balloon system, mainly by captive balloon sphere
100, four parts such as balloon borne equipment 200, shelter for guaranteeing 300 and tether cable 400 are constituted.
In conjunction with Fig. 7-Fig. 9, a kind of microminiature captive balloon system of the invention, can be under the support of haulage vehicle 500
Inflating expanded on haulage vehicle 500, anchoring and work in sky, to realize that the fast reserve of system is disposed.
Claims (10)
1. a kind of captive balloon sphere, including utricule, be set to utricule lower part pocket windward, be set to utricule upper and lower part
Outside charge valve, vent valve and warning lamp, the pressure measurement interface for being set to utricule bottom, the tether cable being connect with utricule and utricule
The layback rope that surface is fixedly connected, it is characterised in that：The utricule is single utricule structure made of lightweight flexible composite material；It is all
The parts installed on utricule constitute a modularization entirety together with utricule, can be with utricule one folding storage.
2. captive balloon sphere according to claim 1, it is characterised in that：The vent valve is set at the top of utricule, institute
Warning lamp is stated to be set at the top of vent valve；
Also report includes the power cord and signal wire that can be electrically connected vent valve, warning lamp with balloon borne equipment, the power cord and signal
The epimere of line is embedded in utricule inner surface, hypomere is pierced by from utricule inner surface, in being pierced by position equipped with through walls for utricule surface
Electric connector；
The pressure measurement interface is connected with the pressure guiding pipe that can be connect with balloon borne equipment, and power cord and signal wire hypomere are together with pressure guiding pipe
It is packaged in sleeve and is pierced by from casing.
3. captive balloon sphere according to claim 1, it is characterised in that：The utricule is with aramid fiber or supra polymer
Composite material based on polyethylene or Vectran fabrics is made；
Or, the utricule is made of the composite material based on nylon or terylene；
Or, the utricule is made of PU, PE macromolecule membrane material.
4. captive balloon sphere according to claim 1, it is characterised in that：The tether cable includes main push-towing rope rope and divides cable
Rope, all points of hawser upper ends are connect with utricule, lower end is converged and are connected to main push-towing rope rope upper end；
Main push-towing rope rope is power supply compound mooring rope or optoelectronic composite cable rope, and main push-towing rope rope upper end is equipped with electric slip ring or photoelectricity slip ring, divides hawser
By link up with on main push-towing rope rope electric slip ring or photoelectricity slip ring connect.
5. a kind of shelter for guaranteeing, including hollow box shell, it is characterised in that：Housing cavity by partition wall be separated into equipment compartment and
Monitor cabin；
It is equipped with the utricule case for utricule after storing folding in equipment compartment inner top, storage is respectively provided in utricule case both sides
The gas tube storage bin of gas tube and balloon borne equipment box for storing balloon borne equipment；
Utricule case, gas tube storage bin, balloon borne equipment box three connection, and case lid is equipped on the shell at the top of three；
It is equipped with the gas supply device being connect with gas tube in equipment compartment, is connect with the tether cable in utricule bottom portion is passed through
First capstan winch, first capstan winch are fixed on Housing Base；
System report control platform is installed in monitoring cabin, the system report control platform includes controller, display unit, the control
Device is electrically connected with control panel, the gas supply device on the first capstan winch, the second capstan winch, balloon borne equipment, utricule；
Multiple folding horizontal mounting arms are equipped in housing bottom horizontal extension, being equipped on each horizontal mounting arm can correspond to and side
Second capstan winch of drag-line connection.
6. shelter for guaranteeing according to claim 5, it is characterised in that：It is provided on partition wall for the saturating of observation device cabin
Bright observation window or camera.
7. shelter for guaranteeing according to claim 5, it is characterised in that：Power supply and distribution device, the confession are equipped in equipment compartment
Power distribution equipment includes generator and power distribution cabinet, and generator is mounted on equipment compartment bottom by guide rail, generator is corresponded on shell
Position is provided with door dynamo.
8. shelter for guaranteeing according to claim 5, it is characterised in that：In the utricule case region of case top, to be tethered at cable
Centered on rope, it is laid with the utricule holder of foldable lodging, the utricule pedestal upper end is equipped with arc identical with balloon shapes
Shape bracket.
9. shelter for guaranteeing according to claim 5, it is characterised in that：It is respectively equipped with liftable supporting leg in shell both sides.
10. a kind of captive balloon system, including balloon borne equipment, the balloon borne equipment includes load mounting platform, is mounted on load
The observing and controlling case of mounting platform upper surface, the payload mounted on load mounting platform lower surface, it is characterised in that：Further include power
Profit requires 1~4 any one of them captive balloon sphere and claim 5~9 any one of them shelter for guaranteeing, described
Tether cable includes main push-towing rope rope and divides hawser, and all points of hawser upper ends are connect with utricule, lower end is converged and are connected on main push-towing rope rope
End, main push-towing rope rope are connect with the first capstan winch；
The load mounting platform is placed within the space that point hawser is surrounded, the edge of load mounting platform with divide hawser corresponding
Connection；
Layback rope correspondence is connect with each second capstan winch when anchoring.
