CN208868307U - A kind of unmanned plane with built-in camera - Google Patents

Abstract

The utility model discloses a kind of unmanned planes with built-in camera, including fuselage, horn, the horn of at least more than one is arranged in the left and right sides of the fuselage, the horn has a first end and a second end, driving device is provided in the first end of the horn, the second end of the horn is movably connected on the left and right sides of the fuselage, the fuselage interior is provided with photographic device, the photographic device includes camera, camerahead rotating device, the camera is fixed in the fuselage by the camerahead rotating device, the camera and camerahead rotating device are rotatablely connected, the elongated slot that the fuselage offers for camera rotation, the camera is exposed to outside fuselage by elongated slot;The unmanned plane can adjust monitoring range in real time and cam device can be protected secured from damage, stable connection.

Description

A kind of unmanned plane with built-in camera

Technical field

The utility model relates to toy unmanned plane device field more particularly to a kind of toy with built-in camera nobody Machine.

Background technique

Current intelligent simulation toy, it is many kinds of, but fidelity and handling are all relatively poor, experience property compared with Difference emulates the needs of of experience to meet consumer to various intelligent toys to the unmanned plane toy of exploitation.It is unmanned to fly Referred to as " unmanned plane ", english abbreviation is " UAV " to machine, is manipulated using radio robot and the presetting apparatus provided for oneself Not manned aircraft, or fully or intermittently automatically operated by car-mounted computer, multi-rotor unmanned aerial vehicle is that have multiple machines The UAV of arm provides power by the motor on horn, to generate physiology.Unmanned plane has gradually appeared various function Can camera, can be used for scouting with benefit, monitor, explore, and the setting of common camera or exposure is outside fuselage, or It is to be fixed on fuselage, is exposed to outside fuselage, the destruction by external force is easy without protective device, when camera stops working It is not given to store the components such as the mirror surface of its camera also and will receive different degrees of loss；Furthermore it is fixed on taking the photograph on fuselage As head, because camera cannot rotate, it is small that a certain region, monitoring range can only be monitored.

Summary of the invention

The purpose of this utility model is that there are problem and shortage for above-mentioned, monitoring model can be adjusted in real time by providing one kind It encloses and cam device can be protected from damage, the firm unmanned plane of stable connection.

In order to realize the purpose of this utility model, adopt the following technical scheme that

A kind of unmanned plane with built-in camera, including fuselage, horn, the left and right sides setting of the fuselage is at least More than one horn, the horn have a first end and a second end, and driving device, institute are provided in the first end of the horn The second end for stating horn is movably connected on the left and right sides of the fuselage, and the fuselage interior is provided with photographic device, described Photographic device includes camera, camerahead rotating device, and the camera is fixed on described by the camerahead rotating device In fuselage, the camera and camerahead rotating device are rotatablely connected, and the fuselage offers for camera rotation Elongated slot, the camera are exposed to outside fuselage by elongated slot.

Further, the camera rotating distance is 90 degree, can pass through camerahead rotating device tune according to real-time needs The monitoring range of whole camera.

Further, the camerahead rotating device includes lens fixed seat, rotation drive device, fixed frame, the first tooth The inner wall of wheel, second gear, third gear, the lens fixed seat and fuselage is fixed, and the camera is pivotally connected by shaft In on lens fixed seat, the fixed frame is fixed on lens fixed seat and is located at the side opposite with fixing camera, The rotation drive device is clamped and fastened between lens fixed seat and fixed frame, and shaft one end of the camera extends to The outside of lens fixed seat and with first gear hole axis connection, the output shaft of the rotation drive device and described the Two gear hole axis connections, the internal tooth of the third gear and the outer tooth engagement of second gear, the external tooth of the third gear and The outer tooth engagement of one tooth.The suitable angle of camera can be needed to adjust according to realizing by camerahead rotating device, it can be flexible Monitoring adjusting range, it is identical do not increase camera under conditions of, the range of monitoring is wider, more efficient.

