Automatic tracking take-off and landing platform for charging unmanned aerial vehicle
By designing the flip shaft, pressure head and other structures on the automatic tracking take-off and landing platform, combined with the threaded rod system driven by the servo motor, the stable locking of the unmanned aircraft and the automatic upward plug-in connection of the charging plug are achieved, solving the problem that the charging plug cannot be plugged smoothly in the existing technology, and improving charging efficiency and energy saving.
Patent Information
- Application Number
- CN202411731271.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-11-29
- Publication Date
- 2025-03-14
- Estimated Expiration
- Not applicable · inactive patent
AI Technical Summary
During the charging process of unmanned aerial vehicles, the existing automatic tracking take-off and landing platform is prone to fail to plug in smoothly due to improper weight of the unmanned aerial vehicle, resulting in the problem of inability to charge normally.
An automatic tracking take-off and landing platform is designed, and the main body of the platform is equipped with a flip shaft, a press head, a flip gear, a pushing gear, a pushing gear and a charging part. The threaded rod is driven by a servo motor to rotate, driving the charging push rack and a pushing gear movement, realizing the automatic upward movement of the charging plug and the locking of the unmanned aerial vehicle, ensuring smooth plug connection.
The stable locking of the unmanned aerial vehicle on the automatic tracking take-off and landing platform and the smooth connection of the charging plug and the charging port are achieved, ensuring the normal operation of charging operations, and reducing energy losses through synchronous operations and improving energy savings.
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Figure CN119611849A_ABST
Abstract
Description
Technical Field
[0001] The invention relates to the field of aircraft, and in particular to an automatic tracking take-off and landing platform for charging unmanned aircraft. Background Art
[0002] Unmanned aerial vehicles are small aircraft that do not require human operators and can fly through remote control or autonomous programs. When charging, unmanned aerial vehicles often use automatic tracking and landing platforms for charging. The automatic tracking and landing platform can locate the location of the unmanned aerial vehicle through functions such as Bluetooth, and automatically track and drive to the location, allowing the unmanned aerial vehicle to land on the automatic tracking and landing platform for charging.
[0003] However, during use of the existing automatic tracking take-off and landing platform, due to the light weight of the unmanned aerial vehicle, the charging plug on the automatic tracking take-off and landing platform is easily lifted up when it moves up to plug into the charging port of the unmanned aerial vehicle, making it impossible for the two to be smoothly plugged in, resulting in a phenomenon of abnormal charging. Summary of the invention
[0004] The purpose of the present invention is to provide an automatic tracking take-off and landing platform for charging an unmanned aerial vehicle, so as to solve the problems raised in the above-mentioned background technology.
[0005] To achieve the above-mentioned purpose, the present invention provides the following technical solutions: an automatic tracking take-off and landing platform for charging unmanned aerial vehicles, comprising a platform body, wherein a flip shaft is installed at the front and rear edges of the upper end of the platform body, a pressure head is installed in the middle of the flip shaft, and a flip gear is coaxially inlaid at one end of the flip shaft, and a pushing tooth plate is meshed at the lower part of the flip gear, and the pushing tooth plate is slidably connected to the platform body, a push gear seat is elastically installed in the middle of the upper end of the platform body, and push gear racks are tiltably installed at both ends of the push gear seat, and the ends of the push gear racks are connected to the pushing tooth plate, and a charging component is installed in the middle of the upper end of the platform body, and the push gear seat is elastically connected to the charging component.
[0006] Preferably, an axle-carrying seat is rotatably mounted on the other end of the flip shaft, the end of the axle-carrying seat is fixed to the platform body, and a rotating frame is fixedly mounted on the upper end of the pressure head, the end of the rotating frame is fixed to the flip shaft.
[0007] Preferably, a T-shaped slide is slidably installed inside the pushing tooth plate, the lower end of the T-shaped slide is fixed to the platform body, a limited resistance ear extends at the edge of the upper end face of the T-shaped slide, a connecting seat is fixedly installed at the side edge of the pushing tooth plate, and the end of the pushing tooth frame is rotatably installed inside the connecting seat.
