CN208963327U - Unmanned plane - Google Patents

Abstract

The utility model provides a kind of unmanned plane, comprising: fuselage, the fuselage are equipped with socket；Holder, the holder, which is equipped with, to be cooperated 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 separating with holder.Unmanned plane provided by the utility model, 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, plug-in type design, structure is simple, easy to operate, only need to be to towards or away from the direction grafting of fuselage of unmanned plane, drawing holder, holder can be made to connect or separate with fuselage, allow users to the installation and removal for quickly grasping and completing holder.

Description

Unmanned plane

Technical field

The utility model relates to air vehicle technique field more particularly to a kind of unmanned planes.

Background technique

The technology of taking photo by plane be widely used aeroplane photography, territory detection, in terms of；When taking photo by plane, often pass through Unmanned plane obtains required image；Unmanned plane includes: fuselage and the holder with shooting function, by the boat for controlling unmanned plane The image of the available needs of walking along the street line.

In the prior art, holder can be connected by way of being fixedly connected with the fuselage of unmanned plane；Quick Release can also be passed through 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.

Utility model content

In view of this, the present invention provides a kind of unmanned planes, to solve the quick-disassembly structure of the holder of existing unmanned plane Complicated, user is not easy the problem of grasping, and provides a kind of simple unmanned plane of structure, allows users to quickly grasp and complete cloud The installation and removal of platform.

The utility model provides a kind of unmanned plane, comprising: fuselage, the fuselage are equipped with socket；Holder, the holder are set Have and cooperates with the socket the holder to be connected to the contact pin of the fuselage；And locking device, the locking device are used It is separated in the prevention fuselage 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 the positioning hole, so that socket described in the contact pin face.

In some embodiments, the positioning region includes cylinder and the guide part that the post tips are arranged in, described Guide part is in coniform, and the biggish end face of 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 with guide part cooperation.

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 and the clamping portion are clamped.

In some embodiments, there is horizontally disposed mounting plate, the clamping portion is in the installation 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 protruded into the bottom surface for stating mounting plate towards ground, and the stop surface is supported on the mounting plate away from the bottom On the top surface in face.

In some embodiments, the first guide surface is additionally provided on the fixture block, first guiding is 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 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 are attracted each other.

In some embodiments, the first attraction part and the second attraction part are magnet.

In some embodiments, the locking device includes: the clamping block being arranged on the holder, on the clamping block It is 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 institute It states in 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 connection；The Lock spring is for driving movement of the bolt into the lock slots.

In some embodiments, the locking device further includes operating stick, 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 stick 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 stick is provided with pressing plate on the operating side at the driving end, described to press The surface area of pressing plate is greater than the area of section of the operating stick.

Unmanned plane provided by the utility model can be with by the mating connection of the socket on the contact pin and fuselage on holder Realize being detachably connected for holder and unmanned aerial vehicle body, plug-in type design, structure is simple, easy to operate, only need to towards or Direction grafting, drawing holder away from the fuselage of unmanned plane, can be such that holder connects or separates with fuselage, allow users to fast Speed is grasped and completes the installation and removal of holder.

Detailed description of the invention

In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is Some embodiments of the utility model, for those of ordinary skill in the art, without creative efforts, It is also possible to obtain other drawings based on these drawings.

Fig. 1 is the schematic perspective view for the unmanned plane that the one of embodiment of the utility model 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；

The structural schematic diagram of locking device in the unmanned plane that Fig. 4 provides for another embodiment of the utility model；

The structural schematic diagram of locking device in the unmanned plane that Fig. 5 provides for the utility model another embodiment.

Description of symbols:

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 stick；

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 embodiment

It is practical new below in conjunction with this to keep the objectives, technical solutions, and advantages of the embodiments of the present invention clearer Attached drawing in type embodiment, the technical scheme in the utility model embodiment is clearly and completely described, it is clear that is retouched The embodiment stated is the utility model a part of the embodiment, instead of all the embodiments.Based on the implementation in the utility model Example, every other embodiment obtained by those of ordinary skill in the art without making creative efforts belong to The range of the utility model protection.