Further, the photographic device is located at the bottom of fuselage head end, and photographic device is set to the bottom of fuselage head end, just In unmanned aerial vehicle (UAV) control camera shooting azimuth, monitoring flexibly, is blocked by fuselage to prevent camera view, influences the acquisition of image.

Further, the fuselage includes upper cover and pedestal, and the photographic device is fixed on the chassis interior, the elongated slot It is opened on the pedestal, the camera is exposed to the outside of pedestal, upper cover and pedestal by elongated slot according to public affairs known in this field Method assembly positioning, then be fixed by screw, camerahead rotating device is coated in fuselage, in case external force is direct It causes to impact, improves connective stability.

Further, the lens fixed seat is extended with surrounding edge along pedestal direction and is provided with support column, described to enclose Side, support column can extend to base inner wall, to improve the stability of photographic device connection.

Further, the lens fixed seat is provided with positioning column, the positioning column setting along the direction of the fixed frame There are three more than, the positioning column is distributed in the marginal position of the fixed frame, the fixed frame and the lens fixed seat It mutually is provided with positioning sleeve on fixed face, the fixed frame is sheathed on the positioning column by the positioning sleeve to connect In on the lens fixed seat.Driving device by the external force from two opposite directions be held on fixed fixed frame with Between lens fixed seat, reduce and shaken in driving device work, to improve the stability of photographic device work.

Further, the horn is to be detachably connected, and horn is flexibly dismantled so that unmanned plane is placed convenient for receiving, carried.

Further, it is provided with range light on the outside of the horn, facilitates the orientation of confirmation unmanned plane, and the face for passing through range light Color judges the state of unmanned plane, determines the instantaneous position of aircraft.

Further, the fuselage includes the first housing and the second housing that is movably connected on above the first housing, institute The second end for stating horn is movably connected on the first housing, and the second housing has push-pull structure, passes through the push-pull structure It can include shell, battery fixed frame, the upper end of the battery fixed frame with the convenient dismounting of the first housing, the second housing With opening, the inner cavity of the battery fixed frame is used for placing battery, and the shell, which is fixed on battery fixed frame upper end, to be opened It is described on mouth and to extending to and more than half can be coated on battery fixed frame wherein at left and right sides of battery fixed frame The first housing has with the battery fixed frame not by the matched mounting groove of shell covered section grafting, the shell with The first housing cooperatively forms close type chamber, so that it is intracavitary that battery fixed frame is stable in type；Battery is fixed in fuselage, is mentioned High battery mounting stability, machine body separating type setting and vertical grafting installation, realize that battery charging is convenient, electrical connection is stablized Property, it when unmanned plane is without electricity, can also be worked, be saved by the fast quick-recovery unmanned plane of the spare second housing of quick-replaceable The unmanned plane charging time improves the service efficiency of unmanned plane, and the service life of unmanned plane is no longer influenced by battery.

The utility model has the beneficial effects that: photographic device is set in fuselage, unmanned plane is by external collision When, to prevent directly contributing damage to photographic device, the destruction to camera is reduced, and avoid directly being imaged by external force collision and fill It sets to influence the stability of its connection, by the way that camerahead rotating device is arranged, can flexibly monitor adjusting range, not increase identical Under conditions of adding camera, the range of monitoring is wider.

Detailed description of the invention

It is more particularly described by the preferred embodiment in the utility model shown in the drawings, the above and other mesh of the utility model , feature and advantage will become more fully apparent.Identical appended drawing reference indicates identical part in all the attached drawings, and does not carve Meaning draws attached drawing by actual size equal proportion scaling, it is preferred that emphasis is shows this purport.

Fig. 1 is the overall structure stereoscopic schematic diagram of the utility model.

Fig. 2 is the first housing and second housing structural upright schematic diagram.

Fig. 3 is link arm structural upright schematic diagram.

Fig. 4 is the Section View of the part B of Fig. 6.

Fig. 5 second housing decomposing state stereoscopic schematic diagram.

Fig. 6 is the first housing and second housing positive structure schematic.

Fig. 7 is fuselage and photographic device frontal perspective schematic diagram.