[0008] Preferably, two guide columns are symmetrically and slidably installed on the side of the push gear seat, and fixing caps are fixedly installed at both ends of the guide columns. The lower ends of the fixing caps are fixed to the platform body, and a return spring is wound around the outer side of the guide column, one end of the return spring is fixed to the push gear seat, and the other end of the return spring is fixed to one of the fixing caps.
[0009] Preferably, the charging component includes a guide edge rod installed in the middle of the upper end of the platform body, a guide sleeve is fitted on the outer surface of the guide edge rod, a plug socket is fixedly installed on the end of the guide sleeve, a charging plug is fixedly installed on the end of the plug socket, and the end of the charging plug is electrically connected to the platform body.
[0010] Preferably, rod frames are fixedly installed at both ends of the guide edge rod, a bracket is fixedly installed in the middle of the rod frame, the end of the bracket is fixed to the platform body, an arc groove is opened in the middle of the upper end surface of the platform body near the front of the bracket, a threaded rod is arranged above the arc groove, a threaded sleeve is screwed on the outer surface of the threaded rod, a charging push rack is rotatably installed on the upper end of the threaded sleeve, the end of the charging push rack is rotatably connected to the plug socket, and the charging push rack is arranged at an angle.
[0011] Preferably, the threaded rod passes through the middle part of the push gear seat, a push spring is wound around the outside of the threaded rod, one end of the push spring is fixed to the threaded sleeve, and the other end of the push spring is fixed to the push gear seat, a rod frame is rotatably installed on the outer surface of the threaded rod near the edge, the lower end of the rod frame is fixed to the platform body, a servo motor is installed at the edge of the upper end surface of the platform body, and the servo motor is connected to the threaded rod.
[0012] Preferably, a guide ridge is extended from the inner bottom surface of the arc-shaped groove, a concave seat is extended from the lower end surface of the threaded sleeve, the concave seat is fitted to the outer surface of the guide ridge, a No. 2 pulley is coaxially embedded in the end of the threaded rod, a No. 1 pulley is coaxially embedded in the output end of the servo motor, a synchronous belt is connected between the No. 1 pulley and the No. 2 pulley, and motor frames are fixedly installed at the front and rear ends of the servo motor, and the ends of the motor frames are fixed to the platform body.
[0013] Compared with the prior art, the present invention has the following beneficial effects: 1. When the unmanned aerial vehicle stops on the platform body, the servo motor drives the threaded rod to rotate, so that the threaded sleeve tightened on the threaded rod can move, and then drive the charging push frame to move, so as to push the charging plug on the plug seat, so that the charging plug moves up under the guidance of the guide edge rod and the guide sleeve to be plugged into the charging port of the unmanned aerial vehicle for charging. In this process, the threaded sleeve will also push the push gear seat through the jacking spring to drive the push gear frame to move, push the push gear plate, so that the push gear plate can slide on the T-shaped slide seat, so as to drive the flip gear to rotate, and then drive the pressure head on the flip shaft to flip, so as to press on the landing gear of the unmanned aerial vehicle, so as to firmly fix the unmanned aerial vehicle on the platform body, so that the charging plug and the charging port of the unmanned aerial vehicle can be smoothly plugged, thereby ensuring the normal charging operation.
[0014] 2. The present invention completes the locking operation of the unmanned aerial vehicle simultaneously while pushing the charging plug and the charging port of the unmanned aerial vehicle for insertion. The process does not require an additional driving source, effectively reduces energy loss, and improves energy saving. BRIEF DESCRIPTION OF THE DRAWINGS
[0015] Figure 1 This is a schematic diagram of the structure of the automatic tracking take-off and landing platform for charging an unmanned aerial vehicle according to the present invention; Figure 2 A schematic diagram of another perspective of the automatic tracking take-off and landing platform for charging an unmanned aerial vehicle according to the present invention; Figure 3 The invention is an automatic tracking take-off and landing platform for charging unmanned aerial vehicles Figure 1 A magnified view of middle; Figure 4 A partial view of the automatic tracking take-off and landing platform for charging an unmanned aerial vehicle according to the present invention; Figure 5 The invention is an automatic tracking take-off and landing platform for charging unmanned aerial vehicles Figure 4 Enlarged view of middle B; Figure 6 This is a schematic diagram of the threaded rod of the automatic tracking take-off and landing platform for charging an unmanned aerial vehicle according to the present invention.