Fig. 1 is the schematic perspective view for the unmanned plane that the one of embodiment of the utility model provides；Fig. 2 is Fig. 1 institute Show the structural schematic diagram of positioning region in unmanned plane；Fig. 3 is the structural schematic diagram of locking device in unmanned plane shown in Fig. 1；Fig. 4 is this The structural schematic diagram of locking device in the unmanned plane that another embodiment of utility model provides；Fig. 5 is that the utility model is further implemented The structural schematic diagram of locking device in the unmanned plane that example provides.

Fig. 1 is please referred to, for a kind of structural schematic diagram for unmanned plane that the one of embodiment of the utility model provides.The nothing Man-machine 1 structure includes 10, four, fuselage from the horn 11 of the extension of fuselage 10 and is respectively installed in dynamic on each horn 11 Power component 12.That is, the unmanned plane 1 of the utility model is quadrotor drone, the quantity of Power Component 12 is four.Other can In the embodiment of energy, unmanned plane 1 can be the rotor wing unmanned aerial vehicle of other any suitable types, such as DCB Specimen unmanned plane, six rotations Wing unmanned plane etc..It is applied to the occasion of other types unmanned plane in Power Component 12, the quantity of Power Component 13 can be according to reality Border needs to change, and the utility model embodiment 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 dress The disturbance being subject to is set, guarantees the steady and audible of the video of camera or the shooting of other photographic devices.

In an embodiment of the utility model, horn 11 is fixedly connected with fuselage 10, it is preferable that horn 11 and fuselage 10 It is integrally formed.In other possible embodiments, horn 11 can by can relative to fuselage 10 be unfolded or fold in a manner of and machine Body 10 is connected.For example, horn 11 can be connected by a rotating shaft mechanism with fuselage 10, to realize horn 11 relative to fuselage 10 Expansion folds.

In an embodiment of the utility model, Power Component 12 includes motor 13 and the propeller 14 driven by motor 13, Propeller 14 is installed on the output shaft of motor 13, and propeller 14 is rotated to produce under the driving of motor 13 flies unmanned plane 1 Capable lift or thrust.Motor 13 can be the motor of any suitable type, for example, brush motor, brushless motor, direct current generator, Stepper motor, AC induction motor etc..The Power Component 12 of the utility model further includes being arranged in 11 shapes of fuselage 10 or horn At cavity in electron speed regulator (not shown), which is used to be generated according to throttle control or throttle generator Throttle signal generate for controlling the motor control signal of motor speed with obtain unmanned plane needs flying speed or flight Posture.

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 It can be processing module (processing unit), specific integrated circuit (Application Specific Integrated Circuit, ASIC) or field programmable gate array (Field Programmable Gate Array, FPGA).

When instruction of the user by 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 send to motor for being started to motor, With the motor control signal of the revolving speed of control motor operation etc..

- Fig. 5 referring to figure 2..The present embodiment provides the fuselage 1 of unmanned plane 1 be equipped with socket, holder 2 be equipped with it is described Socket cooperates so that the holder to be connected to the contact pin and locking device of the fuselage 10, and the locking device is for preventing machine Body 10 is separated 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 cooperated Position hole, the positioning region 30 is threaded through positioning hole, so that contact pin face socket.

Specifically, connector is additionally provided on holder 20, contact pin is arranged on the connectors, installs on contact pin and holder 20 Image acquisition equipment electrical connection, image acquisition equipment can be for video camera or camera etc.；It is provided with and is used on fuselage 10 The slave computer of unmanned plane operation is controlled, slave computer can be the single-chip microcontroller etc. of the 10 each electrical work in inside of control fuselage；Socket with The next mechatronics；Contact pin is plugged in socket, to realize being electrically connected between image acquisition equipment and slave computer；Slave computer is also It is wirelessly connected with hand-held remote controller, such operator can control image acquisition equipment by hand-held remote controller, to obtain Need 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 in the regular shapes such as coniform perhaps 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, to wear in 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 perhaps 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, be provided with mounting hole on holder 20, and screw hole is provided on fuselage 10, lock Determine screw to cooperate with screw hole after the mounting hole, to prevent holder 20 and fuselage 10 from being detached from, realize holder 20 and fuselage 10 it Between locking.