Fig. 8 is fuselage and photographic device rear perspective schematic diagram.

Fig. 9 is fuselage and photographic device connection relationship stereoscopic schematic diagram.

Figure 10 is that photographic device is inverted positive stereoscopic diagram.

Figure 11 is that photographic device is inverted stereoscopic schematic diagram below.

Figure 12 is that photographic device assembles exploded perspective schematic diagram.

Figure 13 is the first housing, fixed cell apparatus, shell mechanism schematic diagram.

Specific embodiment

The application is described more fully below with reference to relevant drawings for the ease of understanding the utility model,.

In the present embodiment, it is to be understood that term " centre ", " upper ", " under ", " top ", " right side ", " left end ", " Top ", " back side ", " middle part ", etc. the orientation or positional relationships of instructions be to be based on the orientation or positional relationship shown in the drawings, be only It is of the invention for ease of description, rather than the device or element of indication or suggestion meaning must have a particular orientation, with specific Orientation construction and operation, therefore be not considered as limiting the invention.

In addition, the connection or fixed form between component if not otherwise specified in this embodiment, connection or solid Determine mode can for fixed by bolt commonly used in the prior art or pin fix or pin shaft connection etc. modes, therefore, this It is not described in detail in embodiment.

A kind of unmanned plane with built-in camera, as shown in Fig. 1,7,8, including fuselage 1, horn 2, the fuselage 1 The horn 2 of at least more than one is arranged in left and right sides, and the horn 2 has a first end and a second end, and the first of the horn 2 Driving device 5 is provided on end, the second end of the horn 2 is movably connected on the left and right sides of the fuselage 1, the fuselage 1 is internally provided with photographic device 14, and the photographic device 14 includes camera 15, camerahead rotating device 46, the camera 15 are fixed in the fuselage 1 by the camerahead rotating device 46, the camera 15 with 46 turns of camerahead rotating device Dynamic connection, the elongated slot 22 that the fuselage 1 offers for the camera 15 rotation, the camera 15 are exposed to by elongated slot 22 Outside fuselage 1, photographic device is set in fuselage, unmanned plane is when by external collision, to prevent directly contributing to photographic device Damage reduces the destruction to camera, and avoids the stability that its connection is directly influenced by external force collision photographic device.

In further preferred embodiments, as shown in Fig. 1,7,8,15 rotating distance of camera is 90 degree, Ke Yigen It is needed when factually, the monitoring range of camera 15 is adjusted by camerahead rotating device 46.

In further preferred embodiments, as shown in figure 9, the camerahead rotating device 46 includes lens fixed seat 16, rotation drive device 17, fixed frame 18, first gear 19, second gear 20, third gear 21, the lens fixed seat 16 fix with the inner wall of fuselage 1, and the camera 15 is articulated on lens fixed seat 16 by shaft 47, the fixed frame 18 It is fixed on lens fixed seat 16 and is located at the side opposite with fixing camera 15, the rotation drive device 17 clamps It is fixed between lens fixed seat 16 and fixed frame 18,47 one end of shaft of the camera 15 extends to lens fixed seat 16 outside and with the 19 hole axis connection of first gear, the output shaft of the rotation drive device 17 and the second gear The outer tooth engagement of 20 hole axis connections, the internal tooth of the third gear 21 and second gear 20, the external tooth of the third gear 21 with The outer tooth engagement of first gear 19.Driving device 17 provides power source, and first gear 19 is driven to rotate, and is passed by third gear 21 It is dynamic, second gear 20 is driven, the elongated slot 22 is opened up along 47 transverse direction of shaft, so that camera 15 can rotate different angles Degree.The suitable angle of camera 15 can be needed to adjust according to realizing by camerahead rotating device 46, can flexibly monitor tune Whole range, it is identical do not increase camera under conditions of, the range of monitoring is wider, more efficient.

