CN103612741B - Engine driven type captive balloon lift-off recovery system - Google Patents
Engine driven type captive balloon lift-off recovery system Download PDFInfo
- Publication number
- CN103612741B CN103612741B CN201310690943.7A CN201310690943A CN103612741B CN 103612741 B CN103612741 B CN 103612741B CN 201310690943 A CN201310690943 A CN 201310690943A CN 103612741 B CN103612741 B CN 103612741B
- Authority
- CN
- China
- Prior art keywords
- winch
- balloon
- turn table
- mooring
- mooring line
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Landscapes
- Jib Cranes (AREA)
Abstract
The invention discloses a kind of motor driven captive balloon lift-off regenerative apparatus, comprise hawser, balloon, superimposed trailer, turn table, leadfair, mooring mast, control cabin and equipment compartment, revolving support by arranging in the middle of wherein said superimposed trailer is connected with described turn table, described leadfair is settled in one end of described turn table, the other end settles described mooring mast, close described mooring mast is outside arranging apparatus cabin and control cabin successively along described turn table axis, is provided with and drives winch and storage winch in described equipment compartment; One end of described hawser is entered in described equipment compartment by the cable channel that described leadfair is arranged along described turn table axis place and successively connects with driving winch and storage winch; The other end connects described balloon.Compact conformation of the present invention, deployment can be shifted flexibly, meet 2000-3500 rice ascending balloon and ball and carry the lift-off of equipment, recovery, to be detained and surface detention demand in the air, and there is good reliability, safety and comformability.
Description
Technical field
The present invention relates to a kind of lift-off recovery system, especially a kind of based on load-bearing, the Engine driven type captive balloon lift-off recovery system of one hawser of transmitting electricity, be in communication in.
Background technology
Captive balloon is a kind ofly used as the carrier of low idle task, and its difference is compared with hydrogen balloon with ordinary hot balloon, and have load-carrying capacity large, 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 weight, go up to the air height, wind loading rating and the attitude stability requirement of carrying equipment, required aerial buoyancy is greatly about the scope of 1-10 ton.For ensureing the safety of equipment on ball, the helium of certain pressure is filled in spheroid, after inflation, spheroid is blimp shape, end has empennage, can aloft keep stable attitude, 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 maximum countries applied by current captive balloon, dispose a large amount of low latitude captive balloons for traffic in drugs, the investigation tasks of smuggling and crossing illegally border in the U.S. and South American nations border, the U.S. also once used small-sized motor driven captive balloon for military purposes in the war in Iraq.The function relative satellite of captive balloon and prior-warning plane have unique advantage, have the advantages such as aerial delay, all-weather, real-time, cost is low of fixing a point.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, and the wayside equipment of fixed type captive balloon fixedly mounts with the earth, and scantling of structure can not be subject to space constraint, is applicable to the occasion that spheroid volume is comparatively large, load-carrying capacity is comparatively large and lift-off is highly higher.The lift-off reclaiming scrap of motor driven captive balloon is in-vehicle, can shift deployment flexibly, mobility strong by after balloon helium recovery.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 Engine driven type captive balloon lift-off recovery system based on special hawser.
Summary of the invention
The invention provides a kind of Engine driven type 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: the revolving support 26 by arranging in the middle of described superimposed trailer 20 is connected with described turn table 30, described leadfair 40 is settled in one end of described turn table 30, the other end settles described mooring mast 50, close described mooring mast 50 is outside arranging apparatus cabin 33 and control cabin 32 successively along described turn table 30 axis, be provided with in described equipment compartment 33 and drive winch 90 and storage winch 100, one end of described hawser 1 is entered in described equipment compartment 33 by the cable channel that described leadfair 40 is arranged along described turn table 30 axis place stores up cable through driving winch 90 to enter storage winch 100, described hawser 1 other end connects described balloon 10.
The both sides of described superimposed trailer 20 be also respectively equipped with at least 2 fixed supporting legs 22 and at least 2 be connected with the extensile rotary support 23 stretching supporting leg 24.
