CN208360510U - A kind of movable unmanned helicopter high-altitude reclaimer - Google Patents
A kind of movable unmanned helicopter high-altitude reclaimer Download PDFInfo
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- CN208360510U CN208360510U CN201820774466.0U CN201820774466U CN208360510U CN 208360510 U CN208360510 U CN 208360510U CN 201820774466 U CN201820774466 U CN 201820774466U CN 208360510 U CN208360510 U CN 208360510U
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Abstract
The utility model relates to movable unmanned helicopter high-altitude reclaimers, open the first telescopic arm, the second telescopic arm and lower cross arm, after the completion of hawser passes around, in the U-shaped opening for the side opening for ensuring to be made of the boom system and wiring, without any other barrier, flown in the space of wiring two sides for unmanned plane.And equipment stability integrates vehicle carrying by this in institute strong and torque and the perpendicular that aircraft generates when recycling.Foldable lower cross arm and foldable upper cantilever crane are able to achieve wide-angle and large-scale luffing and stretching, extension, equipment adjustability and adaptable, and have the characteristics that integration degree is high, mobility strong, work efficiency is high, by full-automation manipulation, electro-hydraulic jointly control, it is able to achieve the motor-driven recycling of full automatic high efficiency of unmanned plane, either can play good recyclability on the recovery test of unmanned plane or formal recyclable device.
Description
Technical field
The utility model belongs to unmanned plane reclaimer technical field, sets more particularly to the recycling of movable unmanned helicopter high-altitude
It is standby.
Background technique
Unmanned plane recovery technology is always priority fields of study, with Industrial Economic Development and unmanned air vehicle technique progress with
And unmanned plane commercial applications, so that the equipment about unmanned plane recycling is more concerned.It recycles about unmanned plane there are many mode,
A kind of currently popular recycling is exactly the straight recycling of hawser weight, but there are no auxiliary facilities for the fixed equipment of hawser.It is existing to set
After opening, reserved space is small for its standby jib fold mechanism, and bearing capacity is small (general only carrying 30kg or less unmanned plane).Separately
Outside, it need to separately match transport vehicle about reclaimer, transmitting equipment, control equipment etc., be to need two to four vehicles on, equipment connects
Connect, factory site transfer etc. low efficiencys, fault point is more after connection.Based on these unfavorable factors, the purpose of this patent is to provide a kind of collection
Unmanned plane emits, recycles, being controlled in integrated integrated vehicle.Meanwhile the bearing capacity of unmanned plane recycling and rank being improved to 75kg.
Equipment, reclaimer and control integration of equipments will be emitted on a vehicle, for improving efficiency.
Utility model content
To solve the above-mentioned problems, the purpose of this utility model is to provide a kind of collection unmanned planes to emit, recycles, is controlled in
The movable unmanned helicopter high-altitude reclaimer of one, mobility strong, the wide-angle for being able to achieve unmanned plane recycling hawser are adjustable
Deployment, the impulse force and torque generated when recycling unmanned plane are born by the equipment, and the full automatic high efficiency for being able to achieve unmanned plane is motor-driven
Recycling.
