Unmanned aerial vehicle lift force inspection equipment

Abstract

The utility model relates to the field of lift force detection devices, in particular to unmanned aerial vehicle lift force detection equipment which comprises a detection frame, a sensor, a controller and a display screen are installed on the detection frame, a pull rod is arranged on the sensor, a pull rope is tied on the pull rod, and the sensor comprises a plurality of high-precision tension sensors. The high-precision tension sensor is used for corresponding to different positions of the unmanned aerial vehicle, the detection frame adopts a double-layer structure design, when the unmanned aerial vehicle is subjected to a lift force test, the unmanned aerial vehicle is separated from testing equipment, and meanwhile, the opening and the pull ropes are used for dredging, so that the situation that multiple pull ropes are easily wound together in the rising process of the unmanned aerial vehicle is avoided; the whole equipment adopts an intelligent control mode, the detection efficiency is improved, a battery pack is further arranged on the test frame and provides power for the sensor, the controller and the display screen, and through the design, the unmanned aerial vehicle lift force detection equipment is simple in structure, convenient to operate and capable of rapidly and accurately detecting the lift force performance of an unmanned aerial vehicle.

Description

Technical Field

[0001] The utility model relates to the field of lift detection devices, in particular to a lift inspection device for unmanned aerial vehicles. Background Art

[0002] With the rapid development of drone technology, drones are increasingly used in various fields. However, due to differences in drone lift performance, different drones and application scenarios have different lift requirements. Therefore, in order to ensure the safety and stable flight of drones, accurate detection of drone lift is particularly important. The existing drone lift detection equipment on the market generally has a complex structure, a large size, and is not easy to move. Therefore, it is necessary to develop a drone lift inspection device that is easy to operate and easy to move. Utility Model Content

[0003] 1. Technical issues to be resolved

[0004] In view of the deficiencies in the prior art, the utility model provides a lift inspection device for an unmanned aerial vehicle.

[0005] (II) Technical solution

[0006] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: the lift inspection equipment of the unmanned aerial vehicle of the utility model comprises a detection frame, a sensor, a controller and a display screen are installed on the detection frame, a tension rod is arranged on the sensor, a pull rope is tied to the tension rod, the sensor comprises a plurality of high-precision tension sensors, the high-precision tension sensors are used to correspond to different positions of the unmanned aerial vehicle, the high-precision tension sensors are connected to the controller via a data cable, the controller is connected to the display screen via a data cable, a plurality of operation buttons are arranged on the controller, a ferrule is provided at the end of the pull rope, and the ferrule is used to tie up the unmanned aerial vehicle equipment.

[0007] Preferably, the detection frame is a double-layer structure, including an equipment frame and a test frame, and the equipment frame is located above the test frame, the sensor, controller and display screen are arranged on the test frame, and the equipment frame is provided with a plurality of openings, and the pull rope passes through the openings.

[0008] Further preferably, the controller includes a processor and a storage module, the processor is used to integrate test data of a plurality of high-precision tension sensors, and the storage module is used to store working records of the high-precision tension sensors.

[0009] Again preferably, the ring is a strip structure, the outer surface of the ring is a Velcro tape, the inner surface of the ring is a Velcro mother tape, and the Velcro mother tape is bonded to the Velcro tape.

[0010] Preferably, a slot is provided at the corner of the test frame, a fixing slot is provided around the outside of the slot, the equipment frame is adapted to be connected to the slot through a support rod, and a fixing ring is provided on the support rod, and the fixing ring is respectively connected to the support rod and the fixing slot through a threaded structure.

[0011] Further preferably, a vertical plate is provided on one side of the equipment rack, and a pull rod is installed on the vertical plate.

[0012] Again preferably, the test stand is provided with a battery pack, the battery pack is a storage battery structure, and the storage battery is electrically connected to the sensor and the controller.