In further preferred embodiments, as shown in Figures 9 and 10, the photographic device 14 is located at the bottom of 1 head end of fuselage, Photographic device 14 is set to the bottom of 1 head end of fuselage, is convenient for unmanned aerial vehicle (UAV) control camera shooting azimuth, monitoring is flexible, to prevent camera 15 The visual field is blocked by fuselage 1, influences the acquisition of image.

In further preferred embodiments, as shown in figure 9, the fuselage 1 includes upper cover 48 and pedestal 49, the camera shooting Device 14 is fixed on inside the pedestal 49, and the elongated slot 22 is opened on the pedestal 49, and the camera 15 passes through elongated slot 22 are exposed to the outside of pedestal 49, and unmanned plane is when by by external force collision to reduce the destruction to camera 15.Upper cover 48 and bottom Seat 49 is according to common method known in this field assembly positioning, then is fixed by screw, and camerahead rotating device 46 is wrapped It is overlying in fuselage 1, in order to avoid external force directly contributes impact, improves connective stability.

In further preferred embodiments, as shown in figs9-12, the lens fixed seat 16 extends along 49 direction of pedestal There is surrounding edge 54 and be provided with support column 53, the surrounding edge 54, support column 53 can extend to 49 inner wall of pedestal.The fixation Seat 16 is fixed on the inner wall of body 1 by support column 53 and surrounding edge 54, is anchored on bottom by support column 53 and screw cooperation In seat.The support column 53 is provided with two or more.In further preferred embodiments, as shown in Figure 11,12, the camera Fixing seat 16 is provided with positioning column 51 along the direction of the fixed frame 18, and the setting of positioning column 51 is described fixed there are three more than Position column 51 is distributed in the marginal position of the fixed frame 18, the fixed frame 18 face fixed with 16 phase of lens fixed seat On be provided with positioning sleeve 50, the fixed frame 18 is sheathed on the positioning column 51 by the positioning sleeve 50 to connect In on the lens fixed seat 16.Positioning sleeve 50 and positioning column 51 are interference fitted or screw is fixed with the fixed frame 18 In on lens fixed seat 16.Driving device 17 is held on fixed fixed frame 18 by the external force from two opposite directions Between lens fixed seat 16, reduce and shaken in the work of driving device 17, to improve the stability of the work of photographic device 14.

Driving device 17 provides power source, and first gear 19 is driven to rotate, and is driven by third gear 21, drives the second tooth Wheel 20, to realize that camera 15 rotates；It is needed to adjust camera shooting according to realization by remote control control photographic device 14 (not shown) First 15 suitable angles, can flexibly monitor adjusting range, it is identical do not increase camera under conditions of, the range of monitoring is more Extensively, more efficient.Driving device 17 described in the present embodiment is motor.

In further preferred embodiments, there are four the settings of horn 2, and the horn 2 is to be detachably connected, specially 1 two sides of fuselage may extend away a protrusion 4, and protrusion 4 opens up the connecting hole (not shown) for horn 2 along the direction that horn 2 is unfolded, even It connects hole to set internal screw thread (not shown), 2 second end of horn is provided with the external screw thread (not shown) matched with connecting hole internal screw thread, machine Arm 2 and fuselage 1 are screwed on by screw thread carries out fast quick-detach installation, when not needing using unmanned plane, can be disassembled with horn 2 Receiving is placed, and horn 2 is flexibly dismantled so that unmanned plane is placed convenient for receiving, carried.

In further preferred embodiments, as shown in Figure 1, being provided with range light 13 on the outside of the horn 2, facilitate confirmation nothing Man-machine orientation, and judge by the color of range light 13 state of unmanned plane, determine the instantaneous position of aircraft；The range light 13 are provided with more than one, and in the present embodiment, there are two the settings of leading lamp 13, and is set to two symmetrical horns 2 On, 13 clamping of range light is fixed on the outside of 2 first end of horn, 13 line of range light according to common method known in this field with Radio receiver is connected.

