CN109110099A - A kind of telescopic folding type anchoring platform - Google Patents
A kind of telescopic folding type anchoring platform Download PDFInfo
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- CN109110099A CN109110099A CN201810277138.4A CN201810277138A CN109110099A CN 109110099 A CN109110099 A CN 109110099A CN 201810277138 A CN201810277138 A CN 201810277138A CN 109110099 A CN109110099 A CN 109110099A
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- chassis
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- 238000004873 anchoring Methods 0.000 title claims abstract description 75
- 238000009434 installation Methods 0.000 abstract description 6
- 230000008901 benefit Effects 0.000 abstract description 5
- 238000004064 recycling Methods 0.000 abstract description 3
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- 238000000034 method Methods 0.000 description 20
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- 238000010586 diagram Methods 0.000 description 19
- 230000008569 process Effects 0.000 description 18
- 240000008042 Zea mays Species 0.000 description 9
- 235000005824 Zea mays ssp. parviglumis Nutrition 0.000 description 9
- 235000002017 Zea mays subsp mays Nutrition 0.000 description 9
- 235000005822 corn Nutrition 0.000 description 9
- 230000003014 reinforcing effect Effects 0.000 description 7
- 238000003466 welding Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 4
- 239000001307 helium Substances 0.000 description 4
- 229910052734 helium Inorganic materials 0.000 description 4
- 238000012423 maintenance Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- 238000007667 floating Methods 0.000 description 3
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 3
- 238000012544 monitoring process Methods 0.000 description 3
- 239000003351 stiffener Substances 0.000 description 3
- 238000004804 winding Methods 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000004891 communication Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000007257 malfunction Effects 0.000 description 2
- 238000003860 storage Methods 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 241000233855 Orchidaceae Species 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
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- 230000008030 elimination Effects 0.000 description 1
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- 230000037431 insertion Effects 0.000 description 1
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- 230000002045 lasting effect Effects 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/66—Mooring attachments
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The invention belongs to kite balloon airship fields, are related to a kind of telescopic folding type kite balloon airship anchoring platform comprising chassis, revolving support, revolving platform fold arm, mooring mast, hoist system and control cabinet.Wherein support and automatic loading and unloading, the revolving platform of the chassis installation Telescopic rotary hydraulic leg for the platform that entirely anchors is connected with chassis by revolving support, can be rotated around the centre of gyration, and revolving platform can be flexible along platform truck length direction.Advantage of the invention is that compact-sized, mobility is good, can carry the anchoring, lift-off, resident and recycling demand of 500-3000 meters of different size kite balloon airships, stability, safety and economy with higher.
Description
Technical field
The invention belongs to kite balloon airship fields, are related to a kind of telescopic folding type kite balloon airship anchoring platform, especially a kind of
Based on the big frame that stretches, arm, telescopic outrigger are folded in the kite balloon airship anchoring platform of one.
Background technique
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, consume energy low for a long time, 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 general character platform required for 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, and maintenance is simple, 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 high altitude operation.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 the days such as replacement 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 and the earth are fixedly mounted, 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 for the advantage that both have anchoring platform.
Summary of the invention
In order to meet the needs of this field is for novel kite balloon airship anchoring platform, the present invention is specifically proposed.
It is compact-sized the present invention provides a kind of telescopic folding type anchoring platform, it is more efficient.
One aspect of the present invention provides a kind of telescopic folding type anchoring platform comprising chassis, the revolution being set on chassis
The revolving platform support, being set on revolving support and the folding arm being set on revolving platform, mooring mast, hoist system and
Control cabinet.
In one aspect of the invention, the chassis includes chassis skeleton, positioned at stretching for four endpoints of the chassis skeleton
Contracting formula hydroboom and main supporting leg and rotary type hydraulic auxiliary leg positioned at the hydroboom outer end.The chassis skeleton is excellent
It is selected as rectangle, four telescopic hydraulic support arms including being located at four endpoints of rectangle, the support arm can be stretched at work
Out except the skeleton of chassis, when anchoring platform storage within retraction chassis skeleton.