Specifically, the installation process of unmanned plane provided in this embodiment are as follows: positioning region 30 is penetrated in location hole first, this When contact pin face socket；Continue to drive positioning region 30 mobile to positioning 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 separated 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 the socket on the contact pin and 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, structure is simple, 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 connect or separate with fuselage, so that with 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 cooperated with positioning region 30, positioning region 30 is threaded through positioning hole, and locking device prevent holder 20 with Fuselage 10 separates；Positioning region 30 and location hole cooperate, and can limit the relative position between holder 20 and fuselage 10, and then make The socket on contact pin face fuselage 10 on holder 20, contact pin can be accurately plugged on socket, to realize that image acquisition is set The standby electrical connection between slave computer.

In other embodiments, positioning region 30 can be set 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 positioning hole；To limit cloud Relative position between platform 20 and fuselage 10；Holder 20 and fuselage 10 are locked by locking device again, with prevent holder 20 and Fuselage 10 separates.

With continued reference to Fig. 2.Specifically, positioning region 30 includes cylinder 301 and the guide part that 301 end of cylinder is arranged in 302, guide part 302 is in coniform, and the biggish 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 more difficult into positioning hole；Deviate from holder in cylinder 301 20 end setting is in coniform guide part 302, and guide part 302 is easier to insert into positioning hole, backward fuselage 10 push away Dynamic holder 20, can make cylinder 301 penetrate into positioning 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 be non-circular in rectangle, triangle etc., and corresponding location hole is identical as the cross sectional shape of cylinder 301, with Just when cylinder 301 is threaded through positioning 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 cooperated with guide part 302.The conical surface and guide part 302 Cooperation, can play the role of self-centering, and then enhance the position precision between positioning region 30 and location hole, to improve positioning region 30 locating effect.It should be noted that the reasonable 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 are two, and connector is arranged between two cylinders 301.

Specifically, the installation process of unmanned plane are as follows: 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 of positioning hole；In the process, the contact pin on holder 20 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 separate 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 and clamping portion are clamped.It is realized by way of clamping to holder 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 is fastened on fixture block 401 in card slot, the clamping of fixture block 401 Yu 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 Yu clamping portion.

With continued reference to Fig. 3.Specifically, there is horizontally disposed mounting plate 101, clamping portion is in mounting plate 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 protrude into card hole 1011 by the bottom surface on mounting plate 101 towards ground, and stop surface 4011 is supported on mounting plate 101 bottom of away from 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 being detached from holder 20 and fuselage 10 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, is provided with fixture block 401, fuselage 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 be enhanced holder 20 with Bonding strength between fuselage 10.

Preferably, every 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 on different side walls respectively.

Specifically, the installation process of unmanned plane are as follows: 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 The first guide surface 4012 contacted with the side wall of card hole 1011, 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 of positioning 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 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 the second attraction part 60 to have It is magnetic, the first attraction part 50 and the second attraction part 60 are attracted each other.Part 50 and second is attracted to attract between part 60 by first Attraction realize to the 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 attract part 50 be magnet, phase It can be the metal, such as iron, cobalt, nickel etc. that can be attracted by magnet that second answered, which attracts part 60,；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, the first attraction part 50 and the second attraction part 60 are magnet, need to guarantee that the first attraction part 50 attracts towards second at this time 60 one end of part magnetism with second attract part 60 towards first attract 50 one end of part magnetism on the contrary, so as to by holder 20 lean on into When fuselage 10, the first attraction part 50 and the second attraction part 60 are attracted each other.