To achieve the goals above, technical solution adopted in the utility model is:
Movable unmanned helicopter high-altitude reclaimer, including automobile chassis, automobile chassis is equipped with swing mechanism assembly, described
Swing mechanism assembly includes turntable, and the turntable lower end and upper end have been respectively articulated with foldable lower cross arm and foldable upper cantilever crane,
The foldable lower cross arm includes that next joint arm, lower two joint arms and lower jib lubbing mechanism, one end of next joint arm are hinged on institute
It states on turntable, the other end of next joint arm is connected by two opposite pins with lower two joint arms, when removing wherein
After one pin, lower two joint arms can be rotated by axis of another pin close to next joint arm and by described upper one
Withdrawal lock pin in the middle part of joint arm and upper two joint arm, which is realized, folds connection, the both ends of the lower jib lubbing mechanism respectively with it is described under
One joint arm is connected with the turntable；The foldable upper cantilever crane include the first telescopic arm, the second telescopic arm, the first jib lubbing mechanism and
Second jib lubbing mechanism, the arm tail of the first telescopic arm basic arm hingedly on the turntable, pacify by one end of the second jib lubbing mechanism
On the arm head of the first telescopic arm minor details arm, the other end of second jib lubbing mechanism and second telescopic arm are cut with scissors
It connects, the both ends of first jib lubbing mechanism are hinged with first telescopic arm and the turntable respectively, first jib lubbing mechanism
For driving first telescopic arm in vertical rotation in surface and adjusting the angle of first telescopic arm and horizontal plane, described
Two jib lubbing mechanisms for drive second telescopic arm vertical rotation in surface and adjust second telescopic arm and horizontal plane it
Between angle, the foldable lower cross arm and the foldable upper cantilever crane form the U-shaped opening of a side opening after being unfolded simultaneously；
The end of the minor details arm of first telescopic arm is also equipped with the arm head pulley blocks for hanging suspension hook, and turntable upper end is additionally provided with for driving
The hoisting mechanism of dynamic suspension hook movement.
First telescopic arm and second telescopic arm include multiple joint arms and for driving multiple joint arms sequence to stretch
Out or retract telescoping mechanism.
The telescoping mechanism includes oil cylinder.
Second jib lubbing mechanism is link mechanism, specifically includes pulling plate, support frame, tripod, Eagle-mouth type truss foundation frame, pushes away
Bar and amplitude oil cylinder, the head end of Eagle-mouth type truss foundation frame are mounted on the end of the first telescopic arm, Eagle-mouth type truss foundation frame
End is hinged with tripod and support frame respectively at different location, and one end of push rod is hinged in the second telescopic arm basic arm
Pulling plate is hinged between portion, the other end and tripod, the end of the second telescopic arm basic arm is hinged on Eagle-mouth type truss foundation frame
Olecranon end, support frame is hinged between pull rod and Eagle-mouth type truss foundation frame, and amplitude oil cylinder is hinged on another angle of tripod
Between the head end of Eagle-mouth type truss foundation frame；Amplitude oil cylinder, the first side of tripod, amplitude oil cylinder and Eagle-mouth type truss foundation frame
Hinge constitute a variable delta link to line between tripod and the hinge of Eagle-mouth type truss foundation frame；Triangle
Frame constitutes a fixed triangle shape connecting rod；Push rod, the second telescopic arm basic arm and Eagle-mouth type truss foundation frame hinge are to push rod
With the second telescopic arm basic arm hinge line, the second telescopic arm basic arm and Eagle-mouth type truss foundation frame hinge to support frame and hawk
Line, the support frame of mouth formula truss foundation frame arm head hinge constitute a quadrilateral connecting rod；Support frame, pulling plate, tripod
On one side, tripod and Eagle-mouth type truss foundation frame hinge are constituted to the line of support frame and Eagle-mouth type truss foundation frame arm head hinge
Another quadrilateral connecting rod.
First jib lubbing mechanism, second jib lubbing mechanism and the lower jib lubbing mechanism include oil cylinder.
The automobile chassis is universal chassis, is equipped with the vehicle frame for carrying operating mechanism on universal chassis, described turn
Platform is mounted on vehicle frame by pivoting support, and the two sides on the Universal automobile chassis are respectively equipped with telescopic outrigger.
The swing mechanism assembly further includes pivoting support, rotary motion mechanism and slewing limit mechanism, and the turntable is solid
On the pivoting support, the rotary motion mechanism is for driving the pivoting support to rotate.
The slewing limit mechanism includes left slewing limit part, right-hand rotation locating part, recycling state lockpin hole and traveling shape
State lockpin hole, left slewing limit part and right-hand rotation locating part are used to limit the revolution range of swing mechanism assembly, recycle status lock
It can guarantee that swing mechanism assembly will not be swung under unmanned plane recycling state after pin hole insertion lock pin, driving status lockpin hole insertion lock
It can guarantee that swing mechanism assembly will not be swung under vehicle driving status after pin.
