CN108750132A - Unmanned plane - Google Patents
Unmanned plane Download PDFInfo
- Publication number
- CN108750132A CN108750132A CN201810912174.3A CN201810912174A CN108750132A CN 108750132 A CN108750132 A CN 108750132A CN 201810912174 A CN201810912174 A CN 201810912174A CN 108750132 A CN108750132 A CN 108750132A
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- CN
- China
- Prior art keywords
- fuselage
- holder
- unmanned plane
- bolt
- locking device
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Accessories Of Cameras (AREA)
- Toys (AREA)
Abstract
The present invention provides a kind of unmanned plane, including：Fuselage, the fuselage are equipped with socket；Holder, the holder, which is equipped with, to be coordinated with the socket the holder to be connected to the contact pin of the fuselage；And locking device, the locking device is for preventing fuselage from being detached with holder.Unmanned plane provided by the invention, pass through the mating connection of the socket on the contact pin and fuselage on holder, being detachably connected for holder and unmanned aerial vehicle body may be implemented, the plug-in type designs, it is simple in structure, it is easy to operate, it only need to be to towards or away from the direction grafting of fuselage of unmanned plane, drawing holder, holder can be made to be connected or separated with fuselage so that user can quickly grasp and complete the installation and removal of holder.
Description
Technical field
The present invention relates to air vehicle technique field more particularly to a kind of unmanned planes.
Background technology
The technology of taking photo by plane is widely used in aeroplane photography, territory detection, forest fire protection etc.；When taking photo by plane, often pass through
Unmanned plane obtains required image；Unmanned plane includes：Fuselage and holder with shooting function pass through the boat for controlling unmanned plane
Walking along the street line can obtain the image of needs.
In the prior art, holder can be connected by way of being fixedly connected with the fuselage of unmanned plane；Also it can pass through Quick Release
The fuselage of formula connection structure and unmanned plane is detachably connected.However, the Quick-dismantling structure of existing holder is complex, behaviour
It is more to make step, if the installation and removal of holder can not be often rapidly completed not by training in user.
Invention content
In view of this, the present invention provides a kind of unmanned plane, with solve the quick-disassembly structure of holder of existing unmanned plane it is complicated,
User is not easy the problem of grasping, and provides a kind of unmanned plane simple in structure so that user can quickly grasp and complete holder
Installation and removal.
The present invention provides a kind of unmanned planes, including：Fuselage, the fuselage are equipped with socket；Holder, the holder be equipped with
The holder to be connected to the contact pin of the fuselage by the socket cooperation；And locking device, the locking device is for hindering
Only the fuselage is detached with the holder.
In some embodiments, it is additionally provided with positioning region on the holder, is additionally provided on the fuselage and the positioning
The location hole of portion's cooperation, the positioning region is threaded through in the location hole, so that socket described in the contact pin face.
In some embodiments, the positioning region includes cylinder and guide part in the post tips is arranged, described
Guide part is in coniform, and the larger end face of the guide part area of section is connect with the post tips.
In some embodiments, the bottom of the location hole is provided with the conical surface coordinated with the guide part.
In some embodiments, the positioning region is multiple, the setting at multiple positioning region intervals.
In some embodiments, the locking device includes the clip-connecting rod being arranged on the holder, on the clip-connecting rod
It is provided with fixture block, clamping portion is provided on the fuselage, the fixture block is clamped with the clamping portion.
In some embodiments, it is in the installation to have horizontally disposed mounting plate, the clamping portion on the fuselage
The card hole being arranged on plate, and the card hole runs through the mounting plate；Stop surface is provided on the fixture block, the clip-connecting rod is by institute
The card hole is stretched into the bottom surface for stating mounting plate towards ground, and the stop surface is supported and deviates from the bottom on the mounting plate
On the top surface in face.
In some embodiments, the first guide surface is additionally provided on the fixture block, described first is oriented to towards the clamping
Column extends away from the end of the holder and gradually deviates from the side wall of the card hole, and first guide surface is used for the clamping
Column is oriented to.
In some embodiments, the clip-connecting rod is multiple, and the fixture block is both provided on each clip-connecting rod, described
Multiple clamping portions are provided on fuselage, each fixture block and a clamping portion are clamped.
In some embodiments, the locking device includes the first attraction part and second attracts part, and described first attracts
Part is arranged on the holder, and described second attracts part to be arranged on the fuselage；Described first attracts part and/or described second
Attract part that there is magnetism, the first attraction part and the second attraction part to attract each other.
In some embodiments, the first attraction part and the second attraction part are magnet.
In some embodiments, the locking device includes：Clamping block on the holder, the clamping block are set
On be provided with slot；It is provided with lock slots on the fuselage and is through to the jack of the lock slots；The clamping block is accommodated in
In the lock slots, bolt is plugged in the jack and the slot.
In some embodiments, the locking device further includes Lock spring, and the first stopper section is provided on the bolt,
The second stopper section is provided on the fuselage, the both ends of the Lock spring are stopped with first stopper section and described second respectively
Stopper connects；The Lock spring is for driving movement of the bolt into the lock slots.
In some embodiments, the locking device further includes operating lever, and slide opening, the operation are provided on the fuselage
The driving end of bar is threaded through in the slide opening, and the driving end is provided with inclined-plane；It is provided on the bolt and matches with the inclined-plane
The driving portion of conjunction, with when pressing the operating lever into the slide opening, it is described to drive that the driving portion is supported on the inclined-plane
External movement of the bolt to the lock slots.