[0016] In the accompanying drawings, the list of components represented by each reference number is as follows: 1. Platform body; 2. Unmanned aerial vehicle; 3. Servo motor; 4. Charging push frame; 5. Threaded rod; 6. Charging plug; 7. Plug seat; 8. Arc groove; 9. Motor frame; 10. Push tooth plate; 11. Pressure head; 12. Rotating frame; 13. Axle seat; 14. Flip shaft; 15. Flip gear; 16. Limit stop ear; 17. T-shaped slide; 18. Guide rib rod; 19. Rod frame; 20. Guide sleeve; 21. Bracket; 22. Pulley No. 1; 23. Synchronous belt; 24. Rod frame; 25. Fixed cap; 26. Reset spring; 27. Guide column; 28. Push gear seat; 29. Push gear frame; 30. Connecting seat; 31. Pushing spring; 32. Guide ridge; 33. Concave seat; 34. Threaded sleeve; 35. Pulley No. 2. DETAILED DESCRIPTION
[0017] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.
[0018] The present invention provides a technical solution: Figure 1 - Figure 6The automatic tracking take-off and landing platform for charging unmanned aerial vehicles shown in the figure includes a platform body 1. The platform body 1 in the present invention is the automatic tracking take-off and landing platform. The automatic tracking take-off and landing platform uses Bluetooth and other functions to locate the location of the unmanned aerial vehicle 2, and automatically tracks and drives to the location, so that the unmanned aerial vehicle 2 can land on the automatic tracking take-off and landing platform. This is a prior art and has been widely used, so it is not elaborated on here. A flip shaft 14 is installed at the front and rear edges of the upper end of the platform body 1, and a pressure head 11 is installed in the middle of the flip shaft 14. The flip shaft 14 plays a role in driving the pressure head 11 to flip. A flip gear 15 is coaxially inlaid at one end of the flip shaft 14, and a pushing tooth plate 10 is meshed at the lower part of the flip gear 15. The pushing tooth plate 10 is slidably connected to the platform body 1, and the pushing tooth plate 10 is The flip gear 15 drives the flip shaft 14 to rotate. A pushing gear seat 28 is elastically installed in the middle of the upper end of the platform body 1. Pushing gear frames 29 are installed at both ends of the pushing gear seat 28 for tilting and rotation. The ends of the pushing gear frame 29 are connected to the pushing tooth plate 10. The pushing gear seat 28 can drive the pushing gear frame 29 to move to push the pushing tooth plate 10. A charging component is installed in the middle of the upper end of the platform body 1. The pushing gear seat 28 is elastically connected to the charging component. The moving pushing gear seat 28 drives the pushing gear frame 29 to move and push the pushing tooth plate 10, so that the pushing tooth plate 10 can slide on the T-shaped slide 17 to drive the flip gear 15 to rotate, thereby driving the pressure head 11 on the flip shaft 14 to flip, so as to press on the landing gear of the unmanned aerial vehicle 2, so as to firmly fix the unmanned aerial vehicle 2 on the platform body 1.
[0019] The other end of the flip shaft 14 is rotatably mounted with an axle seat 13, the end of which is fixed to the platform body 1, and the axle seat 13 serves to support the flip shaft 14. The upper end of the pressure head 11 is fixedly mounted with a rotating frame 12, the end of which is fixed to the flip shaft 14, and the rotating frame 12 serves to fix the pressure head 11 and the flip shaft 14 together.