Specifically, the first attraction part 50 can be set in holder 20 towards on the side of fuselage 10, and corresponding second attracts Part 60 is arranged on the side for attracting 50 face of part on fuselage 10 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 is gradually increased；When positioning region 30 Be threaded through positioning 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 are as follows: 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 is gradually increased；When tapered guide part 302 is bonded with the conical surface of positioning hole, contact pin is inserted completely Enter into socket, and then realize the installation between holder 20 and fuselage 10, attracts part 50 and second to attract between part 60 first Attraction under the action of holder 20 will not be separated with fuselage 10.When disassembly, need to only support or oppose the direction drawing holder of body 10 of disembarking 20, and then separate holder 20 with fuselage 10, contact pin is separated with socket at the same time and cylinder 301 is extracted by positioning hole, Realize holder 20 and fuselage 10 and between disassembly.

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, it is more firm to lock.

Preferably, lock slots 1013 are arranged on fuselage 10 for the mounting plate 101 of location hole, the center of jack to be arranged 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 that positioning region 30 is threaded through to positioning hole and guide part 302 and positioning hole When face paste is closed, slot face jack, and then bolt 80 is threaded through in jack, and push bolt 80 to the inside of jack, into And penetrating into the end of bolt 80 in 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 the front end that need to protect bolt 80 is located at peace when the end for inserting bolt 80 is inserted into slot The outside of loading board 101, so as to disassembly when, by the front end of drawing bolt 80 with by bolt 80 by being extracted in slot and jack, It is detached from clamping block 70 and 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 protrusion formed on 80 side wall of bolt for the annular flange formed on bolt 80 or the first stopper section 801 Portion；It is arranged on the first protrusion in mounting plate 101 towards the first protrusion, jack is formed on the bottom surface of holder 20, 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 respectively the both ends of torsional spring in the first stopper section 801 and the On two stopper sections 1012, driving bolt 80 it can be penetrated into slot under the effect of the elastic force 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 the side wall that lock slots 1013 have jack, to plug by clamping block 70 During in lock slots 1013, bolt 80 slides on the second guide surface 701 towards one end of lock slots 1013, in order to avoid Bolt 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 rationally Setting bolt 80 length, to guarantee when clamping block 70 to be threaded through in lock slots 1013, the second guide surface 701 is first It is contacted with bolt 80, in order to avoid bolt 80 is too long, bolt 80 is supported in the end of clamping block 70, and then clamping block 70 is hindered to enter In lock slots 1013.

With continued reference to Fig. 5.Specifically, locking device further includes operating stick 90, and slide opening, operating stick 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 cooperated 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 move 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, convenient for the disassembly of holder 20.

Preferably, the central axis of the center line of slide opening and bolt 80 is arranged；The one end of operating stick 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 Make bar 90 to when the movement of the inside of slide opening, inclined-plane 901 can drive bolt 80 mobile to the direction for deviating from lock slots 1013, in turn It is detached from the slot on bolt 80 and clamping block 70；By clamping block 70 by lock slots 1013 take out after, discharge operating stick 90, So that bolt 80 is moved into lock slots 1013 under the driving of Lock spring 802, driving portion supports inclined-plane 901 at the same time, into And drive operating stick 90 by stretching out in slide opening.

Specifically, in the present embodiment driving portion can there are many, such as: driving portion can for 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 is mobile when man-machine work, and then causes inclined-plane 901 that cannot contact with driving portion.

With continued reference to Fig. 5.Preferably, operating stick 90 is provided with pressing plate 902 on the operating side at driving end, presses The surface area of plate 902 is greater than the area of section of operating stick 90.Pressing plate 902 can increase the contact between operator's hand Area, and then improve the comfort of pressing operation bar 90.

Specifically, the installation process of unmanned plane are as follows: guide part 302 is penetrated in location hole first, backward fuselage 10 push away Dynamic holder 20, makes cylinder 301 be threaded through positioning hole, and the contact pin on holder 20 is also gradually plugged in the socket on fuselage 10, Clamping block 70 progresses into lock slots 1013 at the same time；When the conical surface of tapered guide part 302 and positioning 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 realizes the locking to holder 20 and fuselage 10.