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| CN201810619298.2A CN108557051B (en) | 2018-06-15 | 2018-06-15 | Tethered balloon sphere, guaranteeing shelter and tethered balloon system thereof |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810619298.2A CN108557051B (en) | 2018-06-15 | 2018-06-15 | Tethered balloon sphere, guaranteeing shelter and tethered balloon system thereof |
Publications (2)
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| CN108557051A true CN108557051A (en) | 2018-09-21 |
| CN108557051B CN108557051B (en) | 2023-10-24 |
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| CN109436284A (en) * | 2018-09-30 | 2019-03-08 | 中国特种飞行器研究所 | A kind of compact wind resistance captive balloon system |
| CN109693806A (en) * | 2019-01-15 | 2019-04-30 | 中国特种飞行器研究所 | A kind of captive balloon anchoring platform and application method |
| CN109760817A (en) * | 2018-12-26 | 2019-05-17 | 中国电子科技集团公司第三十八研究所 | A kind of small-sized high motor driven captive balloon platform system |
| CN109850115A (en) * | 2018-12-03 | 2019-06-07 | 中国电子科技集团公司第三十八研究所 | A kind of motor driven captive balloon ball library |
| CN109995433A (en) * | 2019-03-08 | 2019-07-09 | 北京航空航天大学 | A kind of fibre optic data transmission device for oil well logging equipment |
| CN111547225A (en) * | 2020-06-01 | 2020-08-18 | 中国科学院空天信息创新研究院 | Rotary damping system in high-altitude balloon flight |
| CN111683226A (en) * | 2020-06-16 | 2020-09-18 | 中南大学 | Regional monitoring mooring system |
| CN112498652A (en) * | 2021-02-07 | 2021-03-16 | 中国科学院空天信息创新研究院 | Wireless sensor for captive balloon and captive balloon |
| CN112660356A (en) * | 2020-12-30 | 2021-04-16 | 中国特种飞行器研究所 | Double-person captive balloon manned platform and double-person captive balloon |
| CN112722230A (en) * | 2021-03-02 | 2021-04-30 | 湖南航天远望科技有限公司 | Marine type captive balloon system and using method thereof |
| 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 |
| CN113942627A (en) * | 2021-11-17 | 2022-01-18 | 上海交大重庆临近空间创新研发中心 | High-altitude balloon stabilizing device and high-altitude balloon system |
| CN114313208A (en) * | 2021-12-28 | 2022-04-12 | 中国特种飞行器研究所 | Mooring balloon rapid automatic inflation and flying water-flow anchoring platform |
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| CN109436284A (en) * | 2018-09-30 | 2019-03-08 | 中国特种飞行器研究所 | A kind of compact wind resistance captive balloon system |
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| CN109693806B (en) * | 2019-01-15 | 2022-04-19 | 中国特种飞行器研究所 | Mooring balloon anchoring platform and using method |
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| CN111547225A (en) * | 2020-06-01 | 2020-08-18 | 中国科学院空天信息创新研究院 | Rotary damping system in high-altitude balloon flight |
| CN111683226B (en) * | 2020-06-16 | 2021-06-15 | 中南大学 | Regional monitoring mooring system |
| CN111683226A (en) * | 2020-06-16 | 2020-09-18 | 中南大学 | Regional monitoring mooring system |
| CN112660356A (en) * | 2020-12-30 | 2021-04-16 | 中国特种飞行器研究所 | Double-person captive balloon manned platform and double-person captive balloon |
| CN112498652A (en) * | 2021-02-07 | 2021-03-16 | 中国科学院空天信息创新研究院 | Wireless sensor for captive balloon and captive balloon |
| CN112722230A (en) * | 2021-03-02 | 2021-04-30 | 湖南航天远望科技有限公司 | Marine type captive balloon system and using method thereof |
| CN112722230B (en) * | 2021-03-02 | 2023-02-28 | 湖南航天远望科技有限公司 | Ocean type captive balloon system and using method thereof |
| 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 |
| CN113942627A (en) * | 2021-11-17 | 2022-01-18 | 上海交大重庆临近空间创新研发中心 | High-altitude balloon stabilizing device and high-altitude balloon system |
| CN114313208A (en) * | 2021-12-28 | 2022-04-12 | 中国特种飞行器研究所 | Mooring balloon rapid automatic inflation and flying water-flow anchoring platform |
| CN114313208B (en) * | 2021-12-28 | 2023-06-23 | 中国特种飞行器研究所 | Quick automatic inflation of captive balloon is put and is flown off streamlined anchoring platform |
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