In some embodiments, the driving portion includes the drive hole being arranged on the bolt, and the driving end is worn
In the drive hole, and the inclined-plane is supported on the side wall of the drive hole.
In some embodiments, the operating lever is provided with pressing plate on the operating side at the driving end, described to press
The surface area of pressing plate is more than the area of section of the operating lever.
Unmanned plane provided by the invention may be implemented by the mating connection of the socket on the contact pin and fuselage on holder
Holder and unmanned aerial vehicle body are detachably connected, plug-in type design, simple in structure, easy to operate, only need to towards or deviate from
The direction grafting of the fuselage of unmanned plane, drawing holder, can be such that holder is connected or separated with fuselage so that user can quickly slap
Hold and complete the installation and removal of holder.
Description of the drawings
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below
There is attached drawing needed in technology description to be briefly described, it should be apparent that, the accompanying drawings in the following description is this hair
Some bright embodiments for those of ordinary skill in the art without creative efforts, can be with root
Other attached drawings are obtained according to these attached drawings.
Fig. 1 is the dimensional structure diagram for the unmanned plane that the one of embodiment of the present invention provides；
Fig. 2 is the structural schematic diagram of positioning region in unmanned plane shown in Fig. 1；
Fig. 3 is the structural schematic diagram of locking device in unmanned plane shown in Fig. 1；
Fig. 4 is the structural schematic diagram of locking device in the unmanned plane that another embodiment of the present invention provides；
Fig. 5 is the structural schematic diagram of locking device in the unmanned plane that yet another embodiment of the invention provides.
Reference sign：
1, unmanned plane；
10, fuselage；
11, horn；
12, Power Component；
13, motor；
14, propeller；
20, holder；
30, positioning region；
40, clip-connecting rod；
50, first attracts part；
60, second attracts part；
70, clamping block；
80, bolt；
90, operating lever；
101, mounting plate；
301, cylinder；
302, guide part；
401, fixture block；
701, the second guide surface；
801, the first stopper section；
802, Lock spring；
901, inclined-plane；
902, pressing plate；
1011, card hole；
1012, the second stopper section；
1013, lock slots；
4011, stop surface；
4012, the first guide surface.
Specific implementation mode
In order to make the object, technical scheme and advantages of the embodiment of the invention clearer, below in conjunction with the embodiment of the present invention
In attached drawing, technical scheme in the embodiment of the invention is clearly and completely described, it is clear that described embodiment is
A part of the embodiment of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, those of ordinary skill in the art
The every other embodiment obtained without creative efforts, shall fall within the protection scope of the present invention.
Fig. 1 is the dimensional structure diagram for the unmanned plane that the one of embodiment of the present invention provides；Fig. 2 is nothing shown in Fig. 1
The structural schematic diagram of man-machine middle positioning region；Fig. 3 is the structural schematic diagram of locking device in unmanned plane shown in Fig. 1；Fig. 4 is the present invention
The structural schematic diagram of locking device in the unmanned plane that another embodiment provides；Fig. 5 be yet another embodiment of the invention provide nobody
The structural schematic diagram of locking device in machine.
Fig. 1 is please referred to, for a kind of structural schematic diagram for unmanned plane that the one of embodiment of the present invention provides.The unmanned plane
1 structure includes 10, four horns 11 extended from fuselage 10 of fuselage and the power packages being respectively installed on each horn 11
Part 12.That is, the unmanned plane 1 of the present invention is quadrotor drone, the quantity of Power Component 12 is four.In other possible implementations
In example, unmanned plane 1 can be the rotor wing unmanned aerial vehicle of other any suitable types, such as DCB Specimen unmanned plane, six rotor wing unmanned aerial vehicles
Deng.It is applied to the occasion of other types unmanned plane in Power Component 12, the quantity of Power Component 13 can change according to actual needs
Become, the embodiment of the present invention is not construed as limiting this.
In the present embodiment, unmanned plane 1 can also include holder 20 as shown in Figure 2, which is installed on fuselage 10
Bottom, holder 20 for carry high-definition digital camera or other photographic devices with eliminate high-definition digital camera or other camera shooting fill
The disturbance being subject to is set, ensures the steady and audible of the video that camera or other photographic devices are shot.
In one embodiment of this invention, horn 11 is fixedly connected with fuselage 10, it is preferable that horn 11 and 10 one of fuselage
Molding.In other possible embodiments, horn 11 can by can relative to fuselage 10 be unfolded or fold in a manner of with fuselage 10
It is connected.For example, horn 11 can be connected by a rotating shaft mechanism with fuselage 10, to realize expansion of the horn 11 relative to fuselage 10
Or it folds.
In an embodiment of the present invention, Power Component 12 includes motor 13 and the propeller 14 driven by motor 13, spiral
Paddle 14 is installed on the output shaft of motor 13, and propeller 14 is rotated to produce under the driving of motor 13 makes the flight of unmanned plane 1
Lift or thrust.Motor 13 can be the motor of any suitable type, such as brush motor, brushless motor, direct current generator, stepping
Motor, AC induction motor etc..The Power Component 12 of the present invention further includes being arranged to be formed by cavity in fuselage 10 or horn 11
Interior electron speed regulator (not shown), the electron speed regulator are used to be believed according to the throttle that throttle control or throttle generator generate
Number generate for control the motor control signal of motor speed with obtain unmanned plane needs flying speed or flight attitude.
