CN206926992U - Unmanned plane is resident base station - Google Patents
Unmanned plane is resident base station Download PDFInfo
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- CN206926992U CN206926992U CN201720584091.7U CN201720584091U CN206926992U CN 206926992 U CN206926992 U CN 206926992U CN 201720584091 U CN201720584091 U CN 201720584091U CN 206926992 U CN206926992 U CN 206926992U
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- unmanned plane
- base station
- clamping limb
- drive
- arm
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Abstract
The utility model discloses a kind of unmanned plane and is resident base station, the first fixed mechanism set including base station and on base station, wherein the first fixed mechanism includes the paddle arm that clamp assemblies are used to clamp unmanned plane, also include the second fixed mechanism, second fixed mechanism includes supporting arm and drive component, and this supports arm for being held in the fuselage of the unmanned plane to realize the fixation of vertical dimension.Pass through the cooperation of the first fixed mechanism and the second fixed mechanism, unmanned plane is fixed on base station, so that unmanned plane need not dismantle unmanned plane and be packed again after use, but unmanned plane directly can be fixed on unmanned plane and be resident on base station, directly transported to destination after packaging；When needing to use unmanned plane, also only need unmanned plane being resident on base station from unmanned plane remove i.e. can be used.Solved using the resident base station of unmanned plane of the present utility model before unmanned plane uses every time or be required for assembling or dismantling unmanned plane after, save the time of user.
Description
Technical field
Unmanned air vehicle technique field is the utility model is related to, more particularly to a kind of unmanned plane is resident base station.
Background technology
Unmanned plane be it is current start a kind of gradually practical aircraft, it has maneuverability, rapid reaction, nobody flies
Row, operation require low advantage.
After the storage of existing unmanned plane and traffic program are the blade dismounting by unmanned plane, then by head and load dismounting point
Not Zhuan Jin packing case stored, transport is again assembled blade, head, load, unmanned plane when arriving at.Such one
It will be taken a substantial amount of time to assemble and dismantle the process of unmanned plane, the user for being unfamiliar with unmanned plane, it assembles plus torn open
Unload flight time of the time possibly even beyond unmanned plane of unmanned plane.
In view of the defects of above-mentioned, it is necessary to which a kind of transport that unmanned plane can be realized without assembly and disassembly unmanned plane is provided
Scheme so that unmanned plane after transporting to destination i.e. can be used.
Utility model content
Main purpose of the present utility model is to provide a kind of unmanned plane and is resident base station, it is intended to solves each use of unmanned plane
The problem of being both needed to dismantle with preservation or be inconvenient caused by assembling.
To achieve the above object, the utility model proposes unmanned plane be resident base station, including：
Pedestal, for carrying unmanned plane；
At least one first fixed mechanism, on the pedestal, including clamp assemblies, described in the clamp assemblies clamping
The paddle arm of unmanned plane is to realize the fixation of horizontal dimensions；
Second fixed mechanism, including arm and drive component are supported, the arm that supports supports under the driving of the drive component
The fuselage of the unmanned plane is held in realize the fixation of vertical dimension.
Preferably, first fixed mechanism also includes lifting assembly, and the lifting assembly is fixed on the pedestal, described
Clamp assemblies are arranged on the lifting assembly.
Preferably, the clamp assemblies include：
Fixed seat on the lifting assembly；
The first clamping limb being arranged in the fixed seat, and relative first clamping limb may move in the fixed seat
The second clamping limb that ground is set, first clamping limb and paddle arm of second clamping limb for clamping the unmanned plane；
Fastening assembly, for locking and unclamping movement of second clamping limb in fixed seat, to allow described second
Movement or fixed second clamping limb position on fixed seat of the clamping limb in fixed seat.
Preferably, the clamp assemblies also include the drive division being arranged in fixed seat, and the drive division is used to drive institute
State movement of second clamping limb in the fixed seat.
Preferably, the drive division includes rotating valve, the movable plate being connected with second clamping limb and is connected to institute
The connecting rod between rotation valve and the movable plate is stated, the connecting rod is used to the rotation for rotating valve being changed into the movable plate in institute
The movement in fixed seat is stated, so as to drive second clamping limb to be moved in the fixed seat；The fastening assembly is used to limit
Make or allow the rotation valve to rotate, to lock and unclamp movement of second clamping limb in fixed seat.
