CN103612741A - Engine driven type captive balloon lift-off recovery system - Google Patents
Engine driven type captive balloon lift-off recovery system Download PDFInfo
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- CN103612741A CN103612741A CN201310690943.7A CN201310690943A CN103612741A CN 103612741 A CN103612741 A CN 103612741A CN 201310690943 A CN201310690943 A CN 201310690943A CN 103612741 A CN103612741 A CN 103612741A
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Abstract
The invention discloses an engine driven type captive balloon lift-off recovery system. The engine driven type captive balloon lift-off recovery system comprises a cable, a balloon, a semitrailer, a revolving platform, a cable guide device, a captive tower, an operating room and an equipment compartment. The middle of the semitrailer is connected with the revolving platform through an arranged revolving support, the cable guide device is arranged at one end of the revolving platform, the captive tower is arranged at the other end of the revolving platform, the equipment compartment and the operating room are sequentially arranged outwards close to the captive tower and along the central axis of the revolving platform, and a drive winch and a cable storage winch are arranged in the equipment compartment. One end of the cable enters the equipment compartment through the cable guide device along a cable channel formed in the central axis of the revolving platform and then sequentially connected with the drive winch and the cable storage winch, and the other end of the cable is connected with the balloon. The engine driven type captive balloon lift-off recovery system is compact in structure and capable of being flexibly transferred and arranged, meets the requirements for liftoff, recovery, retention in air and retention on the ground of balloons which are lifted off by 2000-3500 meters and balloon-mounted equipment, and has good reliability, safety and adaptability.
Description
Technical field
The present invention relates to a kind of lift-off recovery system, especially a kind of based on load-bearing, transmit electricity, be in communication in the motor driven captive balloon lift-off recovery system of one hawser.
Background technology
Captive balloon is a kind of carrier as low idle task, and its difference is compared with hydrogen balloon with ordinary hot balloon, has load-carrying capacity large, and safety is good, goes up to the air highly higher, and wind loading rating by force and the feature such as thunder-lightning ability.General lift-off is highly 2000-3500 rice, can the aerial 15-30 days of prolonged stay.Balloon need provide enough large buoyancy, and according to the weight of carrying equipment, lift-off height, wind loading rating and attitude stability requirement, required aerial buoyancy is greatly about the scope of 1-10 ton.For guaranteeing the safety of equipment on ball, in spheroid, fill the helium of certain pressure, after inflation, spheroid is dirigible shape, end has empennage, can keep stable attitude aloft, and epidermis is high strength, high density light material, there is good hidden function, mainly can be used as communication repeating, topography and geomorphology prospecting, high-altitude photo, the civilian and military purposes such as border reconnaissance.The U.S. is that current captive balloon is applied maximum countries, on the U.S. and South American nations border, dispose a large amount of low latitude captive balloons for traffic in drugs, the investigation tasks of smuggling and crossing illegally border, the U.S. was also once used small-sized motor driven captive balloon for military purposes in the war in Iraq.The relative satellite of function and the prior-warning plane of captive balloon have unique advantage, have fixed point aerial delay, all-weather, an advantage such as real-time, cost is low.Due to importance and the higher-value of carrying equipment on balloon itself and ball, captive balloon lift-off recovery system, as the key equipment of whole system ground supports, has vital impact to the safety of captive balloon work, reliability and validity.
Captive balloon is divided into fixed type and motor driven, the fixed installation of the wayside equipment of fixed type captive balloon and the earth, and scantling of structure can not be subject to space constraint, is applicable to that spheroid volume is large, load-carrying capacity is large and the highly higher occasion of lift-off.The lift-off reclaiming scrap of motor driven captive balloon is in-vehicle, will after balloon helium recovery, can shift flexibly deployment, mobility strong.The present invention, on the technological accumulation basis of the regenerative apparatus of triturating machine dynamic formula captive balloon lift-off for many years, proposes a kind of motor driven captive balloon lift-off recovery system based on special hawser.