In one implementation, throttle control or throttle generator can be the flight control modules of unmanned plane.Fly
Row control module perceives the environment around unmanned plane by various sensors, and controls the flight of unmanned plane.Flight control modules
Can be processing module (processing unit), application-specific integrated circuit (Application Specific Integrated
Circuit, ASIC) or field programmable gate array (Field Programmable Gate Array, FPGA).
When instruction of the user by the flight attitude of remote controler input control unmanned plane etc., the winged control module of unmanned plane to
Electric tuned plate sends a throttle signal, and electric tuned plate receives the throttle signal, generate and sent to motor for being started to motor,
With the motor control signal of the rotating speed of control motor operation etc..
Please refer to Fig. 2-Fig. 5.The present embodiment provides the fuselage 1 of unmanned plane 1 be equipped with socket, holder 2 be equipped with it is described
The holder to be connected to the contact pin and locking device of the fuselage 10 by socket cooperation, and the locking device is for preventing machine
Body 10 is detached with holder 20.It is additionally provided with positioning region 30 on holder 20, is additionally provided on fuselage 10 and determines with what positioning region 30 coordinated
Position hole, the positioning region 30 is threaded through in location hole, so that contact pin face socket.
Specifically, connector is additionally provided on holder 20, contact pin is arranged on the connectors, is installed on contact pin and holder 20
Image acquisition equipment is electrically connected, and image acquisition equipment can be video camera or camera etc.；It is provided on fuselage 10 for controlling
The slave computer of unmanned plane processed operation, slave computer can the 10 each electrical work in inside of fuselage in order to control microcontroller etc.；Socket is under
Position mechatronics；Contact pin is plugged in socket, to realize being electrically connected between image acquisition equipment and slave computer；Slave computer also with
Hand-held remote controller is wirelessly connected, and such operating personnel can control image acquisition equipment by hand-held remote controller, needed for acquisition
Image.
Specifically, in the present embodiment, the shape of positioning region 30 can there are many, as long as enough with location hole cooperation, so as to
When holder 20 is installed, the relative position between holder 20 and fuselage 10 is limited so that contact pin can be with face socket, Jin Er
While locking device locks fuselage 10 and holder 20, contact pin is inserted into socket.
Preferably, positioning region 30 can be in the regular shapes such as coniform either pyramid-shaped or positioning region 30 in him not
The shape of regular shape, corresponding location hole is identical as the shape of positioning region 30, in wearing location hole in positioning region 30
Afterwards, it can prevent holder 20 that opposite slide occurs with fuselage 10.
Specifically, the material of the positioning region 30 in the present embodiment can there are many, such as：Positioning region 30 can mainly by
The metal materials such as copper, iron, aluminium are constituted or positioning region 30 is mainly made of non-metallic materials such as plastics.
Specifically, the connection type between the positioning region 30 in the present embodiment and holder 20 can there are many, such as：Positioning
Can be integrally formed by way of being molded and either casting between portion 30 and holder 20 or positioning region 30 and holder 20 between lead to
The mode for being bolted or welding is crossed to connect.
In the present embodiment, locking device can there are many, as long as holder 20 and fuselage 10 can be prevented to be detached from；Example
Such as：Locking device may include lock screw, and mounting hole is provided on holder 20, and screw hole is provided on fuselage 10, lock
Determine screw with screw hole to coordinate after the mounting hole, to prevent holder 20 from being detached from fuselage 10, realize holder 20 and fuselage 10 it
Between locking.
Specifically, the installation process of unmanned plane provided in this embodiment is：Positioning region 30 is penetrated in location hole first, this
When contact pin face socket；Continue that positioning region 30 is driven to move into location hole later, in the process, contact pin on holder 20 by
It is gradually plugged in the socket on fuselage 10；Holder 20 and fuselage 10 are locked by locking device later, and then prevent holder 20
It is detached with fuselage 10, to realize the connection between holder 20 and fuselage 10.
Unmanned plane provided in this embodiment can by the mating connection of contact pin and the socket on fuselage 10 on holder 20
To realize being detachably connected for holder 20 and the fuselage 10 of unmanned plane 1, plug-in type design is simple in structure, easy to operate, only needs
To towards or away from the direction grafting of fuselage of unmanned plane, drawing holder, holder can be made to be connected or separated with fuselage so as to use
Family can quickly grasp and complete the installation and removal of holder.Further, positioning region 30 is set on holder 20, on fuselage 10
Be provided with the location hole coordinated with positioning region 30, positioning region 30 is threaded through in location hole, and locking device prevent holder 20 with
Fuselage 10 detaches；Positioning region 30 coordinates with location hole, can limit the relative position between holder 20 and fuselage 10, and then make cloud
The socket on contact pin face fuselage 10 on platform 20, contact pin can be accurately plugged on socket, to realize image acquisition equipment
Being electrically connected between slave computer.
In other embodiments, positioning region 30 can be arranged on fuselage 10, and corresponding location hole is arranged on holder 20,
When installation, location hole need to be only located to the outside of positioning region 30, so that positioning region 30 is threaded through in location hole；To limit holder
Relative position between 20 and fuselage 10；Holder 20 and fuselage 10 are locked by locking device again, to prevent holder 20 and machine
Body 10 detaches.
With continued reference to Fig. 2.Specifically, positioning region 30 includes cylinder 301 and is arranged guide part in 301 end of cylinder
302, guide part 302 is in coniform, and the larger end face of 302 area of section of guide part is connect with 301 end of cylinder.Due to cylinder
301 terminus area is larger, at this time merely wears cylinder 301 into more difficult in location hole；Deviate from holder 20 in cylinder 301
End setting be in coniform guide part 302, guide part 302 is easier to insert into location hole, the promotion of backward fuselage 10
Holder 20, you can make cylinder 301 penetrate into location hole, in order to the connection between positioning region 30 and location hole.