Preferably, connected between the movable plate and the fixed seat by elastic component.
Preferably, stopper protrusion is provided with the rotation valve of the drive division, the stopper protrusion is used to limit the drive
The rotational travel in dynamic portion.
Preferably, the arm that supports of second fixed mechanism includes connecting rod, and what the connecting rod included being oppositely arranged supports
End and drive end, the end that supports is provided with the support division for supporting at the top of unmanned aerial vehicle body；
The drive end of the connecting rod is rotatably connected on the drive component；
The drive component drives the connecting rod to rotate, and supports on the unmanned aerial vehicle body or releases to institute to realize
State supporting for unmanned aerial vehicle body.
Preferably, the drive rod being removably attachable in the connecting rod is also included on the drive end
Preferably, the button for closing the drive component is additionally provided with the drive component, on the drive end
Also corresponding be provided with can trigger the lug boss of the button with the rotation for supporting arm.
In technical solutions of the utility model, unmanned plane is resident the first fixation that base station includes base station and set on base station
Mechanism, wherein the first fixed mechanism, which includes clamp assemblies, is used to clamping the paddle arm of unmanned plane, in addition to the second fixed mechanism, second
Fixed mechanism includes supporting arm and drive component, and this supports arm for being held in the fuselage of the unmanned plane to realize vertical dimension
Fixation.By the cooperation of the first fixed mechanism and the second fixed mechanism, unmanned plane is fixed on base station, so that nobody
Machine need not dismantle unmanned plane and be packed again after use, but unmanned plane directly can be fixed on into unmanned plane and be resident base station
On, directly transported to destination after packaging；When needing to use unmanned plane, also only need unmanned plane being resident from unmanned plane
Remove on base station and can be used.Base station is resident using unmanned plane of the present utility model to solve before unmanned plane uses every time or use
After be required for assembling or dismantling unmanned plane, save the time of user.
Brief description of the drawings
, below will be to embodiment in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art
Or the required accompanying drawing used is briefly described in description of the prior art, it should be apparent that, drawings in the following description are only
It is some embodiments of the utility model, for those of ordinary skill in the art, is not paying the premise of creative work
Under, other accompanying drawings can also be obtained according to the structure shown in these accompanying drawings.
Fig. 1 is that the unmanned plane of the utility model embodiment is resident the structure chart of base station；
Fig. 2 is the structure chart of the first fixed mechanism in Fig. 1；
Fig. 3 is Fig. 2 exploded view；
Fig. 4 is the structure chart of the second fixed mechanism in Fig. 1；
Fig. 5 is Fig. 4 exploded view；
Fig. 6 is the exploded view at Fig. 4 another visual angle.
Drawing reference numeral explanation：
Realization, functional characteristics and the advantage of the utility model purpose will be described further referring to the drawings in conjunction with the embodiments.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only part of the embodiment of the present utility model, rather than all
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not making creative work premise
Lower obtained every other embodiment, belong to the scope of the utility model protection.
It is to be appreciated that the directional instruction (such as up, down, left, right, before and after ...) of institute in the utility model embodiment
It is only used for explaining relative position relation under a certain particular pose (as shown in drawings) between each part, motion conditions etc., such as
When the fruit particular pose changes, then directionality instruction also correspondingly changes therewith.
In addition, and it can not be managed in the utility model such as relating to the description of " first ", " second " etc. is only used for describing purpose
Solve to indicate or implying its relative importance or the implicit quantity for indicating indicated technical characteristic.Thus, define " the
One ", at least one this feature can be expressed or be implicitly included to the feature of " second ".It is " more in description of the present utility model
It is individual " it is meant that at least two, such as two, three etc., unless otherwise specifically defined.
In the utility model, unless otherwise clearly defined and limited, term " connection ", " fixation " etc. should do broad sense reason
Solution, for example, " fixation " can be fixedly connected or be detachably connected, or integrally；Can mechanically connect, also may be used
Be electrical connection；Can be joined directly together, can also be indirectly connected by intermediary, can be the connection of two element internals
Or the interaction relationship of two elements, limited unless otherwise clear and definite.For the ordinary skill in the art, can be with
Concrete meaning of the above-mentioned term in the utility model is understood as the case may be.
In addition, the technical scheme between each embodiment of the utility model can be combined with each other, but must be with ability
Domain those of ordinary skill can be implemented as basis, will be understood that when the combination appearance of technical scheme is conflicting or can not realize
The combination of this technical scheme is not present, also not within the protection domain of the requires of the utility model.
