CN208021702U - A kind of telescopic folding type anchoring platform - Google Patents
A kind of telescopic folding type anchoring platform Download PDFInfo
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- CN208021702U CN208021702U CN201820444623.1U CN201820444623U CN208021702U CN 208021702 U CN208021702 U CN 208021702U CN 201820444623 U CN201820444623 U CN 201820444623U CN 208021702 U CN208021702 U CN 208021702U
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Abstract
The utility model belongs to kite balloon airship field, is related to a kind of telescopic folding type anchoring platform comprising chassis, revolving support, revolving platform fold arm, mooring mast, hoist system and switch board.The wherein described chassis installation Telescopic rotary hydraulic leg is connected by revolving support with chassis for the entirely support of anchoring platform and automatic loading and unloading, the revolving platform, can be rotated around the centre of gyration, revolving platform can be flexible along platform truck length direction.The advantage of the utility model is compact-sized, and mobility is good, can carry the anchoring, lift-off, resident and recycling demand of 500-3000 meters of different size kite balloon airships, have higher stability, safety and economy.
Description
Technical field
The utility model belongs to kite balloon airship field, is related to a kind of telescopic folding type kite balloon airship anchoring platform, especially
It is a kind of based on stretch big frame, fold arm, telescopic outrigger in one kite balloon airship anchor platform.
Background technology
Vehicle-mounted kite balloon airship system is a kind of high maneuverability, can rapid deployment equipment, can carry various payload with
Support is taken photo by plane and communication task.It compared to unmanned plane of taking photo by plane, can be resident for a long time, energy consumption is low, and area of taking photo by plane is wide, is side sea
Anti-, environmental monitoring, anti-smuggling anti-terrorism, early warning and electronic countermeasure, technical search, information relaying, sighting distance extension, myriametric wave communication etc. one
Series is related to the required general character platform of the significant problems such as national defence and the people's livelihood.The working depth of general low latitude kite balloon airship is 500-
3000 meters, single airborne period is 10-30 days, and wind loading rating is strong, safeguards simply, has extensive civilian and military purposes.
Vehicle-mounted kite balloon airship system is mainly made of floating platform and ground safeguard system two parts.Floating platform utilizes sky
Lift of gas, it can be achieved that in from ground to ceiling section arbitrary height it is long-term resident, payload is promoted to object height, it is complete
At lasting working at height.Ground safeguard system includes anchor parking platform, energy safeguard system, inflation system and monitoring station.It should
System provides support for the fast reserve of floating platform, rapid deployment, while can ensure and replace the days such as battery and supplement helium
The implementation of normal maintenance task.
Anchor parking system can be divided into fixed and motor driven, and fixed anchoring platform is fixedly mounted with the earth, for large size
The anchoring of kite balloon airship is let fly away and is recycled, and has feature simple and reliable for structure, at low cost.Motor driven anchoring platform is vehicle-mounted
Formula, for middle-size and small-size kite balloon airship anchoring, let fly away and recycle, can flexible deployment in the areas such as city, forest, grassland, coastal,
Mobility strong.
This field needs to have both the novel kite balloon airship anchoring platform of the advantage of both existing anchoring platforms.
Utility model content
In order to meet the needs of this field is for novel kite balloon airship anchoring platform, spy proposes the utility model.
The utility model provides a kind of telescopic folding type anchoring platform, compact-sized, more efficient.
On the one hand the utility model provides a kind of telescopic folding type anchoring platform comprising chassis is set on chassis
Revolving support, the revolving platform being set on revolving support and the folding arm being set on revolving platform, mooring mast, hoist engine system
System and switch board.
In the one side of the utility model, the chassis includes chassis skeleton, is located at four endpoints of the chassis skeleton
Telescopic hydraulic support arm and main supporting leg and rotary type hydraulic auxiliary leg positioned at the hydroboom outer end.The chassis bone
Frame is preferably rectangle, including is located at four telescopic hydraulic support arms of four endpoints of rectangle, which can work
When stretch out chassis skeleton except, anchor platform storage when retraction chassis skeleton within.
In the one side of the utility model, the revolving support is driven by the hydraulic motor being set on revolving platform.
In the one side of the utility model, the revolving platform includes revolution fixed platform, and the big frame that stretches is put down with flexible
Platform；The revolution fixed platform is connect with the revolving support, can be rotated relative to the chassis by the revolving support；
The scaling platform by it is described stretch big frame relative to the revolution fixed platform it is overhanging and contraction.
The installing and dismounting formula dirigible holder in the one side of the utility model, the big frame that stretches.
Guardrail is installed in the one side of the utility model, the revolution fixed platform.
In the one side of the utility model, the opposite sides for folding arm and being mounted on the scaling platform, i.e. left and right
Both sides, and include folding arm, hydraulic cylinder assists hoist engine and hanging basket,
Described folding arm one end and the scaling platform are hinged and are folded by the hydraulic cylinder.
In the one side of the utility model, the mooring mast includes mooring mast body frame, nose cone, lifting motor, mooring mast
Pedestal, head drawstring hoist engine and tower drag, and the mooring mast body frame is hinged with tower base is tethered at, and is realized by the lifting motor
The folding of the mooring mast body frame, the head drawstring hoist engine are located at described be tethered in tower base.
In the one side of the utility model, the hoist system includes main winch, head pulley and drag-line, the master
The drag-line that hoist engine folding and unfolding is oriented to through the head pulley, the drag-line other end connect kite balloon airship.
In the one side of the utility model, the mooring mast and the head pulley are respectively arranged in the revolving platform
Opposite sides, i.e. front and rear sides, the main winch is close to the mooring mast.
In the above-mentioned aspect of the utility model, by scaling platform, arm is folded, the expansion of mooring mast and hydroboom,
Can meet anchoring platform the anchoring of middle-size and small-size kite balloon airship let fly away and removal process in requirement, while passing through above-mentioned portion
The contraction of part folds, and anchoring platform can be made to meet the requirement of vehicle-mounted transport size, is launched convenient for containerzation transport.
On the other hand the utility model provides a kind of specific nose cone, the nose cone includes inward turning unlocking type nose cone lock, is used
It is lockked in by the nose cone of kite balloon airship.
