Unmanned aerial vehicle cabin lifting mechanism and unmanned inspection vehicle

By using screw assembly and slide rail lifting mechanism in the drone inspection vehicle, the problems of inadequate inspection and unstable lifting in the existing technology have been solved, and the smooth lifting and efficient inspection of the drone have been achieved, and the quality and efficiency of the inspection have been improved.

CN222769602UActive Publication Date: 2025-04-18HUBEI GUORUI INTELLIGENT EQUIP
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Patent Information

Application Number
CN202421755879.6
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-07-23
Publication Date
2025-04-18
Estimated Expiration
2034-07-23

AI Technical Summary

Technical Problem

The existing drone inspection vehicles have problems such as inadequate inspection, blind spots in the substation inspection, and inability to cover the insulation and leads of the equipment during the inspection, and the stability of the automatic take-off and landing mechanism is insufficient, which affects the take-off and landing of the drone.

Method used

A lifting mechanism with screw assembly and four slide rails is installed in four to ensure the stability of the lifting process, and an energy storage module and sunroof mechanism are set up in the unmanned patrol vehicle to simplify operation and expand the box space.

Benefits of technology

It has achieved smooth lifting and efficient inspection of drones, reduced the demand for manual inspection, improved the quality, safety and efficiency of inspections, and extended the use time of drones and the driving distance of unmanned vehicles.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model discloses an unmanned aerial vehicle cabin lifting mechanism and an unmanned inspection vehicle, and relates to the technical field of unmanned aerial vehicles. The device further comprises a lifting tray, sliding rails are arranged on the opposite faces of the two fixing frames, the lifting tray is arranged between the two fixing frames, and the two sides of the lifting tray are connected with the sliding rails through sliding blocks respectively. At least one fixing frame is provided with a driving mechanism used for driving the lifting tray to ascend and descend. The driving mechanism comprises a lead screw, a motor and a speed reducer. The lead screw is connected with the fixing frame through a bearing seat, and a nut seat on the lead screw is connected with the lifting tray. And driving shafts of the motor and the speed reducer are connected with the screw rod.
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Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to a lifting mechanism for a cabin of an unmanned aerial vehicle and an unmanned inspection vehicle. Background Art

[0002] With the rapid development of electric power technology, people's demand for electricity is getting higher and higher. Therefore, the normal operation of substations is particularly important to people. However, due to the complex spatial installation of substation equipment, the current conventional inspection methods include manual and wheeled robot inspections. This inspection method often fails to inspect in place and has inspection blind spots. It cannot cover the external insulation, leads, wire clamps, connectors, meters, etc. of various equipment in the substation, making it difficult to ensure the quality, safety and efficiency of the inspection.

[0003] The existing substation inspection vehicle with automatic take-off and landing of drones, although it avoids the need for inspectors to get off the vehicle to take off and recover the drone, still requires personnel to drive the vehicle to the destination. In addition, the scissor-fork connecting rod mechanism used in the automatic take-off and landing mechanism is lightweight, but the lifting is not stable, which affects the take-off and landing of the drone. When driving on uneven roads, the overall mechanism will slow down, and long-term use will affect the service life of the drone nest. After each use, it is extremely inconvenient to refuel the vehicle and charge the nest. Utility Model Content

[0004] In view of the defects existing in the prior art, the purpose of the utility model is to provide a UAV cabin lifting mechanism and an unmanned inspection vehicle, which adopt a screw assembly and add four slide rails to ensure a smooth lifting process.

[0005] In order to achieve the above purpose, the technical solution adopted by the utility model is: a UAV cabin lifting mechanism, including two relatively arranged fixed frames; also including a lifting tray, the opposite surfaces of the two fixed frames are provided with slide rails, the lifting tray is arranged between the two fixed frames, and the two sides of the lifting tray are respectively connected to the slide rails through sliders; at least one fixed frame is provided with a driving mechanism for driving the lifting tray to rise and fall, the driving mechanism includes a screw rod, a motor and a reducer; the screw rod is connected to the fixed frame through a bearing seat, and the nut seat on the screw rod is connected to the lifting tray; the driving shaft of the motor and the reducer is connected to the screw rod.

[0006] A further improvement is that a vibration-damping pad is provided at the bottom of the fixing frame, and a buffer pad is provided at the bottom of the lifting tray.

[0007] A further improvement is that a guardrail is provided at the edge of the lifting tray.

[0008] A further improvement is that an in-place detection component and a buffer limit block are arranged on the fixing frame.

[0009] The utility model also provides an unmanned inspection vehicle, comprising a chassis and a vehicle box arranged on the chassis, wherein the vehicle box is provided with a lifting mechanism for the cabin of the unmanned aerial vehicle as described above, and the cabin and the unmanned aerial vehicle are arranged on the lifting tray.