Main purpose of the present utility model is to provide a kind of unmanned plane and is resident base station 100, it is intended to solves unmanned plane 200
Use or preserve every time the problem of inconvenient caused by being both needed to dismantle or assembling.
It refer to Fig. 1 to Fig. 6, in a kind of embodiment of the present utility model, the unmanned plane, which is resident base station 100, includes base
Seat 30, the pedestal 30 are used to carry unmanned plane 200；
At least one first fixed mechanism 10, on the pedestal 30, including clamp assemblies 11, the clamp assemblies 11
The paddle arm 210 of the unmanned plane 200 is clamped to realize the fixation of horizontal dimensions；And
Second fixed mechanism 20, second fixed mechanism 20 includes supporting arm 21 and drive component, described to support arm 21
The fuselage 220 of the unmanned plane 200 is held under the driving of the drive component 22 to realize the fixation of vertical dimension.
Unmanned plane of the present utility model be resident base station 100 by set the second fixed mechanism 20 and the first fixed mechanism 10 come
The fixation to unmanned plane 200 is realized, first fixed mechanism 10 realizes the clamping to the paddle arm 210 of unmanned plane 200, with limit
The transverse shifting of unmanned plane 200 processed；Second fixed mechanism 20 is realized to the longitudinal spacing of unmanned plane 200；So as to realize
In the transport of unmanned plane 200, it is only necessary to which unmanned plane 200 is fixed on by the second fixed mechanism 20 with first fixed structure 10
Unmanned plane is resident on base station 100 so that has been used every time after unmanned plane 200 without placing into packaging after unmanned plane 200 is dismantled
Transported in case, but whole unmanned plane directly can be resident base station 100 and be fixed on the nothing that unmanned plane is resident on base station 100
Man-machine 200 are put into packing case transport together；When using unmanned plane 200 next time, without reinstalling unmanned plane 200,
But it can be resident on base station 100 to remove from unmanned plane directly by unmanned plane 200 and can be used.Substantially reduce unmanned plane 200
The time of unmanned plane 200 is dismantled before using every time after installation unmanned plane 200 and use, the use for unmanned plane 200 provides
Great convenience.
It is understood that first fixed mechanism 10 is set directly on pedestal 30, it clamps the mode of paddle arm 210
It can be clamped, can also be clamped, etc. by hydraulic-driven clamping device by manipulator clamping mechanism.Described second is solid
Determining mechanism 20 includes supporting arm 21, and its set-up mode can be connected directly between by supporting arm 21 on pedestal 30, and this supports arm
21 reduction can support spacing between arm 21 and pedestal 30 to adjust up and down, so as to realize the fuselage of fixed unmanned plane 200
220 support and unmanned plane 200 are released into fixation；Certainly, in other embodiments, second fixed mechanism 20 supports arm 21
To supporting for the fuselage 220 of unmanned plane 200, and release can be by supporting the rotation of arm 21 to supporting for the fuselage 220 of unmanned plane 200
To realize, the specifically rotation by supporting arm 21 realizes that will support arm 21 supports on the fuselage 220 of unmanned plane 200, with
And release supporting to the fuselage 220 of unmanned plane 200.Further, second fixed mechanism 20 can also include being used to clamp
The clamp assemblies of fuselage 220, the clamp assemblies are clamped in the position of corresponding fuselage between adjacent two paddle arm, the clamp assemblies with
Support arm 21 to coordinate, realize supporting and gripping to fuselage 220.
Simultaneously, it is necessary to which explanation, second fixed mechanism 20 can equally be arranged on the pedestal 30, also may be used
To be the setting separated with pedestal 30, second fixed mechanism 10 is used for the fuselage 220 for supporting unmanned plane 200.Specifically can be with
To support the top of the fuselage 220 of unmanned plane 200 by the second fixed mechanism 100.First fixed mechanism 20 is used to clamp
The paddle arm 210 of fixed unmanned plane 200, is specifically as follows and fixes nobody from the bottom of unmanned plane 200 by the first fixed mechanism 20
The paddle arm 210 of machine 200.The purpose being so designed that is：Fixed by the second fixed mechanism 10 from the top of unmanned plane 200 and first
Mechanism 20 realizes the fixation to the above-below direction of unmanned plane 200 from the bottom of unmanned plane 200, and unmanned plane 200 is consolidated in above-below direction
It is fixed stuck；Clamping of first fixed mechanism 10 to paddle arm 210 simultaneously, also defines motion of the unmanned plane 200 in horizontal direction, i.e.,
Also it is unmanned plane 200 is stuck in a lateral direction, and then unmanned plane 200 is stably fixed to unmanned plane and is resident on base station 100,
Prevent from causing damage to unmanned plane 200 because rocking in transportation.