It is equipped with unmanned plane transmitter and can from the inside to the outside in the swing mechanism assembly is ipsilateral on the Universal automobile chassis
Folding is walked on stage, and foldable walk on stage can stretch out expansion to operate the unmanned plane transmitter and retract and be folded so as to deposit
It puts.
It is described it is foldable walk on stage including walking platen and walking on stage guardrail, it is described walk platen pass through and walk on stage ear mount and the vehicle frame is cut with scissors
Connect, it is described walk on stage guardrail by railing cut with scissors ear with it is described walk platen it is hinged.
When in use, the first telescopic arm of opening, second stretch the movable unmanned helicopter high-altitude reclaimer of the utility model
Arm and lower cross arm, after the completion of hawser passes around, it is ensured that in the U-shaped opening for the side opening being made of the boom system and wiring, nothing
Any other barrier is flown in the space of wiring two sides for unmanned plane.And the strong and power of institute that aircraft generates when recycling
Equipment stability integrates vehicle carrying by this in square and perpendicular.Foldable lower cross arm and foldable upper cantilever crane can be real
Existing wide-angle and large-scale luffing and stretching, extension, equipment adjustability and adaptable, and have that integration degree is high, mobility
By force, the characteristics of work efficiency is high, by full-automation manipulation, it is electro-hydraulic jointly control, be able to achieve the full automatic high efficiency machine of unmanned plane
Dynamic recycling either can play good recyclability on the recovery test of unmanned plane or formal recyclable device.It hangs
The setting of hook and hoisting mechanism makes the movable unmanned helicopter high-altitude reclaimer of the utility model also have the function of to hang load.
Detailed description of the invention
Fig. 1 is the main view of the working condition of the movable unmanned helicopter high-altitude reclaimer of the utility model；
Fig. 2 is the top view of the working condition of the movable unmanned helicopter high-altitude reclaimer of the utility model；
Fig. 3 is under the complete retracted state of foldable cantilever crane of the movable unmanned helicopter high-altitude reclaimer of the utility model
Shaft side figure；
Fig. 4 is the enlarged diagram of the portion A structure in Fig. 2；
Fig. 5 is the structural schematic diagram of the swing mechanism assembly of the utility model；
Fig. 6 is the structural schematic diagram of second jib lubbing mechanism of the utility model；
Fig. 7 is the structural schematic diagram of the Eagle-mouth type truss foundation frame of the utility model；
Fig. 8 is the structure rough schematic view of Fig. 7；
Fig. 9 is the structural schematic diagram of the folding of the foldable lower cross arm of the utility model；
Figure 10 is the structural schematic diagram of the foldable folding walked on stage of the utility model.
Specific embodiment
In order to deepen the understanding to technical solutions of the utility model, the utility model is made below in conjunction with Figure of description
It is further described.
As Figure 1-10 shows, the utility model provides movable unmanned helicopter high-altitude reclaimer, including Universal automobile chassis
1, the vehicle frame for carrying operating mechanism is installed on universal chassis, it is total by pivoting support to be equipped with swing mechanism on vehicle frame
At 3, the lower end and upper end of swing mechanism assembly 3 are respectively arranged with foldable lower cross arm 4 and foldable upper cantilever crane 5, swing mechanism
The two sides of assembly 3 are respectively equipped with unmanned plane transmitter 6 and goods and materials case 7, and the front side of swing mechanism assembly 3 is equipped with comprehensively control case 8.
Vehicle includes horizontal support legs and vertical leg configured with supporting leg 2 all around, supporting leg 2, and horizontal support legs and vertical leg are liquid
Pressure driving, whole vehicle stability when for improving unmanned plane recycling.1 two sides of universal chassis are additionally provided with access step 10.
