Crossing machine
The wearable device addresses the limitations of camera angle adjustment and equipment mounting by incorporating a camera mount with adjustable rods and quick-release mechanisms, enhancing its adaptability and efficiency in image capture.
Patent Information
- Application Number
- CN202422483170.1
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-10-15
- Publication Date
- 2025-07-15
- Estimated Expiration
- 2034-10-15
AI Technical Summary
The existing cross-border machine lacks a structure for carrying camera equipment, and cannot adjust the shooting angle of the camera equipment, which limits its application in camera tasks.
A crossing machine is designed, including a support frame, a camera frame, an arm, a lifter and a transmission camera holder. The angle adjustment of the camera equipment is achieved through the angle adjustment holes of the camera support and the side support rod, and a camera quick loading plate is installed on the camera support to quickly load and unload the equipment.
It improves the universality and work efficiency of the crossover machine in camera tasks and meets the shooting needs of users.
Smart Images

Figure CN223101039U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of unmanned aerial vehicles, and more specifically, to a racing quadcopter. Background Art
[0002] An unmanned aerial vehicle, abbreviated as "UAV", is an unpiloted aircraft controlled by a radio remote control device and a self-contained program control device. With the development of UAV technology, racing quadcopters have gradually become popular, and the "wave" of UAV racing has officially arrived.
[0003] Currently, the highest speed of a racing quadcopter can reach 260 kilometers per hour. The acceleration from 1 kilometer to 100 kilometers is less than 2 seconds, and the 0-100 km / h acceleration is less than 2 seconds. Some experts can make the racing quadcopter and UAV even faster, and the pursuit of speed is also the most common pursuit among players. In addition to speed, players also constantly demand to install various different devices on the racing quadcopter to complete different tasks. For example, it is a common demand among players to use a UAV equipped with a camera device for shooting and be able to adjust the shooting angle of the camera device.
[0004] The racing quadcopter frame and racing quadcopter disclosed in Chinese Patent CN202022119579.7 include an upper frame, which includes an upper skeleton extending in the front-rear direction, and upper duct support rings symmetrically distributed on both sides of the upper skeleton in the left-right direction and integrally formed with the upper skeleton. There are at least two upper duct support rings on the same side of the upper skeleton, and the upper duct support rings on the same side are integrally connected; a lower frame, which includes a lower skeleton extending in the front-rear direction, and lower duct support rings symmetrically distributed on both sides of the lower skeleton in the left-right direction and integrally formed with the lower skeleton. The lower duct support rings correspond to the upper duct support rings one by one and are coaxially arranged. The lower duct support rings on the same side of the lower skeleton are integrally connected;
[0005] Connecting columns, including a skeleton connecting column and a support ring connecting column. The skeleton connecting column is used to connect the upper skeleton and the lower skeleton together, and the support ring connecting column is used to connect two corresponding upper duct support rings and lower duct support rings together. There are at least two support ring connecting columns between the two corresponding upper duct support rings and lower duct support rings and they are circumferentially distributed. The connecting columns connect the upper frame and the lower frame into an integral whole; the corresponding upper duct support rings, lower duct support rings, and the support ring connecting columns arranged between the two duct support rings form a duct through which air can flow. The ducts are used to install flight motors and propellers, and all the ducts are interconnected;
[0006] Duct protection cover, arranged at the duct, used to form the duct wall of the duct and make the duct form a semi-open structure; anti-collision buffer pad, fixedly connected to the outer side of the duct protection cover; both the upper frame and the lower frame are made of carbon fiber material; this utility model adopts a semi-open duct, which can facilitate the passage of air flow, reduce air flow resistance, and the ducts communicate with each other, making the drone more smooth during flight and improving the flight efficiency of the drone. However, this utility model only carries a transmission camera device and does not have a structure for carrying a camera device, so the shooting angle of the camera device cannot be changed. Summary of the Invention
[0007] The main purpose of this utility model is to overcome the defects existing in the above-mentioned background technology, and provide a drone. This utility model can meet the actual shooting needs of users. By setting up a camera bracket, the drone can carry a camera device to perform shooting tasks. By moving the side strut on the angle adjustment holes, the shooting angle of the camera device on the camera bracket can be adjusted, enabling the camera device to adjust the shooting angle based on actual shooting needs, improving the versatility of the drone in shooting tasks. At the same time, a camera quick-release plate is set on the camera bracket to quickly load and unload the camera device, improving work efficiency.