Certainly, in other embodiments, second fixed mechanism 20 can also be from the bottom of the fuselage 220 of unmanned plane 200
Portion's fixed main body 220, at this moment, in order to coordinate this fixed form of the second fixed mechanism 20, first fixed mechanism 10 needs
To be fixed using by the way of the top of unmanned plane 200 fixation paddle arm 210.It is not particularly limited herein, main purpose is with energy
Realize from unmanned plane about 200 both direction fixation of the realization to unmanned plane 200 simultaneously be defined.
It should be noted that first fixed mechanism 10 and second fixed mechanism 20 may each be dismountable solid
It is scheduled on the pedestal 30, on the pedestal 30, setting is multiple to install the first fixed mechanism 10 and the second fixed mechanism 20
Mount point, so as to make the first fixed mechanism 10 and the second fixed mechanism 20 to convert installation according to different unmanned planes 200
Position.
In addition, position of first fixed mechanism 10 on the pedestal 30 can be adjusted as needed, with not
With the location matches of the paddle arm 210 of unmanned plane 200；Or be arranged to can for the clamp assemblies 11 on first fixed mechanism 10
Rotate in the horizontal direction, be also to adapt to the position of the paddle arm 210 of different unmanned planes 200, so that clamp assemblies 11
The paddle arm 210 of unmanned plane 200 can be clamped.
As a kind of preferred embodiment, 2~Fig. 3 of reference picture, first fixed mechanism 10 includes lifting assembly, described
Lifting assembly is fixed on the pedestal, and the clamp assemblies are arranged on the lifting assembly.Specifically, in the present embodiment
In, the lifting assembly 12 includes fixed part and lifting unit, and the fixed part is fixed on the pedestal 30, the lifting unit with
It is fixed or dismountable connected between the clamp assemblies 11.Further, the lifting assembly 11 is hydraulic lifting component,
Wherein, the fixed part is piston sleeve, and the lifting unit is piston rod.
It is understood that in another embodiment, the lifting assembly 12 can be held in not using with holding part
The regulation of height is realized with the stretching structure of gear.Now, the lifting assembly 12 includes telescopic rod, this lifting assembly 12
Structure can be the direct position that expansion link can be held in different stalls using being set on the expansion link of lifting assembly 12
Holding part, to realize the regulation of different height.In this embodiment, the corresponding three kinds of different height of three kinds of different stalls are set
Degree, so as to adapt to the height of different unmanned planes 200.
Certainly, in other embodiments, the lifting assembly 12 can be also electric lifting mechanism, not do specific limit herein
System, is defined by the regulation that can carry out height.
Further, in the present embodiment, the clamp assemblies 11 include：
Fixed seat 13 on the lifting assembly 12；
The first clamping limb 15 being arranged in the fixed seat 13, and relative first clamping limb in the fixed seat 13
15 the second clamping limbs 14 being movably disposed, first clamping limb 15 are used to clamp the nothing with second clamping limb 14
Man-machine 200 paddle arm 210；
Fastening assembly 101, for locking and unclamping second clamping limb 14, to allow second clamping limb 14 solid
The position of movement or fixed second clamping limb 14 in fixed seat 13 in reservation 13.
Specifically, reference picture 2 and Fig. 3, the clamp assemblies 11 pass through the first clamping limb 15 for being arranged in fixed seat 13
The clamping to the paddle arm 210 of unmanned plane 200 is realized with the second clamping limb 14.Wherein, second clamping limb 14 can be in fixation
Moved on seat 13 relative to the first clamping limb 15, between increasing or reduce between the first clamping limb 15 and the second clamping limb 14
Away from, and then adapt to the size of the paddle arm 210 of different unmanned planes 200.And movement of second clamping limb 14 in fixed seat 13 can
It is accomplished in several ways, for example, promoting the second clamping limb 14 by the push-and-pull component being connected with the second clamping limb 14 to realize
Moved to the first clamping limb 15, or the second clamping limb 14 of traction moves away from first clamping limb 15.The push-and-pull component can be with
It is arranged on pedestal 30, and is connected with the second clamping limb 14, the push-and-pull component pushes away including one with what the second clamping limb 14 was connected
Pull bar and the driving reciprocating drive device of pull bar.