The outside of unmanned plane transmitter 6 be additionally provided with it is foldable walk on stage 9, foldable walk on stage 9 can stretch out expansion to facilitate behaviour
Make unmanned plane transmitter 6 and retract to be folded so as to store.Foldable walk on stage 9 includes walking platen 91 and walking on stage guardrail 92, is walked on stage
Plate 91 is hinged with vehicle frame by ear mount 93 of walking on stage, and guardrail 92 of walking on stage cuts with scissors ear 94 by railing and walks platen 91 hingedly.
Swing mechanism assembly 3 includes turntable 32, pivoting support 31, rotary motion mechanism 33 and slewing limit mechanism.Turntable
32 are fixedly arranged on pivoting support 31, and rotary motion mechanism 33 is for driving pivoting support 31 to rotate.Slewing limit mechanism includes a left side
Slewing limit part 34, right-hand rotation locating part 35, recycling state lockpin hole 36 and driving status lockpin hole 37, left slewing limit part 34
It is used to limit the revolution range of swing mechanism assembly 3 with right-hand rotation locating part 35.Recycling state lockpin hole 36 is inserted into energy after lock pin
Guarantee that swing mechanism assembly 3 will not be swung under recycling drone status, can guarantee after the insertion lock pin of driving status lockpin hole 37 whole
Swing mechanism assembly will not be swung under vehicle travelling state, guarantee the security performance of vehicle.
Different location has been respectively articulated with foldable lower cross arm 4 and foldable upper cantilever crane 5, foldable lower cross arm 4 on turntable 32
The U-shaped opening of horizontal opening is formed after being unfolded simultaneously with foldable upper cantilever crane 5, U-shaped opening is flown into for unmanned plane to realize
Recycling.Hawser specifically is worn between the U-shaped mouth of horizontal opening, is recycled for unmanned plane lanyard.
Foldable lower cross arm 4 includes next joint arm 41, lower two joint arms 42 and lower jib lubbing mechanism 43, one end of next joint arm 41
It is hinged on turntable 32, the other end of next joint arm 41 is connected by two opposite pins 44 and lower two joint arm 42, when removing
After one of pin, lower two joint arms 42 can be rotated with close next joint arm 41 as axis using another pin and pass through next joint arm
41 and lower two joint arm 42 in the middle part of the withdrawal lock pin 45 that is arranged is realized and folds connection, lower jib lubbing mechanism 43 includes oil cylinder, both ends point
It is not articulated and connected with next joint arm 41 and turntable 32.
Foldable upper cantilever crane 5 includes the first telescopic arm 51, the second telescopic arm 53, the first jib lubbing mechanism 52 and the second luffing machine
Structure 54.First telescopic arm 51 and the second telescopic arm 53 are including multiple joint arms and for driving multiple joint arms sequences to stretch out or retract
Telescoping mechanism 55, the first jib lubbing mechanism 52, the second jib lubbing mechanism 54 and telescoping mechanism 55 include oil cylinder.First telescopic arm 51
The arm tail of basic arm is hinged on turntable 32, and one end of the second jib lubbing mechanism 54 is mounted on the end of the first telescopic arm 51, and second
The other end of jib lubbing mechanism 54 and the second telescopic arm 53 are hinged, the both ends of the first jib lubbing mechanism 52 respectively with the first telescopic arm 51 and
Turntable 32 is hinged, and the first jib lubbing mechanism 52 is for driving the first telescopic arm 51 in vertical rotation in surface and adjusting the first telescopic arm 51
With the angle of horizontal plane, the second jib lubbing mechanism 54 is for driving the second telescopic arm 53 in vertical rotation in surface and to adjust second flexible
Angle between arm 53 and horizontal plane.
Since vehicle-mounted other devices etc. for unmanned plane transmitting need to move, it is therefore desirable to use and hang load function.Thus
The end of the minor details arm of first telescopic arm 51 is also equipped with the arm head pulley blocks 57 for hanging suspension hook 56, and 32 upper end of turntable is also set
There is the hoisting mechanism 11 for driving suspension hook 56 to move, when hanging load, as long as needed while opening Top Crossbeam 5, it will
Lower cross arm 4 is retracted into maximum angle completely, and under the control of integrated control cabinet 8, hoisting mechanism 11 can work, and load is hung in realization.