In one aspect of the invention, the revolving support is driven by the hydraulic motor being set on revolving platform.
In one aspect of the invention, the revolving platform includes revolution fixed platform, and stretch big frame and scaling platform；Institute
It states revolution fixed platform to connect with the revolving support, can be rotated by the revolving support relative to the chassis；It is described
Scaling platform is overhanging relative to the revolution fixed platform by the big frame that stretches and shrinks.
In one aspect of the invention, installing and dismounting formula dirigible bracket on the big frame that stretches.
In one aspect of the invention, guardrail is installed in the revolution fixed platform.
In one aspect of the invention, the opposite sides for folding arm and being mounted on the scaling platform, the i.e. left and right sides,
And including 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 one aspect of the invention, the mooring mast includes mooring mast body frame, nose cone, and lifting motor is tethered at tower base,
Head drawstring hoist engine and tower drag, the mooring mast body frame and to be tethered at tower base hinged, realized by the lifting motor described in
The folding of mooring mast body frame, the head drawstring hoist engine are located at described be tethered in tower base.
In one aspect of the invention, the hoist system includes main winch, head pulley and drag-line, the master winch
The drag-line that machine folding and unfolding is oriented to through the head pulley, the drag-line other end connect kite balloon airship.
In one aspect of the invention, the mooring mast and the head pulley are respectively arranged in the opposite of the revolving platform
Two sides, i.e. front and rear sides, the main winch is close to the mooring mast.
In aforementioned aspect of the present invention, by scaling platform, arm is folded, the expansion of mooring mast and hydroboom can be with
Meet anchoring platform middle-size and small-size kite balloon airship anchoring let fly away and removal process in requirement, while by above-mentioned component
It shrinks and folds, anchoring platform can be made to meet the requirement of vehicle-mounted transport size, convenient for containerzation transport dispensing.
Another aspect of the present invention provides a kind of specific nose cone, and the nose cone includes inward turning unlocking type nose cone lock, and being used for will
The nose cone of kite balloon airship locks.
The nose cone is locked
With the bell-mouthed Cavity unit of cavity,
It is mounted on n lock bolt unit of the cavity horn mouth exterior, each lock bolt unit has insertion cavity
The closing piece of horn mouth through-hole and the pressure 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 guidance of cavity, opens the closing piece, described
Closing piece is sprung back under the pressure of pressure spring, locks nose cone,
During nose cone release, inward turning unlocking unit rotation, the unlock side wall of through-hole opens the closing piece, discharges nose cone.
In one aspect of the invention, n is the natural number of 2-4, and the n lock bolt unit is uniformly mounted on the cavity loudspeaker
The position of mouth neck portion outer surface, the n through-hole and the lock bolt unit is corresponding.
In one aspect of the invention, n=3.
In one aspect of the invention, the closing piece has inclined-plane and/or pulley towards cavity iiared port direction,
The process that the inclined-plane or pulley are intended to that nose cone is made to open closing piece is more smooth and smooth.
In one aspect of the invention, the closing piece has inclined-plane and/or pulley towards the unlock side wall, described oblique
The process that face or pulley are intended to that unlock side wall is made to open closing piece is more smooth and smooth.
In one aspect of the invention, inward turning unlocking type nose cone lock further includes driving unit, and the driving unit drives institute
The rotation of inward turning unlocking unit is stated, therefore the release process of nose cone without carrying out manually.
In one aspect of the invention, the driving unit drives the inward turning unlocking unit rotation by stepper motor motor
Turn, therefore inward turning unlocking unit does not make 360 ° of rotations, but is rotated back and forth during the latching of nose cone and release.
In one aspect of the invention, the Cavity unit and the opposite one end of the cavity horn mouth have cavity method
Orchid is fixed in mounting base.
In one aspect of the invention, 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, the band plug rod that the other end is equipped with and main shaft is vertical,
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, shallow grooves are embedded in after rotation,
Then closing piece leaves the lockhole of nose cone, and nose cone can freely discharge.