[0020] A T-shaped slide 17 is slidably installed inside the pushing tooth plate 10, and the lower end of the T-shaped slide 17 is fixed to the platform body 1. The T-shaped slide 17 plays a role in guiding the pushing tooth plate 10. A limited stop ear 16 extends at the edge of the upper end surface of the T-shaped slide 17. The limited stop ear 16 can limit the pushing tooth plate 10, and then limit the pressure head 11 pressed on the landing gear of the unmanned aerial vehicle 2 to ensure that it is in a stationary state. A connecting seat 30 is fixedly installed at the side edge of the pushing tooth plate 10. The connecting seat 30 plays a role in facilitating the connection of the pushing gear frame 29, and the end of the pushing gear frame 29 is rotatably installed inside the connecting seat 30.
[0021] Two guide columns 27 are symmetrically and slidably installed on the side of the push gear seat 28. Fixed caps 25 are fixedly installed at both ends of the guide columns 27. The guide columns 27 play a role in guiding the push gear seat 28. The lower end of the fixed cap 25 is fixed to the platform body 1. The fixed cap 25 plays a role in fixing the guide columns 27. A return spring 26 is wound around the outer side of the guide column 27. One end of the return spring 26 is fixed to the push gear seat 28. The return spring 26 can push the push gear seat 28 to reset the pushed gear seat 28 after moving. The other end of the return spring 26 is fixed to one of the fixed caps 25.
[0022] The charging component includes a guide rib 18 installed in the middle of the upper end of the platform body 1. A guide sleeve 20 is fitted on the outer surface of the guide rib 18. The guide rib 18 and the guide sleeve 20 play a role in vertically guiding the charging plug 6. A plug socket 7 is fixedly installed at the end of the guide sleeve 20. The charging plug 6 is fixedly installed at the end of the plug socket 7. The plug socket 7 plays a role in supporting the charging plug 6. The end of the charging plug 6 is electrically connected to the platform body 1.
[0023] A rod frame 19 is fixedly installed at both ends of the guide edge rod 18, and the rod frame 19 serves to connect the guide edge rod 18. A bracket 21 is fixedly installed in the middle of the rod frame 19, and the end of the bracket 21 is fixed to the platform body 1. The bracket 21 serves to support and fix the guide edge rod 18. An arc groove 8 is provided in the middle of the upper end surface of the platform body 1 near the front of the bracket 21, and a threaded rod 5 is provided above the arc groove 8. The outer surface of the threaded rod 5 is tightened with a threaded sleeve 34. The threaded rod 5 and the threaded sleeve 34 serve to drive the charging push frame 4 to move. The charging push frame 4 is rotatably installed on the upper end of the threaded sleeve 34. The charging push frame 4 The end portion is rotatably connected to the plug socket 7, and the charging push frame 4 plays a role in pushing the plug socket 7. The charging push frame 4 is inclined, and the threaded sleeve 34 drives the charging push frame 4 to move to push the plug socket 7, so that the charging plug 6 moves up under the guidance of the guide edge rod 18 and the guide sleeve 20 to approach the charging port of the unmanned aerial vehicle 2. When the pressure head 11 is pressed tightly on the landing gear of the unmanned aerial vehicle 2, the toothed plate 10 is pushed to just press against the limit stop ear 16, so that the pressure head 11 remains stationary, and then the threaded sleeve 34 continues to move to drive the charging plug 6 to continue to move up, so as to be plugged into the charging port of the unmanned aerial vehicle 2 for charging.
[0024] The threaded rod 5 passes through the middle part of the pushing gear seat 28, and a pushing spring 31 is wound around the outer side of the threaded rod 5. One end of the pushing spring 31 is fixed to the threaded sleeve 34, and the threaded sleeve 34 can push the pushing gear seat 28 through the pushing spring 31 to make it move, and the other end of the pushing spring 31 is fixed to the pushing gear seat 28. A rod frame 24 is rotatably installed on the outer surface of the threaded rod 5 near the edge, and the lower end of the rod frame 24 is fixed to the platform body 1. The rod frame 24 plays a role in supporting the threaded rod 5. A servo motor 3 is installed at the edge of the upper end surface of the platform body 1. The servo motor 3 plays a role in driving the threaded rod 5 to rotate. The servo motor 3 is connected to the threaded rod 5. The servo motor 3 drives the threaded rod 5 to rotate when it works, so that the threaded sleeve 34 tightened on the threaded rod 5 can move, so as to push the pushing gear seat 28 through the pushing spring 31. At this time, the reset spring 26 contracts and deforms, allowing the pushing gear seat 28 to move normally.