[0008] To achieve the above purpose, a drone proposed by this utility model includes a support frame, a camera frame, arms, a lifter and a transmission camera mount, characterized in that: the transmission camera mount is fixed at the front end of the support frame, the camera frame is fixed on the top surface of the support frame, one end of the side of the support frame is fixedly connected to one end of the arm, the other end of the arm is fixedly connected to the lifter, the camera frame includes a camera bracket, a side strut, a movable support frame and a camera quick-release plate, the camera bracket is fixed on the support frame, there are a plurality of angle adjustment holes on the side wall of the camera bracket, the side strut is fixed inside the camera bracket and both ends of the side strut penetrate out of the camera bracket, the side strut includes a front strut and a rear strut, the rear strut is hinged to the rear end of the movable support frame, the front strut passes through any one of the angle adjustment holes and is connected to the front end of the movable support frame, and the camera quick-release plate is fixed on the movable support frame. Assembling a drone containing a support frame, a camera frame, arms and a lifter, while realizing the high-speed flight of the drone, through the connection of the camera bracket and the side strut, and by changing the position of the side strut on the angle adjustment holes, the angle adjustment of the camera device is realized, improving the versatility of the drone in shooting tasks.
[0009] Furthermore, the support frame includes a frame top plate, a frame bottom plate, and support side plates. The frame top plate and the frame bottom plate are symmetrically arranged. The upper and lower ends of the support side plates are respectively fixedly connected to the frame top plate and the frame bottom plate. Side holes for equipment heat dissipation are provided on the support side plates. The support frame is built by the frame top plate, the frame bottom plate, and the support side plates to provide a fixed base for the drone and the equipment inside the drone, and the heat dissipation of the drone equipment inside the support frame is enhanced by providing side holes on the support side plates.
[0010] Furthermore, it further includes a lifting mounting seat and an extended antenna. The lifting mounting seat is fixed to the side of the support frame, and the extended antenna is fixed to the end of the support frame away from the transmission camera seat. By providing a lifting mounting seat on the support frame, it provides a mounting condition for the setting of the drone arms, and by providing a transmission camera seat, it provides a condition for mounting the camera equipment.
[0011] Furthermore, a GPS fixing seat is provided at one end of the top surface of the support frame close to the transmission camera seat. The GPS fixing seat is arranged in a groove shape. By providing a GPS fixing seat on the top surface of the support frame, a GPS device can be set on the drone, which is convenient for determining the position of the drone in real time and preventing the loss of the drone.
[0012] Furthermore, the drone arms are integrally formed. The drone arms are divided into a support end and an extended end. The support end extends downward, a buffer pad is provided on the bottom surface of the support end, and a motor tube seat is provided at the top end of the extended end. By providing integrally formed drone arms and a motor tube seat at the extended end thereof, it provides a power condition for the lifter carried thereon. At the same time, the landing of the drone is protected by providing the support end and the buffer pad on the bottom surface of the support end.
[0013] Furthermore, the lifter includes a propeller and a flight motor. The flight motor is fixed to the upper and lower ends of the motor tube seat, and the propeller is electrically connected to the flight motor. By fixing the propeller and the flight motor on the motor tube seat, the flight of the drone is realized.
[0014] Furthermore, the movable support frame includes camera support side plates, a camera board, and fixing gaskets. The camera support side plates are arranged on both sides of the top of the camera bracket. The camera support side plates include a front support plate and a rear support plate. The front support plate is longer than the rear support plate. The bottom end of the front support plate is fixedly connected to the front support rod through a fixing gasket, and the bottom end of the rear support plate is hinged to the rear support rod through the fixing gasket. The camera board is fixedly connected to the top ends of the front support plate and the rear support plate. Connecting the front support plate, the rear support plate, and the camera board, and at the same time, the front support plate is fixed to the front support rod through a fixing gasket, and the rear support plate is hinged to the rear support rod through a fixing gasket, which provides necessary conditions for the angle adjustment of the camera equipment.