Summary of the invention
The invention provides a kind of motor driven captive balloon lift-off recovery system, the technical scheme of employing is as follows:
A kind of motor driven captive balloon lift-off regenerative apparatus, comprise hawser 1, balloon 10, superimposed trailer 20, turn table 30, leadfair 40, mooring mast 50, control cabin 32 and equipment compartment 33, it is characterized in that: in the middle of described superimposed trailer 20, by the revolution arranging, support 26 and be connected with described turn table 30, described leadfair 40 is settled in one end of described turn table 30, the other end is settled described mooring mast 50, near described mooring mast 50 along described turn table 30 axis outwards arranging apparatus cabin 33 and control cabin 32 successively, in described equipment compartment 33, be provided with and drive winch 90 and storage winch 100, it is interior through driving winch 90 to enter storage winch 100 storage cables that the cable channel that one end of described hawser 1 arranges along described turn table 30 places, axis by described leadfair 40 enters described equipment compartment 33, described hawser 1 other end connects described balloon 10.
The both sides of described superimposed trailer 20 are also respectively equipped with at least 2 fixed supporting legs 22 and at least 2 extensile rotary supports 23 that are connected with stretching, extension supporting leg 24.
Described leadfair 40 comprises leads cable wheel 41, the rolling deflection device 42,Hu cable He Rulan of mechanism measurement of dip angle mechanism; Described leadfair 40 is positioned at turn table 30 middle parts, rear end, leads cable wheel 41 and is connected with turn table 30 by the rolling deflection device 42 on introduction support.
Described driving winch 90 comprises initiatively capstan winch 91, driven capstan winch 92, reducing motor 93, safety pin device 94, friction stopping device 95 and capstan winch casing 96; After high before the installation axis of described active capstan winch 91 and driven capstan winch 92, in the low capstan winch casing 96 that is arranged in parallel, in capstan winch casing 96 spaces between active capstan winch 91 and driven capstan winch 92, be provided with friction stopping device 95, can implement braking to driven capstan winch.
The tower height of described mooring mast 50 is >1/2 balloon 10 height+equipment compartments 33 height+2 meters.
The both sides of the turn table 30 between described leadfair 40 and described control cabin 32 are also symmetrical arranged is with standoff air cushion bag 37, the height of described air cushion bag 37 to be greater than the height of described equipment compartment 33 more than 2 meters.
Described balloon 10 is dirigible shape, comprises oval spherical spheroid 11, three empennages 12 and fairings 13 that are positioned at spheroid 11 lower rear; Described spheroid 11 head circular arc central authorities are provided with nose cone 19, in spheroid 11 bilateral symmetry, are provided with multiply bifurcated mooring line, and mooring line converges to together and by latch closure, is connected with the tension pick-up 17 of below afterwards, and tension pick-up 17 belows are connected with rotary connector 18; Described rotary connector 18 upper and lowers can relatively rotate, and below hawser 1 provides power supply and communication containing the cable 1a of optical fiber to balloon 10 through rotary connector 18 output; Mooring line 14 before balloon 10 head nose cone 19 exits are provided with, the left and right sides, rear portion is respectively equipped with left mooring line 15 and right mooring line 16.
The hollow straight-bar that described nose cone 19 is spherical for head is provided with, during for Ground Mooring and nose cone lock 54 lockings that are provided with of described mooring mast 50, described front mooring line 14 is drawn from nose cone 19 holes.
The length of described front mooring cable 14, left mooring cable 15 and right mooring cable 16 is all greater than 40 meters; The length of front mooring cable 14 is greater than left mooring cable 15 and right mooring cable 16, and during balloon 10 lift-off, the lower end of front mooring cable 14, left mooring cable 15 and right mooring cable 16 is all substantially in sustained height.
