Same-frequency debugging device for empennage controller
By using speed sensors and pressure sensors in the tail controller co-frequency debugging device, combined with the camera, the problem of inaccurate manual observation is solved, accurate judgment of the tail response is achieved, and the stability of the aircraft is improved.
Patent Information
- Application Number
- CN202420944382.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-05-06
- Publication Date
- 2025-01-10
- Estimated Expiration
- 2034-05-06
AI Technical Summary
In the debugging of existing tail controllers at the same frequency, due to the inaccurate response of manual observation of tail controllers, it is easy to lead to judgment errors and affect the stability of the aircraft.
A tail controller co-frequency debugging device including a speed measuring mechanism and a detection mechanism is designed to detect the tail speed through a speed sensor, and use a pressure sensor and a camera to judge the tail response status to ensure the accuracy of the judgment.
Accurate judgment of the tail response condition is achieved, judgment errors are avoided, and the stability of the aircraft is improved.
Smart Images
Figure CN222337496U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the field of debugging devices, in particular to a same-frequency debugging device for a tail controller. Background Art
[0002] Tail controller frequency synchronization refers to the process of ensuring that the remote control (transmitter) and tail control receiver (receiver) operate at the same frequency in a radio remote control model or drone system, and performing precise matching and performance optimization.
[0003] The existing co-frequency debugging of the tail controller is to send instructions through the remote control, make the tail control receiver receive the instructions, and then observe the response of the tail to achieve the co-frequency debugging of the tail controller. However, since the response of the tail is judged by manual observation, it is difficult to ensure the accuracy of the judgment of the response of the tail during manual observation, and errors are prone to occur, which in turn affects the stability of the aircraft and is relatively inconvenient.
[0004] Therefore, a tail controller synchronous frequency debugging device has been developed to ensure the accuracy of the judgment of the tail response and avoid the influence of judgment errors on the stability of the aircraft. Utility Model Content
[0005] In order to overcome the shortcomings of the existing tail controller co-frequency debugging, in which the response of the tail is difficult to ensure the accuracy of the judgment through manual observation, errors are prone to occur, and thus affect the stability of the aircraft, the utility model provides a tail controller co-frequency debugging device that can ensure the accuracy of the judgment of the tail response and avoid errors in judgment that affect the stability of the aircraft.
[0006] The technical solution is: a tail controller frequency synchronization debugging device, including a base, a controller, a remote control, an electric push rod, a tail, a bottom rod seat, a side seat, a central axis, a speed measuring mechanism and a detection mechanism. The upper right side of the base is connected to the controller, the right side of the controller is connected to the remote control, the upper front and rear sides of the controller are connected to electric push rods, the upper left side of the base is connected to the front and rear side seats, the side seats are rotatably connected to the tail, the lower sides of the tail are connected to the bottom rod seats, the bottom rod seats are movably connected to the telescopic ends of the adjacent electric push rods, the upper middle side of the controller is connected to the central axis, the tail is rotatably connected to the central axis, the side seats are provided with speed measuring mechanisms capable of testing the tail rotation speed, and the base is provided with a detection mechanism capable of accurately judging the response of the tail.
[0007] Furthermore, the remote controller is provided with buttons.
[0008] Furthermore, a display screen is provided on the remote controller.
[0009] Furthermore, the speed measuring mechanism includes a fixed seat and a rotation speed sensor. The fixed seat is connected to one side of the upper part of the side seat that is away from each other. The rotation speed sensor is connected to the fixed seat. The rotation speed sensor is rotatably connected to the adjacent tail wing.
[0010] Furthermore, the detection mechanism includes a bottom plate, a background plate and a pressure sensor. The left part of the base is connected to the bottom plate, the upper left side of the bottom plate is connected to the background plate, and the right side of the background plate is connected to two front and rear pressure sensors.
[0011] Furthermore, it also includes a camera, and two front and rear cameras are connected to the upper right side of the bottom plate.
[0012] The beneficial effects of the utility model are as follows: the utility model detects the rotation speed of the tail wing through the rotation speed sensor on the fixed seat, and when the tail wing rotates to the highest point, it contacts the pressure sensor on the background plate, and detects the pressure sensed by the tail wing through the pressure sensor to judge the response of the tail wing, thereby achieving the effect of ensuring the accuracy of the judgment of the response of the tail wing and avoiding the effect of judgment errors affecting the stability of the aircraft. BRIEF DESCRIPTION OF THE DRAWINGS
[0013] Figure 1 It is a three-dimensional structural schematic diagram of the utility model.
[0014] Figure 2 It is a partial three-dimensional structural schematic diagram of the utility model.
[0015] Figure 3 It is a bottom view schematic diagram of a partial three-dimensional structure of the utility model.
[0016] Figure 4 It is a three-dimensional structural schematic diagram of the speed measuring mechanism of the utility model.
[0017] Figure 5 It is a three-dimensional structural schematic diagram of the detection mechanism of the utility model.
[0018] The names and serial numbers of the parts in the figure are: 1_base, 2_controller, 3_remote control, 4_electric push rod, 5_tail wing, 50_bottom rod seat, 6_side seat, 7_middle axis, 8_speed measuring mechanism, 81_fixed seat, 82_speed sensor, 9_detection mechanism, 91_bottom plate, 92_camera, 93_background plate, 94_pressure sensor. DETAILED DESCRIPTION
[0019] The utility model is described in detail below in conjunction with the accompanying drawings.