Specifically, the section of the present embodiment middle column body 301 can be rounded；In order to enhance the locating effect of cylinder 301, column
The section of body 301 can also rectangular, triangle etc. it is non-circular, corresponding location hole is identical as the cross sectional shape of cylinder 301, with
Just when cylinder 301 to be threaded through in location hole, location hole prevents cylinder 301 from rotating.
Preferably, it can be connected by welding between guide part 302 and cylinder 301 or guide part 302 and column
It is integrally formed by way of casting or being molded between body 301.
It is further preferred that the bottom of location hole is provided with the conical surface coordinated with guide part 302.The conical surface and guide part 302
Cooperation, can play the role of self-centering, and then enhance the positional precision between positioning region 30 and location hole, to improve positioning region
30 locating effect.It should be noted that the rational position of the setting conical surface, with when the conical surface and guide part 302 contact, contact pin
It is plugged in socket completely.
With continued reference to Fig. 2.Specifically, positioning region 30 is multiple, the setting that multiple positioning regions 30 are spaced.To further increase
The locating effect of positioning region 30, in order to avoid holder 20 is rotated relative to fuselage 10, caused contact pin is unable to face socket.The present embodiment
Preferably, cylinder 301 is two, and connector is arranged between two cylinders 301.
Specifically, the installation process of unmanned plane is：Guide part 302 is penetrated in location hole first, backward fuselage 10 push away
Dynamic holder 20, so that tapered guide part 302 is bonded with the conical surface in location hole；In the process, the contact pin on holder 20
Gradually it is plugged in the socket on fuselage 10；Holder 20 and fuselage 10 are locked by locking device later, and then prevent holder
20 detach with fuselage 10, to realize the connection between holder 20 and fuselage 10.
With continued reference to Fig. 3.Specifically, locking device includes the clip-connecting rod 40 being arranged on holder 20, is set on clip-connecting rod 40
It is equipped with fixture block 401, clamping portion is provided on fuselage 10, fixture block 401 is clamped with clamping portion.It is realized to holder by way of clamping
Locking between 20 and fuselage 10, it is easy for installation and quick.
Preferably, recess is formed with groove on fuselage 10, and clamping portion is the card slot formed on the side wall of groove, by card
It connects column 40 to be threaded through in groove, and fixture block 401 is made to be fastened in card slot, the clamping of fixture block 401 and clamping portion may be implemented；Or
There is the card access surface being arranged with 40 centerline parallel of clip-connecting rod, clamping portion is the protrusion formed in card access surface on person's fuselage 10
Portion, fixture block 401 are supported in card access surface, are pushed holder 20 to fuselage 10, so that fixture block 401 crosses protrusion, and then are fastened on
The side for deviating from holder 20 on protrusion, can also realize the clamping of fixture block 401 and clamping portion.
With continued reference to Fig. 3.Specifically, it is in mounting plate to have horizontally disposed mounting plate 101, clamping portion on fuselage 10
The card hole 1011 being arranged on 101, and card hole 1011 runs through mounting plate 101；Stop surface 4011, clip-connecting rod are provided on fixture block 401
40 stretch into card hole 1011 by the bottom surface on mounting plate 101 towards ground, and stop surface 4011 is supported and deviates from bottom on mounting plate 101
On the top surface in face.Clip-connecting rod 40 is arranged inside card hole 1011, in order to avoid external object is contacted with clip-connecting rod 40, leads to fixture block 401
With shackle portion from and then making holder 20 and fuselage 10 be detached from and lock.
Preferably, stop surface 4011 and the top surface of mounting plate 101 are arranged in parallel, with improve fixture block 401 and mounting plate 101 it
Between bonding strength, in order to avoid the top surface of fixture block 401 and mounting plate 101 is detached from.
With continued reference to Fig. 3.Specifically, it is additionally provided with the first guide surface 4012 on fixture block 401, the first guide surface 4012 is to card
The side wall that column 40 extends away from the end of holder 20 and gradually deviates from card hole 1011 is connect, the first guide surface 4012 is used for clip-connecting rod
40 are oriented to.In order to which clip-connecting rod 40 is extend into card hole 1011, facilitate the installation of clip-connecting rod 40.
With continued reference to Fig. 3.Preferably, clip-connecting rod 40 is multiple, and fixture block 401, fuselage are both provided on each clip-connecting rod 40
Multiple clamping portions are provided on 10, each fixture block 401 and a clamping portion are clamped.Multiple clip-connecting rods 40 can enhance holder 20 with
Bonding strength between fuselage 10.
Preferably, each two clip-connecting rod 40 is oppositely arranged the present embodiment, is had in corresponding card hole 1011 and is oppositely arranged two
A side wall, two clip-connecting rods 40 being oppositely arranged are threaded through in same card hole 1011, and are supported respectively on different side walls.
Specifically, the installation process of unmanned plane is：Guide part 302 is penetrated in location hole first, backward fuselage 10 push away
Dynamic holder 20, in the process, the contact pin on holder 20 is gradually plugged in the socket on fuselage 10, and on clip-connecting rod 40
First guide surface 4012 is contacted with the side wall of card hole 1011, and elastic deformation occurs for clip-connecting rod 40, and clip-connecting rod 40 enters card hole
In 1011；When tapered guide part 302 is bonded with the conical surface in location hole, the stop surface 4011 on fixture block 401 is just worn
Card hole 1011 is crossed, the stop surface 4011 on fixture block 401 is supported on the top surface of mounting plate 101, and in addition contact pin is completely inserted into slotting
In seat, and then realize the installation between holder 20 and fuselage 10.