In one aspect of the invention, the pressure spring both ends are contacted with the bottom of the closing piece and the sliding chamber lid respectively,
And around a part of the lock pin.
Another aspect of the present invention provides a kind of specific kite balloon airship comprising a kind of high intensity nose cone attachment device.Institute
It states kite balloon airship and anchoring platform collocation of the invention uses, in other words, anchoring platform of the invention can further comprise herein
The kite balloon airship.
The high intensity nose cone attachment device includes kayak body covering and is successively welded thereon and adds for circular first
The nose skin of Qiang Bu, the second reinforcement cloth and round shape,
The first reinforcement cloth and the second reinforcement cloth respectively have 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 one aspect of the invention, the internal radius of the first reinforcement cloth, the second reinforcement cloth and kayak body covering is basic
It is identical.It is of the present invention " essentially identical ", refer to numerical value difference within 1%.In the case, first reinforces cloth and the
Two reinforce the inner ring contact of the junction and kayak body covering between the respective ring part of cloth and marginal portion, kayak body covering it is interior
Ring reinforces cloth and second to first and reinforces the ring part formation constraint of cloth.
In one aspect of the invention, the second reinforcement cloth, the annulus outer diameter of the first reinforcement cloth and the circle of nose skin
Outer diameter is incremented by successively.
In one aspect of the invention, the nose skin is circle, has a diameter larger than described first and reinforces cloth and second
Reinforce the annulus outer diameter of cloth.
In one aspect of the invention, the internal diameter of the kayak body covering is less than the diameter of nose skin.
In one aspect of the invention, the Edge Enhancement item has V-arrangement cross section, and the both arms of V-arrangement add with first respectively
The edge of the edge of strong cloth and the second reinforcement cloth welds together.
In one aspect of the invention, the edge and the Edge Enhancement item of the first reinforcement cloth and the second reinforcement cloth
With multiple connecting holes.
In one aspect of the invention, the connecting hole installs corn button.
In one aspect of the invention, the nose cone attachment device further includes being welded on the first reinforcement cloth and second to add
Third among strong cloth reinforces cloth the even further 4th and reinforces cloth.It is described third and fourth reinforce cloth structure and effect and
Described first, which reinforces cloth and second, reinforces the similar of cloth.
In one aspect of the invention, the described first internal radius for reinforcing cloth is 900-1100mm, and internal-and external diameter difference is
100-300mm, the described first width for reinforcing the edge of cloth is 50-100mm.
In one aspect of the invention, the described second internal radius for reinforcing cloth is 900-1100mm, and internal-and external diameter difference is 80-
200mm, the described second width for reinforcing the edge of cloth is 50-100mm.
It is worth noting that circle described in aforementioned aspect of the present invention or annulus refer both to that kite balloon airship head can be bonded
The circle or annulus of shape.More precisely, a part of circular surface or ellipse of round substantially sphere of the present invention
A part of surface at the top of sphere, the side of annulus of the present invention substantially rotary table or intercept at the top of the spheroid one
Partial circle shape surface.In three-dimensional system of coordinate, using the plane where round or annulus periphery as x/y plane, then round or circle
The center of circle of ring is not on x/y plane.Or in simple terms, round or annulus the center of circle and periphery are non-coplanar.
Another aspect of the present invention provides a kind of kite balloon airship emergency draw off gear, the device optionally can be set to anchoring vehicle
On, for example be set on the revolving platform of anchoring vehicle, cope 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
To after pulley guiding, it is wound on the undinding and rewinding drum with the direction basically perpendicular to the axis, or by opposite trend
Unwinding.
In one aspect of the invention, the turning unit includes the first driving motor and driving gear, the sliding tooth
Wheel engages the gear of the outer ring of the pivoting support, and the first driving motor driving turning unit turns around the axis of undinding and rewinding drum
It is dynamic, realize winding or the unwinding of tether cable.