[0020] A tail controller frequency adjustment device, such as Figure 1-Figure 3As shown, it includes a base 1, a controller 2, a remote control 3, an electric push rod 4, a tail wing 5, a bottom rod seat 50, a side seat 6, a central axis 7, a speed measuring mechanism 8 and a detection mechanism 9. The controller 2 is connected to the upper right side of the base 1, and the remote control 3 is connected to the right side of the controller 2. The remote control 3 is provided with buttons for sending instructions, and the remote control 3 is provided with a display screen for displaying and sending instructions. The front and rear upper sides of the controller 2 are connected to the electric push rod 4, the front and rear side seats 6 are connected to the upper left side of the base 1, and the side seats 6 are rotatably connected with the tail 5, and the bottom rod seats 50 are connected to the lower sides of the tail wing 5. The bottom rod seats 50 are movably connected to the telescopic ends of the adjacent electric push rods 4, the central axis 7 is connected to the upper middle side of the controller 2, and the tail wing 5 is rotatably connected to the central axis 7. The side seats 6 are provided with speed measuring mechanisms 8, and the base 1 is provided with a detection mechanism 9.
[0021] like Figure 1 and Figure 4 As shown, the speed measuring mechanism 8 includes a fixed seat 81 and a speed sensor 82. The fixed seat 81 is connected to the side of the upper part of the side seat 6 that is away from each other. The fixed seat 81 is connected to the speed sensor 82. The speed sensor 82 is rotatably connected to the adjacent tail wing 5.
[0022] like Figure 1 and Figure 5 As shown, the detection mechanism 9 includes a base plate 91, a camera 92, a background plate 93 and a pressure sensor 94. The base 1 is connected to the base plate 91 on the left, and the front and rear cameras 92 are connected to the upper right side of the base plate 91. The upper left side of the base plate 91 is connected to the background plate 93, and the front and rear pressure sensors 94 are connected to the right side of the background plate 93.
[0023] When using the utility model, first place the base 1 in the frequency debugging area of the tail 5 controller 2, and then send a command to the controller 2 through the remote control 3 to rotate the tail 5 to the highest point. After receiving the command, the controller 2 controls the electric push rod 4 to start and push the bottom rod seat 50 to move, so that the tail 5 rotates between the side seat 6 and the middle axis 7. When the tail 5 rotates, the speed sensor 82 on the fixed seat 81 detects the speed of the tail 5. When the tail 5 rotates to the highest point, it contacts the pressure sensor 94 on the background plate 93. The pressure sensed by the tail 5 is detected by the pressure sensor 94 to judge the response of the tail 5, thereby ensuring the accuracy of the judgment of the response of the tail 5 and avoiding the judgment error that affects the stability of the aircraft. The camera 92 on the bottom plate 91 can shoot the movement of the tail 5, which is convenient for the detection personnel to record data.
[0024] The above is only a specific implementation of the utility model, but the protection scope of the utility model is not limited thereto. Any technician familiar with the technical field can easily think of changes or substitutions within the technical scope disclosed by the utility model, which should be included in the protection scope of the utility model. Therefore, the protection scope of the utility model should be based on the protection scope of the claims.
Claims
1. A tail controller frequency adjustment device, characterized in that: The invention comprises a base (1), a controller (2), a remote controller (3), an electric push rod (4), a tail wing (5), a bottom rod seat (50), a side seat (6), a central axis (7), a speed measuring mechanism (8) and a detection mechanism (9). The upper right side of the base (1) is connected to the controller (2), the right side of the controller (2) is connected to the remote controller (3), the upper front and rear sides of the controller (2) are both connected to the electric push rod (4), the upper left side of the base (1) is connected to the front and rear side seats (6), and the side seat (6) is connected to the speed measuring mechanism (8). ) are rotatably connected to the tail wing (5), the lower side of the tail wing (5) is connected to the bottom rod seat (50), the bottom rod seat (50) is movably connected to the telescopic end of the adjacent electric push rod (4), the middle upper side of the controller (2) is connected to the middle axis (7), the tail wing (5) is rotatably connected to the middle axis (7), the side seat (6) is provided with a speed measuring mechanism (8) capable of testing the rotation speed of the tail wing (5), and the base (1) is provided with a detection mechanism (9) capable of accurately judging the response of the tail wing (5).
2. A tail controller frequency synchronization device according to claim 1, characterized in that: The remote controller (3) is provided with buttons.
3. A tail controller frequency adjustment device according to claim 1, characterized in that: The remote controller (3) is provided with a display screen.
4. A tail controller frequency adjustment device according to claim 1, characterized in that: The speed measuring mechanism (8) comprises a fixed seat (81) and a rotation speed sensor (82). The fixed seat (81) is connected to the side of the upper part of the side seat (6) that is away from each other. The fixed seat (81) is connected to the rotation speed sensor (82). The rotation speed sensor (82) is rotatably connected to the adjacent tail wing (5).
5. A tail controller frequency synchronization device according to claim 4, characterized in that: The detection mechanism (9) comprises a bottom plate (91), a background plate (93) and a pressure sensor (94); the left portion of the base (1) is connected to the bottom plate (91); the upper left portion of the bottom plate (91) is connected to the background plate (93); and the right side of the background plate (93) is connected to two front and rear pressure sensors (94).
6. A tail controller frequency synchronization device according to claim 5, characterized in that: It also includes a camera (92), and the upper right side of the bottom plate (91) is connected to two front and rear cameras (92).