The nose cone is locked：
With the bell-mouthed Cavity unit of cavity,
Mounted on n lock bolt unit of the cavity horn mouth exterior, each lock bolt unit has embedded cavity
The closing piece of horn mouth through-hole and the compression spring being attached thereto,
It is nested in inside the Cavity unit and co-axial inward turning unlocking unit, the inward turning unlocking unit has n
A through-hole,
During nose cone locks, nose cone enters Cavity unit under the bell-mouthed guiding of cavity, and the open-top closing piece is described
Closing piece is sprung back under the pressure of compression spring, locks nose cone,
During nose cone release, inward turning unlocking unit rotation, the open-top closing piece of unlock side wall of through-hole discharges nose cone.
In the one side of the utility model, n is the natural number of 2-4, and the n lock bolt unit is uniformly mounted on the chamber
The position of body horn mouth exterior, the n through-hole and the lock bolt unit corresponds to.
In the one side of the utility model, n=3.
In the one side of the utility model, the closing piece have inclined-plane towards cavity iiared port direction and/or
Pulley, the inclined-plane or pulley are intended to keep the process of the open-top closing piece of nose cone more smooth and smooth.
In the one side of the utility model, the closing piece has inclined-plane and/or pulley towards the unlock side wall, institute
It states inclined-plane or pulley is intended to keep the process of the open-top closing piece of unlock side wall more smooth and smooth.
In the one side of the utility model, inward turning unlocking type nose cone lock further includes driving unit, and the driving unit drives
The dynamic inward turning unlocking unit rotation, therefore the release process of nose cone without carrying out manually.
In the one side of the utility model, the driving unit drives the inward turning to unlock list by stepper motor motor
Member rotation, therefore inward turning unlocking unit does not make 360 ° of rotations, but rotated back and forth during the latching of nose cone and release.
In the one side of the utility model, the Cavity unit and the opposite one end of the cavity horn mouth have cavity
Flange is fixed in mounting base.
In the one side of the utility model, the lock bolt unit further includes lock pin, and closing piece slides chamber and sliding chamber lid,
Described lock pin one end connects the closing piece, and the other end is equipped with the band plug rod vertical with main shaft,
Cross one another one group of deep groove and one group of shallow grooves are equipped at the top of the sliding chamber lid,
When needing manual releasing nose cone, it will can lift from deep groove with plug rod manually, embedded shallow grooves after rotation,
Then closing piece leaves the lockhole of nose cone, and nose cone can freely discharge.
In the one side of the utility model, bottom of the compression spring both ends respectively with the closing piece and the sliding chamber lid connects
It touches, and around a part for the lock pin.
On the other hand the utility model provides a kind of specific kite balloon airship comprising a kind of high intensity nose cone connection dress
It sets.The collocation of the anchoring platform of the kite balloon airship and the utility model uses, and in other words, the anchoring platform of the utility model can be into
One step includes kite balloon airship described herein.
The high intensity nose cone attachment device includes kayak body covering and is welded thereon and adds for circular first successively
The nose skin of Qiang Bu, the second reinforcement cloth and round shape,
Described first, which reinforces cloth and the second reinforcement cloth, respectively has across the edge of kayak body covering inner ring,
The edge of the first reinforcement cloth and the second reinforcement cloth is welded together by Edge Enhancement item.
In the one side of the utility model, described first reinforces cloth, and second reinforces the internal radius of cloth and kayak body covering
It is essentially identical.It is described in the utility model " essentially identical ", refer to numerical value difference within 1%.In the case, first adds
The inner ring contact of junction and kayak body covering between strong cloth and the respective ring part of the second reinforcement cloth and marginal portion, kayak body
The inner ring pair first of covering reinforces cloth and second and reinforces the ring part formation constraint of cloth.
In the one side of the utility model, described second reinforces the annulus outer diameter and nose skin of cloth, the first reinforcement cloth
Circle outer diameter it is incremented by successively.
In the one side of the utility model, the nose skin is circle, have a diameter larger than described first reinforce cloth and
Second reinforces the annulus outer diameter of cloth.
In the one side of the utility model, the internal diameter of the kayak body covering is less than the diameter of nose skin.
In the one side of the utility model, the Edge Enhancement item has a V-arrangement cross section, and the both arms of V-arrangement are respectively with the
The edge of the edge of one reinforcement cloth and the second reinforcement cloth welds together.
In the one side of the utility model, the edge and the edge of the first reinforcement cloth and the second reinforcement cloth add
Strong item has multiple connecting holes.
In the one side of the utility model, the connecting hole installs corn button.
In the one side of the utility model, the nose cone attachment device further includes being welded on described first to reinforce cloth and the
Two thirds for reinforcing among cloth reinforce the even further 4th reinforcement cloth of cloth.Described third and fourth reinforces the structure and work of cloth
Reinforce the similar of cloth with cloth and second is reinforced with described first.
In the one side of the utility model, the described first internal radius for reinforcing cloth is 900-1100mm, and internal-and external diameter is poor
For 100-300mm, the described first width for reinforcing the edge of cloth is 50-100mm.
In the one side of the utility model, the described second internal radius for reinforcing cloth is 900-1100mm, and internal-and external diameter is poor
For 80-200mm, the described second width for reinforcing the edge of cloth is 50-100mm.
It is worth noting that the circle or annulus described in the above-mentioned aspect of the utility model refer both to that kite balloon airship can be bonded
The circle or annulus of head shape.More precisely, a part of round table of round substantially sphere described in the utility model
Face either a part of surface annulus described in the utility model substantially side of round platform at the top of spheroid or from spheroid
A part of circular surface of top interception.It is flat for xy with the plane where round or annulus periphery in three-dimensional system of coordinate
Face, then round or annulus the center of circle is not on x/y plane.Or in simple terms, round or annulus the center of circle and periphery are non-coplanar.
On the other hand the utility model provides a kind of emergent draw off gear of kite balloon airship, can the device be optionally set to anchor
It on parking, for example is set on the revolving platform of anchoring vehicle, copes with special circumstances.
The draw off gear includes undinding and rewinding drum, turning unit and pivoting support；
The outer ring of the pivoting support is connected with one end of the undinding and rewinding drum, the inner ring of the pivoting support and described time
Turn unit connection；
The turning unit can rotate under the action of the pivoting support around the axis of the undinding and rewinding drum；
Conducting wire pulley A on the turning unit, wire guide pulley wheels B and Universal pulley；
Tether cable is to be basically parallel to the direction of the axis, successively through the wire guide pulley wheels A, wire guide pulley wheels B and ten thousand
After being oriented to pulley, it is wound on the undinding and rewinding drum with the direction basically perpendicular to the axis, or by opposite trend
Unwinding.