In one aspect of the invention, the tether cable is through the wire guide pulley wheels A, wire guide pulley wheels B and Universal pulley
Guiding is respectively substantially 90 ° of angles.
Term " substantially " of the present invention refer to deviation existing for numerical value or geometrical relationship in ± 10% range,
Such as " substantially 90 ° of angles " described herein refer to the angle within the scope of 81-99 °.
In one aspect of the invention, the turning unit has tower structure, is in rectangular shape.
In one aspect of the invention, the turning unit specifically include rotary rack, wire guide pulley wheels A, wire guide pulley wheels B,
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, preferably guides tether cable for basic water by substantially vertical
Square to；
The wire guide pulley wheels B is installed on by proximal edges side at the top of rotary rack, preferably by tether cable by basic horizontal
Direction guidance 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 one aspect of the invention, the kite balloon airship draw off gear further includes support frame, under the undinding and rewinding drum
Support frame as described above is fixed at end, therefore during the folding and unfolding of tether cable, undinding and rewinding drum does not rotate relative to support frame,
But turning unit rotates.
In one aspect of the invention, support frame as described above is removable is fixed on anchoring vehicle, and in other words, of the invention is tethered at
Dirigible draw off gear can be used as emergency set and temporarily use.Certainly kite balloon airship draw off gear of the invention can also be according to reality
Demand is permanently secured on anchoring vehicle.
In one aspect of the invention, the kite balloon airship draw off gear further includes row's cable unit, row's cable unit packet
Include Universal pulley, pulley bracket, row's cable screw rod, conducting wire polished rod and the second driving motor；
The Universal pulley connects pulley bracket, preferably guides tether cable for basic horizontal side by substantially vertical
To；
The conducting wire polished rod and row's cable screw rod are parallel to the axis installation, the guide rail as the pulley bracket；
Second driving motor drives row's cable screw rod for the cable screw rod rotation of the row of driving, by motor positive and inverse, makes to slide
Wheel support is moved axially along the axis.
Compared to the prior art, advantage technology effect of the invention includes following one or more:
1. the present invention is non-wheeled motor anchoring platform compared with tradition anchors platform, it is public to solve tradition anchoring platform
The problem of road transport defeated superelevation, by the reasonable Arrangement of Optimal Structure Designing and load, so that anchoring platform truck overall structure is simple
Reliably, manufacturing cost is reduced；
2. using scaling platform structure, the length of anchoring platform can adjust, realize that a vehicle is multi-purpose, complete Multiple Type and be tethered at
The anchoring of dirigible is let fly away and is recycled, and the anchoring, lift-off, resident and recycling that can carry 500-3000 meters of different size kite balloon airships 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.
Detailed description of the invention
Invention is further described in detail with reference to the accompanying drawings and detailed description.
Fig. 1 shows the schematic diagram of the anchoring of the embodiment of the present invention 1 platform in a folded configuration；
Fig. 2 indicates schematic diagram of the anchoring platform of the embodiment of the present invention 1 under entrucking state；
Fig. 3 indicates schematic diagram of the anchoring platform of the embodiment of the present invention 1 in transport process；
Fig. 4 indicates the schematic diagram of the anchoring platform anchoring kite balloon airship of the embodiment of the present invention 1；
Fig. 5 indicates the top view (not showing kite balloon airship) of Fig. 4；
Fig. 6 indicates the schematic diagram under kite balloon airship lift-off state of the present invention；
The stereoscopic schematic diagram of Fig. 7 expression 2 nose cone lock construction of the embodiment of the present invention；
Fig. 8 shows the diagrammatic cross-sections of 2 nose cone lock construction of the embodiment of the present invention；
Fig. 9 indicates the structural schematic diagram of 2 nose cone of embodiment of the present invention lock Cavity unit；
Figure 10 indicates the structural schematic diagram of 2 nose cone of embodiment of the present invention lock inward turning unlocking unit；
Figure 11 indicates the structural schematic diagram of 2 nose cone of embodiment of the present invention lock lock bolt unit；
Figure 12 indicates the structural schematic diagram of 2 nose cone of embodiment of the present invention lock driving unit；
The local axonometric drawing of Figure 13 expression 3 nose cone attachment device of the embodiment of the present invention；
The partial front elevation view of Figure 14 expression 3 nose cone attachment device of the embodiment of the present invention；
The Structure explosion diagram of Figure 15 expression 3 nose cone attachment device of the embodiment of the present invention；
The axonometric drawing of Figure 16 expression 3 nose cone of the embodiment of the present invention；
Figure 17 indicates the scheme of installation of 3 nose cone of the embodiment of the present invention and nose cone attachment device；
Figure 18 indicates the pre- take-up status diagram of the emergency draw off gear of the embodiment of the present invention 4；
Figure 19 indicates the folding and unfolding status diagram of the emergency draw off gear of the embodiment of the present invention 4；
Figure 20 indicates the turning unit schematic diagram of the emergency draw off gear of the embodiment of the present invention 4；
Figure 21 indicates row's cable cell schematics of the emergency draw off gear of the embodiment of the present invention 4；
Figure 22 indicates the using effect schematic diagram of the emergency draw off gear of the embodiment of the present invention 4.