Second jib lubbing mechanism 54 is by pulling plate 541, support frame 542, tripod 543, Eagle-mouth type truss foundation frame 544, push rod
545 and amplitude oil cylinder 546 constitute, the head end of Eagle-mouth type truss foundation frame 544 is mounted on the end of the first telescopic arm 51, Eagle-mouth type
The end of truss foundation frame 544 is hinged with tripod 543 and support frame 542, one end hinge of push rod 545 respectively at different location
The middle part in the first joint arm of the second telescopic arm 53, hinged pulling plate 541 between the other end and tripod 543 are connect, the second telescopic arm 53 is first
The end of joint arm is hinged on the olecranon end of Eagle-mouth type truss foundation frame 544, and support frame 542 is hinged on pulling plate 541 and Eagle-mouth type purlin
Between frame foundation frame 544, amplitude oil cylinder 546 is hinged on another angle of tripod 543 and the head end of Eagle-mouth type truss foundation frame 544
Between.
It is the hinge axes of push rod 545 and pulling plate 541 in figure, at A, is the articulated shaft of tripod 543 and push rod 545 at B
Line, is the hinge axes of tripod 543 and Eagle-mouth type truss foundation frame 544 at C, is Eagle-mouth type truss foundation frame 544 and the at D
The hinge axes of the first joint arm of two telescopic arm 53, the place E are the hinge axes of tripod 543 and amplitude oil cylinder 546, are second to stretch at F
The hinge axes of contracting arm 53 first joint arm and push rod 545 are the articulated shaft of Eagle-mouth type truss foundation frame 544 and amplitude oil cylinder 546 at G
Line is the hinge axes of support frame 542 and Eagle-mouth type truss foundation frame 544 at H.
Second jib lubbing mechanism is multi-connecting-rod mechanism, specifically includes a variable delta link, a fixed triangle
Shape connecting rod, two variable quadrilateral connecting rods.One of them variable three side of delta link (triangle CGE) is respectively by luffing
Oil cylinder 546,543 first side of tripod, amplitude oil cylinder 546 and Eagle-mouth type truss foundation frame 544 hinge to tripod 543 and hawk
Line is constituted between the hinge of mouth formula truss foundation frame 544；Fixed triangle shape connecting rod (triangle BCE) is tripod；First
A variable quadrangle (quadrangle AHDF) first is the first joint arm of the second telescopic arm 53 and olecranon while for push rod 545(AF), second
544 hinge of formula truss foundation frame stretches to push rod 545 and the first joint arm hinge line (FD) of the second telescopic arm 53, third side for second
The first joint arm of arm 53 and 544 hinge of Eagle-mouth type truss foundation frame to support frame 542 and 544 arm head hinge of Eagle-mouth type truss foundation frame
Line (DH), the 4th side are support frame 542(AH)；Second variable the first side of quadrangle (quadrangle ABCH) is support frame 542
(AH), second be one side (BC), the 4th side of tripod 543 while for pulling plate 541(AB), third is tripod 543 and olecranon
Line (CH) of 544 hinge of formula truss foundation frame to support frame 542 and 544 arm head hinge of Eagle-mouth type truss foundation frame.
For foldable cantilever crane of the invention under retracted state, amplitude oil cylinder 546 is in stretches state entirely.Amplitude oil cylinder 546 is stretched
When out, tripod 543 is pushed to rotate at C, tripod 543 pushes the second telescopic arm 53 by pushing pulling plate 541, push rod 545
First joint arm rotates at D, and the linear movement of amplitude oil cylinder 546 is converted to the rotary motion of the first joint arm of the second telescopic arm 53.When
When shifting terminal onto, the second telescopic arm 53 is folded back on completely, parallel with the first telescopic arm 51.When amplitude oil cylinder 546 retracts, draw
Dynamic tripod 543 rotates at C, and tripod 543 pulls the second telescopic arm 53 around D by pulling pulling plate 541, push rod 545
Place's rotation.When amplitude oil cylinder 546 is retracted into terminal, 53 change angle of the second telescopic arm is maximum, reaches in the first telescopic arm 51
When maximum change angle, the second telescopic arm 53 is parallel to the horizontal plane.During no matter opening or withdrawing, support frame 542 is supported
In the hinged place of pulling plate 541 and push rod 545, can be rotated at H.