[0015] Further, the transmission camera base includes a U-shaped mounting member and a transmission camera. The U-shaped mounting member is fixed between the top plate and the bottom plate of the frame. Arc-shaped holes are provided on both side walls of the U-shaped mounting member, and limit buckles are provided below the arc-shaped holes. Rotating shafts are provided on both sides of the transmission camera, and the transmission camera is connected to the arc-shaped holes and the limit buckles through the rotating shafts respectively. By setting the U-shaped mounting member and providing arc-shaped holes and limit buckles thereon, the transmission camera can be fixed on the U-shaped mounting member through the rotating shafts and the angle can be adjusted, broadening the angle that the transmission camera can see.
[0016] Further, a circuit board is provided inside the support frame, and the circuit board is electrically connected to the lifter. Through the circuit board, electrical connections are made for devices such as the motor base inside the aircraft, enabling them to cooperate and work in coordination.
[0017] The beneficial effects of the present utility model include meeting the actual shooting requirements of users for the aircraft. By setting up the camera bracket, the aircraft can carry a camera device for shooting tasks. By moving the side support rod on the angle adjustment hole, the shooting angle of the camera device on the camera bracket can be adjusted, enabling the camera device to adjust the shooting angle based on actual shooting requirements, improving the versatility of the aircraft in shooting tasks. At the same time, setting a camera quick-release plate on the camera bracket can quickly load and unload the camera device, improving work efficiency. BRIEF DESCRIPTION OF THE DRAWINGS
[0018] Figure 1 is a schematic structural diagram of an aircraft in an embodiment of the present utility model;
[0019] Figure 2 is a schematic structural diagram of the support frame in an embodiment of the present utility model;
[0020] Figure 3 is a schematic structural diagram of the camera frame in an embodiment of the present utility model;
[0021] Figure 4 is a schematic structural diagram of the arm in an embodiment of the present utility model;
[0022] Figure 5 is a schematic structural diagram of the movable support frame in an embodiment of the present utility model;
[0023] Figure 6 is a schematic structural diagram of the transmission camera base in an embodiment of the present utility model;
[0024] Reference numerals: 1 support frame; 2 camera frame; 3 arm; 4 lifter; 6 circuit board; 11 top plate of the frame; 12 bottom plate of the frame; 13 support side plate; 14 side hole; 15 lifting mounting seat; 16 transmission camera seat; 17 extended antenna; 18 GPS fixing seat; 21 camera bracket; 22 side support rod; 23 movable support frame; 24 camera quick release plate; 25 angle adjustment hole; 26 front support rod; 27 rear support rod; 31 support end, 32 extended end; 33 buffer pad; 34 motor base; 41 propeller; 42 flight motor; 51 camera support side plate; 52 camera board; 53 fixing gasket; 54 front end support plate; 55 rear end support plate; 61 U-shaped mounting part; 62 arc hole; 63 limit bayonet; 64 transmission camera; 65 rotating shaft. Detailed implementation manners
[0025] In order to make the technical problems, technical solutions and beneficial effects to be solved by the embodiments of the present utility model clearer, the present utility model will be further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain the present utility model, and are not used to limit the present utility model.
[0026] It should be noted that when an element is referred to as being "fixed to" or "disposed on" another element, it can be directly on the other element or indirectly on the other element. When an element is referred to as being "connected to" another element, it can be directly connected to the other element or indirectly connected to the other element. In addition, the connection can be for a fixing function or for a circuit connection function.
[0027] It should be understood that the orientation or positional relationship indicated by the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc. is based on the orientation or positional relationship shown in the accompanying drawings, and is only for the convenience of describing the embodiments of the present utility model and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus cannot be understood as a limitation to the present utility model.
[0028] In addition, the terms "first" and "second" are only used for descriptive purposes, and cannot be understood as indicating or implying relative importance or implicitly indicating the number of the indicated technical features. Thus, the features defined with "first" and "second" may explicitly or implicitly include one or more of such features. In the description of the embodiments of the present utility model, "a plurality" means two or more, unless otherwise specifically defined.