Certainly, in other embodiments, slide rail can also be set in fixed seat 13 so that the second clamping limb 14 can be along this
Slide rail moves, and then realizes movement of second clamping limb 14 relative to the first clamping limb 15.Specifically, so that the second clamping limb can be realized
14 are defined relative to the movement of the first clamping limb 15.
When the second clamping limb 14 is moving in fixed seat 13 relative to the first clamping limb 15, can be known with beyond all doubt
It is, it is necessary to the second clamping limb 14 is fixed by position after movement using a fastening assembly 101, to realize the second clamping limb
14 fix, and can coordinate the clamping realized to the paddle arm 210 of unmanned plane 200 with the first clamping limb 15.When the second clamping limb
14 by push-and-pull component to realize mobile when, can use in the second clamping limb 14 with open up screwed hole in fixed seat 13, pass through spiral shell
Second clamping limb 14 is fixed in fixed seat 13 by female cooperation with screwed hole, and the screwed hole open up it is multiple, by second
Clamping limb 14 is fixed on different positions.Certainly, the design of this fastening assembly 101 is also applied for by being set in fixed seat 13
Put slide rail, since realize the second clamping limb 14 movement mode.
Certainly, it is necessary to which explanation, the adjustment of the spacing between the first clamping limb 15 and the second clamping limb 14, are not limited only
Can be realized by the movement of the second clamping limb 14, first clamping limb 15 equally could be arranged to can in fixed seat 13
Mobile mounting means, specific move mode equally refer to the move mode of the second clamping limb 14, not repeated one by one herein.
As a kind of preferred embodiment, the clamp assemblies 11 also include the drive division 16 being arranged in fixed seat 13,
The drive division 16 is used to drive movement of second clamping limb 14 in the fixed seat 13.Specifically, the drive division
The movement of 16 driving second clamping limbs 14 equally refers to the second above-mentioned clamping limb 14 and movement is realized in fixed seat 13
Mode.
Further, in the present embodiment, the drive division 16 includes rotating valve 162, connects with second clamping limb 14
The movable plate 163 connect and the connecting rod 17 being connected between the rotation valve 162 and the movable plate 163, the connecting rod 17 are used
In rotation valve 162 is changed into movement of the movable plate 163 in the fixed seat 13, so as to drive described second
Clamping limb 14 moves in the fixed seat 13；The fastening assembly 101 is used to adjust the elastic of the rotation valve 162, so that
The rotation valve 162 is rotated or fixed.
Reference picture 2 and Fig. 3, the rotation valve 162 of the drive division 16 are rotatably connected in the fixed seat 13, described turn
When dynamic valve 162 rotates around the axis, when rotation valve 162 rotates clockwise, the movable plate 163 being attached thereto is driven in fixed seat 13
Upper movement, the movable plate 163 further drive second clamping limb 14 to move, in particular close in fixed seat 13
One clamping limb 15 moves so that the spacing between the first clamping limb 15 and the second clamping limb 14 diminishes, so that spacing is big
The small clamping of paddle arm 210 for just making unmanned plane 200 is fixed between the first clamping limb 15 and the second clamping limb 14.When determining
Behind the position of two clamping limbs 14, stop operating and rotate valve 162, and will rotate after valve 162 is fastened on rotation by fastening assembly 101
Position, so just complete the adjustment of the position of the second clamping limb 14.
, can be according to the big ditty of the paddle arm 210 of unmanned plane 200 using the clamp assemblies 11 in the utility model embodiment
The position of whole second clamping limb 14, and then meet the clamping for adapting to the paddle arm 210 of different unmanned planes 200.
Referring to Fig. 3, the fastening assembly 101 in the present embodiment includes pin (not indicating) and for locking the pin
Knob (is not indicated), and spring (not shown) is arranged with the pin.Specifically, installation institute is offered in the fixed seat 13
The first pin hole (not indicating) of pin is stated, while second pin hole is also installed on the rotation valve 162, the pin is worn
First pin hole is crossed, and is inserted under the force of a spring in the second pin hole, so as to realize to rotating determining for valve 162
Position, then realized by knob and pin is locked in the second pin hole, so as to realize fixation and rotation to rotating valve 162
Control.