With continued reference to Fig. 4.Specifically, locking device includes that the first attraction part 50 and second attracts part 60, and first attracts
Part 50 is arranged on holder 20, and second attracts part 60 to be arranged on fuselage 10；First attracts part 50 and/or second that part 60 is attracted to have
It is magnetic, the first attraction part 50 and second attracts part 60 to attract each other.Between attracting part 50 and second to attract part 60 by first
Attraction realize locking between holder 20 and fuselage 10, facilitate the dismounting between holder 20 and fuselage 10.
Specifically, in the present embodiment first attract part 50 can there are many, such as：First attracts part 50 for magnet, phase
The the second attraction part 60 answered can be the metal, such as iron, cobalt, nickel etc. that can be attracted by magnet；Or first attract part 50 by
Magnetic material is constituted, such as：The metal that iron, cobalt, nickel etc. can be attracted by magnet, second attracts part 60 excellent for magnet the present embodiment
Selection of land, first, which attracts part 50 and second to attract part 60, is magnet, needs to ensure that first attracts part 50 towards second to attract at this time
The magnetism of 60 one end of part with second attract magnetism that part 60 attracts part 50 one end towards first on the contrary, so as to by holder 20 lean on into
When fuselage 10, the first attraction part 50 and second attracts part 60 to attract each other.
Specifically, the first attraction part 50 can be arranged in holder 20 towards on the side of fuselage 10, and corresponding second attracts
Part 60 is arranged on fuselage 10 on the side for attracting 50 face of part with first, and when by holder 20 close to fuselage 10, second attracts
Part 60 attracts first to attract part 50, and during holder 20 is close to fuselage 10, attraction gradually increases；When positioning region 30
Be threaded through in location hole, and when the contact pin on holder 20 is completely inserted into the socket on fuselage 10, first attract part 50 with
Second attracts part 60 to contact, and then realizes the connection between holder 20 and fuselage 10.
Preferably, holder 20 is internally provided with accommodating chamber to the present embodiment, and first attracts part 50 to be arranged inside accommodating chamber,
And accommodating chamber is attached to towards on the side wall of fuselage 10；Correspondingly, mounting plate 101 is provided on fuselage 10,101 direction of mounting plate
Holder 20 is arranged, and card hole 1011 is arranged on mounting plate 101；Second attracts the setting of part 60 to deviate from holder in mounting plate 101
On 20 side.Further, internally recess forms fluted, the second suction on the side in mounting plate 101 away from holder 20
Draw part 60 to be arranged in groove.
Specifically, the installation process of unmanned plane is：Guide part 302 is penetrated in location hole first, backward fuselage 10 push away
Holder 20 is moved, the contact pin on holder 20 is gradually plugged in the socket on fuselage 10, and first attracts part 50 and second to attract
Attraction between part 60 gradually increases；When tapered guide part 302 is bonded with the conical surface in location hole, contact pin is inserted completely
Enter into socket, and then realize the installation between holder 20 and fuselage 10, between first attracts part 50 and second to attract part 60
Attraction under the action of holder 20 will not be detached with fuselage 10.When dismounting, need to only support or oppose the direction drawing holder of body 10 of disembarking
20, and then holder 20 is made to be detached with fuselage 10, at the same time contact pin is detached with socket and cylinder 301 in location hole by extracting,
Realize holder 20 and fuselage 10 and between dismounting.
With continued reference to Fig. 5.Specifically, locking device includes：The clamping block 70 being arranged on holder is provided on clamping block
Slot；It is provided with lock slots 1013 on fuselage 10 and is through to the jack of lock slots 1013；Clamping block 70 is accommodated in lock slots
In 1013, bolt 80 is plugged in jack and in slot.Clamping block 70 is locked in lock slots 1013 by bolt 80,
And then locking of the realization to holder 20 and fuselage 10, locking are more firm.
Preferably, the mounting plate 101 for location hole to be arranged, the center of jack is arranged on fuselage 10 in lock slots 1013
The side wall of line and lock slots 1013 is vertically arranged, also, jack runs through mounting plate 101；Further, clamping block is reasonably set
The position of slot on 70, it is ensured that in the cone being threaded through positioning region 30 in location hole and in guide part 302 and location hole
When face paste is closed, slot face jack, and then bolt 80 is threaded through in jack, and bolt 80 is pushed to the inside of jack, into
And the end of bolt 80 is made to penetrate into slot, bolt 80 prevents clamping block 70 to the external mobile of lock slots 1013, to realize
Locking to holder 20 and fuselage 10.
It is further preferred that when the end for inserting bolt 80 is inserted into slot, the front end that need to protect bolt 80 is located at peace
The outside of loading board 101, so as to dismounting when, by the front end of drawing bolt 80 with by bolt 80 by being extracted in slot and jack,
So that clamping block 70 is detached from lock slots 1013, realizes the unlock to holder 20 and fuselage 10.