[0013] (III) Beneficial effects

[0014] Compared with the prior art, the utility model provides a UAV lift inspection device, which has the following beneficial effects:

[0015] The detection frame of the utility model adopts a double-layer structure design, which separates the drone from the measuring equipment when performing lift test on the drone, and uses openings and pull ropes to guide, so as to prevent multiple pull ropes from being easily entangled during the rise of the drone;

[0016] The entire equipment adopts intelligent control mode to improve the detection efficiency. The test frame is also equipped with a battery pack to provide power for the sensor, controller and display screen. Through this design, the UAV lift inspection equipment has a simple structure, is easy to operate, and can quickly and accurately detect the lift performance of the UAV. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Figure 1 This is a front structural schematic diagram of the utility model;

[0018] Figure 2 This is a side view of the structure of the utility model;

[0019] Figure 3 This is a schematic diagram of the top view of the test stand of the utility model;

[0020] Figure 4 This is a schematic diagram of the ferrule structure of the utility model;

[0021] In the figure: 1. detection frame; 2. test frame; 3. equipment frame; 4. high-precision tension sensor; 5. controller; 6. display screen; 7. opening; 8. support rod; 9. fixing ring; 10. vertical plate; 11. pull rod; 12. tension rod; 13. battery pack; 14. slot; 15. fixing groove; 16. ring; 17. magic mother tape; 18. magic child tape. DETAILED DESCRIPTION

[0022] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0023] See also Figure 1-4 The utility model of the UAV lift inspection equipment includes a detection frame 1, a sensor, a controller 5 and a display screen 6 are installed on the detection frame 1, a tension rod 12 is arranged on the sensor, a pull rope is tied to the tension rod 12, the sensor includes a plurality of high-precision tension sensors 4, the high-precision tension sensors 4 are used to correspond to different positions of the UAV, the high-precision tension sensors 4 are connected to the controller 5 through a data line, the controller 5 is connected to the display screen 6 through a data line, a plurality of operation buttons are arranged on the controller 5, and a ring 16 is arranged at the end of the pull rope, and the ring 16 is used to tie up the UAV equipment.

[0024] In a preferred embodiment of the above-mentioned UAV lift inspection equipment, the inspection frame 1 is a double-layer structure, including an equipment frame 3 and a test frame 2, and the equipment frame 3 is located above the test frame 2, and the sensor, controller 5 and display screen 6 are arranged on the test frame 2, and a plurality of openings 7 are opened on the equipment frame 3, and the pull rope passes through the opening 7. This design separates the UAV from the test equipment when performing a lift test on the UAV, and at the same time utilizes the opening 7 and the pull rope for guidance to prevent multiple pull ropes from being easily entangled during the rising process of the UAV.

[0025] In a preferred embodiment of the above-mentioned UAV lift inspection equipment, the controller 5 includes a processor and a storage module. The processor is used to integrate the test data of multiple high-precision tension sensors 4, and the storage module is used to store the working records of the high-precision tension sensors 4. The processor integrates and processes the test data of multiple high-precision tension sensors 4, and transmits them to the display screen 6 for display to ensure the detection efficiency. The storage module can store the working records of the high-precision tension sensors 4 to facilitate subsequent data analysis and processing. The storage module can use a conventional storage disk.

[0026] In the preferred embodiment of the above-mentioned UAV lift inspection equipment, the ring 16 is a strip structure, the outer surface of the ring 16 is a Velcro 18, the inner surface of the ring 16 is a Velcro mother tape 17, and the Velcro mother tape 17 is bonded to the Velcro 18. This design can adjust the inner diameter of the ring 16 to adapt to the binding position of the UAV according to different test positions of the UAV, such as the fuselage and the wing rod where the propeller is installed.

[0027] In the preferred embodiment of the above-mentioned UAV lift inspection equipment, a slot 14 is provided at the corner of the test frame 2, a fixing slot 15 is provided around the outside of the slot 14, the equipment frame 3 is adapted to be connected to the slot 14 through a support rod 8, and a fixing ring 9 is provided on the support rod 8, and the fixing ring 9 is respectively connected to the support rod 8 and the fixing slot 15 through a threaded structure. This design facilitates the separation of the test frame 2 and the equipment frame 3 when the test equipment is inspected and repaired.

[0028] In a preferred embodiment of the above-mentioned UAV lift inspection device, a vertical plate 10 is provided on one side of the equipment frame 3, and a pull rod 11 is installed on the vertical plate 10. This design uses the pull rod 11 as a force application point, which makes it easier to carry and move the device.

