A flying machine with remote control launching function

Abstract

The invention relates to the field of unmanned aerial vehicles, and discloses a flying drone with a remote control launch function, comprising a fuselage and wings, wherein the wings are arranged around the fuselage, and the characteristic is that the fuselage comprises a main frame and a fixing device installed on the main frame for fixing an external device, the fixing device comprises a fixing plate and a slide rail, a mounting frame is arranged on the surface of the fixing plate, the slide rail is installed at the end of the mounting frame, the external device is installed on the slide rail through an adjusting member, when the external device is placed on the adjusting member, a magnetic plate 1 will first contact with the lower end of the external device and generate a preliminary adsorption force due to its protruding position and strong magnetic force, the preliminary adsorption force is sufficient to prevent the external device from sliding or moving during the placement process, and the elastic characteristics of the rubber deformation block absorb the small gap or unevenness that may exist between the external device and the magnetic plate.

Description

Technical Field

[0001] The invention relates to the field of unmanned aerial vehicles, in particular to a flying drone with a remote control launch function. Background Art

[0002] A FPV drone usually refers to a micro-UAV designed for fast crossing and first-person perspective (FPV) flight. This type of drone is known for its high speed, high maneuverability and compact design, and is very suitable for complex flying movements and crossing narrow spaces. However, although FPV drones have many advantages in design and performance, in the existing technology, FPV drones are usually designed with a compact structure and cannot be adapted to other external devices, resulting in certain functional limitations of FPV drones. Therefore, a FPV drone that can increase the number of external devices that can be adapted is needed to improve the application scenarios of FPV drones. Summary of the invention

[0003] The present invention provides a flying drone with a remote control transmission function, which overcomes the shortcomings described in the background technology.

[0004] The technical solution adopted by the present invention to solve its technical problem is:

[0005] A flying drone with a remote control launch function comprises a fuselage and wings, wherein the wings are arranged around the fuselage, the fuselage comprises a main frame and a fixing device installed on the main frame for fixing an external device, the fixing device comprises a fixing plate and a slide rail, a mounting frame is arranged on the surface of the fixing plate, the slide rail is installed at the end of the mounting frame, and the external device is installed on the slide rail through an adjusting member;

[0006] The adjusting member is provided with fixing mechanisms 1 and 2, wherein the fixing mechanism 1 is arranged in the middle of the adjusting member, and the fixing mechanism 2 is arranged on the side of the fixing mechanism 1. The surface of the adjusting member extends to the step edge 1 at both ends, and the fixing mechanism 1 is located in the middle of the step edge 1.

[0007] A preferred technical solution, the fixing mechanism 1 includes a symmetrically arranged adsorption assembly, the adsorption assembly includes a symmetrically arranged movable adsorption mechanism and a mounting groove arranged on the surface of the adjustment member, the movable adsorption mechanism is installed in the mounting groove, the movable adsorption mechanism includes a magnetic plate 1, a magnetic plate 2, a connecting rod, a rubber deformation block, and a rotating shaft 3, the connecting rod is rotatably installed on the rotating shaft 3, the rubber deformation block is fixed to the head and tail ends of the connecting rod, the magnetic plate 1 and the magnetic plate 2 are fixed by two rubber deformation blocks respectively, the height of the magnetic plate 1 is higher than the height of the magnetic plate 2, the magnetic plate 1 protrudes from the surface of the adjustment member, and the magnetic plate 2 does not protrude from the surface of the adjustment member;

[0008] When installing the external device, the first magnetic plate is attached to the lower end of the external device before the second magnetic plate.

[0009] A preferred technical solution is that the connecting rod is a V-shaped structure, and the magnetic plates 1 in the two movable adsorption mechanisms are arranged close to each other. When the two magnetic plates 1 are pressed downward, the connecting rod swings upward with its connection end with the rotating shaft 3 as a guide to fix the magnetic plate 2;

[0010] The two movable adsorption mechanisms are installed in the installation groove through a movable plate. A rubber airbag is arranged between the movable plate and the installation groove. The middle of the installation groove is provided with an inwardly concave step edge 2. When the rubber airbag is squeezed, it expands and deforms toward the step edge 2.

[0011] A preferred technical solution, the fixing mechanism includes a positioning groove arranged on the surface of the adjusting component, there are two positioning grooves, the two positioning grooves are arranged in a layer-by-layer sunken shape, the lower positioning groove is arranged close to the step edge, and the surfaces of the two positioning grooves are provided with suction cups for adsorbing external equipment.