In the one side of the utility model, the turning unit includes the first driving motor and driving gear, the drive
Moving gear engages the gear of the outer ring of the pivoting support, axis of the first driving motor driving turning unit around undinding and rewinding drum
Line rotates, and realizes winding or the unwinding of tether cable.
In the one side of the utility model, the tether cable is through the wire guide pulley wheels A, wire guide pulley wheels B and universal cunning
The guiding of wheel is respectively substantially 90 ° of angles.
Term described in the utility model " substantially " refers to that deviation is in ± 10% model existing for numerical value or geometrical relationship
In enclosing, such as " substantially 90 ° of angles " described herein refer to the angle within the scope of 81-99 °.
In the one side of the utility model, the turning unit has tower structure, is in rectangular shape.
In the one side of the utility model, the turning unit specifically includes rotary rack, wire guide pulley wheels A, conducting wire and slides
Take turns B, the first driving motor, driving gear and transverse slat；
The rotary rack is in rectangular shape, has tower structure；
The transverse slat is located at turn around frame top and connects the inner ring of pivoting support；
The wire guide pulley wheels A is installed on above transverse slat, is preferably basic water by substantially vertical guiding by tether cable
Square to；
The wire guide pulley wheels B, which is installed at the top of rotary rack, leans on proximal edges side, preferably by tether cable by basic horizontal
Direction guiding is substantially vertical；
First driving motor is installed on above transverse slat, exports axis connection sliding tooth wheel, and the driving gear is located at cross
It is engaged below plate and with the outer ring gear of pivoting support, to drive turning unit unitary rotation.
In the one side of the utility model, the kite balloon airship draw off gear further includes supporting rack, the undinding and rewinding drum
Lower end be fixed on support frame as described above, therefore during the folding and unfolding of tether cable, undinding and rewinding drum does not occur relative to supporting rack
Rotation, but turning unit rotates.
In the one side of the utility model, support frame as described above is removable to be fixed on anchoring vehicle, and in other words, this practicality is new
The kite balloon airship draw off gear of type can be used as emergency set and use temporarily.The kite balloon airship draw off gear of certain the utility model
It can be permanently secured to according to actual demand on anchoring vehicle.
In the one side of the utility model, the kite balloon airship draw off gear further includes row's cable unit, row's cable list
Member includes Universal pulley, pulley bracket, row's cable lead screw, conducting wire polished rod and the second driving motor；
The Universal pulley connects pulley bracket, is preferably basic horizontal side by substantially vertical guiding by tether cable
To；
The conducting wire polished rod and row's cable lead screw are parallel to the axis installation, the guide rail as the pulley bracket；
Second driving motor drives row's cable lead screw for the cable lead screw rotation of the row of driving, by motor positive and inverse, makes cunning
Wheel support is moved axially along the axis.
Compared to the prior art, the advantage technology effect of the utility model includes following one or more：
1. compared with tradition anchors platform, the utility model is non-wheeled motor anchoring platform, and it is flat to solve tradition anchoring
The problem of platform highway transportation superelevation, pass through the reasonable Arrangement of Optimal Structure Designing and load so that anchoring platform truck overall structure
It is simple and reliable, reduce manufacturing cost；
2. using scaling platform structure, the length of anchoring platform is can adjust, realizes that a vehicle is multi-purpose, Multiple Type is completed and is tethered at
The anchoring of dirigible is let fly away and is recycled, and can carry the anchoring, lift-off, resident and recycling of 500-3000 meters of different size kite balloon airships and need
It asks；
3. using Telescopic rotary hydraulic leg technology, it can be achieved that the process that anchoring platform actively loads and unloads, reaches motor-driven fortune
The purpose of defeated dispensing.
Description of the drawings
The utility model is described in further detail with reference to the accompanying drawings and detailed description.
Fig. 1 shows the schematic diagram of the anchoring of the utility model embodiment 1 platform in a folded configuration；
Fig. 2 indicates schematic diagram of the anchoring platform of the utility model embodiment 1 under entrucking state；
Fig. 3 indicates schematic diagram of the anchoring platform of the utility model embodiment 1 in transport process；
Fig. 4 indicates the schematic diagram of the anchoring platform anchoring kite balloon airship of the utility model embodiment 1；
Fig. 5 indicates the vertical view (not showing kite balloon airship) of Fig. 4；
Fig. 6 indicates the schematic diagram under the utility model kite balloon airship lift-off state；
Fig. 7 indicates the stereoscopic schematic diagram of 2 nose cone lock construction of the utility model embodiment；
Fig. 8 shows the diagrammatic cross-sections of 2 nose cone lock construction of the utility model embodiment；
Fig. 9 indicates the structural schematic diagram of 2 nose cone of the utility model embodiment lock Cavity unit；
Figure 10 indicates the structural schematic diagram of 2 nose cone of the utility model embodiment lock inward turning unlocking unit；
Figure 11 indicates the structural schematic diagram of 2 nose cone of the utility model embodiment lock lock bolt unit；
Figure 12 indicates the structural schematic diagram of 2 nose cone of the utility model embodiment lock driving unit；
Figure 13 indicates the local axonometric drawing of 3 nose cone attachment device of the utility model embodiment；
Figure 14 indicates the partial front elevation view of 3 nose cone attachment device of the utility model embodiment；
Figure 15 indicates the Structure explosion diagram of 3 nose cone attachment device of the utility model embodiment；
Figure 16 indicates the axonometric drawing of 3 nose cone of the utility model embodiment；
Figure 17 indicates 3 nose cone of the utility model embodiment and the scheme of installation of nose cone attachment device；
Figure 18 indicates that the utility model embodiment 4 is met an urgent need the pre- take-up status diagram of draw off gear；
Figure 19 indicates that the utility model embodiment 4 is met an urgent need the folding and unfolding status diagram of draw off gear；
Figure 20 indicates that the utility model embodiment 4 is met an urgent need the turning unit schematic diagram of draw off gear；
Figure 21 indicates that the utility model embodiment 4 is met an urgent need row's cable cell schematics of draw off gear；
Figure 22 indicates that the utility model embodiment 4 is met an urgent need the using effect schematic diagram of draw off gear.