In other embodiments, the fastening assembly can also be screw rod.The side for rotating valve 162 offers first
Screwed hole, the second screwed hole corresponding with the first screwed hole is offered in the fixed seat 13, the screw rod passes through the first screw thread
Hole and the second screwed hole, realize the fastening to rotating valve 162.In use, when needing to rotate valve 162, screw rod is unscrewed,
And when complete rotate valve 162 rotation after, it is necessary to will rotate valve 162 be fixed on the turned position when, then only need screw rod 101
Tighten.Can be by the 162 securing screw rod of rotation valve after rotation, phase by being set on valve 162 and fixed seat 13 is rotated
When in realizing to the second fixation for supporting the position of arm 14, arm is supported so as to which the paddle arm 210 of unmanned plane 200 is held in into second
14 and first between clamping limb 15, and is not in loosen.
Certainly, in other embodiments, the fastening assembly can also be other structures, for example, can be on valve 162 is rotated
Spacing preiection is set, limit card slot is set in fixed seat 13, makes spacing preiection holding to limiting card when rotating valve 162 and turning to
When in groove, that is, realize the spacing fixation to rotating valve 162.It is not particularly limited, can be realized to driving with fastening assembly herein
The fixation of portion turned position.
In the present embodiment, connected between the movable plate 163 and rotation valve 162 by connecting rod 17.Referring to Fig. 2 and Fig. 3,
Rotating valve 162 needs to drive movable plate 163 movable relative to the first clamping limb 15 in fixed seat 13, therefore, is rotating
Connected between valve 162 and movable plate 163 by connecting rod 17.The present embodiment uses bar linkage structure, realizes to rotate the rotation of valve 162
Linear motion of the movable plate 163 in fixed seat 13 is converted to, while makes the structure of whole clamp assemblies 11 compacter.
Further, connected between the movable plate 163 and the fixed seat 13 by elastic component.The elastic component can be
When the fastener 101 releases the locking to the rotation valve 162, the rotation valve 162 is set to return to original position.
Elastic component in the present embodiment is using spring 141.
Further, in order to limit stroke of the rotation valve 162 in rotation process, set on the rotation valve 162
It is equipped with stopper protrusion 161.The stopper protrusion 161 can turn to stop position in the rotation valve 162 towards the fixed seat 13
When putting, supported with fixed seat 13, continue to rotate towards fixed seat 13 so as to hinder to rotate valve 162, define the fortune for rotating valve 162
Dynamic stroke.
As another preferred embodiment, 4~Fig. 6 of reference picture, the arm 21 that supports of second fixed mechanism 20 includes connecting
Extension bar 211, the connecting rod 211 support end and drive end 213 including what is be oppositely arranged, and the end that supports is provided with for supporting nothing
The support division 212 of man-machine fuselage roof；
Reference picture 4, described to support 21 substantially L-shaped structure of arm, the one end for supporting arm 21 is connected with for supporting at nobody
The support division 212 at the top of fuselage 220 of machine 200, the support division 212 are detachably connected to support one end of arm 21, and described
The drive end 213 for supporting arm 21 is then connected with drive component 22, and the drive component 22 drive supports arm 21 and rotated, and makes to support arm 21
It can be rotated in 0 °~90 °, realize supporting to the top of fuselage 220 of unmanned plane 200.
The drive end 213 of the connecting rod 211 is rotatably connected on the drive component 22；
The drive component 22 drive it is described support arm 21 and rotate, end will be supported and support machine in the unmanned plane 200
Body 220 or releasing support end and the fuselage 220 of the unmanned plane 200 are supported.
It can be seen that from Fig. 1 and Fig. 4, support arm 21 and support at the top of the fuselage 220 of unmanned plane 200, will can drive
Component 22 suspends, and when needing fuselage 220 when supporting of the releasing to unmanned plane 200, then drive component 22 is opened, drive supports
The opposite direction of arm 21 rotates, to release supporting for the fuselage 220 for supporting arm 21 to unmanned plane 200.It should be noted that driving group
The startup and pause of part 22 can be controlled by controlling remote.