With continued reference to Fig. 5.Specifically, locking device further includes Lock spring 802, and the first stopper section is provided on bolt 80
801, the second stopper section 1012 is provided on fuselage 10, and the both ends of Lock spring 802 are stopped with the first stopper section 801 and second respectively
Stopper 1012 connects；Lock spring 802 is for driving movement of the bolt 80 into lock slots 1013.In slot face jack,
Bolt 80 is threaded through in slot automatically under the driving of Lock spring 802, completes locking to holder 20 and fuselage 10, when installation
It is easy for installation and quick without operating bolt 80.
Preferably, Lock spring 802 can be helical spring, and bolt 80 is threaded through in Lock spring 802；First stopper section
801 can be the annular flange formed on bolt 80 or the first stopper section 801 is the protrusion formed on 80 side wall of bolt
Portion；It is arranged on the first protrusion towards the first protrusion, jack is formed on the bottom surface of holder 20 in mounting plate 101, the
On the outside of the one protrusion and position of face jack is formed with the second protrusion, and the second protrusion is the second stopper section 1012；The
Between the first protrusion and the second protrusion, the both ends of Lock spring 802 are supported respectively in the second protrusion for one stopper section 801
In portion and the first stopper section 801, and then under the effect of the elastic force of Lock spring 802, driving bolt 80 is moved into slot.
Or Lock spring 802 is torsional spring, at this time only need to be supported at the both ends of torsional spring respectively in the first stopper section 801 and the
On two stopper sections 1012, you can driving bolt 80 penetrates into slot under the elastic force effect of torsional spring.
Preferably, the second guide surface 701 is provided on clamping block 70, the second guide surface 701 deviates from cloud by clamping block 70
The tip forward end of platform 20 extends, and moves closer to side wall of the lock slots 1013 with jack, to be plugged by clamping block 70
During in lock slots 1013, bolt 80 is slided towards one end of lock slots 1013 on the second guide surface 701, in order to avoid insert
Pin 80 supports the end of clamping block 70, causes clamping block 70 that cannot be inserted into lock slots 1013.It should be noted that rational
The length of bolt 80 is set, to ensure when clamping block 70 to be threaded through in lock slots 1013, the second guide surface 701 first with insert
Pin 80 contacts, in order to avoid bolt 80 is long, bolt 80 is supported in the end of clamping block 70, and then clamping block 70 is hindered to enter locking
In slot 1013.
With continued reference to Fig. 5.Specifically, locking device further includes operating lever 90, and slide opening, operating lever 90 are provided on fuselage 10
Driving end be threaded through in slide opening, driving end be provided with inclined-plane 901；The driving portion coordinated with inclined-plane 901 is provided on bolt 80,
With in the pressing operation bar 90 into slide opening, driving portion is supported to drive bolt 80 to be moved to the external of lock slots 1013 in inclined-plane 901
It is dynamic.The disengaging to bolt 80 and slot can be realized by pressing operation bar 90, and then realize the solution to holder 20 and fuselage 10
Lock is convenient for the dismounting of holder 20.
Preferably, the center line of slide opening and the central axis of bolt 80 are arranged；The one end of operating lever 90 away from driving end
With operating side, inclined-plane 901 towards operating side one end compared with one end away from operating side further from lock slots 1013, grasping in this way
When making bar 90 and being moved to the inside of slide opening, inclined-plane 901 can drive bolt 80 to be moved to away from the direction of lock slots 1013, in turn
Bolt 80 is set to be detached from the slot on clamping block 70；After clamping block 70 is taken out by lock slots 1013 are interior, operating lever 90 is discharged,
So that bolt 80 is moved into lock slots 1013 under the driving of Lock spring 802, at the same time driving portion supports inclined-plane 901, into
And drive operating lever 90 by being stretched out in slide opening.
Specifically, in the present embodiment driving portion can there are many, such as：Driving portion can be to be arranged on 80 side wall of bolt
Protrusion, protrusion supports on inclined-plane 901.Preferably, driving portion includes the drive hole being arranged on bolt 80 to the present embodiment, is driven
Moved end is threaded through in drive hole, and inclined-plane 901 is supported on the side wall of drive hole.Motion arm is threaded through in drive hole, in order to avoid in nothing
Motion arm moves when man-machine work, and then causes inclined-plane 901 that cannot be contacted with driving portion.
With continued reference to Fig. 5.Preferably, operating lever 90 is provided with pressing plate 902, pressing plate on the operating side at driving end
902 surface area is more than the area of section of operating lever 90.Pressing plate 902 can increase the contact surface between operating personnel's hand
Product, and then improve the comfort of pressing operation bar 90.
Specifically, the installation process of unmanned plane is：Guide part 302 is penetrated in location hole first, backward fuselage 10 push away
Dynamic holder 20, makes cylinder 301 be threaded through in location hole, and the contact pin on holder 20 is also gradually plugged in the socket on fuselage 10,
At the same time clamping block 70 progresses into lock slots 1013；When the conical surface in tapered guide part 302 and location hole pastes
When conjunction, contact pin is completely inserted into socket, and the slot face jack on clamping block 70, is made in the elastic force of Lock spring 802
Under, bolt 80 is moved into lock slots 1013 and the end of bolt 80 is threaded through in slot, and bolt 80 can prevent clamping block 70
To the external mobile of lock slots 1013, and then realize the locking to holder 20 and fuselage 10.
When dismounting, pressing plate 902 on pressing operation bar 90, so that operating lever 90 is moved to the inside of slide opening, at the same time
The side wall of drive hole is supported on inclined-plane 901, with drive bolt 80 to away from the direction of lock slots 1013 move so that bolt 80 with insert
Slot is detached from, and then realizes locking to clamping block 70, the direction drawing holder 20 of body 10 of disembarking of supporting or opposing later, you can make cylinder
301 are detached from location hole, and at the same time contact pin is detached from socket, to realize the dismounting between holder 20 and fuselage 10.