[0029] In the preferred solution of the above-mentioned UAV lift inspection equipment, a battery pack 13 is configured on the test frame 2. The battery pack 13 is a storage battery structure. The storage battery is electrically connected to the sensor and the controller 5. The battery pack 13 with the storage battery structure provides power for the sensor, the controller 5 and the display screen 6, avoiding the trouble of frequent replacement of power supplies, and is also beneficial to environmental protection.

[0030] The lift inspection equipment for the unmanned aerial vehicle measures the lift of the unmanned aerial vehicle through a high-precision tension sensor 4 installed on a detection frame 1. The sensor is provided with a pull rod 11 and a pull rope. A ring 16 is provided at the end of the pull rope for binding the fuselage of the unmanned aerial vehicle equipment and the wing rod to detect the lift of the unmanned aerial vehicle. During the inspection, only the fuselage can be bound, or only the wings of the unmanned aerial vehicle can be bound, and the fuselage and wings can also be bound at the same time. The sensor transmits the measured data to the controller 5, and the controller 5 integrates and processes the data and transmits it to the display screen 6 for display via a data line. At the same time, the controller 5 also includes a storage module that can store the working records of the high-precision tension sensor 4. The equipment frame 3 is connected to the test frame 2 through a support rod 8, and the connection between the fixing ring 9 and the fixing groove 15 is utilized to facilitate the disassembly and assembly between the test frame 2 and the equipment frame 3.

[0031] The entire device adopts an intelligent control method to improve the detection efficiency. The test frame 2 is also equipped with a battery pack 13 to provide power for the sensor, controller 5 and display screen 6. Through this design, the drone lift inspection equipment has a simple structure, is easy to operate, and can quickly and accurately detect the lift performance of the drone.

[0032] 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. UAV lift inspection equipment, characterized in that: The invention comprises a detection frame (1), a sensor, a controller (5) and a display screen (6) are installed on the detection frame (1), a tension rod (12) is arranged on the sensor, a pull rope is tied to the tension rod (12), the sensor comprises a plurality of high-precision tension sensors (4), the high-precision tension sensors (4) are used to correspond to different positions of a drone, the high-precision tension sensors (4) are connected to the controller (5) via a data line, the controller (5) is connected to the display screen (6) via a data line, a plurality of operation buttons are arranged on the controller (5), a ferrule (16) is arranged at the end of the pull rope, and the ferrule (16) is used to tie up the drone equipment.

2. The UAV lift inspection device according to claim 1, characterized in that: The detection frame (1) is a double-layer structure, comprising an equipment frame (3) and a test frame (2), wherein the equipment frame (3) is located above the test frame (2), the sensor, the controller (5) and the display screen (6) are arranged on the test frame (2), and the equipment frame (3) is provided with a plurality of openings (7), and the pull rope passes through the openings (7).

3. The UAV lift inspection device according to claim 2, characterized in that: The controller (5) comprises a processor and a storage module, the processor being used to integrate test data of a plurality of high-precision tension sensors (4), and the storage module being used to store working records of the high-precision tension sensors (4).

4. The UAV lift inspection device according to claim 3, characterized in that: The ferrule (16) is a strip-shaped structure, the outer surface of the ferrule (16) is a Velcro tape (18), the inner surface of the ferrule (16) is a Velcro mother tape (17), and the Velcro mother tape (17) is bonded to the Velcro tape (18).

5. The UAV lift inspection device according to claim 4, characterized in that: The test frame (2) is provided with a slot (14) at a corner, and a fixing slot (15) is provided around the outer side of the slot (14). The equipment frame (3) is adaptively connected to the slot (14) via a support rod (8), and a fixing ring (9) is provided on the support rod (8). The fixing ring (9) is respectively connected to the support rod (8) and the fixing slot (15) via a threaded structure.

6. The UAV lift inspection device according to claim 5, characterized in that: A vertical plate (10) is provided on one side of the equipment rack (3), and a pull rod (11) is installed on the vertical plate (10).

7. The UAV lift inspection device according to claim 6, characterized in that: The test stand (2) is provided with a battery pack (13), the battery pack (13) being a storage battery structure, and the storage battery is electrically connected to the sensor and the controller (5).

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