[0029] Embodiment 1
[0030] Please refer to Figure 1 and Figure 3, the drone disclosed in Embodiment 1, including a support frame 1, a camera frame 2, arms 3, a lifter 4, and a transmission camera mount 16, is characterized in that: the transmission camera mount 16 is fixed to the front end of the support frame 1, the camera frame 2 is fixed to the top surface of the support frame 1, one side of the support frame 1 is fixedly connected to one end of the arm 3, the other end of the arm 3 is fixedly connected to the lifter 4, the camera frame 2 includes a camera bracket 21, side struts 22, a movable support frame 23, and a camera quick-release plate 24, the camera bracket 21 is fixed to the support frame 1, a plurality of angle adjustment holes 25 are provided on the side wall of the camera bracket 21, the side struts 22 are fixed inside the camera bracket 21 and both ends of the side struts penetrate out of the camera bracket 21, the side struts 22 include a front strut 26 and a rear strut 27, the rear strut 27 is hinged to the rear end of the movable support frame 23, the front strut 26 passes through any one of the angle adjustment holes 25 and is connected to the front end of the movable support frame 23, and the camera quick-release plate 24 is fixed to the movable support frame 23;
[0031] The camera frame 2 and the arms 3 are arranged on the support frame 1, and at the same time, the lifter 4 is installed on the arms 3. The lifter 4 fixed to the arms 3 drives the entire support frame 1 and the camera bracket 2 to move. On the basis of realizing the basic functions of the drone, by respectively mounting a transmission device and a camera device on the transmission camera mount 16 and the camera frame 2 at one end of the support frame 1, by mounting an FPV camera in the transmission camera mount 16 to meet the need of the drone to observe the flight path, and by using the camera frame 2 to mount the camera device to realize the photographing function, and by quickly loading and unloading the camera device onto the camera frame 2 through the camera quick-release plate 24, the loading and unloading efficiency is improved.
[0032] Preferably, the camera frame 2 is composed of a camera bracket 21, side struts 22, a movable support frame 23, and a camera quick-release plate 24. By passing the side struts 22 through the front and rear ends of the top of the camera bracket 21, the side struts 22 are divided into a front strut 26 and a rear strut 27. At the same time, the front strut 26 is connected to the front end of the movable support frame 23, and the rear strut 27 is hinged to the rear end of the movable support frame 23. The angle of the movable support frame 23 and the camera quick-release plate 24 can be adjusted by moving the front strut 26 in the angle adjustment holes 25 on the side wall of the camera bracket 21, so as to adjust the angle that the camera device mounted on the camera quick-release plate 24 can shoot, meet the actual shooting needs of users, and improve the versatility of the drone in terms of shooting. Embodiment
[0033] Please refer to Figure 2, in Embodiment 2, it is disclosed that the support frame 1 includes a frame top plate 11, a frame bottom plate 12, and support side plates 13. The frame top plate 11 and the frame bottom plate 12 are symmetrically arranged, and the support side plates 13 are fixedly connected to the frame top plate 11 and the frame bottom plate 12 at the upper and lower ends respectively. Side holes 14 for equipment heat dissipation are provided on the support side plates 13; the support frame 1 further includes a lifting mounting seat 15 and an extended antenna 17. The lifting mounting seat 15 is fixed to the side of the support frame 1, and the extended antenna 17 is fixed on the support frame 1 at one end away from the transmission camera seat 16; a GPS fixing seat 18 is provided on the top surface of the support frame 1, and the GPS fixing seat 18 is arranged in a groove shape; a circuit board 6 is arranged in the support frame 1, and the circuit board 6 is electrically connected to the lifter 4
[0034] By symmetrically arranging the frame top plate 11 and the frame bottom plate 12 and connecting and fixing them through the support side plates 13 to form the support frame 1, installation conditions are provided for the drone and drone equipment. The side holes 14 provided on the support side plates 13 facilitate the contact between the drone equipment in the support frame 1 and the air, improving the heat dissipation of the drone equipment; the support frame 1 is also provided with a lifting mounting seat 15, an extended antenna 17, and a GPS fixing seat 18. The lifting mounting seat 15 provides installation conditions for the lifter 4, the extended antenna 17 is used to strengthen the signal transceiver of the drone, improving the information reception and output capabilities of the drone, and the GPS fixing seat 18 enables the drone to carry a GPS, enabling the acquisition of the drone's position information at any time, improving the safety of the drone. The circuit board in the support frame 1 is electrically connected to equipment in the drone such as the motor socket 34, enabling the equipment in the drone to work in coordination. Embodiment
[0035] Please refer to Figure 4 , in Embodiment 3, it is disclosed that the drone arm 3 is integrally formed. The drone arm 3 is divided into a support end 31 and an extended end 32. The support end 31 extends downward, and a buffer pad 33 is provided on the bottom surface of the support end 31. A motor socket 34 is provided at the top end of the extended end 32; the lifter 4 includes a propeller 41 and a flight motor 42. The flight motor 42 is fixed at the upper and lower ends of the motor socket 34, and the propeller 41 is electrically connected to the flight motor 42;