[0012] A preferred technical solution, the adjustment component is composed of two symmetrically arranged clamping mechanisms, the clamping mechanism includes a movable block, an adjustment knob, and a limit plate body, the adjustment knob is installed on the movable block through a rotating shaft, and the limit plate body is installed on the movable block through a rotating shaft.

[0013] A protrusion is provided at the end of the lower side of the limiting plate body, and a groove is provided at the lower side of the adjusting knob corresponding to the protrusion. The protrusion abuts against the surface of the adjusting knob. When the adjusting knob is rotated, the adjusting knob rotates with the first rotating shaft as the guide, squeezing the protrusion so that the limiting plate body swings toward the slide rail with the second rotating shaft as the fulcrum and abuts against the surface of the slide rail.

[0014] A preferred technical solution is that a limiting protrusion is obliquely provided on one side of the limiting plate body close to the adjusting knob, and the limiting protrusion is inclined toward the adjusting knob to limit the rotation angle of the adjusting knob through the limiting protrusion.

[0015] A preferred technical solution is that a rubber layer is respectively provided on the left and right sides of the upper end of the slide rail, and a plurality of mounting holes are arranged in an equidistant array at the corresponding positions of the movable block and the two rubber layers. A ball is movably installed in each mounting hole, and the ball is fixed by a spring. The spring pushes the ball out of the surface of the movable block. When the adjusting component is installed on the slide rail, the ball is pressed against the surface of the rubber layer.

[0016] Compared with the prior art, this technical solution has the following advantages:

[0017] Fixing mechanism 1 is used to install and fix external equipment of various sizes and weights. This mechanism may use locking screws, buckles, elastic clamps and other mechanisms to ensure that the external equipment will not loosen or fall off due to vibration or airflow during high-speed flight. By adjusting the tightening force and position of fixing mechanism 1, it can adapt to the installation requirements of equipment of different sizes, such as high-definition cameras, sensor modules, and even small cargo boxes, thereby greatly increasing the functional diversity and practicality of the cross-country drone. Fixing mechanism 2 is mainly used to provide additional stability and support, especially when carrying heavy or large external equipment, which can effectively prevent the equipment from shaking and shifting during flight, ensuring the safety and stability of flight. The design of fixing mechanism 2 may be more flexible, and can be sliding, adjustable in angle, or even replaceable to adapt to external equipment of different shapes and weights. This design not only improves the adaptability of the cross-country drone, but also allows pilots to quickly replace different external equipment according to mission requirements, improving the convenience and efficiency of operation.

[0018] When the external device is placed on the adjusting member, magnetic plate one, due to its protruding position and strong magnetic force, will first contact the lower end of the external device and generate a preliminary adsorption force. This preliminary adsorption force is sufficient to prevent the external device from slipping or moving during the placement process, laying the foundation for subsequent stable adsorption. As the external device is further placed, magnetic plate two also gradually contacts the external device and generates adsorption force. At this time, the elastic buffering effect of the rubber deformation blocks begins to appear. They not only provide the necessary connection strength, but also absorb the tiny gaps or unevenness that may exist between the external device and the magnetic plate through their elastic properties. This elastic buffering effect helps to reduce the shaking of the equipment caused by vibration or airflow during flight, ensuring that the external device remains stable. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] The present invention will be further described below in conjunction with the accompanying drawings and embodiments.

[0020] Figure 1 This is an overall diagram of the present invention.

[0021] Figure 2 for Figure 1 A three-dimensional schematic diagram of .

[0022] Figure 3 It is a schematic diagram of the fixing device 12 and the external equipment 100.

[0023] Figure 4 It is a schematic diagram of the fixing device 12.

[0024] Figure 5 for Figure 4 Schematic diagram from top view.

[0025] Figure 6 for Figure 4 Exploded diagram.

[0026] Figure 7 for Figure 6 Schematic side view.

[0027] Figure 8 is a schematic diagram of the clamping mechanism.

[0028] Fig. 9 A schematic diagram of the clamping mechanism from another perspective.

[0029] Fig.10 It is a schematic diagram of the structure of the adsorption component 311.