Feature of the present invention and beneficial effect are: the relevant device of captive balloon lift-off recovery system and device are motor driven vehicle-mounted structure, comprise hawser, balloon, superimposed trailer, turn table, leadfair, mooring mast, front auxiliary hoist, left redundant winch, right redundant winch, drive winch and storage winch, the lift-off of balloon is reclaimed task and has been coordinated by the main winch that drives winch and storage winch to form and three auxiliary hoistes, the main lift-off of long distance is reclaimed and aerial mooring task is born by main winch, subaerial auxiliary folding and unfolding and Ground Mooring are by front auxiliary hoist, left redundant winch and right redundant winch complete simultaneously.System architecture is compact, can shift flexibly deployment, meets lift-off that 2000-3500 rice ascending balloon and ball carry equipment, recovery, is detained and surface detention demand in the air, and have good reliability, safety and comformability.
Accompanying drawing explanation
Accompanying drawing 1; Native system lift-off status architecture sketch;
The birds-eye view of accompanying drawing 2: Fig. 1;
The mooring constitution diagram of accompanying drawing 3: Fig. 1;
Accompanying drawing 4: Fig. 1 equipment compartment right lateral side axonometric drawing;
Accompanying drawing 5: Fig. 1 equipment compartment forward right side axonometric drawing.
In figure: 1, hawser, 1a, cable, 10, balloon, 11, spheroid, 12, empennage, 13, fairing, 14, front mooring line, 15, left mooring line, 16, right mooring line, 17, rotary connector I, 18, tension pick-up, 19, nose cone, 20, superimposed trailer, 21, vehicle body, 22, fixed supporting leg, 23, rotary support, 24, stretch supporting leg, 25, wheel, 26, revolution is supported, and 30, turn table, 31, platform body, 32, OPS, 33, equipment compartment, 34, platform pivoted arm, 35, operation suspension, 36, winding stair, 37, air cushion bag, 40, leadfair, 41, lead cable wheel, 42, rolling turning gear, 50, mooring mast, 51, tower seat, 52, pylon, 53, ascending stair, 54, nose cone lock, 55, front jocket wheel, 60, front auxiliary hoist, 70, left redundant winch, 71, left guide wheel, 80, right redundant winch, 81, right guide wheel, 90, drive winch, 91, active capstan winch, 92, driven capstan winch, 93, reducing motor, 94, safety pin device, 95, friction stopping device, 96, capstan winch casing, 100, storage winch, 101, cable collection tube, 102, driven unit, 103, Dao Lan mechanism, 104, cable sector.
The specific embodiment
Below by the embodiment that is applied as of the motor driven captive balloon lift-off recovery system based on special hawser, and by reference to the accompanying drawings, technical scheme of the present invention is described in further detail.
Fig. 1 is motor driven captive balloon lift-off recovery system lift-off status architecture sketch, Fig. 2 is that Fig. 1 conceals the birds-eye view after balloon, Fig. 3 is that balloon 10 is in Ground Mooring status architecture sketch, Fig. 4 is equipment compartment 33 right lateral side axonometric three-dimensional views, drives installation site and the spatial relationship of winch 90 and storage winch 100 in main indication equipment cabin 33.Fig. 5 is the forward right side axonometric three-dimensional view of equipment compartment 33.Before the orientation identifying in the present embodiment figure is described and is oriented to based on 10 nose cones 19 of balloon in Fig. 1.
System chief component comprises hawser 1, balloon 10, superimposed trailer 20, turn table 30, leads cable wheel 40, mooring mast 50, front auxiliary hoist 60, left redundant winch 70, right redundant winch 80, driving winch 90 and storage winch 100.
The present embodiment balloon 10 is helium balloon, in spheroid 11 and fairing 13, be loaded with the many special equipments that comprise many cover computing machines, GPS, air speed measuring apparatus etc., contained equipment is extremely important and be worth expensive, therefore this lift-off recovery system is focused on the safety in lift-off recovery and aerial delay process especially except meeting folding and unfolding and the Ground Mooring function external demand of balloon 10, ensures being perfectly safe of balloon and load bearing equipment.Hawser 1 is a kind of special cable that collects load-bearing, transmits electricity, is in communication in one, it is the main load-bearing cable in balloon 10 lift-off removal process, hawser 1 is respectively from outside to inside skin, gauze screen, supporting course, four power leads and three optical fiber and forms, and exocuticle adds the semi-conducting material of conductive metal powder for take polythene material as substrate.Balloon is when lift-off, and on ball, the power lead of the required power supply of equipment in hawser 1 provides, and also has storage battery as emergency source of electrical power on ball, and on ball, the data communication on computing machine and ground is by the Optical Fiber Transmission in hawser 1.