In figure：
1- anchoring platforms,
The chassis 2-, 4- revolving platforms, 5- fold arm, 6- mooring masts, 7- hoist systems；
The chassis 20- skeleton, the main supporting legs of 21-, 22- hydraulic pressure auxiliary legs, 23- hydrobooms；
30- revolving supports, 31- hydraulic motors, 32- electric slip rings；
40- turns round fixed platform, and 41- stretches big frame, 42- scaling platforms, 43- guardrails, 44- dirigible holders；
50- folding arms, 51- hydraulic cylinders, 52- assist hoist engine, 53- hanging baskets；
60- mooring mast body frames, 61- nose cones, 62- lifting motors, 63- are tethered at tower base, the heads 64- drawstring hoist engine, 65-
Tower drags；
70- main winch, 71- head pulleys, 72- drag-lines；
80- switch boards, 81- operation consoles；
90- dirigible utricules, 100- flat cars, 101- helium tanks, 102- supply vehicles；
501- Cavity units, 5011- cavitys flange, 5012- cavitys horn mouth, 50121- cavity horn mouth through-holes；
502- inward turnings unlocking unit, 5021- rotation unlock piece, 5022- driven gears, the first deep groove ball bearings of 5023-,
5024- planes needle roller thrust bearing, the second deep groove ball bearings of 5025-, 5026- taper roll bearings, 50211- through-holes, 50212-
Unlock side wall；
503- lock bolts unit, 5031- slide chamber lid, 5032- lock pins, 5033- compression springs, 5034- closing pieces slide chamber, 5035- closing pieces,
5036- band plugs rod, the inclined-planes 50351-, 50352- pulleys；
505- driving units, 5051- drivings gear, 5052- motor mounts, 5053- stepper motor motors；
504- mounting bases, 506- leading block units；
91- kayak body coverings, 92- nose skins, 93- first reinforce cloth, and 94- second reinforces cloth, 95- Edge Enhancement items, 96-
Corn button, 97- ropes, 98- nose cones, 980- connection annulus, 981- bearing diagonal rod pieces, 982- adapter flanges；
461- undinding and rewinding drums, 462- supporting racks, 463- turning units, 464- pivoting supports, 465- arrange cable unit, 466- systems
Stay hawser；
4631- rotary racks, the first driving motor of 4632- wire guide pulley wheels A, 4633- wire guide pulley wheels B, 4634-, 4635- drive
Moving gear, 4636- transverse slats；
4651- Universal pulleys, 4652- pulley brackets, 4653- row's cable lead screws, 4654- conducting wire polished rods, 4655- are dismantled and assembled
Frame, the second driving motors of 4656-.
Specific implementation mode
The utility model is further described below by specific embodiment combination attached drawing, described preferred implementation
Example is only used for describing and explaining the present invention, and is not used to limit the utility model.
Embodiment 1
The utility model embodiment 1 provides a kind of specific telescopic folding type anchoring platform.
Fig. 1 is structure diagram of the telescopic folding type anchoring platform after complete fold under storage configuration, and Fig. 2 is this
Telescopic folding anchoring platform automatic loading schematic diagram, Fig. 3 are telescopic folding anchoring platform transfer process schematics, and Fig. 4 is vehicle-mounted
Kite balloon airship anchored condition structure diagram, Fig. 5 are the vertical views that Fig. 4 conceals dirigible, and Fig. 6 is under vehicle-mounted kite balloon airship lift-off state
Schematic diagram.
The present embodiment is based on Fig. 1 and mark orientation is described, and before 6 position of mooring mast is, 71 institute of head pulley is in place
After being set to.
As shown in Figure 1, telescopic folding type anchoring platform includes chassis 2, revolution support 30, revolving platform 4, arm 5 is folded,
Mooring mast 6, hoist system 7, switch board 80.
Chassis 2 includes chassis skeleton 20, main supporting leg 21, hydraulic pressure auxiliary leg 22 and hydroboom 23.
Chassis skeleton 20 is welded by two crossbeams and more longerons, is connect with revolving platform 4 by revolving support 30,
It is used to support the rotation of entire anchoring platform.
Chassis 2 is landed by main supporting leg 21 realizes the support of whole system.
Above-mentioned hydroboom 23, is installed at left and right sides of chassis, 23 end of hydroboom is disposed with detachably totally by 4
Main supporting leg 21 and hydraulic pressure auxiliary leg 22 realize anchoring by flexible and hydraulic pressure auxiliary leg 22 the rotation of hydroboom 23
Automatic loading and unloading process of the platform 1 on haulage vehicle.Working condition is landed by main supporting leg 21, and hydraulic pressure auxiliary leg 22 is packed up.Drop
Low anchoring platform center of gravity improves anti-overturning energy.The span for increasing main supporting leg 21 using hydroboom 23 improves anchoring platform 1
Stability, while again to greatest extent ensure that anchoring platform 1 conveyor width.
Above-mentioned revolving support 30, is driven by hydraulic motor 31.It is flat to turn round by the electrical mixing slip ring of centre installation
Platform 4 provides the energy and fluid pressure line.
Above-mentioned revolving platform 4, including revolution fixed platform 40, stretch big frame 41, scaling platform 42, guardrail 43, dirigible
Holder 44.It turns round fixed platform 40 to be connected with revolving support 30,360 degree of rotations can be carried out around revolving support 30 by control.It stretches
Contracting platform 42 carries out the overhanging of platform by the big frame 41 of hydraulically extensible and shrinks, and carries mechanical lock, on the big frame of hydraulically extensible 41
Detachable dirigible holder 44 is installed, scaling platform 42 is rotated around the centre of gyration together with revolution fixed platform 40.
Above-mentioned folding arm 5 includes folding arm 50, and hydraulic cylinder 51 assists hoist engine 52, hanging basket 53.Folding arm 50
Portion and 42 left and right sides of scaling platform are hinged, and unfolded action is completed by hydraulic cylinder；Outer end is equipped with auxiliary hoist engine
52 operate hanging basket 53 with detachable, and dirigible both sides assist drawstring by 52 folding and unfolding of auxiliary hoist engine.
Above-mentioned mooring mast 6 includes mooring mast body frame 60, nose cone 61, and lifting motor 62 is tethered at tower base 63, head drawstring
Hoist engine 64, tower drags 65.Mooring mast 6 is mounted on 4 front end of revolving platform, and mooring mast body frame 60 is by lifting motor under travel position
62 are folded, and drag 65 fixations by detachable tower；By lifting motor 62 or hydraulic cylinder by mooring mast body frame 60 under working condition
It erects.6 bottom securement head drawstring hoist engine 64 of mooring mast carries out the folding and unfolding of head hawser, total with left and right auxiliary 52 machine of elevator
With 3 points of anchorings for realizing kite balloon airship.