[0030] In the figure: fuselage 1;

[0031] Main frame 11, fixing device 12, fixing plate 121, mounting frame 1211, slide rail 122, rubber layer 1221, adjusting member 123, movable block 231, positioning groove 2311, suction cup 2312, mounting hole 2313, spring 2314, ball bearing 2315, adjusting knob 232, rotating shaft 1 2321, limiting plate 233, rotating shaft 2 2331, limiting protrusion 2332;

[0032] Adsorption component 311, magnetic plate 1 3111, magnetic plate 2 3112, connecting rod 3113, rubber deformation block 3114, rotating shaft 3115, mounting groove 3116, rubber airbag 3117;

[0033] Wing 2;

[0034] External device 100. DETAILED DESCRIPTION

[0035] like Figures 1 to 10 As shown, the present invention proposes a flying drone with a remote control launch function, comprising a fuselage 1 and wings 2, wherein the wings 2 are arranged around the fuselage 1, the fuselage 1 comprises a main frame 11 and a fixing device 12 installed on the main frame 11 for fixing an external device 100, the fixing device 12 comprises a fixing plate 121 and a slide rail 122, a mounting frame 1211 is arranged on the surface of the fixing plate 121, the slide rail 122 is installed at the end of the mounting frame 1211, and the external device 100 is installed on the slide rail 122 through an adjusting member 123;

[0036] The adjusting member 123 is provided with fixing mechanisms 1 and 2, wherein the fixing mechanism 1 is provided in the middle of the adjusting member 123, and the fixing mechanism 2 is provided on the side of the fixing mechanism 1. The surface of the adjusting member 123 extends to the step edge 1 at both ends, and the fixing mechanism 1 is located in the middle of the step edge 1.

[0037] The fixing mechanism 1, located in the middle of the adjustment member 123, is the main fixing point. Its design takes versatility and stability into consideration and aims to provide a reliable connection point for installing and fixing external equipment of various sizes and weights. This mechanism may use locking screws, buckles, elastic clamps and other mechanisms to ensure that the external equipment will not loosen or fall off due to vibration or airflow during high-speed flight. By adjusting the tightening strength and position of the fixing mechanism 1, it can adapt to the installation requirements of equipment of different sizes, such as high-definition cameras, sensor modules, and even small cargo boxes, thereby greatly increasing the functional diversity and practicality of the cross-country drone.

[0038] Fixing mechanism 2 is arranged on the side of fixing mechanism 1, which is a supplement and enhancement of fixing mechanism 1. Its main function is to provide additional stability and support, especially when carrying heavy or large external equipment. It can effectively prevent the equipment from shaking and shifting during flight, and ensure the safety and stability of flight. The design of fixing mechanism 2 may be more flexible. It can be sliding, adjustable in angle, or even replaceable to adapt to external equipment of different shapes and weights. This design not only improves the adaptability of the cross-country drone, but also allows pilots to quickly replace different external equipment according to mission requirements, thereby improving the convenience and efficiency of operation.

[0039] The fixing mechanism 1 includes a symmetrically arranged adsorption assembly 311, the adsorption assembly 311 includes a symmetrically arranged movable adsorption mechanism and a mounting groove 3116 arranged on the surface of the adjustment member 123, the movable adsorption mechanism is installed in the mounting groove 3116, the movable adsorption mechanism includes a magnetic plate 1 3111, a magnetic plate 2 3112, a connecting rod 3113, a rubber deformation block 3114, and a rotating shaft 3115, the connecting rod 3113 is rotatably installed on the rotating shaft 3115, and the rubber deformation block 3114 is installed on the rotating shaft 3115. 114 is fixed to the head and tail ends of the connecting rod 3113, and the magnetic plate 1 3111 and the magnetic plate 2 3112 are fixed by two rubber deformation blocks 3114 respectively. The height of the magnetic plate 1 3111 is higher than that of the magnetic plate 2 3112. The magnetic plate 1 3111 protrudes from the surface of the adjusting member 123, while the magnetic plate 2 3112 does not protrude from the surface of the adjusting member 123. When the external device 100 is installed, the magnetic plate 1 3111 is attached to the lower end of the external device 100 in priority to the magnetic plate 2 3112.

[0040] When the external device 100 is placed on the adjustment member 123, the magnetic plate 1 3111, due to its protruding position and strong magnetic force, will first contact the lower end of the external device and generate a preliminary adsorption force. This preliminary adsorption force is sufficient to prevent the external device from slipping or moving during the placement process, laying the foundation for subsequent stable adsorption. As the external device is further placed, the magnetic plate 2 3112 also gradually contacts the external device and generates adsorption force. At this time, the elastic buffering effect of the rubber deformation block 3114 begins to appear. They not only provide the necessary connection strength, but also absorb the tiny gaps or unevenness that may exist between the external device and the magnetic plate through their elastic properties. This elastic buffering effect helps to reduce the shaking of the equipment caused by vibration or airflow during flight, ensuring that the external device remains stable.