This captive balloon lift-off recovery system is motor driven, lift-off reclaiming scrap and relevant auxiliary device are all carried on the turn table 30 of superimposed trailer 20, turn table 30 supports 26 by revolution and is connected with superimposed trailer 20, turn table 30 can around and superimposed trailer 20 between revolution support 26 rotations, when balloon 10 is subject to windage aloft and changes orientation, turn table is followed free rotation.Superimposed trailer 20 is through special repacking, except vehicle body 21 and wheel 25, also be provided with some fixed supporting legs 22, rotary support 23, stretch supporting leg 24, before implementing lift-off task, by some fixed supporting legs 22 that front and back are arranged, support ground and hanged wheel 25, and in superimposed trailer 20 left and right, expand distance and implement supplemental support ground by launching the stretching, extension supporting leg 24 of swinging strut 23 ends, what keep superimposed trailer 20 grabs ground stability.
Keystone configuration on turn table 30 forms and comprises from left to right leadfair 40 by Fig. 1, left redundant winch 70, right redundant winch 80, two air cushion bags 37 that left and right arranges, OPS 32, equipment compartment 33, mooring mast 50 and front auxiliary hoist 60, leadfair 40 is by leading cable wheel 41, rolling turning gear 42, the compositions such as the He Rulan of Hu Lan mechanism measurement of dip angle mechanism, the effect of leading cable wheel 41 is to import in equipment compartment 33 transferring horizontal direction to balloon 10 connection cables, rolling turning gear 42 can be led cable according to the automatic adjustment of the deflection of aerial hawser 1 and be taken turns 41 pivot angles, prevent hawser and lead circular arc grooving side friction on cable wheel 41, Hu Lan mechanism seals hawser 1 by rotating nylon jacket and exports at the circular arc grooving of leading on cable wheel 41, prevent that hawser from skidding off the grooving of leading cable wheel 41.Front auxiliary hoist 60 is located on the tower seat 51 of mooring mast 50, left redundant winch 70 and right redundant are divided into the left and right of leadfair 40, when the auxiliary take-up of balloon 10 when mooring state discharges and approaches ground, by the front jocket wheel 55 arranging at mooring mast 50 tops, front mooring line 14 is received to front auxiliary hoist 60, the left guide wheel 71 of platform pivoted arm 34 ends by turn table 30 platform body 31 left and right sides, rear end and right guide wheel 81 are respectively by left mooring line 15 and right mooring cable 16 income left redundant winch 70 and right redundant winches 80.During the work of left and right auxiliary hoist, two operating personals lay respectively in the operation suspension 35 of left and right auxiliary hoist one side and operate and monitor.The effect of two air cushion bags 37 that turn table 30 both sides, rear portion are overhead is when balloon 10 Ground Mooring, and the hardware configuration grazing on isolated sphere 11 and turn table 30 plays isolation buffer protective effect.Operating personal is by aft mounted winding stair turn table 30 Shang Xia 36.
When balloon 10 is during in Ground Mooring state, the nose cone 19 of balloon 10 heads inserts in the nose cone lock 19 at mooring mast 50 tops, and pins nose cone 19 outlets by the electromagnetic lock in nose cone lock 19.The Ground Mooring of balloon 10 is before holding respectively by three auxiliary hoistes, left and right mooring line, on the spheroid 11 of balloon 10, be also provided with some auxiliary mooring lines (not representing in accompanying drawing), fix with the platform body 31 of turn table 30 and vehicle body 21 moorings of superimposed trailer 20, to guarantee the Ground Mooring safety of balloon 10.