[0036] By connecting the integrally formed arm 3 with the lifting mount 15, the support frame 1 can be driven to move and fly. The arm 3 is divided into a support end 31 and an extension end 32. The support end 31 extends downward and a buffer pad 33 is provided on the bottom surface. The support end 31 and the buffer pad 33 can better protect the drone. When the drone lands, the buffer pad 33 can slow down the impact force and reduce the overall impact force received by the drone. The extension end 32 of the arm 3 extends outward and a motor socket 34 is provided at one end of the extension. The propeller 41 and the flight motor 42 are symmetrically fixed at the upper and lower ends of the motor socket 34, which can provide the flight basis and flight conditions for the drone. At the same time, by symmetrically arranging the propellers 41 up and down, the mutual influence of the wind resistance generated when the propellers 41 rotate can be reduced, ensuring the flight power of the drone. Embodiment
[0037] Please refer to Figure 5 , in Embodiment 4, it is disclosed that the movable support frame 23 includes a camera support side plate 51, a camera plate 52 and a fixing gasket 53. The camera support side plates 51 are arranged on both sides of the top of the camera bracket 2. The camera support side plate 51 includes a front end support plate 54 and a rear end support plate 55. The front end support plate 54 is longer than the rear end support plate 55. The bottom end of the front end support plate 54 is fixedly connected to the front support rod 26 through the fixing gasket 53. The bottom end of the rear end support plate 55 is hinged to the rear support rod 27 through the fixing gasket 53. The camera plate 52 is fixedly connected to the top ends of the front end support plate 54 and the rear end support plate 55;
[0038] By fixing the camera support side plate 51 on the top of the camera bracket 2 and dividing the camera support side plate 51 into a front end support plate 54 and a rear end support plate 55, connecting the front end support plate 54 with the front support rod 26 and the rear end support plate 55 with the rear support rod 27 respectively, necessary adjustment is provided for the camera support plate 51 to move along with the side plate support rod 22 on the angle adjustment hole 25, enabling the drone to adjust the angle of the camera device carried by the drone and improving the versatility of the drone in the camera task.
[0039] Please refer to Figure 6 , in Embodiment 5, it is disclosed that the transmission camera mount 16 includes a U-shaped mounting member 61 and a transmission camera 64. The U-shaped mounting member is fixed between the top plate 11 and the bottom plate 12 of the frame. Arc-shaped holes 62 are provided on both side walls of the U-shaped mounting member 61. A limit bayonet 63 is provided below the arc-shaped holes 62. Rotating shafts 65 are provided on both sides of the transmission camera 64. The transmission camera 64 is connected to the arc-shaped holes 62 and the limit bayonet 63 through the rotating shafts 65 respectively;
[0040] By setting the U-shaped mounting member 61 and respectively providing an arc-shaped hole 62 and a limit bayonet 63 on the U-shaped mounting member 61, the transmission camera 64 can be moved within the U-shaped mounting member 61 through the rotating shaft 65 to adjust the angle. At the same time, the angle of movement of the transmission camera 64 within the U-shaped mounting member 61 is limited through the cooperation of the limit bayonet 63 and the rotating shaft 65, preventing the camera device from falling and being damaged when it moves. The safety of the camera device is improved.
[0041] The above content is a further detailed description of the present utility model in combination with specific / preferred embodiments, and it cannot be determined that the specific implementation of the present utility model is only limited to these descriptions. For those of ordinary skill in the technical field to which the present utility model belongs, without departing from the concept of the present utility model, several alternatives or modifications can be made to these described embodiments, and these alternative or modified forms should all be regarded as belonging to the protection scope of the present utility model. In the description of this specification, the description with reference to terms such as "an embodiment", "some embodiments", "preferred embodiment", "example", "specific example", or "some examples" means that the specific features, structures, materials, or characteristics described in connection with the embodiment or example are included in at least one embodiment or example of the present utility model. In this specification, the schematic representations of the above terms do not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials, or characteristics described can be combined in a suitable manner in any one or more embodiments or examples. Without contradiction, those skilled in the art can combine and combine the different embodiments or examples described in this specification and the features of different embodiments or examples. Although the embodiments of the present utility model and their advantages have been described in detail, it should be understood that various changes, substitutions, and alterations can be made herein without departing from the scope of protection of the patent application.