Above-mentioned hoist system 7 includes main winch 70, head pulley 71, drag-line 72.Main winch 70, which is installed on, to be tethered at
6 rear of tower, head pulley 71 are installed on scaling platform 42, are moved with scaling platform 42.
Above-mentioned switch board 80 is installed on 70 left side of main winch.
Arm 5, mooring mast 6 are folded in Fig. 1, hydroboom 23 is in folding shrinking state, and effective solution anchoring is flat
The transportation problem of platform 1.
As shown in Fig. 2, wooden handcart 100 is equipped with helium tank 101, supply vehicle 102 and anchoring platform 1.Using same flat car
100 carry out transport dispensing, and advantage is mobility height.
The platform 1 that anchors uses self-loading and unloading technology, and four hydrobooms 23 are protruded horizontally up outward to specified during entrucking
Then four rotations of hydraulic pressure auxiliary leg 22 to vertical position and are locked, start hydraulic pressure auxiliary leg 22 anchoring is flat by position
Platform is raised to 1.4 meters, and flat car 100 pours into anchoring 1 lower section neutral gear of platform, as shown in Figure 3.Then hydraulic pressure auxiliary leg 22 starts
It shrinks, anchoring platform 1 is positioned on flat car 100, rotating hydraulic auxiliary leg 22 to horizontal position simultaneously locks, and by four
Hydroboom 23 is withdrawn, that is, completes entrucking process, as shown in Figure 2.
Four hydrobooms 23 are protruded horizontally up to designated position outward during unloading, and by four hydraulic pressure auxiliary legs 22
Rotation is to vertical position and locks, and starts hydraulic pressure auxiliary leg 22 and anchoring platform is raised to 1.4 meters, main supporting leg 21 is mounted on
23 end of hydroboom, hydraulic pressure auxiliary leg 22 starts to shrink at after flat car 100 sails out of anchoring platform 1, and anchoring platform 1 is placed
In ground, subsequent rotating hydraulic auxiliary leg 22 is to horizontal position and locks.
Dollie 100 is general-purpose vehicle.
As shown in Figures 4 and 5, anchoring platform 1 is positioned over using area, and the big frame 41 that stretches is hydraulically operated to be unfolded backward, together
When fold arm 5 and be unfolded around cradle head, mooring mast 6 is lifted to vertical working condition by lifting motor 62.Installation dirigible holder 44,
Guardrail 43, operation console 81 remove tower support 65.Dirigible utricule 90 is anchored at anchoring platform by mooring mast 6 and auxiliary hoist engine 52
On vehicle 1, the flexible effective active length for having adjusted anchoring platform 1 of scaling platform 42 enables anchoring platform 1 to complete a variety of
The launch mission of specification kite balloon airship, while the transportation clearance of anchoring platform is reduced, it is readily transported.Large span hydroboom 23
And main supporting leg 21, the structure centre of anchoring platform 1 is reduced, overall stability is improved.
As shown in fig. 6, dirigible utricule 90 is connected via head pulley 71 with main winch 70 by drag-line 72, drag-line 72 is
The compound cable of high-strength light provides electric power and transmission signal for dirigible, and head pulley 71 is two degrees of freedom pulley, is equipped with dynamometry
Meter monitors the stress of drag-line 72, has the function of overload-alarm in real time.It is adjustable that main winch 70 goes out rope speed, by arranging cable automatically
Mechanism carries out the arrangement of drag-line 72 during take-up.During dirigible utricule 90 is let fly away, nose cone 61 is unlocked, passes through head drawstring
Hoist engine 64 and the auxiliary hoist engine 52 of left and right two, which discharge nose cone drawstring and auxiliary drawstring, makes dirigible utricule slowly rise, and reaches one
Determine 70 rope closing of main winch after height, complete buoyancy transfer, subsequent main winch 70, which puts rope and carries out the lift-off of dirigible utricule 90, to be made
Industry.
The big frame 41 that stretches during lift-off is contracted in revolution fixed platform 40, to reduce the revolution of anchoring platform 1
Radius improves whole control accuracy.
The control system integration of anchoring platform 1 is operated by operating personnel on operating platform 81 in switch board 80,
81 fast demountable of operating platform.
Embodiment 2
The utility model embodiment 2 provides a kind of specific nose cone lock, it is a kind of inward turning unlocking type nose cone lock.
Referring to Fig. 7 and 8, the inward turning unlocking type nose cone lock described in the present embodiment includes Cavity unit 501, inward turning unlocking unit
502, lock bolt unit 503, mounting base 504, driving unit 505, leading block unit 506.
Referring to Fig. 9, the Cavity unit 501 includes cavity flange 5011, cavity horn mouth 5012.The cavity flange
There is flange face at 5011 both ends, wherein larger one side flanged joint mounting base 504, smaller one side flanged joint cavity horn mouth
5012 flanged sides.The smaller one end of 5012 diameter of cavity horn mouth, i.e. neck, outer surface on open there are three through-hole
50121, it is passed through for closing piece 5035.Three lock bolt units 503 are installed on corresponding position, as shown in Figure 7.These three lock bolt units
503, closing piece 5035, realize the function that nose cone is locked or discharged in other words.
Referring to Figure 10, the inward turning unlocking unit 502 includes rotation unlock piece 5021, driven gear 5022, the first zanjon
Ball bearing 5023, plane needle roller thrust bearing 5024, the second deep groove ball bearing 5025, taper roll bearing 5026.And cavity
When unit 501 assembles, the rotation unlock piece 5021 puts on the first deep groove ball bearing 5023 and plane needle roller thrust bearing 5024,
It is inserted into from horn mouth 5012 along 501 axis of Cavity unit, until 5024 two sides of plane needle roller thrust bearing is respectively against cavity flange
5011 planes and rotation 5021 open bottom plane of unlock piece, then the second deep groove ball bearing 5025 is inserted in rotation unlock piece
5021, Internal and external cycle is respectively cooperating with rotation 5021 cylindrical surface of unlock piece and 5011 inner cavity surface of cavity flange.The taper roller axis
It holds 5026 to be inserted in from the other side of 5021 open end of rotation unlock piece, 5026 outer ring of taper roll bearing is justified with cavity flange 5011
Connected in star coordinates.5022 side of the driven gear carries the groove for making rotation unlock piece 5021 be embedded in, and driven gear 5022 is recessed
Plane outside slot preferentially resists 5026 inner ring of taper roll bearing, rotates unlock piece 5021 and driven gear by screw connection
5022.So that the inward turning unlocking unit 502 is overlapped with the axis of Cavity unit 501 and inward turning unlocking unit 502 can be around axis certainly
By rotating.As shown in Figure 10, through-hole 50211 there are three being set on unlock piece 5021, wherein one end side wall structure of through-hole 50211 are rotated
At unlock side wall 50212.It is also inclined-plane to unlock side wall 50212, is similar to inclined-plane 50351 described below.