Before balloon 10 lift-offs, first untie all auxiliary mooring lines, first energising discharges the nose cone lock 54 at mooring mast 50 tops, then the front mooring line 14 of front auxiliary hoist 60 is loosened slightly, at this moment the spring of locking in 19 by nose cone ejects the nose cone of balloon 10 19, then start three auxiliary hoistes simultaneously, slowly discharge balloon 10, when three auxiliary hoist near-earths discharge balloon 10, hawser 1 is relaxed state, until hawser 1 completely stressed after, continue to discharge three auxiliary hoistes mooring cable until front mooring line 14, left mooring line 15 and right mooring line 16 emitted completely.When three auxiliary hoistes are after by three, auxiliary mooring cable discharges completely, balloon 10 just enters the mode of operation that drives winch 90, at this moment can start reducing motor 93 and implement cable laying, during cable laying, by the operating personal of OPS 32 by the first low speed cable laying of control operation handle, and gradually speedup to normal cable releasing speed.Drive the speed control mode work of the reducing motor 93 employing frequency controls of winch 90, the drive motor of storage winch 100 is permanent torque control mode work, keeps driving the tension force substantially constant of the hawser 1 between winch 90 and storage winch 100.During cable laying, due to the effect of balloon 10 buoyancy, reducing motor 93 work, for generating state, consume generated energy by discharging resistance is set in circuit.
When aerial balloon 10 is carried out to take-up, by reducing motor 93, drive initiatively capstan winch 91 rotations, behind hawser 1 access arrangement cabin, from driving the cable mouth that enters of the capstan winch casing 96 of winch 90 to enter the driven capstan winch 92 that drives winch 90, through driven capstan winch 92, near the first grooving of reducing motor 93, from top, enter the first grooving of active capstan winch 91, at active capstan winch 91 and driven capstan winch 92, be wound to that capstan winch initiatively keeps right successively finally together with after grooving, the cable mouth that goes out through the rightest grooving bottom of driven capstan winch 92 from capstan winch casing 96 is derived Dao Lan mechanism 103 to the cable collection tube 101 that enters storage winch 100 and is arranged cable.
Driving winch 90 and storage winch 100 is major equipments (referring to Fig. 4 and Fig. 5) of balloon 10 folding and unfoldings, driving active capstan winch 91 cylindricals of winch 90 to be provided with 8 equidistantly with diameter circular arc grooving, at driven capstan winch 92 cylindricals, be provided with 9 equidistantly with diameter circular arc grooving, drive winch 90 to provide the folding and unfolding of hawser 1 to drive by friction force between the circular arc grooving on active capstan winch 91 and driven capstan winch 92 and hawser 1, on capstan winch casing 96, plane is initiatively provided with respectively safety pin device 94 in the both sides of capstan winch 91, in every cover safety pin device 94, be provided with independently two groups of latches, in the arc groove hole that can guarantee at least can insert active capstan winch 91 end faces by one group of latch separately in two cover safety pin devices 94 when initiatively capstan winch 91 is parked in optional position.Driving winch 90 capstan winch casing 96 middle parts to be also provided with friction stopping device 95, by the braking to driven capstan winch 92, increase the friction cornerite between hawser 1 and capstan winch, make the original initiatively capstan winch 91 that only relies on increase to 16 π with the 8 π cornerites that hawser 1 forms, the friction force of capstan winch to hawser 1 when increasing exponentially balloon 10 and being aloft detained, guarantee that balloon 10 is detained while there is exceedingly odious strong wind weather during skies, does not occur slippage between hawser 1 and two capstan winches.