Unmanned plane provided by the invention may be implemented by the mating connection of the socket on the contact pin and fuselage on holder
Holder and unmanned aerial vehicle body are detachably connected, plug-in type design, simple in structure, easy to operate, only need to towards or deviate from
The direction grafting of the fuselage of unmanned plane, drawing holder, can be such that holder is connected or separated with fuselage so that user can quickly slap
Hold and complete the installation and removal of holder.
In the present invention, unless otherwise specific regulation, the terms such as term " installation ", " connected ", " connection ", " fixation " are answered
It is interpreted broadly, can also be dismountable connection for example, it may be being fixedly connected, or be integrally formed, can be that machinery connects
It connects, can also be to be electrically connected or can communicate each other；It can be directly connected, can also be indirectly connected with by intermediate medium, it can
To be the interaction relationship of connection or two elements inside two elements, unless otherwise restricted clearly.For ability
For the those of ordinary skill in domain, the specific meanings of the above terms in the present invention can be understood according to specific conditions.
Finally it should be noted that：The above embodiments are only used to illustrate the technical solution of the present invention., rather than its limitations；To the greatest extent
Present invention has been described in detail with reference to the aforementioned embodiments for pipe, it will be understood by those of ordinary skill in the art that：Its according to
So can with technical scheme described in the above embodiments is modified, either to which part or all technical features into
Row equivalent replacement；And these modifications or replacements, various embodiments of the present invention technology that it does not separate the essence of the corresponding technical solution
The range of scheme.
Claims (16)
1. a kind of unmanned plane, which is characterized in that including：
Fuselage, the fuselage are equipped with socket；
Holder, the holder, which is equipped with, to be coordinated with the socket the holder to be connected to the contact pin of the fuselage；And
Locking device, the locking device is for preventing the fuselage from being detached with the holder.
2. unmanned plane according to claim 1, which is characterized in that be additionally provided with positioning region, the fuselage on the holder
On be additionally provided with the location hole coordinated with the positioning region, the positioning region is threaded through in the location hole, so that the contact pin
Socket described in face.
3. unmanned plane according to claim 2, which is characterized in that the positioning region includes cylinder and is arranged in the column
The guide part of body end, the guide part is in coniform, and the larger end face of the guide part area of section and the cylinder are last
End connection.
4. unmanned plane according to claim 3, which is characterized in that the bottom of the location hole is provided with and the guide part
The conical surface of cooperation.
5. according to claim 2-4 any one of them unmanned planes, which is characterized in that the positioning region be it is multiple, it is multiple described
The setting at positioning region interval.
6. according to claim 1-5 any one of them unmanned planes, which is characterized in that the locking device includes being arranged described
Clip-connecting rod on holder is provided with fixture block on the clip-connecting rod, and clamping portion, the fixture block and the card are provided on the fuselage
Socket part is clamped.
7. unmanned plane according to claim 6, which is characterized in that have horizontally disposed mounting plate, institute on the fuselage
It is the card hole being arranged on the mounting plate to state clamping portion, and the card hole runs through the mounting plate；It is provided on the fixture block
Stop surface, the clip-connecting rod stretches into the card hole by the bottom surface on the mounting plate towards ground, and the stop surface is supported
On the mounting plate on the top surface of the bottom surface.
8. unmanned plane according to claim 7, which is characterized in that the first guide surface is additionally provided on the fixture block, it is described
First guiding deviates from the end extension of the holder towards the clip-connecting rod and gradually deviates from the side wall of the card hole, and described first
Guide surface is for being oriented to the clip-connecting rod.
9. according to claim 6-8 any one of them unmanned planes, which is characterized in that the clip-connecting rod be it is multiple, it is each described
It is both provided with the fixture block on clip-connecting rod, multiple clamping portions, each fixture block and an institute are provided on the fuselage
State clamping portion clamping.
10. according to claim 1-9 any one of them unmanned planes, which is characterized in that the locking device includes the first attraction
Part and the second attraction part, described first attracts part to be arranged on the holder, and described second attracts part to be arranged in the fuselage
On；Described first attracts part and/or the second attraction part to have magnetism, and described first attracts part and described second to attract part mutual
Mutually attract.
11. unmanned plane according to claim 10, which is characterized in that described first attracts part and described second to attract part equal
For magnet.
12. according to claim 1-11 any one of them unmanned planes, which is characterized in that the locking device includes：Setting exists
Clamping block on the holder is provided with slot on the clamping block；It is provided with lock slots on the fuselage and is through to described
The jack of lock slots；The clamping block is accommodated in the lock slots, and bolt is plugged in the jack and the slot.
13. unmanned plane according to claim 12, which is characterized in that the locking device further includes Lock spring, described
Be provided with the first stopper section on bolt, be provided with the second stopper section on the fuselage, the both ends of the Lock spring respectively with institute
The first stopper section is stated to connect with second stopper section；The Lock spring is for driving the bolt into the lock slots
It is mobile.
14. unmanned plane according to claim 12 or 13, which is characterized in that the locking device further includes operating lever, institute
It states and is provided with slide opening on fuselage, the driving end of the operating lever is threaded through in the slide opening, and the driving end is provided with inclined-plane；Institute
State the driving portion for being provided on bolt and coordinating with the inclined-plane, with when pressing the operating lever into the slide opening, it is described tiltedly
The driving portion is supported to drive the bolt to the external mobile of the lock slots in face.