Described leadfair 40 comprises leads cable wheel 41, rolling deflection device 42, Hu Lan mechanism and Ru Lan measurement of dip angle mechanism; Described leadfair 40 is positioned in the middle part of 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.
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; Lowly after high before the installation axis of described active capstan winch 91 and driven capstan winch 92 be arranged in parallel in capstan winch casing 96, be provided with friction stopping device 95 in capstan winch casing 96 space between active capstan winch 91 and driven capstan winch 92, braking can be implemented to driven capstan winch.
The tower height of described mooring mast 50 is >1/2 balloon 10 height+equipment compartment 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 the standoff air cushion bag 37 of band, and the height of described air cushion bag 37 is greater than the height more than 2 meters of described equipment compartment 33.
Auxiliary hoist 60 before the turn table 30 of described mooring mast 50 one end is also provided with; The both sides platform of the turn table 30 of described leadfair 40 one end is also provided with left redundant winch 70 and right redundant winch 80.Three auxiliary hoistes are made up of cable cylinder, retarder and drive motor, and power of motor, retarder specification and contour structure size are identical, and drive motor is two-speed AC asynchronous dynamo.
Described balloon 10 is blimp shape, comprises the fairing 13 that oval spherical spheroid 11, three empennages 12 and are positioned at spheroid 11 lower rear; Described spheroid 11 head circular arc central authorities are provided with nose cone 19, and spheroid 11 bilateral symmetry is provided with multiply bifurcated mooring line, and mooring line is converged to and is connected with the tension pick-up 17 of below by latch closure afterwards together, is connected below tension pick-up 17 with rotary connector 18; Described rotary connector 18 upper and lower can relatively rotate, and the cable 1a that below hawser 1 exports containing optical fiber through rotary connector 18 provides power supply and communication to balloon 10; Mooring line 14 before balloon 10 head nose cone 19 exit is 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 rod that described nose cone 19 is spherical for head is provided with, for during Ground Mooring and the nose cone that is provided with of described mooring mast 50 lock 54 and lock, described front mooring line 14 is drawn from nose cone 19 hole.
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 when balloon 10 goes up to the air, the lower end of front mooring cable 14, left mooring cable 15 and right mooring cable 16 is in sustained height all substantially.
Feature of the present invention and beneficial effect are: relevant device and the device of captive balloon lift-off recovery system 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 driving 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 deployment flexibly, meets 2000-3500 rice ascending balloon and ball and carries the lift-off of equipment, recovery, to be 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 captive figure 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, revolving support, 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 is locked, and 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, initiatively 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.
Detailed description of the invention
Be applied as embodiment below by the Engine driven type captive balloon lift-off recovery system based on special hawser, and by reference to the accompanying drawings, technical scheme of the present invention be described in further detail.
Fig. 1 is Engine driven type captive balloon lift-off recovery system lift-off status architecture sketch, Fig. 2 is the birds-eye view after Fig. 1 conceals 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 view, 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 identified in the present embodiment figure describes and is oriented to based on balloon in Fig. 1 10 nose cone 19.
System mainly forms and comprises hawser 1, balloon 10, superimposed trailer 20, turn table 30, lead 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, the many special equipments comprising and overlap computing machine, GPS, air speed measuring apparatus etc. more are loaded with in spheroid 11 and fairing 13, contained equipment is extremely important and value is expensive, therefore this lift-off recovery system is focused on especially going up to the air except the folding and unfolding and Ground Mooring function external demand that meet balloon 10 and is reclaimed and safety in aerial delay process, guarantee balloon and being perfectly safe of load bearing equipment.Hawser 1 be a kind ofly collect load-bearing, the special cable of one of transmitting electricity, be in communication in, it is the main load-bearing cable that balloon 10 goes up to the air in removal process, hawser 1 is respectively skin, gauze screen, supporting course, four power leads and three optical fiber from outside to inside and forms, and exocuticle is take polythene material as the semi-conducting material that substrate adds conductive metal powder.Balloon is when going up to the air, and on ball, power supply needed for equipment is provided by the power lead in hawser 1, ball also has storage battery as emergency source of electrical power, and on ball, the data communication on computing machine and ground is by the Optical Fiber Transmission in hawser 1.