Because the lift-off of balloon 10 highly reaches more than 2500 meters, storage winch 100 is main is responsible for storage cable and neat row's cable task, and be provided with that storage cable-end cable tension is measured, cable is long measures and other is about stable and safe additional function.The system of original early development is located at the long measurement mechanism of cable to drive in winch 90, but active capstan winch 91 and hawser 1 tension force between driven capstan winch 92 in winch 90 are larger owing to driving, hawser has certain stretch ratio, cause the folding and unfolding measured error that cable is grown back and forth to reach 10-20m, now the long measurement mechanism of cable is located in the Dao Lan mechanism of storage winch 100, owing to storing up the cable tension of cable-end, only have 50-100kg, such benefit is to have avoided cable stress to extend the measured error bringing.
When native system needs position shift or transportation, first the equipment of removing on ball installs to supporting special transport vehicle, with the helium service truck with system support, the helium recovery in balloon 10 purification are stored, separated hawser 1 is connected with balloon, by balloon 10 folding parcel entruckings, remove the pylon 52 of mooring mast 50.After tractor truck and superimposed trailer 20 are articulated, pack up fixed supporting leg 22, the rotary support 23 on superimposed trailer 20 and ground and stretch supporting leg 24, and the platform pivoted arm 34 of turn table 30 auxiliary hoist both sides, the left and right platform both sides of turning back are fixed, the revolution between locking turn table 30 and superimposed trailer 20 can be carried out transition transportation after supporting 26.Transition operates by above reverse order before enabling, and after comprehensive inspection is errorless, makes balloon 10 recover lift-off states.
The present embodiment is with regard to a kind of composition of the motor driven captive balloon lift-off recovery system based on special hawser, constructional feature and radical function are illustrated, because native system function is complicated, structure is various, emphasis of the present invention is lift-off recovery system, some and the lift-off non-directly related device in reclaiming scrap and local structure details in accompanying drawing, have been simplified, and in other related application patent, describe in detail about driving the concrete composition 26S Proteasome Structure and Function feature of winch 90 and storage winch 100, as friction-driven winch, storage winch and inside arrange friction stopping device, safety pin device, tension measuring device, storage winch end tension measuring device, the long measurement mechanism of folding and unfolding cable etc., if desired, can be with reference to other patent application document related to the present invention.
Claims (10)
1. motor driven captive balloon lift-off regenerative apparatus, comprise hawser (1), balloon (10), superimposed trailer (20), turn table (30), leadfair (40), mooring mast (50), control cabin (32) and equipment compartment (33), it is characterized in that: in the middle of described superimposed trailer (20), by the revolution arranging, support (26) and be connected with described turn table (30), described leadfair (40) is settled in one end of described turn table (30), the other end is settled described mooring mast (50), near described mooring mast (50) along described turn table (30) axis outwards arranging apparatus cabin (33) and control cabin (32) successively, in described equipment compartment (33), be provided with and drive winch (90) and storage winch (100), the cable channel that one end of described hawser (1) arranges along place, described turn table (30) axis by described leadfair (40) enters in described equipment compartment (33) through driving winch (90) to enter storage winch (100) storage cable, described hawser (1) other end connects described balloon (10).
2. a kind of motor driven captive balloon lift-off regenerative apparatus according to claim 1, is characterized in that: the both sides of described superimposed trailer (20) are also respectively equipped with at least 2 fixed supporting legs (22) and at least 2 extensile rotary supports (23) that are connected with stretching, extension supporting leg (24).
3. a kind of motor driven captive balloon lift-off regenerative apparatus according to claim 1, is characterized in that: described leadfair (40) comprises leads cable wheel (41), rolling deflection device (42) the ,Hu cable He Rulan of mechanism measurement of dip angle mechanism; Described leadfair (40) is positioned at middle part, turn table (30) rear end, leads cable wheel (41) and is connected with turn table (30) by the rolling deflection device (42) on introduction support.
4. a kind of motor driven captive balloon lift-off regenerative apparatus according to claim 1, is characterized in that: described driving winch (90) comprises initiatively capstan winch (91), driven capstan winch (92), reducing motor (93), safety pin device (94), friction stopping device (95) and capstan winch casing (96); In the front high rear low capstan winch casing (96) that is arranged in parallel of installation axis of described active capstan winch (91) and driven capstan winch (92), between active capstan winch (91) and driven capstan winch (92) capstan winch casing (96) space in be provided with friction stopping device (95), can implement braking to driven capstan winch.