In figure:
1- anchoring platform,
The chassis 2-, 4- revolving platform, 5- fold arm, 6- mooring mast, 7- hoist system；
The chassis 20- skeleton, the main supporting leg of 21-, the hydraulic auxiliary leg of 22-, 23- hydroboom；
30- revolving support, 31- hydraulic motor, 32- electric slip ring；
40- turns round fixed platform, and 41- stretches big frame, 42- scaling platform, 43- guardrail, 44- dirigible bracket；
50- folding arm, 51- hydraulic cylinder, 52- assist hoist engine, 53- hanging basket；
60- mooring mast body frame, 61- nose cone, 62- lifting motor, 63- are tethered at tower base, the head 64- drawstring hoist engine, 65-
Tower drags；
70- main winch, 71- head pulley, 72- drag-line；
80- control cabinet, 81- station；
90- dirigible utricule, 100- flat car, 101- helium tank, 102- supply vehicle；
501- Cavity unit, 5011- cavity flange, 5012- cavity horn mouth, 50121- cavity horn mouth through-hole；
502- inward turning unlocking unit, 5021- rotation unlock piece, 5022- driven gear, the first deep groove ball bearing of 5023-,
5024- plane needle roller thrust bearing, the second deep groove ball bearing of 5025-, 5026- tapered roller bearing, 50211- through-hole, 50212-
Unlock side wall；
The sliding chamber of the sliding chamber lid of 503- lock bolt unit, 5031-, 5032- lock pin, 5033- pressure spring, 5034- closing piece, 5035- closing piece,
5036- band plug rod, the inclined-plane 50351-, 50352- pulley；
505- driving unit, 5051- drive gear, 5052- motor mount, 5053- stepper motor motor；
504- mounting base, 506- leading block unit；
91- kayak body covering, 92- nose skin, 93- first reinforce cloth, and 94- second reinforces cloth, 95- Edge Enhancement item, 96-
Corn button, 97- rope, 98- nose cone, 980- connection annulus, 981- bearing diagonal rod piece, 982- adapter flange；
461- undinding and rewinding drum, 462- support frame, 463- turning unit, 464- pivoting support, 465- arrange cable unit, 466- system
Stay hawser；
4631- rotary rack, the first driving motor of 4632- wire guide pulley wheels A, 4633- wire guide pulley wheels B, 4634-, 4635- drive
Moving gear, 4636- transverse slat；
4651- Universal pulley, 4652- pulley bracket, 4653- row's cable screw rod, 4654- conducting wire polished rod, 4655- are removable
Frame, the second driving motor of 4656-.
Specific embodiment
Below by specific embodiment combination attached drawing, invention is further explained, and described preferred embodiment is only
For instruction and explanation of the present invention, it is not intended to limit the present invention.