In further preferred embodiments, as shown in Figure 1, 2, including fuselage 1, horn 2, the left and right sides of the fuselage 1 There are four horn 2, the horn 2 is had a first end and a second end for face setting, is provided with driving in the first end of the horn 2 Device 5, the fuselage 1 includes the first housing 37 and the second housing 38 being movably connected on above the first housing 37, described The second end of horn 2 is movably connected on the first housing 37, and the second housing 38 has push-pull structure 36, passes through the plug Mechanism 36 can include shell 27, battery fixed frame 26, the battery with the convenient dismounting of the first housing 37, the second housing 38 The upper end of fixed frame 26 has opening, and the inner cavity of the battery fixed frame 26 is used for placing battery 25, and the shell 27 is solid Due in 26 upper end opening of battery fixed frame and extend to the left and right sides of battery fixed frame 26 can be by battery fixed frame More than half is coated on wherein frame 26, and the first housing 37 has not to be wrapped by the shell 27 with the battery fixed frame 26 Cover the matched mounting groove 23 of part grafting, the shell 27 and the first housing 37 cooperatively form close type chamber, shell 27 and the One body 37 cooperatively forms close type chamber, and it is intracavitary that battery fixed frame 26 is secured in type, and battery fixed frame 26 will be to will Battery 25 is firmly installed in fuselage 1, and reducing collisions alleviates impact force, improve battery 25 and install surely to battery destructive power It is qualitative；Secondly, 1 separate type of fuselage is arranged, realizes battery 25 and charge convenient, when charging is required, the second housing 38 is dismantled Get off, by the USB interface being arranged with 25 connection of battery punching (not shown) electricity, the second housing 38, which is vertically inlayed, is installed on the One body 37, avoids battery 25 and the relative movement of horizontal direction occurs for fuselage 1, keeps away since the gravity of the second housing 38 is used as Exempt from its vertical displacement, to improve electrical connection stability；It, can also be spare by quick-replaceable when unmanned plane is without electricity The work of the fast quick-recovery unmanned plane of the second housing 38, saves the unmanned plane charging time, improves the service efficiency of unmanned plane；Again Secondary, shell 27 and battery fixed frame 26 are detachably arranged, and by removing shell 27, can also take out battery 26 and replace, nothing Man-machine service life is not only restricted to battery 25.

As shown in figure 13, in a further preferred embodiment, the battery 25 has electrical connector, the electrical connector Including socket 40, plug 41, the socket 40 is perpendicularly fixed on the second housing 38, and the plug 41 is perpendicularly fixed at On the first housing 37, to guarantee that electrical connector plug orientation is consistent with the first housing 37 and 38 assembly orientation of the second housing, Specifically, the socket 40 is fixed on the bottom of 24 one end of PCB plate, can be screwed or weld and be anchored on pcb board 24, socket 40 is electrically communicated with pcb board 24, and the opposite position of the first housing 37 offers mounting hole 44, the plug 41 are installed in the first housing, are fixed by screw, and plug 41 is exposed to outside the first housing 37 by mounting hole 44 and socket 40 It realizes and is electrically connected.

As seen in figures 3-6, in a further preferred embodiment, it is provided with card slot 33 at left and right sides of the mounting groove 23, 33 side wall top edge of card slot is extended with upper buckle 32 along interior, and the push-pull structure 36 includes link arm 34, back-off 31, the plug machine Structure 36 is respectively arranged at 38 left and right sides of the second housing and corresponding with the card slot 33, and the link arm 34, which has, to be fixed End and free end, the link arm 34 extend from the left and right sides of the upper end edge battery fixed frame 26 of battery fixed frame 26, institute The fixing end for stating link arm 34 is fixed on the upper end of battery fixed frame 26, and the back-off 31 is set to the free end of link arm 34, institute The length for stating link arm 34 ensures that the buckle 32 can be mutually under the first housing 37 and 38 assembled state of the second housing with back-off 31 It fastens, the link arm 34, back-off 31 are arranged for integral type, and 34 fixing end of link arm is fixed by bolt and the second housing 38, the Two bodies 38 are placed into mounting groove 23, press the link arm 34 of 38 two sides of the second housing at the same time, are squeezed in 23 side wall of mounting groove It overwhelms under 31 collective effects of button, flexible deformation occurs for link arm 34, to realize that back-off 31 slides into card slot 33, unclamps link arm 34, even Arm 34 restores deformation, and upper buckle 32 stings conjunction of linking closely with back-off 31, so that the fixation of the second housing 38 is realized, conversely, can then tear open Except the second housing 38, the dismounting of the second housing 38 can be fast implemented by pressing link arm 34, facilitates operation.