[0025] A guiding ridge 32 extends from the inner bottom surface of the arc-shaped groove 8, and a concave seat 33 extends from the lower end surface of the threaded sleeve 34. The concave seat 33 fits the outer surface of the guiding ridge 32. The cooperation between the guiding ridge 32 and the concave seat 33 guides the threaded sleeve 34. A No. 2 pulley 35 is coaxially inlaid at the end of the threaded rod 5, and a No. 1 pulley 22 is coaxially inlaid at the output end of the servo motor 3. A synchronous belt 23 is connected between the No. 1 pulley 22 and the No. 2 pulley 35. The No. 1 pulley 22 and the No. 2 pulley 35 connect the synchronous belt 23, and the synchronous belt 23 fixes the servo motor 3 and the threaded rod 5 together. The front and rear ends of the servo motor 3 are fixedly mounted with a motor frame 9, and the end of the motor frame 9 is fixed to the platform body 1, and the motor frame 9 fixes the servo motor 3.
[0026] When in use, the unmanned aerial vehicle 2 stops on the platform body 1, and then the servo motor 3 works to drive the threaded rod 5 to rotate, so that the threaded sleeve 34 tightened on the threaded rod 5 can move, so as to push the push gear seat 28 through the jacking spring 31. At this time, the reset spring 26 shrinks and deforms, allowing the push gear seat 28 to move normally, so that the push gear seat 28 drives the push gear frame 29 to move, and pushes the push gear plate 10, so that the push gear plate 10 can slide on the T-shaped slide seat 17, so as to drive the flip gear 15 to rotate, and then drive the pressure head 11 on the flip shaft 14 to flip, so as to press on the landing gear of the unmanned aerial vehicle 2, so as to firmly fix the unmanned aerial vehicle 2 on the platform body 1. In this process, the threaded sleeve 34 will also synchronously drive the charging push frame 4 to move to push the plug socket 7, so that the charging plug 6 moves up under the guidance of the guide edge rod 18 and the guide sleeve 20 to get close to the charging port of the unmanned aerial vehicle 2. When the pressure head 11 is pressed tightly against the landing gear of the unmanned aerial vehicle 2, the tooth plate 10 is pushed to just press against the limit stop ear 16, so that the pressure head 11 remains stationary, and then the threaded sleeve 34 continues to move to drive the charging plug 6 to continue to move up so as to be plugged into the charging port of the unmanned aerial vehicle 2 for charging. In this process, the pushing spring 31 contracts and deforms to offset the force generated by the continued movement of the threaded sleeve 34, so that the movement of the charging plug 6 will not be hindered while the pressure head 11 remains stationary.
[0027] It should be noted that, in this article, relational terms such as first and second, etc. are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprises" or any other variations thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device.
[0028] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.
Claims
1. An automatic tracking take-off and landing platform for charging an unmanned aerial vehicle, comprising a platform body (1), characterized in that: A flip shaft (14) is installed at the front and rear edges of the upper end of the platform body (1), a pressure head (11) is installed in the middle of the flip shaft (14), one end of the flip shaft (14) is coaxially inlaid with a flip gear (15), the lower part of the flip gear (15) is meshed with a push tooth plate (10), the push tooth plate (10) is slidably connected to the platform body (1), a push tooth seat (28) is elastically installed in the middle of the upper end of the platform body (1), and push tooth frames (29) are installed at both ends of the push tooth seat (28) in an inclined and rotatable manner, and the ends of the push tooth frame (29) are connected to the push tooth plate (10), and a charging component is installed in the middle of the upper end of the platform body (1), and the push tooth seat (28) is elastically connected to the charging component.