Embodiment 1
The embodiment of the present invention 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 top 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, control cabinet 80.
Chassis 2 includes chassis skeleton 20, main supporting leg 21, hydraulic auxiliary leg 22 and hydroboom 23.
Chassis skeleton 20 is welded by two crossbeams and more stringers, is connect by revolving support 30 with revolving platform 4,
It is used to support the rotation of entire anchoring platform.
Chassis 2 is landed by main supporting leg 21 and 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 auxiliary leg 22 realize anchoring by flexible and hydraulic 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 auxiliary leg 22 is packed up.Drop
Low anchoring platform center of gravity improves anti-overturning energy.Anchoring platform 1 is improved using the span that hydroboom 23 increases main supporting leg 21
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
Bracket 44.It turns round fixed platform 40 and revolving support 30 is connected, 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 has mechanical lock, on the big frame 41 of hydraulically extensible
Detachable dirigible bracket 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, complete unfolded movement by hydraulic cylinder；Outer end is equipped with auxiliary hoist engine
52 operate hanging basket 53 with detachable, and dirigible two 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 to fix 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 control cabinet 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 hydraulic rotations of auxiliary leg 22 to vertical position and are locked, start hydraulic 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 auxiliary leg 22 starts
It shrinks, anchoring platform 1 is placed on flat car 100, rotating hydraulic auxiliary leg 22 to horizontal position simultaneously locks, and by four
Hydroboom 23 is withdrawn, i.e. completion entrucking process, as shown in Figure 2.
Four hydrobooms 23 are protruded horizontally up to designated position outward during unloading, and by four hydraulic auxiliary legs 22
Rotation is to vertical position and locks, and starts hydraulic auxiliary leg 22 for anchoring platform and is raised to 1.4 meters, main supporting leg 21 is mounted on
23 end of hydroboom, hydraulic auxiliary leg 22 starts to shrink 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 placed in 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 bracket 44,
Guardrail 43, station 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 active length for effectively 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, the stress of real-time monitoring drag-line 72 have the function of overload-alarm.Rope speed is adjustable out for main winch 70, 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, rises dirigible utricule slowly, 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 precision.
The control system integration of anchoring platform 1 is operated by operator on operating platform 81 in control cabinet 80,
81 fast demountable of operating platform.
Embodiment 2
The embodiment of the present invention 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, 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 band flange sides.The lesser 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, tapered roller 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 along 501 axis of Cavity unit from horn mouth 5012, 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 rotation 5021 open end of unlock piece, 5026 outer ring of tapered roller bearing and the circle of cavity flange 5011
Connected in star cooperation.5022 side of driven gear, which has, makes to rotate the groove that unlock piece 5021 is embedded in, and driven gear 5022 is recessed
Plane outside slot preferentially resists 5026 inner ring of tapered roller 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 setting on unlock piece 5021, wherein one end side wall structure of through-hole 50211 are rotated
At unlock side wall 50212.Unlocking side wall 50212 is also inclined-plane, 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, pressure spring 5033, the sliding chamber of closing piece
5034, closing piece 5035.The sliding chamber 5034 of the closing piece passes through the outer surface of 5012 neck of screw connection cavity horn mouth, such as Fig. 7 institute
Show.There are one group of cross recesses, respectively two deep grooves and two shallow grooves at the top of the sliding chamber lid 5031.Sliding 5031 bottom of chamber lid
Portion connects the sliding chamber 5034 of closing piece.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 sliding 5031 upper end of chamber lid is sticked into, pressure 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
It is more smoothly that closing piece 5035 is opened when 5012.Pulley 50352 is intended to make to unlock side wall 50212 and opens the process of closing piece 5035 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
50351 open the closing piece 5035 of lock bolt unit 503, and closing piece 5035 enters the sliding chamber 5034 of closing piece, and pressure spring 5033 is compressed；Until head
Wimble fraction completely into, then inclined-plane 50351 be detached from nose cone, pressure 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 with it, and inward turning unlocking unit 502 is driven to rotate, and in the process, unlocks side wall 50212
The closing piece 5035 of lock bolt unit 503 is opened by pulley 50352, pressure 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, pressure 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；Rotation band plug rod 5036 at this time is discharged after it is gone to scrobicula groove location from the deep groove position of sliding chamber lid 5031, is then locked
The slightly downlink under the elastic force effect of pressure 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 embodiment of the present invention 2 is, is locked by electric-controlled mechanical, it can be achieved that personnel are whole
Operation is completed on the ground, ensure that personnel safety, and easy to operate.Under special circumstances, it can also be discharged by manual mode
Nose cone.