Containing numerous instrument and equipment in balloon 10, it is a complicated task system, the present embodiment only provides balloon 10 and reclaims the structure factor component relevant with Ground Mooring to lift-off, comprise hawser 1, spheroid 11, empennage 12, fairing 13, front mooring line 14, left mooring line 15, right mooring line 16, tension pick-up 17, rotary connector 18 and nose cone 19.The similar dirigible of profile of balloon 10, three empennages 12 contribute to keeping the stable of attitude in the air, fairing 13 is built with the major equipment performing air tasking, long front mooring line 14, left mooring line 15 and the right mooring line 16 of tens of rice respectively with turn table 30 is arranged before auxiliary hoist 60, left redundant winch 70 and right redundant winch 80 corresponding, auxiliary folding and unfolding when bearing balloon 10 near-earth and Ground Mooring.In spheroid 11 both sides, be symmetrical arranged the mooring line of multiply bifurcated, mooring line is converged to and is connected with the tension pick-up 17 of below by latch closure afterwards together, be connected with rotary connector 18 below tension pick-up 17, rotary connector 18 upper and lower can relatively rotate, the cable 1a that below hawser 1 exports containing optical fiber through rotary connector 18 provides power supply and communication to balloon 10, and cable 1a now no longer has weight capacity.The upper end tension force of hawser 1 measured by tension pick-up 17, the situation of buoyancy suffered by balloon 10 and wind-force change is reflected by the real-time dynamic data change of tension force, power lead when rotary connector 18 ensures that balloon rotates with the wind in hawser 1 and optical fiber are connected with the reliable of equipment on ball, the hollow straight rod that nose cone 19 is spherical for head is provided with, lock 54 for nose cone during Ground Mooring and on mooring mast 30 to lock, front mooring line 14 is drawn from nose cone 19 hole.
This captive balloon lift-off recovery system is motor driven, lift-off reclaiming scrap and relevant accessory device are all carried on the turn table 30 of superimposed trailer 20, turn table 30 is connected with superimposed trailer 20 by revolving support 26, turn table 30 can rotate by the revolving support 26 between superimposed trailer 20, when changing orientation when balloon 10 by wind impact aloft, free rotation followed by turn table.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, support ground by the some fixed supporting legs 22 arranged front and back and hang wheel 25, and expand distance enforcement supplemental support ground by the stretching, extension supporting leg 24 launching swinging strut 23 end at superimposed trailer about 20, what keep superimposed trailer 20 grabs ground stability.
Keystone configuration composition on turn table 30 comprises leadfair 40 from left to right by Fig. 1, left redundant winch 70, right redundant winch 80, two air cushion bags 37 that left and right is arranged, OPS 32, equipment compartment 33, mooring mast 50 and front auxiliary hoist 60, leadfair 40 takes turns 41 by leading cable, rolling turning gear 42, Hu Lan mechanism and as compositions such as cable measurement of dip angle mechanisms, the effect leading cable wheel 41 imports in equipment compartment 33 by transferring horizontal direction to balloon 10 connection cable, rolling turning gear 42 automatically can adjust according to the deflection of aerial hawser 1 and lead cable and take turns 41 pivot angles, prevent hawser and lead cable and take turns circular arc grooving side on 41 and rub, Hu Lan mechanism seals hawser 1 by rotating nylon jacket and is leading the circular arc grooving outlet on cable wheel 41, prevent hawser from skidding off and lead the grooving that cable takes turns 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 balloon 10 is from captive release and close to auxiliary take-up during ground, by the front jocket wheel 55 arranged at mooring mast 50 top, front mooring line 14 is received to front auxiliary hoist 60, respectively left mooring line 15 and right mooring cable 16 are taken in left redundant winch 70 and right redundant winch 80 by the left guide wheel 71 of platform pivoted arm 34 end of the left and right sides, turn table 30 platform body 31 rear end and right guide wheel 81.During the work of left and right auxiliary hoist, carry out operating and monitoring in the operation suspension 35 that two operating personals lay respectively at auxiliary hoist side, left and right.The effect of two air cushion bags 37 that both sides, turn table 30 rear portion are overhead is when balloon 10 Ground Mooring, and isolated sphere 11 and the hardware configuration grazing on turn table 30, play isolation buffer protective effect.Operating personal is by aft mounted winding stair about 36 turn table 30.