[0041] Among them, the connecting rod 3113 is a V-shaped structure, and the magnetic plates 1 3111 in the two movable adsorption mechanisms are arranged close to each other. When the two magnetic plates 1 3111 are squeezed downward, the connecting rod 3113 swings upward with its connection end with the rotating shaft 3115 as a guide to fix the magnetic plate 2 3112. When the magnetic plate 1 3111 is squeezed by the external device 100, the V-shaped structure design of the connecting rod 3113 below it will produce an upward tilting action. This action makes the magnetic plate 2 3112, which originally kept a certain distance from the magnetic plate 1 3111, also rise until both can closely contact and adsorb the external device 100. Specifically, the connecting rod 3113, as the core of this mechanism, its V-shaped structure allows it to be connected with the rotating shaft 3115 when under pressure. The fulcrum swings, and this swing not only disperses the pressure to the entire fixing mechanism, but also cleverly uses the lever principle to convert the downward pressure on the magnetic plate 1 3111 into the upward tilting force of the magnetic plate 2 3112. Through such a design, the two magnetic plates can play a role at the same time, ensuring that the external device 100 can maintain a stable fixed state when subjected to various external forces and vibrations. This double adsorption mechanism not only improves the reliability of fixation, but also increases the adaptability of the fixing mechanism to external devices of different shapes and sizes. In short, the design of the magnetic plate 1 3111 being squeezed and the magnetic plate 2 3112 being tilted upward by the connecting rod 3113 cleverly realizes the function of the two magnetic plates simultaneously adsorbing the external device 100, providing a more efficient and stable fixing solution for equipment such as cross-country drones.

[0042] The two movable adsorption mechanisms are installed in the mounting groove 3116 through a movable plate. A rubber airbag 3117 is arranged between the movable plate and the mounting groove 3116. The middle part of the mounting groove 3116 is provided with a step edge 2 which is concave inward. When the rubber airbag 3117 is squeezed, it expands and deforms toward the step edge 2. The two movable adsorption mechanisms are cleverly designed and installed on a movable plate, and this movable plate can move freely in the mounting groove 3116. In order to further enhance the stability and buffering capacity of the structure, a rubber airbag 3117 is specially arranged between the movable plate and the mounting groove 3116. 17. This rubber airbag not only provides the necessary connection and support, but also has excellent elastic deformation characteristics. The middle part of the mounting groove 3116 is designed with an inwardly recessed step edge 2. This detail design plays a key role when the rubber airbag 3117 is squeezed. When the external load equipment applies pressure to the active adsorption mechanism, causing the rubber airbag 3117 to be compressed, the airbag will expand and deform along the step edge 2. This deformation not only effectively absorbs external impact force, but also further stabilizes the position of the active adsorption mechanism by increasing the contact area with the mounting groove.

[0043] Furthermore, the fixing mechanism 1 includes a positioning groove 2311 arranged on the surface of the adjusting member 123, and there are two positioning grooves 2311. The two positioning grooves 2311 are arranged in a layer-by-layer sunken shape, and the lower positioning groove 2311 is arranged close to the step edge. The surfaces of the two positioning grooves 2311 are provided with suction cups 2312 for adsorbing the external device 100.

[0044] Moreover, the adjusting member 123 is composed of two symmetrically arranged clamping mechanisms, the clamping mechanisms including a movable block 231, an adjusting knob 232, and a limiting plate 233. The adjusting knob 232 is rotatably mounted on the movable block 231 via a rotating shaft 1 2321, and the limiting plate 233 is rotatably mounted on the movable block 231 via a rotating shaft 2 2331.

[0045] A protrusion is provided at the lower end of the limiting plate body 233, and a groove is provided at the lower side of the adjusting knob 232 corresponding to the protrusion. The protrusion abuts against the surface of the adjusting knob 232. When the adjusting knob 232 is rotated, the adjusting knob 232 rotates with the first rotating shaft 2321 as a guide, and the protrusion is squeezed to make the limiting plate body 233 swing toward the slide rail 122 with the second rotating shaft 2331 as a fulcrum, and abut against the surface of the slide rail 122.

[0046] When the slide rail 122 needs to be fixed, the user operates the adjustment knob 232. This knob is designed to be rotatable. When it is rotated, a driving force is generated through a mechanical principle. This driving force acts on the limit plate 233, causing the limit plate to swing. The swing of the limit plate is carefully designed, and its end will gradually approach and contact the surface of the slide rail 122. As the pressure exerted by the limit plate on the slide rail increases, the slide rail is effectively clamped between the limit plate and another fixed structure such as a slide rail mounting frame.