When foldable upper cantilever crane 5 is unfolded, if available space is limited at low latitude, can first be increased using the first jib lubbing mechanism 52
The angle of first telescopic arm 51 and horizontal plane, then each arm sequence stretching of the first telescopic arm 51 is controlled, second is controlled later becomes
Width mechanism 54 increases the angle between the second telescopic arm 53 and horizontal plane, and each arm sequence for finally controlling the second telescopic arm 53 is stretched
Out, that is, the full extension of foldable upper cantilever crane 5 is realized.The setting of second jib lubbing mechanism 54 reduces the foldable upper cantilever crane that stretches
Space required for 5 enables the utility model to realize the luffing of wide-angle in small space.The tool of second jib lubbing mechanism 54
The design of body structure keeps its intensity high, can safely and reliably realize the luffing of foldable upper cantilever crane 5, amplifies the change of the second telescopic arm 53
Argument degree.
The course of work of the utility model is: starting electrohydraulic control system operates supporting leg control valve group, opens supporting leg 2, branch
Vehicle is propped up, then switches electrohydraulic control system to the first jib lubbing mechanism 52,51 luffing of the first telescopic arm is driven to reach maximum angular
After degree, while after the foldable lower cross arm 4 of luffing has been allowed to width to proper angle, rotary motion mechanism 33 drives turntable 32 to turn round,
Device on driving turntable 32 is turned back to proper angle, and limits revolution range by slewing limit mechanism.
After being turned back to proper angle, the telescoping mechanism of switching electrohydraulic control system to the first telescopic arm 51, telescoping mechanism is driven
Each joint arm sequence of dynamic first telescopic arm 51 is stretched out, and switches electrohydraulic control system later to the second jib lubbing mechanism 54, amplitude oil cylinder
546 retract, and pull tripod 542, and tripod 542 drives pulling plate 541 and push rod 545, drive 53 luffing of the second telescopic arm, adjustment
To proper angle, then switches electrohydraulic control system to the telescoping mechanism of the second telescopic arm 53, push each of the second telescopic arm 53
Joint arm sequence is stretched out.
Foldable lower cross arm 4 falls width to horizontality, pulls up the receipts of a lower cross arm lower joint arm 41 and lower two joint arm 42 manually
Lock pin is returned, two joint arms 42 is can be manually rotated down to when next joint arm 41 and the docking of lower two joint arm 42, plugs pin, it is foldable in this way
Lower cross arm 4 fully opens, and switches electrohydraulic control system to lower jib lubbing mechanism, foldable lower cross arm 4 is made to fall width to proper angle.
So far, entire unmanned plane reclaimer has fully opened as needed, foldable lower cross arm 4 and foldable upper arm
Frame 5 forms U-shaped opening after being unfolded simultaneously, U-shaped opening flies into realize recycling for unmanned plane.Foldable lower cross arm 4 and can
Cantilever crane 5 is equipped with multiple hawser installation parts for arranging recycling hawser in folding, after recycling wireline deployed, passes through U-shaped
Opening is able to achieve the high-altitude recycling of unmanned plane.After the completion of recovery operation, complete equipment is withdrawn, withdraws process and above-mentioned expansion process
On the contrary, can be completed by electrohydraulic control system.
The above is only the preferred embodiments of the utility model, are not intended to limit the utility model, all in the utility model
Spirit and principle within, made any modifications, equivalent replacements, and improvements etc. should be included in the protection model of the utility model
Within enclosing.