The front center of turn table 30 is located at by mooring mast 50, comprise the operation suspension 35 of the front auxiliary hoist 60 that tower seat 51, pylon 52, ascending stair 53 and tower seat 51 are installed, the nose cone that tower top is arranged lock 54, front jocket wheel 55 and tower top side, before balloon 10 goes up to the air and when reclaiming close to ground, operating personal is climbed in the operation suspension 35 of tower top by ascending stair 53, is responsible for going out lock and entering to be locked into line operate between balloon 10 nose cone 19 and nose cone lock 54.Pylon 52 and tower seat 51 adopt disassembled structure, remove pylon 52 and above equipment when being convenient to transition transport.
Balloon 10 went up to the air and between aerial demurrage, hawser 1 enters the inner cable channel access arrangement cabin 33 arranged, turn table 30 axis through leading cable wheel 41 guiding with horizontal direction, for prevent hawser in cable channel with near steel structure grazing, in cable channel, be provided with some levels and the sinking of restriction hawser 1 when relaxed state of vertical deflector roll and deflection.
When balloon 10 is in Ground Mooring state, the nose cone 19 of balloon 10 head inserts in the nose cone lock 19 at mooring mast 50 top, and the electromagnetic lock pinning nose cone 19 locked in 19 by nose cone exports.The Ground Mooring of balloon 10 is except before holding respectively by three auxiliary hoistes, except left and right mooring line, the spheroid 11 of balloon 10 is 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 mooring of superimposed trailer 20, to ensure the Ground Mooring safety of balloon 10.
Before balloon 10 goes up to the air, first untie all auxiliary mooring lines, the nose cone lock 54 at first energising release mooring mast 50 top, then mooring line 14 before front auxiliary hoist 60 is loosened slightly, at this moment by the spring in nose cone lock 19, the nose cone 19 of balloon 10 is ejected, then start three auxiliary hoistes simultaneously, slow releasing balloon 10, when three auxiliary hoist near-earth release balloons 10, hawser 1 is relaxed state, until hawser 1 completely stressed after, continue the mooring cable of release three auxiliary hoistes until front mooring line 14, left mooring line 15 and right mooring line 16 are released completely.After three auxiliary mooring cables discharge by three auxiliary hoistes completely, balloon 10 just enters the mode of operation driving 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 reducing motor 93 of winch 90 to adopt the speed control mode work of frequency control, the drive motor of storage winch 100 is permanent torque control mode work, keeps the tension force substantially constant of the hawser 1 driven between winch 90 and storage winch 100.During cable laying, due to the effect of balloon 10 buoyancy, reducing motor 93 works as generating state, consumes generated energy by arranging discharging resistance in circuit.
When take-up is carried out to aerial balloon 10, initiatively capstan winch 91 is driven to rotate by reducing motor 93, behind hawser 1 access arrangement cabin, the driven capstan winch 92 driving winch 90 is entered from driving the cable mouth that enters of the capstan winch casing 96 of winch 90, enter the first grooving of initiatively capstan winch 91 from top near the first grooving of reducing motor 93 through driven capstan winch 92, successively active capstan winch 91 and driven capstan winch 92 be wound to that initiatively capstan winch keeps right last 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 entering storage winch 100 and is carried out row's cable.