Embodiment 3
The embodiment of the present invention 3 provides the kite balloon airship that a kind of and embodiment 1 anchoring vehicle collocation uses, the kite balloon airship
Feature is there is a kind of high-intensitive nose cone attachment device.
Specifically, high-intensitive 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
Reinforcing cloth 94 is annular shape, 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 of body covering 91 reinforces cloth 93 and second to first and reinforces the ring part formation constraint of cloth 94.It if necessary, can be in ship
The inner ring of body covering 91 adds a reinforcing ring, wales the ring part of two reinforcement cloth and the junction of marginal portion.
Therefore inner ring that the marginal portion of two reinforcement cloth passes through kayak body covering 91 is exposed, and welds with Edge Enhancement item 95
It connects.Welding back edge stiffener 95 is in " V "-shape, and in the two-arm aperture of " V " character form structure, installs corn button 96, rope 97
Nose cone 98 is fixed by corn button.
After entire kite balloon airship is completed, circle is sealed on the head that above-mentioned nose skin 92 constitutes dirigible.
More specifically, as shown in figs. 13 and 14, first, which reinforces cloth 93 and second, reinforces the ring part overlapping welding of 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 in " V "-shape, edge
Stiffener 95 can effectively prevent the welding position of the first reinforcement cloth 93 and the second reinforcement cloth 94 in use process to be torn, simultaneously
Also improve the intensity of corn button installation site." V " font two-arm has the connection that the uniformly distributed diameter of annular is 6mm
Hole or mounting hole, pitch of holes 100mm, mounting hole are located on the middle 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, the width of annular section, are 120mm, and the width for the marginal portion welded with Edge Enhancement item 95 is 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, the width of annular section, are 100mm, and the width for the 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 the welding glue-line with kayak body covering 91.
Above-mentioned apparatus bearing capacity is strong, designability is good, the feature for having maintenance simple, convenient for disassembly and assembly.
Embodiment 4
The embodiment of the present invention 4 provides a kind of kite balloon airship emergency draw off gear for the vehicle that anchors, and specifically includes retractable volume
Cylinder 461, support frame 462, turning unit 463, pivoting support 464 and row's cable unit 465 and matching used tether cable
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 can be rotated, and the other end, that is, upper end connection pivoting support 464 outer ring, outer ring is equipped with gear；The revolution
The inner ring of the connection pivoting support 464 of unit 463；Row's cable unit 465 connects turning unit 463.
As shown in figs 20 and 21, it arranges cable unit 465 and turning unit 463 is stitched together and forms a cuboid frame later
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, not mutually 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.One piece of transverse slat is welded 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, engage with the gear of 464 outer ring of pivoting support, thus
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 cable screw rod 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 screw rod 4653 are parallel to
The axis of undinding and rewinding drum 461, be installed on it is removable shelve between 4,655 two beams, 4652 both ends of pulley bracket are pierced into respectively
Conducting wire polished rod 4654 and row's cable screw rod 4653 are simultaneously slided using them as guide rail.Second driving motor 4656 is for the row of driving
Cable screw rod 4653 rotates, and drives row's cable screw rod 4652 by motor positive and inverse, moves axially pulley bracket 4652 along screw rod, real
Now arrange cable.