[0047] In addition, a limiting protrusion 2332 is obliquely provided on one side of the limiting plate body 233 close to the adjusting knob 232 , and the limiting protrusion 2332 is inclined toward the adjusting knob 232 so as to limit the rotation angle of the adjusting knob 232 through the limiting protrusion 2332 .

[0048] Furthermore, a rubber layer 1221 is respectively provided on the left and right sides of the upper end of the slide rail 122, and a plurality of mounting holes 2313 are arranged in an equidistant array at the corresponding positions of the movable block 231 and the two rubber layers 1221, and a ball 2315 is movably installed in each mounting hole 2313, and the ball 2315 is fixed by a spring 2314, and the spring 2314 pushes the ball 2315 out of the surface of the movable block 231. When the adjusting member 123 is installed on the slide rail 122, the ball 2315 is pressed against the surface of the rubber layer 1221, and a rubber layer 1221 is respectively provided on the left and right sides of the upper end of the slide rail 122. The rubber layer 1221 not only provides additional cushioning and shock absorption effects, but also increases the friction coefficient of the slide rail surface, which helps to form a more stable connection with the movable block. The movable block 231 and the corresponding parts of the two rubber layers 1221 are evenly arrayed with multiple mounting holes 2313, and balls 2315 are movably installed in these mounting holes. The balls are fixed by springs 2314. The function of the springs is to push the balls out of the surface of the movable block so that they keep in contact with the rubber layer. This design allows the balls to have a certain amount of movement space when subjected to external force, thereby adapting to slide rails of different sizes.

[0049] It should be explained that the external device 100 in the present invention can be used as a smoke bomb for illustration only. The launch or use is controlled by electronic control. The electronic control module is integrated inside the smoke bomb, and the smoke release mechanism can be triggered by receiving a remote signal from the flying drone. This electronic release method not only improves the flexibility and accuracy of the use of smoke bombs, but also allows the timing and range of smoke release to be more finely controlled. Smoke bombs can be used in a variety of scenarios, such as military exercises, fire drills, film and television shooting, stage performances, etc. In military exercises, smoke bombs can be used to simulate battlefield environments and provide participants with a realistic training experience; in fire drills, smoke bombs can be used to simulate fire scenes to help firefighters become familiar with fire-fighting procedures and techniques.

[0050] In addition, the drone in the present invention is equipped with a wireless communication module, which can realize long-distance communication with a ground control station or a remote terminal. This communication capability enables the drone to perform tasks in a wider area without worrying about signal interruption or loss. The remote control system of the drone supports real-time data transmission and feedback, so that the operator can understand the status, position and other information of the drone in real time, and perform precise control accordingly. This real-time control capability is crucial for the precise release of smoke bombs. The drone also has autonomous flight capabilities and can fly automatically according to preset routes or mission plans. When necessary, the operator can also take over control at any time and manually control the drone. In addition, the drone in the present invention can use LYL chips and be placed in the 433 frequency band to facilitate remote start and stop. The above-mentioned LYL chips or 433 frequency bands are only used as illustrations and do not mean that the present invention can only use this setting.

[0051] In summary, the combination of the external device 100 in the present invention and the remote control system of the flying drone not only improves the flexibility and accuracy of smoke release, but also expands the application scope and effect of smoke bombs. This innovative design will provide more efficient, safe and environmentally friendly solutions for military exercises, fire drills, film and television shooting and other fields.

[0052] The above description is only a preferred embodiment of the present invention, and therefore cannot be used to limit the scope of the present invention. That is, equivalent changes and modifications made according to the patent scope of the present invention and the contents of the specification should still fall within the scope of the present invention.