Referring to Figure 11, the lock bolt unit 503 includes sliding chamber lid 5031, lock pin 5032, compression spring 5033, closing piece cunning chamber
5034, closing piece 5035.The closing piece slides outer surface of the chamber 5034 by 5012 neck of screw connection cavity horn mouth, such as Fig. 7 institutes
Show.One group of cross recesses, respectively two deep grooves and two shallow grooves are arranged at 5031 top of the sliding chamber lid.5031 bottom of sliding chamber lid
Portion connects closing piece and slides chamber 5034.The lock pin 5032 is inserted into sliding chamber lid 5031, is inserted into sliding chamber 5034.The band plug rod 5036 of upper end
The deep groove of 5031 upper end of sliding chamber lid is sticked into, compression spring 5033 is then inserted in the lower end of lock pin 5032, and connects closing piece 5035.Then it presses
Spring 5033 is constrained between closing piece 5035 and sliding chamber lid 5031.Two opposite sides of closing piece 5035 are equipped with inclined-plane 50351, separately
Outer two opposite sides are equipped with pulley 50352, as shown in figure 11.Inclined-plane 50351 is intended to that nose cone is made to enter cavity horn mouth
Open-top closing piece 5035 is more smoothly when 5012.Pulley 50352 is intended to make the process of 50212 open-top closing piece 5035 of unlock side wall more
It is smooth.
Referring to Figure 12, the driving unit 505 includes driving gear 5051, motor mount 5052, stepper motor motor
5053.The stepper motor motor 5053 is mounted on motor mount 5052, and the motor mount 5052 connects mounting base
504, the driving gear 5051 connects 5053 output shaft of stepper motor motor, and drives gear 5051 and driven gear 5022
It is meshed.
Referring to Fig. 7, the leading block unit 506 is arranged on platform, for guiding the direction for changing nose cone drawstring.
When use：
Nose cone locks process, and the 5012 seeker coning of horn mouth of the Cavity unit 501 enters cavity, and passes through inclined-plane
The closing piece 5035 of 50351 open-top lock bolt units 503, closing piece 5035 enter closing piece and slide chamber 5034, and compression spring 5033 is compressed；Until head
Wimble fraction completely into, then inclined-plane 50351 be detached from nose cone, compression spring 5033 spring back, closing piece 5035 is pushed up back, nose cone is thus lockked,
Limit nose cone abjection nose cone lock.
Nose cone discharges process, and the stepper motor motor 5053 of the driving unit 505 drives driving gear 5051 to rotate, with
Its driven gear 5022 engaged rotates therewith, and inward turning unlocking unit 502 is driven to rotate, and in the process, unlocks side wall 50212
By the closing piece 5035 of 50352 open-top lock bolt unit 503 of pulley, compression spring 5033 is compressed again；At this point, lock bolt unit 503 solves
Lock, nose cone can freely be deviate from, and release is completed；The subsequent stepper motor motor 5053 is turned back to initial position, drives inward turning
Unlocking unit 502 returns to initial position together, then unlocks side wall 50212 and be detached from pulley 50352, compression spring 5033 is sprung back, by closing piece
5035 push up back lockup state.
When electrical malfunction in special circumstances, hand gear unlock can be used.When unlock, lock bolt unit is pulled one by one
Band plug rod 5036 on 503, by 5032 pull-up of lock pin, compression press spring 5033 drives closing piece 5035 to rise, and is detached from locking shape
State；The rod of rotation band plug at this time 5036, discharges after it is gone to scrobicula groove location from the deep groove position of sliding chamber lid 5031, then locks
The slightly downlink under the elastic force effect of compression spring 5033 of block 5035, remains at unlocked state, nose cone can freely be deviate from this time.
Compared to the prior art, the advantage of the utility model embodiment 2 is, is locked, it can be achieved that personnel by electric-controlled mechanical
It is whole to complete operation on the ground, it ensure that personnel safety, and easy to operate.Under special circumstances, manual mode can also be passed through
Discharge nose cone.
Embodiment 3
The utility model embodiment 3 provides the kite balloon airship that a kind of and embodiment 1 anchoring vehicle collocation uses, this is tethered at winged
The characteristics of ship, is there is a kind of high intensity nose cone attachment device.
Specifically, the high intensity nose cone attachment device described in the present embodiment includes nose skin 92, kayak body covering 91,
One, which reinforces cloth 93, second, reinforces cloth 94, Edge Enhancement item 95, corn button 96 and rope 97.First reinforces cloth 93 and second
It is annular shape to reinforce cloth 94, and ring part overlapping is welded between nose skin 92 and kayak body covering 91, with ring part
The marginal portion of connection passes through the inner ring of kayak body covering 91, is turned down to far from kite balloon airship towards the direction of nose cone, therefore ship
The inner ring pair first of body covering 91 reinforces the ring part formation constraint that cloth 93 and second reinforces cloth 94.It if necessary, can be in ship
The inner ring of body covering 91 adds a reinforcing ring, wales the junction of the ring part and marginal portion of two reinforcement cloth.
The marginal portion of two reinforcement cloth is therefore exposed across the inner ring of kayak body covering 91, and is welded with Edge Enhancement item 95
It connects.It is " V "-shaped to weld back edge stiffener 95, in the two-arm trepanning of " V " character form structure, installation corn button 96, rope 97
Nose cone 98 is fixed by corn button.
After entire kite balloon airship is completed, above-mentioned nose skin 92 constitutes the head envelope circle of dirigible.