In a further preferred embodiment, the push-pull structure 36 further includes snap-fastener 30, and the snap-fastener 30 is located at back-off It 31 tops and is fixed on link arm 34, the transverse width of the snap-fastener 30 between 38 two sidewalls of the second housing is greater than the The transverse width of two bodies 38, the shell 27 two sides corresponding with the snap-fastener 30 offer button hole 35, and the snap-fastener 30 is logical It crosses and sets the button hole 35 for being opened in 27 two sides of shell and highlight in shell 27；The snap-fastener 30 is integral type setting with link arm, second Body 38 is placed into mounting groove 23, the snap-fastener 30 of 38 two sides of the second housing is pressed at the same time, in 23 sidewall extrusion of mounting groove It is buckled under 31 collective effects, flexible deformation occurs for link arm 34, to realize that back-off 31 slides into card slot 33, unclamps link arm 34, link arm 34 restore deformation, and upper buckle 32 stings conjunction of linking closely with back-off 31, so that the fixation of the second housing 38 is realized, conversely, can then remove The second housing 38 can fast implement the dismounting of the second housing 38 by pressing link arm 34, facilitate operation.

In a further preferred embodiment, the push-pull structure 36 further includes by the second machine lateral in the link arm 34 Supporting part 39 made of 38 side wall of body extends, 38 inner wall of the second housing are extended with plate washer 60 corresponding with the supporting part, The supporting part 39 and the plate washer 60 have a certain distance, the position height of 39 vertical direction of supporting part not bottom in described Snap-fastener 30, the supporting part 39 are integral type setting with link arm, and plate washer 60 and the second housing 38 are arranged for integral type, the snap-fastener 30 height for being higher by shell 27 are greater than the set a distance between the supporting part 39 and the plate washer 60, to guarantee to apply to snap-fastener 30 When external force, snap-fastener 30 will not sink into the side arm of the second housing 38, the set a distance between the supporting part 39 and the plate washer 60 Greater than the amount of interference that the first housing 37 and 38 assembled state of the second housing can be fastened mutually, to guarantee the down stroke energy of back-off 31 Enough ensure to separate with upper buckle 32, to ensure that the second housing 38 can be smoothly detached from from mounting groove 23.

In a further preferred embodiment, the supporting part 39 is located at the adjacent top of the snap-fastener 30.

In a further preferred embodiment, 26 upper end of battery fixed frame also sets up battery capacity indication lamp 28, described Battery fixed frame 26 is located at 25 top of battery and is fixed on the upper end of battery fixed frame 26 by pcb board and passes through PCB Plate 24 is fixed on the upper end of battery fixed frame 26, battery capacity indication lamp 28 be fixedly welded on 24 upper surface of pcb board and with Circuit communicates in the pcb board 24, and the pcb board 24 is contained in shell 27, and the battery capacity indication lamp 28 is outer by being opened in The through-hole at 27 top of shell is exposed to outside shell 27, and the battery capacity indication lamp 28 is provided with more than one, and the link arm 34 is consolidated 24 upper surface of pcb board is fixed in fixed end, and battery fixed frame 26, pcb board 24 are screwed in shell 27；Link arm 34 It is screwed in 24 upper surface of pcb board.The pcb board 24 is electrically connected with battery 25.

Each technical characteristic of embodiment described above can be combined arbitrarily, for simplicity of description, not to above-mentioned reality It applies all possible combination of each technical characteristic in example to be all described, as long as however, the combination of these technical characteristics is not deposited In contradiction, all should be considered as described in this specification.