Claims

1. A flying drone with a remote control launch function, comprising a fuselage (1) and wings (2), wherein the wings (2) are arranged around the fuselage (1), and characterized in that: The fuselage (1) comprises a main frame (11) and a fixing device (12) mounted on the main frame (11) for fixing an external device (100); the fixing device (12) comprises a fixing plate (121) and a slide rail (122); a mounting frame (1211) is provided on the surface of the fixing plate (121); the slide rail (122) is mounted on the end of the mounting frame (1211); and the external device (100) is mounted on the slide rail (122) via an adjusting member (123); The adjusting member (123) is provided with fixing mechanisms 1 and 2, wherein the fixing mechanism 1 is provided in the middle of the adjusting member (123), and the fixing mechanism 2 is provided on the side of the fixing mechanism 1, the surface of the adjusting member (123) extends to step edges 1 at both ends, and the fixing mechanism 1 is located in the middle of the step edge 1; The fixing mechanism 1 comprises a symmetrically arranged adsorption assembly (311), the adsorption assembly (311) comprises a symmetrically arranged movable adsorption mechanism and a mounting groove (3116) arranged on the surface of the adjusting member (123), the movable adsorption mechanism is installed in the mounting groove (3116), the movable adsorption mechanism comprises a magnetic plate 1 (3111), a magnetic plate 2 (3112), a connecting rod (3113), a rubber deformation block (3114), and a rotating shaft 3 (3115), and the connecting rod (3113) rotates Installed on the third rotating shaft (3115), the rubber deformation blocks (3114) are fixed to the head and tail ends of the connecting rod (3113), the magnetic plate one (3111) and the magnetic plate two (3112) are respectively fixed by two rubber deformation blocks (3114), the height of the magnetic plate one (3111) is higher than the height of the magnetic plate two (3112), the magnetic plate one (3111) protrudes from the surface of the adjusting member (123), and the magnetic plate two (3112) does not protrude from the surface of the adjusting member (123); When the external device (100) is installed, the first magnetic plate (3111) is adsorbed on the lower end of the external device (100) before the second magnetic plate (3112).

2. The drone with remote control transmission function according to claim 1, characterized in that: The connecting rod (3113) is a V-shaped structure. The magnetic plates (3111) in the two movable adsorption mechanisms are arranged close to each other. When the two magnetic plates (3111) are pressed downward, the connecting rod (3113) swings upward with the connection end with the rotating shaft (3115) as a guide to fix the magnetic plate (3112). The two movable adsorption mechanisms are installed in the mounting groove (3116) via a movable plate, a rubber airbag (3117) is arranged between the movable plate and the mounting groove (3116), and a second step edge concave inwardly is arranged in the middle of the mounting groove (3116). When the rubber airbag (3117) is squeezed, it expands and deforms toward the second step edge.

3. The drone with remote control transmission function according to claim 1, characterized in that: The fixing mechanism 1 comprises a positioning groove (2311) arranged on the surface of the adjusting member (123), two positioning grooves (2311) are arranged, the two positioning grooves (2311) are arranged in a layer-by-layer sunken shape, the lower positioning groove (2311) is arranged close to the step edge 1, and suction cups (2312) for adsorbing the external device (100) are arranged on the surfaces of the two positioning grooves (2311).

4. A flying drone with a remote control transmission function according to any one of claims 2 and 3, characterized in that: The adjusting member (123) is composed of two symmetrically arranged clamping mechanisms, the clamping mechanisms comprising a movable block (231), an adjusting knob (232), and a limiting plate (233); the adjusting knob (232) is rotatably mounted on the movable block (231) via a first rotating shaft (2321); and the limiting plate (233) is rotatably mounted on the movable block (231) via a second rotating shaft (2331); A protrusion is provided at the lower end of the limiting plate body (233), and a groove is provided at the lower side of the adjusting knob (232) at a position corresponding to the protrusion. The protrusion abuts against the surface of the adjusting knob (232). When the adjusting knob (232) is rotated, the adjusting knob (232) rotates with the first rotating shaft (2321) as a guide, squeezing the protrusion so that the limiting plate body (233) swings toward the slide rail (122) with the second rotating shaft (2331) as a fulcrum and abuts against the surface of the slide rail (122).

5. The drone with remote control transmission function according to claim 4, characterized in that: A limiting protrusion (2332) is obliquely provided on one side of the limiting plate body (233) close to the adjusting knob (232), and the limiting protrusion (2332) is inclined toward the adjusting knob (232) so as to limit the rotation angle of the adjusting knob (232) through the limiting protrusion (2332).

6. The drone with remote control transmission function according to claim 5, characterized in that: A rubber layer (1221) is respectively provided on the left and right sides of the upper end of the slide rail (122); a plurality of mounting holes (2313) are arranged in an equidistant array at the corresponding positions of the movable block (231) and the two rubber layers (1221); a ball (2315) is movably installed in each mounting hole (2313); the ball (2315) is fixed by a spring (2314); the spring (2314) pushes the ball (2315) out of the surface of the movable block (231); when the adjustment member (123) is installed on the slide rail (122), the ball (2315) is pressed against the surface of the rubber layer (1221).

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