More specifically, as shown in Figure 13, Figure 14, first reinforces the ring part overlapping welding that cloth 93 and second reinforces cloth 94
Between nose skin 92 and kayak body covering 91, the marginal portion of exposing is not welded then with nose skin.First reinforces 93 He of cloth
Second marginal portion for reinforcing cloth 94 is welded with Edge Enhancement item 95 respectively, and welding back edge stiffener 95 is " V "-shaped, edge
The first welding position for reinforcing the reinforcement cloth 94 of cloth 93 and second is torn during stiffener 95 can effectively prevent use, simultaneously
Also improve the intensity of corn button installation site." V " font two-arm has the connection of the uniformly distributed a diameter of 6mm of annular
Hole or mounting hole, pitch of holes 100mm, mounting hole are located on the center line in chevron portion, and corn button 96 is respectively arranged in respectively
In a mounting hole." V " font both sides can be carried out using multilayer Edge Enhancement item 95 according to the size of eyelet and magnitude of load
Reinforce, using one layer of Edge Enhancement item 95 in the present embodiment.
As shown in figure 15, the first reinforcement cloth 93 is annulus shape, internal radius 1000mm, the welding with kayak body covering 91
Width, that is, annular section width, be 120mm, with Edge Enhancement item 95 weld marginal portion width be 60mm.
Second reinforces cloth 94 as annulus shape, and internal radius 1000mm reinforces cloth 93 with kayak body covering 91 and first
Weld width, that is, annular section width, be 100mm, the width of marginal portion welded with Edge Enhancement item 95 is
60mm.Edge Enhancement item 95 is rectangle or annular bar, width 120mm.
Nose cone is described specifically below.The nose cone attachment device of the present embodiment is i.e. for connecting nose cone with kite balloon airship
Together.
As shown in figure 16, nose cone is mainly welded by the aluminium-alloy pipe that wall thickness is 2mm, including connection annulus 980, oblique branch
Strut member 981 and adapter flange 982, the annular of bearing diagonal rod piece 981 are equably welded on connection annulus 980, the other end with turn
Acting flange 982 is spirally connected.
As shown in figure 17, the connection annulus of nose cone 98 is put into the Edge Enhancement item 95 of " V " shape in installation process, is used
Rope 97 sequentially passes through the corn button 96 on 95 both sides of Edge Enhancement item of " V " shape, the connection annulus bundled fixed with nose cone 98.
Uniform load on nose cone can be passed to the first reinforcement cloth 93 and second and reinforced on cloth 94 by the uniformly distributed corn button 96 of annular, and two
Layer reinforcement cloth passing to uniform load on kayak body covering 91 in the form of shearing force by the welding glue-line with kayak body covering 91.
Above-mentioned apparatus bearing capacity is strong, designability is good, has and safeguards simple, convenient for disassembly and assembly feature.
Embodiment 4
The utility model embodiment 4 provides a kind of emergent draw off gear of the kite balloon airship for the vehicle that anchors, and specifically includes receipts
It unreels cylinder 461, supporting rack 462, turning unit 463, pivoting support 464 and row's cable unit 465 and matching used is tethered at cable
Rope 466, as shown in figure 18.
The undinding and rewinding drum 461 is placed vertically, i.e. axis vertical, perpendicular to the ground.The lower end of undinding and rewinding drum 461 and support
Frame 462 is connected, and not rotatably, the outer ring of the other end, that is, upper end connection pivoting support 464, outer ring is equipped with gear；The revolution
Unit 463 connects the inner ring of pivoting support 464；Row's cable unit 465 connects turning unit 463.
As shown in figs 20 and 21, row's cable unit 465 and turning unit 463 form a cuboid frame after being stitched together
Frame, undinding and rewinding drum 461 are embedded among the frame, and frame can be rotated around the axis of undinding and rewinding drum 461.The present embodiment is for arranging cable
The division of the structure of unit 465 and turning unit 463 does not influence overall structure, is not mutual indepedent, function between two components
It can combine, it is also assumed that entire frame is an individual component.
As shown in figure 20, the turning unit 463 includes rotary rack 4631, wire guide pulley wheels A 4632, wire guide pulley wheels
B4633, the first driving motor 4634, driving gear 4635 and transverse slat 4636.
Above-mentioned rotary rack 4631 includes upper and lower top surface and a side.It is welded with one piece of transverse slat between two beams of top surface
4636, the inner ring of bottom surface connection (for example being spirally connected) pivoting support 464 of the transverse slat 4636.Wire guide pulley wheels A 4632 is installed on cross
4636 upper center of plate substantially passes through the axis of undinding and rewinding drum 461.The wire guide pulley wheels B 4633 is installed on rotary rack 4631
Close to the side of row's cable unit 465, first driving motor 4634 is installed on 4636 top of transverse slat for top surface, and output axis connection is driven
Moving gear 4635, the driving gear 4635 are located at 4636 lower section of transverse slat, are engaged with the gear of 464 outer ring of pivoting support, to
Drive 463 unitary rotation of turning unit.
As shown in figure 21, row's cable unit 465 include Universal pulley 4651, pulley bracket 4652, row's cable lead screw 4653,
Conducting wire polished rod 4654 removable shelves 4655 and second driving motor 4656.
The Universal pulley 4651 connects pulley bracket 4652, and the conducting wire polished rod 4654 and row's cable lead screw 4653 are parallel to
The axis of undinding and rewinding drum 461, be installed on it is removable shelve 4,655 two beams between, 4652 both ends of the pulley bracket are pierced into respectively
Conducting wire polished rod 4654 and row's cable lead screw 4653 are simultaneously slided using them as guide rail.Second driving motor 4656 is for the row of driving
Cable lead screw 4653 rotates, and drives row's cable lead screw 4652 by motor positive and inverse, pulley bracket 4652 is made to be moved axially along lead screw, real
Now arrange cable.