Driving winch 90 and storage winch 100 are major equipments (see Fig. 4 and Fig. 5) of balloon 10 folding and unfolding, 8 are provided with equidistantly with diameter circular arc grooving driving active capstan winch 91 cylindrical of winch 90, 9 are provided with equidistantly with diameter circular arc grooving at driven capstan winch 92 cylindrical, winch 90 is driven 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, the both sides of plane active capstan winch 91 are provided with safety pin device 94 respectively, often overlap in safety pin device 94 and be provided with independently two groups of latches, when can ensure that initiatively capstan winch 91 is parked in optional position, two overlap in safety pin device 94 and at least can be inserted in the arc groove hole of initiatively capstan winch 91 end face by one group of latch separately.Friction stopping device 95 is also provided with in the middle part of driving winch 90 capstan winch casing 96, by the braking to driven capstan winch 92, increase the friction cornerite between hawser 1 and capstan winch, the original 8 π cornerites only relying on active capstan winch 91 and hawser 1 to be formed are made to increase to 16 π, to increase exponentially when balloon 10 is detained capstan winch aloft to the friction force of hawser 1, when guaranteeing to occur exceedingly odious strong wind weather during balloon 10 is detained sky, between hawser 1 and two capstan winches, there is not slippage.
Because the lift-off of balloon 10 highly reaches more than 2500 meters, storage winch 100 primary responsibility 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.Long for cable measurement mechanism is located at and is driven in winch 90 by the system of original comparatively early development, but owing to driving hawser 1 tension force between the active capstan winch 91 in winch 90 and driven capstan winch 92 larger, hawser has certain stretch ratio, the folding and unfolding measured error that cable is long is back and forth caused to reach 10-20m, now long for cable measurement mechanism is located in the Dao Lan mechanism of storage winch 100, because the cable tension storing up cable-end only has 50-100kg, such benefit is that of avoiding cable stress and extends the measured error brought.
When native system needs position shift or transport, first the equipment removed on ball installs to supporting special transport vehicle, with the helium service truck with system support, the helium recovery in balloon 10 is purified and stored, be separated the connection of hawser 1 and balloon, by the entrucking of balloon 10 folding parcel, remove the pylon 52 of mooring mast 50.After tractor truck and superimposed trailer 20 are mounted, pack up fixed supporting leg 22, the rotary support 23 on superimposed trailer 20 and ground and stretch supporting leg 24, and platform both sides of being turned back by the platform pivoted arm 34 of turn table about 30 auxiliary hoist both sides are fixed, after the revolving support 26 between locking turn table 30 and superimposed trailer 20, transition transport can be carried out.Transition operates by above reverse order before enabling, and makes balloon 10 recover lift-off state after comprehensive inspection is errorless.
The present embodiment is with regard to a kind of composition of the Engine driven type 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 lift-off reclaiming scrap non-immediate relevant apparatus and local structure details is simplified in accompanying drawing, and describe in detail in other Related Applications Patent about driving the concrete composition 26S Proteasome Structure and Function feature of winch 90 and storage winch 100, as friction drive 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 necessary, can with reference to other patent application document related to the present invention.