Claims
1. A traversing machine, comprising a support frame (1), a camera frame (2), an arm (3), a lifter (4) and a transmission camera mount (16), characterized in that: The transmission camera base (16) is fixed to the front end of the support frame (1). The camera frame (2) is fixed to the top surface of the support frame (1). One side of the support frame (1) is fixedly connected to one end of the arm (3). The other end of the arm (3) is fixedly connected to the lifter (4). The camera frame (2) includes a camera bracket (21), side struts (22), a movable support frame (23), and a camera quick-release plate (24). The camera bracket (21) is fixed to the support frame (1). A plurality of angle adjustment holes (25) are provided on the side wall of the camera bracket (21). The side struts (22) are fixed inside the camera bracket (21) and both ends of the side struts (22) penetrate through the camera bracket (21). The side struts (22) include a front strut (26) and a rear strut (27). The rear strut (27) is hinged to the rear end of the movable support frame (23). The front strut (26) passes through any one of the angle adjustment holes (25) and is connected to the front end of the movable support frame (23). The camera quick-release plate (24) is fixed to the movable support frame (23).
2. The flying drone according to claim 1, characterized in that: The support frame (1) includes a frame top plate (11), a frame bottom plate (12), and support side plates (13). The frame top plate (11) and the frame bottom plate (12) are symmetrically arranged. The upper and lower ends of the support side plates (13) are respectively fixedly connected to the frame top plate (11) and the frame bottom plate (12). Side holes (14) for equipment heat dissipation are provided on the support side plates (13).
3. The crosser according to claim 2, characterized in that: The support frame (1) further includes a lifting mounting seat (15) and an extended antenna (17). The lifting mounting seat (15) is fixed to the side of the support frame (1). The extended antenna (17) is fixed to the support frame (1) at one end away from the transmission camera base (16).
4. A flying drone as claimed in claim 1, characterized in that: A GPS fixing seat (18) is provided on the top surface of the support frame (1). The GPS fixing seat (18) is arranged in a groove shape.
5. The flying drone according to claim 1, characterized in that: The arm (3) is integrally formed. The arm (3) is divided into a support end (31) and an extended end (32). The support end (31) extends downward. A buffer pad (33) is provided on the bottom surface of the support end (31). A motor socket (34) is provided on the extended end (32).
6. The crosser according to claim 5, characterized in that The lifter (4) includes a propeller (41) and a flight motor (42). The flight motors (42) are respectively fixed to the upper and lower ends of the motor socket (34). The propeller (41) is connected to the output end of the flight motor (42).
7. The flying drone according to claim 1, characterized in that: The movable support frame (23) includes a camera support side plate (51), a camera plate (52) and a fixing gasket (53). The camera support side plate (51) is arranged on both sides of the top of the camera bracket (21). The camera support side plate (51) includes a front end support plate (54) and a rear end support plate (55). The front end support plate (54) is longer than the rear end support plate (55). The bottom end of the front end support plate (54) is fixedly connected to the front support rod (26) through the fixing gasket (53). The bottom end of the rear end support plate (55) is hinged to the rear support rod (27) through the fixing gasket (53). The camera plate (52) is fixedly connected to the tops of the front end support plate (54) and the rear end support plate (55).
8. The flying drone according to claim 2, characterized in that: The transmission camera base (16) includes a U-shaped mounting member (61) and a transmission camera (64). The U-shaped mounting member is fixed between the top plate (11) and the bottom plate (12) of the frame. Arc-shaped holes (62) are provided on both side walls of the U-shaped mounting member (61). A limit bayonet (63) is provided below the arc-shaped holes (62). Rotating shafts (65) are provided on both sides of the transmission camera (64). The transmission camera (64) is connected to the arc-shaped holes (62) and the limit bayonet (63) respectively through the rotating shafts (65).
9. The flying drone according to claim 2, characterized in that: A circuit board (6) is arranged inside the support frame (1), and the circuit board (6) is electrically connected to the lifter (4).
Citation Information
Patent Citations
Crossing machine frame and traversing machine
CN212401539U