When take-up, entire emergency 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 successively limited to wire guide pulley wheels A 4632, wire guide pulley wheels B 4633 and universal cunning
In the rope groove 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 rolling 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 cable unit of the row of drive
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
Reel axial direction equidistantly arranged, 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 distinguish about 90 ° of dog-ear, is left entire along the vertical direction through Universal pulley 4651
Emergency 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.
Emergency 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, guarantee going on smoothly for kite balloon airship task；In addition, can not broken by the device
It is bad, do not change be fixed on retractable equipment end tether cable connection in the case where carry out kite balloon airship folding and unfolding, will not twist with
The tether cable of retractable equipment end connection；The device avoids take maintenance Replacing Scheme bring result uncertainty,
Avoid the safety problem of economic loss and personnel brought 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 anchors 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
It stays tower (6), hoist system (7) and control cabinet (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
It states the telescopic hydraulic support arm (23) of (20) four endpoints of chassis skeleton and is located at the main supporting leg of 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 by the revolving support (30) relative to the chassis (2)；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 the installing and dismounting formula dirigible branch on big frame (41) of stretching
Guardrail (43) are 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 including 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) hingedly and by the hydraulic cylinder (51) 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),
It the mooring mast body frame (60) and is tethered at tower base (63) hingedly, passes through the lifting motor (62) and realize 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 |
|---|---|---|---|
| CN201810277138.4A CN109110099A (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 |
|---|---|---|---|
| CN201810277138.4A CN109110099A (en) | 2018-03-31 | 2018-03-31 | A kind of telescopic folding type anchoring platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109110099A true CN109110099A (en) | 2019-01-01 |
Family
ID=64821820
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810277138.4A Pending CN109110099A (en) | 2018-03-31 | 2018-03-31 | A kind of telescopic folding type anchoring platform |
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| CN (1) | CN109110099A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111746777A (en) * | 2020-06-01 | 2020-10-09 | 中国科学院空天信息创新研究院 | Collapsible hidden captive balloon holds in palm ball device |
| CN112660357A (en) * | 2020-12-30 | 2021-04-16 | 中国特种飞行器研究所 | Container-type captive balloon anchoring platform |
| CN112678140A (en) * | 2020-12-30 | 2021-04-20 | 中国特种飞行器研究所 | Split type captive balloon ground anchoring system |
| CN113247230A (en) * | 2021-06-24 | 2021-08-13 | 中国科学院空天信息创新研究院 | Mobile anchoring facility for captive balloon |
| CN115258125A (en) * | 2022-08-22 | 2022-11-01 | 山东泰开重工机械有限公司 | Mooring vehicle device for mooring airship and using method |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN206841700U (en) * | 2017-03-28 | 2018-01-05 | 东莞前沿技术研究院 | Captive balloon anchoring and mooring system and mooring system |
| CN208021702U (en) * | 2018-03-31 | 2018-10-30 | 丹阳昊天飞行器技术有限公司 | A kind of telescopic folding type anchoring platform |
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Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN206841700U (en) * | 2017-03-28 | 2018-01-05 | 东莞前沿技术研究院 | Captive balloon anchoring and mooring system and mooring system |
| CN208021702U (en) * | 2018-03-31 | 2018-10-30 | 丹阳昊天飞行器技术有限公司 | A kind of telescopic folding type anchoring platform |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111746777A (en) * | 2020-06-01 | 2020-10-09 | 中国科学院空天信息创新研究院 | Collapsible hidden captive balloon holds in palm ball device |
| CN112660357A (en) * | 2020-12-30 | 2021-04-16 | 中国特种飞行器研究所 | Container-type captive balloon anchoring platform |
| CN112678140A (en) * | 2020-12-30 | 2021-04-20 | 中国特种飞行器研究所 | Split type captive balloon ground anchoring system |
| 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 |
| CN113247230A (en) * | 2021-06-24 | 2021-08-13 | 中国科学院空天信息创新研究院 | Mobile anchoring facility for captive balloon |
| CN115258125A (en) * | 2022-08-22 | 2022-11-01 | 山东泰开重工机械有限公司 | Mooring vehicle device for mooring airship and using method |
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