When disassembly, pressing plate 902 on pressing operation bar 90, so that operating stick 90 is mobile to the inside of slide opening, at the same time The side wall of drive hole is supported on inclined-plane 901, to drive bolt 80 mobile to the direction away from lock slots 1013 so that bolt 80 with Slot is detached from, and then realizes locking to clamping block 70, and the direction drawing holder 20 of body 10 of disembarking of supporting or opposing later can make cylinder 301 are detached from location hole, and contact pin and socket are detached from the same time, to realize the disassembly between holder 20 and fuselage 10.

Unmanned plane provided by the utility model can be with by the mating connection of the socket on the contact pin and fuselage on holder Realize being detachably connected for holder and unmanned aerial vehicle body, plug-in type design, structure is simple, easy to operate, only need to towards or Direction grafting, drawing holder away from the fuselage of unmanned plane, can be such that holder connects or separates with fuselage, allow users to fast Speed is grasped and completes the installation and removal of holder.

In the present invention, unless otherwise specific regulation, the arts such as term " installation ", " connected ", " connection ", " fixation " Language shall be understood in a broad sense, for example, it may be being fixedly connected, be also possible to removably connect, or be integrally formed, and can be machinery Connection is also possible 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 be the connection inside two elements or the interaction relationship of two elements, unless otherwise restricted clearly.For this For the those of ordinary skill in field, the concrete meaning of above-mentioned term in the present invention can be understood as the case may be.

Finally, it should be noted that the above various embodiments is only to illustrate the technical solution of the utility model, rather than it is limited System；Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should Understand: it is still possible to modify the technical solutions described in the foregoing embodiments, or to some or all of Technical characteristic is equivalently replaced；And these are modified or replaceed, it does not separate the essence of the corresponding technical solution, and this is practical new The range of each embodiment technical solution of type.

Claims (16)

1. a kind of unmanned plane characterized by comprising

Fuselage, the fuselage are equipped with socket；

Holder, the holder, which is equipped with, to be cooperated 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 separating 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 positioning region cooperation location hole, the positioning region is threaded through the positioning 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 biggish end face of 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. unmanned plane according to claim 2, which is characterized in that the positioning region be it is multiple, between multiple positioning regions Every setting.

6. unmanned plane according to claim 1, which is characterized in that the locking device includes being arranged on the holder Clip-connecting rod is provided with fixture block on the clip-connecting rod, and clamping portion, the fixture block and the clamping portion card are provided on the fuselage It connects.

7. unmanned plane according to claim 6, which is characterized in that have horizontally disposed mounting plate, institute on the fuselage Stating clamping portion is the card hole being arranged on the mounting plate, and the card hole runs through the mounting plate；It is provided on the fixture block Stop surface, the clip-connecting rod protrudes 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 towards the clip-connecting rod away from the holder end extend and gradually deviate from the card hole side wall, described first Guide surface is for being oriented to the clip-connecting rod.

9. unmanned plane according to claim 6, which is characterized in that the clip-connecting rod be it is multiple, on each clip-connecting rod It is provided with the fixture block, multiple clamping portions, each fixture block and a clamping portion are provided on the fuselage Clamping.

10. -9 described in any item unmanned planes according to claim 1, 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. -9 described in any item unmanned planes according to claim 1, which is characterized in that the locking device includes: to be arranged in institute The clamping block on holder is stated, is provided with slot on the clamping block；It is provided with lock slots on the fuselage and is through to the lock Determine the jack of slot；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, which is characterized in that the locking device further includes operating stick, the machine It is provided with slide opening with it, the driving end of the operating stick is threaded through in the slide opening, and the driving end is provided with inclined-plane；It is described to insert The driving portion with inclined-plane cooperation is provided on pin, with when pressing the operating stick into the slide opening, the inclined-plane is supported The driving portion is pushed up to drive the bolt to the external mobile of the lock slots.

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. unmanned plane according to claim 14, which is characterized in that operating side of the operating stick away from the driving end On be provided with pressing plate, the surface area of the pressing plate is greater than the area of section of the operating stick.