When take-up, entire emergent draw off gear is arranged in anchoring platform truck angle pulley top or side, it is pre- to pull
One section of tether cable gets off, and tether cable 466 is limited to wire guide pulley wheels A 4632, wire guide pulley wheels B 4633 and universal cunning successively
In the grooving of wheel 4651, during which need to dismantle wire guide pulley wheels A 4632, wire guide pulley wheels B 4633, Universal pulley 4651, row's cable list
Member 465 and 461 1 side flange of undinding and rewinding drum burst at the seams slot, for tether cable 466 to be penetrated drum center and is drawn from lower end,
It avoids rotary rack 4631 from being rolled up in turning course and stirs tether cable 466.Tether cable 466 in place after, tether cable 466 is consolidated
Due on undinding and rewinding drum 461, the first driving motor 4634 work, turning unit 463 starts to rotate, 465 turns of the row's of drive cable unit
Dynamic, tether cable 466 is wound on the cylinder of undinding and rewinding drum 461, makes the winding edge of tether cable 466 by arranging cable unit 465
The axial direction for reel is equidistantly arranged, and as shown in figure 19, the second driving motor 4656 works at the same time, and makes 4652 He of pulley bracket
Universal pulley 4651 is in suitable height, so that tether cable 466 enters undinding and rewinding drum 461 with horizontal direction；It is in the process
It stays the winding of hawser 466 in undinding and rewinding drum 461, and completes the recycling of kite balloon airship.
The release process of tether cable 466 is similar with above-mentioned removal process, and tether cable 466 is horizontal from undinding and rewinding drum 461
Unwinding after wire guide pulley wheels B and wire guide pulley wheels A about 90 ° of dog-ear of difference, is vertically left entire through Universal pulley 4651
Emergent draw off gear.In the process, turning unit 463 is rotated around undinding and rewinding drum 461 in opposite direction, will finally be tethered at cable
Rope 466 takes out from device, completes letting fly away for kite balloon airship.
Emergent draw off gear through this embodiment, can be in tether cable retractable equipment failure, as reliable standby
With retractable equipment folding and unfolding kite balloon airship, ensure being smoothed out for kite balloon airship task；In addition, by the device, can not break
It is bad, do not change be fixed on retractable equipment end tether cable connection in the case of carry out kite balloon airship folding and unfolding, will not twist with
The tether cable of retractable equipment end connection；The device avoids the uncertainty of result for taking repair Replacing Scheme to bring,
Avoid the safety problem of economic loss and personnel caused by release helium scheme；Furthermore it is possible to be tethered in device completion
After dirigible task, mooring system is transported to designated position and carries out malfunction elimination.
Claims (9)
1. a kind of telescopic folding type anchoring platform (1), which is characterized in that including chassis (2), the revolution being set on chassis (2)
(30), the revolving platform (4) being set on revolving support (30) and the folding arm (5) being set on revolving platform (4) are supported, is
Stay tower (6), hoist system (7) and switch board (80).
2. anchoring platform as described in claim 1, which is characterized in that the chassis (2) includes chassis skeleton (20), is located at institute
State the telescopic hydraulic support arm (23) of (20) four endpoints of chassis skeleton and the main supporting leg positioned at the hydroboom (23) outer end
(21) and rotary type hydraulic auxiliary leg (22).
3. anchoring platform as described in claim 1, which is characterized in that the revolving support (30) is by being set to revolving platform
(4) hydraulic motor (31) driving on.
4. anchoring platform as described in claim 1, which is characterized in that the revolving platform (4) includes revolution fixed platform
(40), stretch big frame (41) and scaling platform (42)；The revolution fixed platform (40) connect with the revolving support (30), energy
Enough rotated relative to the chassis (2) by the revolving support (30)；The scaling platform (42) passes through the big frame that stretches
(41) relative to the revolution fixed platform (40) it is overhanging and shrink.
5. anchoring platform as claimed in claim 4, which is characterized in that installing and dismounting formula dirigible branch on the big frame (41) of stretching
Guardrail (43) is installed on frame (44) and the revolution fixed platform (40).
6. anchoring platform as claimed in claim 4, which is characterized in that the folding arm (5) is mounted on the scaling platform
(42) opposite sides, and include folding arm (50), hydraulic cylinder (51) assists hoist engine (52) and hanging basket (53),
Described folding arm (50) one end and the scaling platform (42) are hinged and pass through the hydraulic cylinder (51) and fold.
7. anchoring platform as described in claim 1, which is characterized in that the mooring mast (6) includes mooring mast body frame (60), nose
It bores (61), lifting motor (62) is tethered at tower base (63), and head drawstring hoist engine (64) and tower drag (65),
The mooring mast body frame (60) and to be tethered at tower base (63) hinged, passes through the lifting motor (62) and realizes the mooring mast
The folding of body frame (60),
The head drawstring hoist engine (64) is located at described be tethered in tower base (63).
8. anchoring platform as described in claim 1, which is characterized in that the hoist system (7) includes main winch (70),
Head pulley (71) and drag-line (72), the drag-line (72) that main winch (70) folding and unfolding is oriented to through the head pulley (71) are described
Drag-line (72) other end connects kite balloon airship.
9. anchoring platform as claimed in claim 8, which is characterized in that the mooring mast (6) and the head pulley (71) are respectively
It is installed on the opposite sides of the revolving platform (4), the main winch (70) is close to the mooring mast (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820444623.1U CN208021702U (en) | 2018-03-31 | 2018-03-31 | A kind of telescopic folding type anchoring platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820444623.1U CN208021702U (en) | 2018-03-31 | 2018-03-31 | A kind of telescopic folding type anchoring platform |
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| Publication Number | Publication Date |
|---|---|
| CN208021702U true CN208021702U (en) | 2018-10-30 |
Family
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820444623.1U Expired - Fee Related CN208021702U (en) | 2018-03-31 | 2018-03-31 | A kind of telescopic folding type anchoring platform |
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| CN (1) | CN208021702U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109110099A (en) * | 2018-03-31 | 2019-01-01 | 丹阳昊天飞行器技术有限公司 | A kind of telescopic folding type anchoring platform |
| 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 |
| CN113264175A (en) * | 2021-06-24 | 2021-08-17 | 中国科学院空天信息创新研究院 | Nose tower structure of anchoring facility for captive balloon |
| CN113277061A (en) * | 2021-05-14 | 2021-08-20 | 中国科学院空天信息创新研究院 | Mooring tower and mooring equipment |
-
2018
- 2018-03-31 CN CN201820444623.1U patent/CN208021702U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109110099A (en) * | 2018-03-31 | 2019-01-01 | 丹阳昊天飞行器技术有限公司 | A kind of telescopic folding type anchoring platform |
| 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 |
| CN113277061A (en) * | 2021-05-14 | 2021-08-20 | 中国科学院空天信息创新研究院 | Mooring tower and mooring equipment |
| CN113264175A (en) * | 2021-06-24 | 2021-08-17 | 中国科学院空天信息创新研究院 | Nose tower structure of anchoring facility for captive balloon |
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