Claims (10)
1. movable unmanned helicopter high-altitude reclaimer, it is characterised in that: including automobile chassis, automobile chassis is equipped with swing mechanism
Assembly, the swing mechanism assembly includes turntable, and the turntable lower end and upper end have been respectively articulated with foldable lower cross arm and can roll over
Stacked on cantilever crane, the foldable lower cross arm include next joint arm, lower two joint arms and lower jib lubbing mechanism, one end of next joint arm
Hingedly on the turntable, the other end of next joint arm is connected by two opposite pins with lower two joint arms, when
After removing one of pin, lower two joint arms can rotate with close next joint arm and pass through using another pin as axis
Withdrawal lock pin in the middle part of a upper joint arm and upper two joint arm, which is realized, folds connection, the both ends difference of the lower jib lubbing mechanism
It is connect with next joint arm and the turntable；The foldable upper cantilever crane includes the first telescopic arm, the second telescopic arm, the first change
Width mechanism and the second jib lubbing mechanism, the arm tail of the first telescopic arm basic arm hingedly on the turntable, the second jib lubbing mechanism
One end be mounted on the arm head of the first telescopic arm minor details arm, the other end of second jib lubbing mechanism is stretched with described second
Contracting arm is hinged, and the both ends of first jib lubbing mechanism are hinged with first telescopic arm and the turntable respectively, and described first becomes
Width mechanism is used to drive first telescopic arm in vertical rotation in surface and adjust the angle of first telescopic arm and horizontal plane,
Second jib lubbing mechanism is for driving second telescopic arm in vertical rotation in surface and adjusting second telescopic arm and water
Angle between plane, the foldable lower cross arm and the foldable upper cantilever crane form the U of a side opening after being unfolded simultaneously
Shape opening；The end of the minor details arm of first telescopic arm is also equipped with the arm head pulley blocks for hanging suspension hook, and turntable upper end is also set
There is the hoisting mechanism for driving suspension hook to move.
2. movable unmanned helicopter high-altitude according to claim 1 reclaimer, it is characterised in that: first telescopic arm and
Second telescopic arm includes multiple joint arms and the telescoping mechanism for driving multiple joint arm sequences to stretch out or retract.
3. movable unmanned helicopter high-altitude according to claim 2 reclaimer, it is characterised in that: the telescoping mechanism includes
Oil cylinder.
4. movable unmanned helicopter high-altitude according to claim 2 reclaimer, it is characterised in that: the second jib lubbing mechanism is to connect
Linkage specifically includes pulling plate, support frame, tripod, Eagle-mouth type truss foundation frame, push rod and amplitude oil cylinder, Eagle-mouth type truss
The head end of foundation frame is mounted on the end of the first telescopic arm, and the end of Eagle-mouth type truss foundation frame is respectively articulated at different location
There are tripod and support frame, one end of push rod is hinged between middle part, the other end and the tripod of the second telescopic arm basic arm and cuts with scissors
It is connected to pulling plate, the end of the second telescopic arm basic arm is hinged on the olecranon end of Eagle-mouth type truss foundation frame, and support frame is hinged on drawing
Between bar and Eagle-mouth type truss foundation frame, amplitude oil cylinder is hinged on another angle of tripod and the head end of Eagle-mouth type truss foundation frame
Between；Amplitude oil cylinder, the first side of tripod, amplitude oil cylinder and Eagle-mouth type truss foundation frame hinge to tripod and Eagle-mouth type purlin
Line constitutes a variable delta link between the hinge of frame foundation frame；Tripod constitutes a fixed triangle shape and connects
Bar；Push rod, the second telescopic arm basic arm and Eagle-mouth type truss foundation frame hinge connect to push rod and the second telescopic arm basic arm hinge
Line, the second telescopic arm basic arm and Eagle-mouth type truss foundation frame hinge to support frame and Eagle-mouth type truss foundation frame arm head hinge
Line, support frame constitute a quadrilateral connecting rod；Support frame, pulling plate, one side of tripod, tripod and Eagle-mouth type truss base
The line of plinth frame hinge to support frame and Eagle-mouth type truss foundation frame arm head hinge constitutes another quadrilateral connecting rod.