The several embodiments of utility model above described embodiment only expresses, the description thereof is more specific and detailed, but It cannot be understood as the limitations to utility model patent range.It should be pointed out that for the ordinary skill of this field For personnel, without departing from the concept of the premise utility, various modifications and improvements can be made, these belong to this The protection scope of utility model.Therefore, the scope of protection shall be subject to the appended claims for the utility model patent.

Claims (10)

1. a kind of unmanned plane with built-in camera, which is characterized in that including fuselage (1), horn (2), the fuselage (1) The horn (2) of at least more than one is arranged in left and right sides, and the horn (2) has a first end and a second end, the horn (2) First end on be provided with driving device (5), the second end of the horn (2) is movably connected on the left and right two of the fuselage (1) Side, the fuselage (1) are internally provided with photographic device (14), and the photographic device (14) includes camera (15), camera Rotating device (46), the camera (15) is fixed in the fuselage (1) by the camerahead rotating device (46), described Camera (15) and camerahead rotating device (46) are rotatablely connected, and the fuselage (1) offers for the camera (15) rotation The elongated slot (22) turned, the camera (15) are exposed to fuselage (1) outside by elongated slot (22).

2. the unmanned plane according to claim 1 with built-in camera, which is characterized in that camera (15) rotation Stroke is 90 degree.

3. the unmanned plane according to claim 1 with built-in camera, which is characterized in that the camerahead rotating device It (46) include lens fixed seat (16), rotation drive device (17), fixed frame (18), first gear (19), second gear (20), third gear (21), the lens fixed seat (16) and the inner wall of fuselage (1) are fixed, and the camera (15) passes through Shaft (47) is articulated on lens fixed seat (16), and the fixed frame (18) is fixed on lens fixed seat (16) and position In the side opposite with fixing camera (15), the rotation drive device (17) be clamped and fastened on lens fixed seat (16) with Between fixed frame (18), shaft (47) one end of the camera (15) extend to the outside of lens fixed seat (16) and with First gear (19) hole axis connection, the output shaft and the second gear (20) hole axle of the rotation drive device (17) connect It connects, the outer tooth engagement of the internal tooth of the third gear (21) and second gear (20), the external tooth of the third gear (21) and the The outer tooth engagement of one gear (19).

4. the unmanned plane according to claim 3 with built-in camera, which is characterized in that photographic device (14) position In the bottom of the fuselage (1) head end.

5. the unmanned plane according to claim 3 with built-in camera, which is characterized in that the fuselage (1) includes upper (48) and pedestal (49) are covered, the photographic device (14) is fixed on the pedestal (49) inside, and the elongated slot (22) is opened in institute It states on pedestal (49), the camera (15) is exposed to the outside of pedestal (49) by elongated slot (22).

6. the unmanned plane according to claim 5 with built-in camera, which is characterized in that the lens fixed seat (16) surrounding edge (54) is extended with along pedestal (49) direction and be provided with support column (53), the surrounding edge (54), support column (53) It can arrive in the inner wall of pedestal (49).

7. the unmanned plane according to claim 6 with built-in camera, which is characterized in that the lens fixed seat (16) it is provided with positioning column (51) along the direction of the fixed frame (18), positioning column (51) setting is described there are three more than Positioning column (51) is distributed in the marginal position of the fixed frame (18), the fixed frame (18) and the lens fixed seat (16) It is mutually provided with positioning sleeve (50) on fixed face, the fixed frame (18) is sheathed on the positioning column by the positioning sleeve (50) (51) to be coupled on the lens fixed seat (16) on.

8. the unmanned plane according to claim 1 with built-in camera, which is characterized in that the horn (2) is removable Unload connection.

9. the unmanned plane according to claim 1 with built-in camera, which is characterized in that set on the outside of the horn (2) It is equipped with range light (13).

10. the unmanned plane according to claim 1 with built-in camera, which is characterized in that the fuselage (1) includes upper (48) and pedestal (49) are covered, the photographic device (14) is fixed on the pedestal (49) inside, and the elongated slot (22) is opened in institute It states on pedestal (49), the camera (15) is exposed to the outside of pedestal (49) by elongated slot (22).