Specifically, the support division 212 includes supporting panel 212a and is fixed on the connector supported on panel 212a
212b, the connector 212b are used to make the support division 212 be detachably connected with the arm 21 that supports, described to support panel
212a is provided with four equally distributed holding block 212c away from the one side of the connector 212b, and the holding block 212c is used for
It is described support arm 21 and turn to the support division 212 can be made to support at the top of fuselage 220 of the unmanned plane 200.By to
Block 212c reductions and the contact area at the top of fuselage 220 of unmanned plane 200 are held, so as to prevent contact area excessive to unmanned plane
The abrasion at 200 top of fuselage 220.Specifically, the holding block can use the flexible material such as rubber to prepare, to subtract
The small abrasion to unmanned aerial vehicle body.
Further, the drive rod being removably attachable in the connecting rod 211 is also included on the drive end 213
(not indicating).The drive rod is supported on arm 21 described in being removably attachable to, and facilitates unmanned plane to be resident tearing open when base station is repaired
Unload and install.
Further, the drive component 22 is provided with for suspending the driving group towards the one side for supporting arm 21
The button 221 of part 22, the side of the drive end 213 towards the drive component 22 are provided with lug boss 213a, the projection
Portion 213a can trigger the button 221 with the rotation for supporting arm 21.It should be noted that the drive component 22 is opened
Opening can be controlled by controlling remote, but the closing of the drive component 22 is then by drive component 22 in the present embodiment
Upper setting is corresponding to be switched to realize.Specifically, in the drive component 22 towards the face settings button for supporting arm 21
221, the button 221 is one raised, and the unlatching of the button 221 passes through the lug boss 213a triggerings on drive end 213.Support arm
21 can rotate in the range of 90 °, and the number of the button 221 is two, and two buttons 221 are oppositely arranged, two buttons 221
In a button 221 set by position be to support arm 21 to support the position on the fuselage 220 of unmanned plane 200 just.
Detailed description below supports the routing motion process of arm 21 and drive component 22：Reference picture 1 and Fig. 4, Fig. 1 are shown
Support arm 21 and support the state on the fuselage 220 of unmanned plane 200, this state unmanned plane 200 is incorporated in unmanned plane and is resident base
Stand on 100, be readily transported.Taken when needing to use unmanned plane 200, it is necessary to which unmanned plane 200 is resident on base station 100 from unmanned plane
Under, now Remote opens drive component 22, and drive component 22 is run, and drives the arm 21 that supports being attached thereto to rotate.Ginseng
According to Fig. 4, now supporting arm 21 will be rotated in the clockwise direction, and support the position that the fuselage 220 for supporting unmanned plane 200 is left at end,
When supporting 221 position of button that arm 21 rotate in place below drive component 22, support convex on the drive end 213 of arm 21
Portion 213a pressing buttons 221 are played, trigger the closing of drive component 22, then supporting arm 21 will stop operating, and rest on the position.And
When needing to be placed into unmanned plane 200 on the resident base station 100 of unmanned plane, then Remote opens drive component 22, now drives
Drive is supported arm 21 and rotated counterclockwise by dynamic component 22, when the button for supporting arm 21 and rotateing in place in drive component 22 by the top
When 221, the lug boss 213a pressing buttons 221 on the drive end 213 of arm are supported, triggering drive component 22 is closed, then supports arm
21 support on 220 fuselages of unmanned plane 200, and rest on the position, until next drive component 22 is opened.
It should be noted that the rotating clockwise for arm 21 that support of foregoing description is supported for supporting arm 21 in Fig. 4
State when on the fuselage 220 of unmanned plane 200, and rotate counterclockwise, original is then returned to after rotating clockwise to support arm 21
The rotation of position.
Certainly, in other embodiments, the opening and closing of the drive component 22 can use Remote to control.This
By setting trigger button 221 on drive component 22 in embodiment, the closing of drive component 22 is triggered by button 221, from
Go to judge to support whether arm 21 is supported on the fuselage 220 of unmanned plane 200 according to observation without user, it also avoid working as nobody
When machine 200 is not supported on the fuselage 220 of unmanned plane 200 completely, just suspend drive component 22.The facility of operation is improved, is
User saves the time.
Preferred embodiment of the present utility model is the foregoing is only, not thereby limits the scope of the claims of the present utility model,
Every equivalent structure under utility model of the present utility model design, made using the utility model specification and accompanying drawing content
Conversion, or directly/be used in other related technical areas indirectly and be included in scope of patent protection of the present utility model.