5. movable unmanned helicopter high-altitude according to claim 1 reclaimer, it is characterised in that: the first luffing machine
Structure, second jib lubbing mechanism and the lower jib lubbing mechanism include oil cylinder.
6. movable unmanned helicopter high-altitude according to claim 1 reclaimer, it is characterised in that: the automobile chassis is logical
With chassis, the vehicle frame for carrying operating mechanism is installed on universal chassis, the turntable is mounted on vehicle frame by pivoting support
On, the two sides on the Universal automobile chassis are respectively equipped with telescopic outrigger.
7. movable unmanned helicopter high-altitude according to claim 1 reclaimer, it is characterised in that: the swing mechanism assembly
It further include pivoting support, rotary motion mechanism and slewing limit mechanism, the turntable is fixedly arranged on the pivoting support, and described time
Turn driving mechanism for driving the pivoting support to rotate.
8. movable unmanned helicopter high-altitude according to claim 7 reclaimer, it is characterised in that: the slewing limit mechanism
Including left slewing limit part, right-hand rotation locating part, recycling state lockpin hole and driving status lockpin hole, left slewing limit part and the right side
Slewing limit part is used to limit the revolution range of swing mechanism assembly, can guarantee unmanned plane after recycling state lockpin hole insertion lock pin
Swing mechanism assembly will not be swung under recycling state, can guarantee vehicle driving status next time after driving status lockpin hole insertion lock pin
Rotation mechanism assembly will not be swung.
9. movable unmanned helicopter high-altitude according to claim 6 reclaimer, it is characterised in that: the Universal automobile chassis
On in the swing mechanism assembly it is ipsilateral from the inside to the outside be equipped with unmanned plane transmitter and it is foldable walk on stage, the foldable energy of walking on stage
It is enough to stretch out expansion to operate the unmanned plane transmitter and retract and be folded so as to store.
10. movable unmanned helicopter high-altitude according to claim 9 reclaimer, it is characterised in that: described foldable to walk on stage
Including walking platen and walking on stage guardrail, it is described walk platen by walk on stage ear mount and the vehicle frame it is hinged, the guardrail of walking on stage passes through column
Bar cut with scissors ear with it is described walk platen it is hinged.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820774466.0U CN208360510U (en) | 2018-05-23 | 2018-05-23 | A kind of movable unmanned helicopter high-altitude reclaimer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820774466.0U CN208360510U (en) | 2018-05-23 | 2018-05-23 | A kind of movable unmanned helicopter high-altitude reclaimer |
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| Publication Number | Publication Date |
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| CN208360510U true CN208360510U (en) | 2019-01-11 |
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ID=64935623
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820774466.0U Expired - Fee Related CN208360510U (en) | 2018-05-23 | 2018-05-23 | A kind of movable unmanned helicopter high-altitude reclaimer |
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| CN (1) | CN208360510U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108502752A (en) * | 2018-05-23 | 2018-09-07 | 河南卫华特种车辆有限公司 | A kind of multistage luffing and flexible foldable arm support |
| CN108688828A (en) * | 2018-05-23 | 2018-10-23 | 河南卫华特种车辆有限公司 | A kind of movable unmanned helicopter high-altitude reclaimer |
| CN109761153A (en) * | 2019-01-26 | 2019-05-17 | 湖南维尔力德科技有限公司 | The stacker crane body of foldable telescopic arm |
-
2018
- 2018-05-23 CN CN201820774466.0U patent/CN208360510U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108502752A (en) * | 2018-05-23 | 2018-09-07 | 河南卫华特种车辆有限公司 | A kind of multistage luffing and flexible foldable arm support |
| CN108688828A (en) * | 2018-05-23 | 2018-10-23 | 河南卫华特种车辆有限公司 | A kind of movable unmanned helicopter high-altitude reclaimer |
| CN109761153A (en) * | 2019-01-26 | 2019-05-17 | 湖南维尔力德科技有限公司 | The stacker crane body of foldable telescopic arm |
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Granted publication date: 20190111 |