Claims (3)
1. a 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), equipment compartment (33), drive winch (90), storage winch (100), the cable channel access arrangement cabin (33) that one end of hawser (1) is arranged along turn table (30) axis place by leadfair (40), hawser (1) other end connects described balloon (10), revolving support (26) by arranging in the middle of superimposed trailer (20) is connected with turn table (30), one end of turn table (30) is provided with leadfair (40), the other end is provided with mooring mast (50), it is characterized in that: near described mooring mast (50) along described turn table (30) axis outwards arranging apparatus cabin (33) and control cabin (32) successively, be provided with in described equipment compartment (33) and drive winch (90) and storage winch (100), hawser (1) enters storage winch (100) storage cable through driving winch (90), 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), before the installation axis of described active capstan winch (91) and driven capstan winch (92), height is low is afterwards arranged in parallel in capstan winch casing (96), is provided with friction stopping device (95) in capstan winch casing (96) space between active capstan winch (91) and driven capstan winch (92), described leadfair (40) comprises leads cable wheel (41), rolling deflection device (42), Hu Lan mechanism and Ru Lan measurement of dip angle mechanism, be positioned in the middle part of turn table (30) rear end, lead cable wheel (41) and be connected with turn table (30) by the rolling deflection device (42) on wheel bracket, the both sides of the turn table (30) between described leadfair (40) and described control cabin (32) are also symmetrical arranged the standoff air cushion bag (37) of band, the turn table (30) of described mooring mast (50) one end is also provided with front auxiliary hoist (60), the both sides platform of the turn table (30) of described leadfair (40) one end is also provided with left redundant winch (70) and right redundant winch (80), described balloon (10) is blimp shape, comprises oval spherical spheroid (11), fairing (13) that three empennages (12) and one are positioned at spheroid (11) lower rear, described spheroid (11) head circular arc central authorities are provided with nose cone (19), spheroid (11) bilateral symmetry is provided with multiply bifurcated mooring line, mooring line is converged to and is connected with the tension pick-up (17) of below by latch closure afterwards together, and tension pick-up (17) below is connected with rotary connector (18), described rotary connector (18) upper and lower can relatively rotate, and the cable (1a) that below hawser (1) exports containing optical fiber through rotary connector (18) provides power supply and communication to balloon (10), be provided with front mooring line (14) at balloon (10) head nose cone (19) exit, the left and right sides, rear portion is respectively equipped with left mooring line (15) and right mooring line (16).
2. a kind of motor driven captive balloon lift-off regenerative apparatus according to claim 1, it is characterized in that: the hollow straight rod that described nose cone (19) is spherical for head is provided with, for during Ground Mooring and the nose cone that is provided with of described mooring mast (50) lock (54) and lock, described front mooring line (14) is drawn from nose cone (19) hole.
3. a kind of motor driven captive balloon lift-off regenerative apparatus according to claim 1, is characterized in that: the length of described front mooring line (14), left mooring line (15) and right mooring line (16) is all greater than 40 meters; The length of front mooring line (14) is greater than left mooring line (15) and right mooring line (16), during balloon (10) lift-off, the lower end of front mooring line (14), left mooring line (15) and right mooring line (16) is in sustained height all substantially.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310690943.7A CN103612741B (en) | 2013-12-16 | 2013-12-16 | Engine driven type captive balloon lift-off recovery system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310690943.7A CN103612741B (en) | 2013-12-16 | 2013-12-16 | Engine driven type captive balloon lift-off recovery system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103612741A CN103612741A (en) | 2014-03-05 |