5. a kind of motor driven captive balloon lift-off regenerative apparatus according to claim 1, is characterized in that: the tower height of described mooring mast (50) be >1/2 balloon (10) highly+highly+2 meters of equipment compartments (33).
6. a kind of motor driven captive balloon lift-off regenerative apparatus according to claim 1, it is characterized in that: the both sides of the turn table (30) between described leadfair (40) and described control cabin (32) are also symmetrical arranged is with standoff air cushion bag (37), the height of described air cushion bag (37) to be greater than the height of described equipment compartment (33) more than 2 meters.
7. a kind of motor driven captive balloon lift-off regenerative apparatus according to claim 1, is characterized in that: on the turn table (30) of described mooring mast (50) one end, be also provided with front auxiliary hoist (60); On the both sides platform of the turn table (30) of described leadfair (40) one end, be also provided with left redundant winch (70) and right redundant winch (80), three auxiliary hoistes are comprised of cable cylinder, retarder and drive motor, power of motor, retarder specification and contour structure size are identical, and drive motor is double speed AC induction motor.
8. a kind of motor driven captive balloon lift-off regenerative apparatus according to claim 1, it is characterized in that: described balloon (10) is dirigible shape, comprise oval spherical spheroid (11), three empennages (12) and a fairing (13) that is positioned at spheroid (11) lower rear; Described spheroid (11) head circular arc central authorities are provided with nose cone (19), in spheroid (11) bilateral symmetry, be provided with multiply bifurcated mooring line, mooring line converges to together and by latch closure, is connected with the tension pick-up (17) of below afterwards, and tension pick-up (17) below is connected with rotary connector (18); Described rotary connector (18) upper and lower can relatively rotate, and cable (1a) to the balloon (10) that below hawser (1) contains optical fiber through rotary connector (18) output provides power supply and communication; At balloon (10) head nose cone (19) exit, be provided with front mooring line (14), the left and right sides, rear portion is respectively equipped with left mooring line (15) and right mooring line (16).
9. a kind of motor driven captive balloon lift-off regenerative apparatus according to claim 8, it is characterized in that: the hollow straight-bar that described nose cone (19) is spherical for head is provided with, the nose cone lock (54) being provided with described mooring mast (50) when the Ground Mooring locks, and described front mooring line (14) is drawn from nose cone (19) hole.
10. a kind of motor driven captive balloon lift-off regenerative apparatus according to claim 8, is characterized in that: the length of described front mooring cable (14), left mooring cable (15) and right mooring cable (16) is all greater than 40 meters; The length of front mooring cable (14) is greater than left mooring cable (15) and right mooring cable (16), and during balloon (10) lift-off, the lower end of front mooring cable (14), left mooring cable (15) and right mooring cable (16) is all substantially in sustained height.
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| CN201310690943.7A CN103612741B (en) | 2013-12-16 | 2013-12-16 | Engine driven type captive balloon lift-off recovery system |
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| CN201310690943.7A CN103612741B (en) | 2013-12-16 | 2013-12-16 | Engine driven type captive balloon lift-off recovery system |
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| CN112550657A (en) * | 2020-11-06 | 2021-03-26 | 中国特种飞行器研究所 | Tethered balloon integrated comprehensive operation guarantee platform and use method thereof |
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| CN113060270A (en) * | 2021-03-09 | 2021-07-02 | 中国科学院空天信息创新研究院 | Mooring balloon anchoring facility |
| CN113548173A (en) * | 2021-06-08 | 2021-10-26 | 青岛德瑞高机械有限公司 | Adjustable side arm structure of captive balloon |
| CN115723936A (en) * | 2022-11-25 | 2023-03-03 | 中国特种飞行器研究所 | Mooring cable take-up and pay-off winch for mooring balloon |
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