2. The automatic tracking take-off and landing platform for charging unmanned aerial vehicles according to claim 1, characterized in that: The other end of the flip shaft (14) is rotatably mounted with an axle carrier (13), the end of the axle carrier (13) is fixed to the platform body (1), the upper end of the pressure head (11) is fixedly mounted with a rotating frame (12), the end of the rotating frame (12) is fixed to the flip shaft (14).
3. The automatic tracking take-off and landing platform for charging unmanned aerial vehicles according to claim 1, characterized in that: A T-shaped slide seat (17) is slidably mounted inside the pushing tooth plate (10), the lower end of the T-shaped slide seat (17) is fixed to the platform body (1), a limited stop ear (16) extends from the edge of the upper end surface of the T-shaped slide seat (17), a connecting seat (30) is fixedly mounted on the side edge of the pushing tooth plate (10), and the end of the pushing tooth frame (29) is rotatably mounted inside the connecting seat (30).
4. The automatic tracking take-off and landing platform for charging unmanned aerial vehicles according to claim 1, characterized in that: Two guide columns (27) are symmetrically and slidably installed on the side surface of the push gear seat (28), and fixing caps (25) are fixedly installed at both ends of the guide columns (27). The lower end of the fixing cap (25) is fixed to the platform body (1), and a return spring (26) is wound around the outer side of the guide column (27). One end of the return spring (26) is fixed to the push gear seat (28), and the other end of the return spring (26) is fixed to one of the fixing caps (25).
5. The automatic tracking take-off and landing platform for charging unmanned aerial vehicles according to claim 1, characterized in that: The charging component comprises a guide rib (18) mounted in the middle of the upper end of the platform body (1); a guide sleeve (20) is fitted on the outer surface of the guide rib (18); a plug socket (7) is fixedly mounted on the end of the guide sleeve (20); a charging plug (6) is fixedly mounted on the end of the plug socket (7); and the end of the charging plug (6) is electrically connected to the platform body (1).
6. The automatic tracking take-off and landing platform for charging unmanned aerial vehicles according to claim 5, characterized in that: A rod frame (19) is fixedly mounted on both ends of the guide edge rod (18), a bracket (21) is fixedly mounted in the middle of the rod frame (19), the end of the bracket (21) is fixed to the platform body (1), an arc groove (8) is provided in the middle of the upper end surface of the platform body (1) near the front of the bracket (21), a threaded rod (5) is arranged above the arc groove (8), a threaded sleeve (34) is screwed on the outer surface of the threaded rod (5), a charging push frame (4) is rotatably mounted on the upper end of the threaded sleeve (34), the end of the charging push frame (4) is rotatably connected to the plug socket (7), and the charging push frame (4) is arranged in an inclined manner.
7. The automatic tracking take-off and landing platform for charging unmanned aerial vehicles according to claim 6, characterized in that: The threaded rod (5) passes through the middle of the push gear seat (28), and a push spring (31) is wound around the outer side of the threaded rod (5). One end of the push spring (31) is fixed to the threaded sleeve (34), and the other end of the push spring (31) is fixed to the push gear seat (28). A rod frame (24) is rotatably mounted on the outer surface of the threaded rod (5) near the edge, and the lower end of the rod frame (24) is fixed to the platform body (1). A servo motor (3) is mounted on the edge of the upper end surface of the platform body (1), and the servo motor (3) is connected to the threaded rod (5).
8. The automatic tracking take-off and landing platform for charging unmanned aerial vehicles according to claim 7, characterized in that: A guide ridge (32) extends from the inner bottom surface of the arc-shaped groove (8), a concave seat (33) extends from the lower end surface of the threaded sleeve (34), the concave seat (33) fits the outer surface of the guide ridge (32), a second pulley (35) is coaxially inlaid on the end of the threaded rod (5), a first pulley (22) is coaxially inlaid on the output end of the servo motor (3), a synchronous belt (23) is connected between the first pulley (22) and the second pulley (35), and a motor frame (9) is fixedly mounted on the front and rear ends of the servo motor (3), and the end of the motor frame (9) is fixed to the platform body (1).