| CN103612741B true CN103612741B (en) | 2016-02-10 |
Family
ID=50163470
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310690943.7A Expired - Fee Related CN103612741B (en) | 2013-12-16 | 2013-12-16 | Engine driven type captive balloon lift-off recovery system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103612741B (en) |
Families Citing this family (37)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105599891B (en) * | 2014-10-31 | 2017-12-26 | 鸿富锦精密工业（深圳）有限公司 | Captive balloon |
| TWI557026B (en) | 2014-10-31 | 2016-11-11 | 鴻海精密工業股份有限公司 | Moored balloon |
| CN106335622A (en) * | 2015-12-11 | 2017-01-18 | 中国特种飞行器研究所 | Motor-driven sightseeing tethered balloon |
| TWI592336B (en) * | 2016-03-03 | 2017-07-21 | 輔英科技大學 | Controlling device of mooring a sounding balloon |
| CN105947170B (en) * | 2016-05-31 | 2018-12-18 | 中国科学院光电研究院 | A kind of detachable windshield and captive balloon of captive balloon |
| CN106043659B (en) * | 2016-06-15 | 2018-10-02 | 中国科学院光电研究院 | A kind of inflating expanded method in aerostatics field |
| CN106275362B (en) * | 2016-08-26 | 2024-03-19 | 深圳光启空间技术有限公司 | Cable junction box, fairing and aerostat |
| CN106477016B (en) * | 2016-10-19 | 2019-03-29 | 东莞前沿技术研究院 | Captive balloon mooring system |
| CN106516069B (en) * | 2016-10-25 | 2018-07-13 | 中国电子科技集团公司第三十八研究所 | It is a kind of to be used for captive balloon folding and unfolding and resident motor-driven anchoring vehicle |
| CN106585744B (en) * | 2016-12-05 | 2018-10-12 | 中国特种飞行器研究所 | Fixed and vehicular integration captive balloon mooring system |
| CN106628099A (en) * | 2016-12-05 | 2017-05-10 | 中国特种飞行器研究所 | Tethered and autonomous flight dual-purpose solar aerostat |
| CN106585743B (en) * | 2016-12-05 | 2018-09-21 | 中国特种飞行器研究所 | A kind of large and medium-sized captive balloon vehicular mooring system |
| CN106769138B (en) * | 2016-12-12 | 2018-11-16 | 中国特种飞行器研究所 | Idiocratically Orly drags simulation test device and method for a kind of captive balloon Limit of Wind Speed static balance |
| CN106976545B (en) * | 2017-03-21 | 2019-03-19 | 中国电子科技集团公司第三十八研究所 | A kind of captive balloon utricule ground lifting apparatus |
| CN108725740B (en) * | 2017-04-17 | 2024-05-28 | 佛山顺德光启尖端装备有限公司 | Aerostat and control method of aerostat |
| CN107628222B (en) * | 2017-08-23 | 2020-04-24 | 中国人民解放军63653部队 | Method for transferring and flying large airship by adopting integrated truss type device |
| CN107697263B (en) * | 2017-08-23 | 2020-07-07 | 中国人民解放军63653部队 | Large airship transferring and flying platform |
| CN207792337U (en) * | 2017-12-25 | 2018-08-31 | 东莞前沿技术研究院 | The dual-purpose lift-off recovery system of cable reclaimer and movement and position |
| CN109231039B (en) * | 2018-09-13 | 2020-11-10 | 江苏科技大学 | Electromechanical winch system for lifting and recovering aerostat and working method |
| CN111294114B (en) * | 2018-12-07 | 2021-06-29 | 华为技术有限公司 | Optical communication node, relay node and optical communication system |
| CN110065648A (en) * | 2019-04-19 | 2019-07-30 | 中国电子科技集团公司第三十八研究所 | A kind of anchoring semi-mounted chassis being tethered at for large-scale captive balloon with transition transport |
| CN110579822A (en) * | 2019-09-17 | 2019-12-17 | 山东鲁普科技有限公司 | mooring air exploration ball winding and unwinding device and control circuit and control method thereof |
| CN110712737B (en) * | 2019-10-12 | 2022-11-18 | 中国特种飞行器研究所 | Follow-up device |
| CN110745230B (en) * | 2019-10-29 | 2023-07-14 | 湖南航天远望科技有限公司 | High-altitude balloon issuing device and method |
| CN111003135A (en) * | 2019-12-19 | 2020-04-14 | 中国电子科技集团公司第三十八研究所 | Five-point type mooring device for mooring balloon |
| CN111114736B (en) * | 2019-12-27 | 2023-03-14 | 中国特种飞行器研究所 | Captive balloon, ground equipment and helium-filled automatic unfolding method |
| CN111413122B (en) * | 2020-03-30 | 2021-11-12 | 江苏科技大学 | Aerostat cable winding and unwinding experimental system based on Profinet communication and control method thereof |
| CN111776192B (en) * | 2020-06-01 | 2021-09-28 | 中国科学院空天信息创新研究院 | Captive balloon main node posture adjusting mechanism |