Claims (10)
1. a kind of unmanned plane is resident base station, it is characterised in that including：
Pedestal, for carrying unmanned plane；
At least one first fixed mechanism, on the pedestal, including clamp assemblies, the clamp assemblies clamping it is described nobody
The paddle arm of machine is to realize the fixation of horizontal dimensions；
Second fixed mechanism, including arm and drive component are supported, the arm that supports is held under the driving of the drive component
The fuselage of the unmanned plane is to realize the fixation of vertical dimension.
2. unmanned plane according to claim 1 is resident base station, it is characterised in that first fixed mechanism also includes lifting
Component, the lifting assembly are fixed on the pedestal, and the clamp assemblies are arranged on the lifting assembly.
3. unmanned plane according to claim 2 is resident base station, it is characterised in that the clamp assemblies include：
Fixed seat on the lifting assembly；
The first clamping limb being arranged in the fixed seat, and relative first clamping limb is movably set in the fixed seat
The second clamping limb put, first clamping limb and paddle arm of second clamping limb for clamping the unmanned plane；
Fastening assembly, for locking and unclamping movement of second clamping limb in fixed seat, to allow second clamping
Movement or fixed second clamping limb position on fixed seat of the arm in fixed seat.
4. unmanned plane according to claim 3 is resident base station, it is characterised in that the clamp assemblies also include being arranged on admittedly
Drive division in reservation, the drive division are used to drive movement of second clamping limb in the fixed seat.
5. unmanned plane according to claim 4 is resident base station, it is characterised in that the drive division includes rotating valve, with institute
The connecting rod stated the movable plate of the second clamping limb connection and be connected between the rotation valve and the movable plate, the connecting rod are used
In rotation valve is changed into movement of the movable plate in the fixed seat, so as to drive second clamping limb to exist
Moved in the fixed seat；The fastening assembly is used to limit or allows the rotation valve to rotate, described to lock and unclamp
Movement of second clamping limb in fixed seat.
6. unmanned plane according to claim 5 is resident base station, it is characterised in that between the movable plate and the fixed seat
Connected by elastic component.
7. unmanned plane according to claim 4 is resident base station, it is characterised in that is provided with the rotation valve of the drive division
Stopper protrusion, the stopper protrusion are used for the rotational travel for limiting the drive division.
8. the unmanned plane according to claim any one of 1-6 is resident base station, it is characterised in that second fixed mechanism
Supporting arm includes connecting rod, and what the connecting rod included being oppositely arranged supports end and drive end, and the end that supports is provided with for supporting
Hold the support division at the top of unmanned aerial vehicle body；
The drive end of the connecting rod is rotatably connected on the drive component；
The drive component drives the connecting rod to rotate, and supports on the unmanned aerial vehicle body or releases to the nothing to realize
Man-machine fuselage supports.
9. unmanned plane according to claim 8 is resident base station, it is characterised in that also includes on the drive end dismountable
The drive rod being connected in the connecting rod.
10. unmanned plane according to claim 8 is resident base station, it is characterised in that is additionally provided with use on the drive component
It is provided with and can be triggered with the rotation for supporting arm in also corresponding on the button for closing the drive component, the drive end
The lug boss of the button.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720584091.7U CN206926992U (en) | 2017-05-23 | 2017-05-23 | Unmanned plane is resident base station |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720584091.7U CN206926992U (en) | 2017-05-23 | 2017-05-23 | Unmanned plane is resident base station |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206926992U true CN206926992U (en) | 2018-01-26 |
Family
ID=61351984
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720584091.7U Withdrawn - After Issue CN206926992U (en) | 2017-05-23 | 2017-05-23 | Unmanned plane is resident base station |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206926992U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107176307A (en) * | 2017-05-23 | 2017-09-19 | 深圳电航空技术有限公司 | Unmanned plane is resident base station |
-
2017
- 2017-05-23 CN CN201720584091.7U patent/CN206926992U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107176307A (en) * | 2017-05-23 | 2017-09-19 | 深圳电航空技术有限公司 | Unmanned plane is resident base station |
| CN107176307B (en) * | 2017-05-23 | 2019-03-01 | 深圳一电航空技术有限公司 | Unmanned plane is resident base station |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20180126 Effective date of abandoning: 20190301 |