15. unmanned plane according to claim 14, which is characterized in that the driving portion includes being arranged on the bolt
Drive hole, the driving end is threaded through in the drive hole, and the inclined-plane is supported on the side wall of the drive hole.
16. the unmanned plane according to claims 14 or 15, which is characterized in that behaviour of the operating lever away from the driving end
Make to be provided with pressing plate on end, the surface area of the pressing plate is more than the area of section of the operating lever.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810912174.3A CN108750132A (en) | 2018-08-10 | 2018-08-10 | Unmanned plane |
| PCT/CN2019/100038 WO2020030133A1 (en) | 2018-08-10 | 2019-08-09 | Unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810912174.3A CN108750132A (en) | 2018-08-10 | 2018-08-10 | Unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108750132A true CN108750132A (en) | 2018-11-06 |
Family
ID=63969685
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810912174.3A Pending CN108750132A (en) | 2018-08-10 | 2018-08-10 | Unmanned plane |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN108750132A (en) |
| WO (1) | WO2020030133A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020030133A1 (en) * | 2018-08-10 | 2020-02-13 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH09171852A (en) * | 1995-10-19 | 1997-06-30 | Japan Aviation Electron Ind Ltd | Multi-conductor connector driving mechanism |
| US20110049288A1 (en) * | 2008-08-21 | 2011-03-03 | Satoshi Suzuki | Unmanned aircraft system and operation method thereof |
| WO2012163249A1 (en) * | 2011-05-27 | 2012-12-06 | Wang Jun | Goods access locking device |
| CN205098486U (en) * | 2015-10-13 | 2016-03-23 | 深圳一电科技有限公司 | Unmanned aerial vehicle |
| CN105539872A (en) * | 2016-01-29 | 2016-05-04 | 北京小米移动软件有限公司 | Pan-tilt of unmanned aerial vehicle and bearing support of pan-tilt |
| CN106794902A (en) * | 2016-10-18 | 2017-05-31 | 深圳市大疆灵眸科技有限公司 | Attachment means and the unmanned plane with the attachment means |
| WO2018076347A1 (en) * | 2016-10-31 | 2018-05-03 | 深圳一电航空技术有限公司 | Unmanned aerial vehicle for aerial photography |
| CN108092088A (en) * | 2017-08-02 | 2018-05-29 | 广州天品科技有限公司 | A kind of electric power connector system of automatic spring |
| WO2018113202A1 (en) * | 2016-12-23 | 2018-06-28 | 深圳市道通智能航空技术有限公司 | Detachable pan-tilt connection device and unmanned aerial vehicle |
| CN208963327U (en) * | 2018-08-10 | 2019-06-11 | 深圳市道通智能航空技术有限公司 | Unmanned plane |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9738380B2 (en) * | 2015-03-16 | 2017-08-22 | XCraft Enterprises, LLC | Unmanned aerial vehicle with detachable computing device |
| CN105620777A (en) * | 2016-02-26 | 2016-06-01 | 深圳行天者创新技术有限公司 | Unmanned aerial vehicle with detachable cradle head |
| CN205707397U (en) * | 2016-02-26 | 2016-11-23 | 深圳行天者创新技术有限公司 | A kind of dismountable unmanned plane of The Cloud Terrace |
| CN108750132A (en) * | 2018-08-10 | 2018-11-06 | 深圳市道通智能航空技术有限公司 | Unmanned plane |
-
2018
- 2018-08-10 CN CN201810912174.3A patent/CN108750132A/en active Pending
-
2019
- 2019-08-09 WO PCT/CN2019/100038 patent/WO2020030133A1/en active Application Filing
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH09171852A (en) * | 1995-10-19 | 1997-06-30 | Japan Aviation Electron Ind Ltd | Multi-conductor connector driving mechanism |
| US20110049288A1 (en) * | 2008-08-21 | 2011-03-03 | Satoshi Suzuki | Unmanned aircraft system and operation method thereof |
| WO2012163249A1 (en) * | 2011-05-27 | 2012-12-06 | Wang Jun | Goods access locking device |
| CN205098486U (en) * | 2015-10-13 | 2016-03-23 | 深圳一电科技有限公司 | Unmanned aerial vehicle |
| CN105539872A (en) * | 2016-01-29 | 2016-05-04 | 北京小米移动软件有限公司 | Pan-tilt of unmanned aerial vehicle and bearing support of pan-tilt |
| CN106794902A (en) * | 2016-10-18 | 2017-05-31 | 深圳市大疆灵眸科技有限公司 | Attachment means and the unmanned plane with the attachment means |
| WO2018076347A1 (en) * | 2016-10-31 | 2018-05-03 | 深圳一电航空技术有限公司 | Unmanned aerial vehicle for aerial photography |
| WO2018113202A1 (en) * | 2016-12-23 | 2018-06-28 | 深圳市道通智能航空技术有限公司 | Detachable pan-tilt connection device and unmanned aerial vehicle |
| CN108092088A (en) * | 2017-08-02 | 2018-05-29 | 广州天品科技有限公司 | A kind of electric power connector system of automatic spring |
| CN208963327U (en) * | 2018-08-10 | 2019-06-11 | 深圳市道通智能航空技术有限公司 | Unmanned plane |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020030133A1 (en) * | 2018-08-10 | 2020-02-13 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
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| Publication number | Publication date |
|---|---|
| WO2020030133A1 (en) | 2020-02-13 |
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