| CN111717737B (en) * | 2020-07-17 | 2021-10-19 | 江苏科技大学 | Deviation rectifying method for winding and unwinding of winch cable of aerostat |
| CN111776193A (en) * | 2020-07-30 | 2020-10-16 | 青岛德瑞高机械有限公司 | Mooring balloon anchoring device |
| CN112550657B (en) * | 2020-11-06 | 2022-09-20 | 中国特种飞行器研究所 | Tethered balloon integrated comprehensive operation guarantee platform and use method thereof |
| CN112678140B (en) * | 2020-12-30 | 2022-11-22 | 中国特种飞行器研究所 | Split type captive balloon ground anchoring system |
| CN113060270B (en) * | 2021-03-09 | 2023-01-31 | 中国科学院空天信息创新研究院 | Mooring balloon anchoring facility |
| CN113548173B (en) * | 2021-06-08 | 2024-08-09 | 青岛德瑞高机械有限公司 | Adjustable tethered balloon side arm structure |
| CN114162303A (en) * | 2021-12-10 | 2022-03-11 | 北京航空航天大学云南创新研究院 | Automatic device and method for mooring airship by multiple cables |
| 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 |
| CN117163863B (en) * | 2023-09-20 | 2024-06-21 | 青岛海洋科技中心 | Device and method for assisting cable arrangement of underwater winch |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4402479A (en) * | 1981-06-19 | 1983-09-06 | Westinghouse Electric Corp. | Small tethered aerostat relocatable system |
| US4421286A (en) * | 1979-08-02 | 1983-12-20 | Otis Engineering Corporation | Mooring system |
| CN101898633A (en) * | 2010-04-28 | 2010-12-01 | 湖南航天管理局 | All-in-one anchoring trailer |
| CN202966651U (en) * | 2012-11-27 | 2013-06-05 | 中国科学院光电研究院 | Anchoring device for captive balloon |
-
2013
- 2013-12-16 CN CN201310690943.7A patent/CN103612741B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4421286A (en) * | 1979-08-02 | 1983-12-20 | Otis Engineering Corporation | Mooring system |
| US4402479A (en) * | 1981-06-19 | 1983-09-06 | Westinghouse Electric Corp. | Small tethered aerostat relocatable system |
| CN101898633A (en) * | 2010-04-28 | 2010-12-01 | 湖南航天管理局 | All-in-one anchoring trailer |
| CN202966651U (en) * | 2012-11-27 | 2013-06-05 | 中国科学院光电研究院 | Anchoring device for captive balloon |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103612741A (en) | 2014-03-05 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103612741B (en) | Engine driven type captive balloon lift-off recovery system | |
| CN101506032A (en) | Hybrid lift air vehicle | |
| CN103963991B (en) | A kind of electromechanical integration unmanned plane onboard system | |
| CN108116668A (en) | The land and air double-used more rotor manned aircraft of full electricity | |
| CN207157480U (en) | Unmanned investigation dirigible system and low latitude detecting system | |
| ITMI20091340A1 (en) | PERFORMED AUTOSTABLE BALLOON AND RELATIVE INVOLVATION AND RECOVERY SYSTEM | |
| CA2829782A1 (en) | Airborne platform | |
| CN102756804A (en) | Method for performing fly-lifting rescue in mountain ravine and off-road ambulance | |
| CN103832508B (en) | There is the helicopter trailer of landing, security function | |
| CN112660357B (en) | Container-type captive balloon anchoring platform | |
| CN112469896A (en) | Unmanned aerial vehicle, control method, associated platform and high altitude turbine | |
| CN106274506A (en) | A kind of urban air public transportation system | |
| CN110745230B (en) | High-altitude balloon issuing device and method | |
| CN112224437A (en) | Vehicle-mounted cabled rotorcraft system | |
| US20030015114A1 (en) | Bolonkin's method movement of vehicles and installation for it | |
| CN203681702U (en) | Helicopter tow truck with take-off and landing and guarantee functions | |
| US20220306267A1 (en) | Devices and methods for extending aircraft cargo bays with replacement tailcones | |
| CN115743511A (en) | Planet detection floating system and planet detection method | |
| CN104477421A (en) | Moon landing high ladder | |
| CN212766817U (en) | Near-earth space exploration and scientific test platform | |
| CN208360472U (en) | A kind of hub motor type anchoring vehicle | |
| CN108298057A (en) | The big dirigible built with more dirigibles and the dirigible ring around earth rotation flight | |
| CN206678984U (en) | Novel cable car system | |
| CN206155762U (en) | Subminiature captive balloon system | |
| CN210793609U (en) | Maneuvering type captive balloon system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160210 Termination date: 20181216 |