[0010] A further improvement is that a sunroof mechanism is arranged on the top of the vehicle box, and the sunroof mechanism comprises a sunroof frame and two day window slides; a guide shaft is arranged on the sunroof frame, and the two day window slides are respectively slidably arranged on the guide shaft through linear bearings.

[0011] A further improvement is that the sunroof mechanism also includes a driving motor, a rack is provided on the bottom surface of the sunroof slide plate, and a gear meshing with the rack is provided on the driving shaft of the driving motor.

[0012] A further improvement is that a waterproof enclosure is arranged around the window in the skylight frame.

[0013] A further improvement is that side doors are respectively provided on both sides of the vehicle box, and the tops of the side doors are connected to the vehicle box through hinges.

[0014] A further improvement is that an energy storage module is arranged inside the vehicle box, and a main radar and a camera are arranged on the top of the vehicle box.

[0015] The beneficial effects of the utility model are:

[0016] 1. The utility model can control the unmanned vehicle to drive to the designated location through the mobile phone APP, and no personnel are required to drive there, which greatly improves the comfort and work efficiency of the inspection personnel.

[0017] 2. The drone nest of this utility model is powered by the unmanned vehicle, and there is no need for personnel to replace the drone battery or charge the nest separately. After use, you only need to insert the charging gun into the charging port of the unmanned vehicle to complete the charging, which is simpler to operate.

[0018] 3. The utility model has a compact structure, a large compartment space, and an energy storage device is provided at the front section, which greatly prolongs the use time of the UAV and the driving distance of the unmanned vehicle.

[0019] 4. The lifting mechanism of the utility model adopts a screw rod assembly and four additional slide rails to ensure a smooth lifting process. In addition, there are buffer pads around the tray and the overall frame is equipped with shock-absorbing pads. Even if it is driving on an uneven road, the mechanism will not slow down too much and will not affect its service life. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] Figure 1 This is a schematic diagram of the structure of the UAV cabin lifting mechanism in the embodiment of the utility model;

[0021] Figure 2This is a schematic diagram of the structure of an unmanned inspection vehicle in an embodiment of the utility model;

[0022] Figure 3 This is a schematic diagram of the structure of the unmanned inspection vehicle after the box is opened in the embodiment of the utility model;

[0023] Figure 4 This is a structural schematic diagram of the skylight mechanism in the embodiment of the utility model;

[0024] Figure 5 It is an enlarged schematic diagram of the gear and rack parts in the embodiment of the utility model.

[0025] Reference numerals:

[0026] 1-fixed frame; 11-slide rail; 12-in-place detection component; 13-buffer limit block; 14-vibration damping pad;

[0027] 2-lifting tray; 21-slider; 22-guardrail; 23-buffer pad;

[0028] 3-driving mechanism; 31-screw rod; 32-nut seat; 33-motor and reducer; 34-bearing seat;

[0029] 4- Chassis;

[0030] 5-carriage; 51-side door; 52-hinge; 53-main radar; 54-camera; 55-energy storage module;

[0031] 6-skylight mechanism; 61-skylight frame; 62-guide shaft; 63-linear bearing; 64-waterproof enclosure; 65-skylight slide plate; 66-rack; 67-drive motor; 68-gear; 69-window;

[0032] 7-cabin; 71-drone. DETAILED DESCRIPTION

[0033] The embodiments of the present invention are described in detail below. The embodiments are shown in the accompanying drawings, wherein the same or similar numbers throughout represent the same or similar elements or elements with the same or similar functions.

[0034] In the description of the present invention, it should be noted that directional words, such as the terms "center", "lateral (X)", "longitudinal (Y)", "vertical (Z)", "length", "width", "thickness", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", "clockwise", "counterclockwise", etc., indicating directions and positional relationships are based on the directions or positional relationships shown in the accompanying drawings, and are only for the convenience of narrating the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and cannot be understood as limiting the specific protection scope of the present invention.

[0035] The following is a further description of the specific implementation of the utility model in conjunction with the drawings of the specification, so that the technical solution and its beneficial effects of the utility model are clearer and more explicit. The following description of the embodiments with reference to the drawings is exemplary and intended to explain the utility model, but cannot be understood as limiting the utility model.

[0036] See also Figure 1 As shown, the embodiment of the utility model provides a UAV cabin lifting mechanism, including two relatively arranged fixed frames 1; and also including a lifting tray 2, the opposite surfaces of the two fixed frames 1 are provided with slide rails 11, the lifting tray 2 is arranged between the two fixed frames 1, and the two sides of the lifting tray 2 are respectively connected to the slide rails 11 through sliders 21; specifically, a vibration-damping pad 14 is arranged at the bottom of the fixed frame 1, and a buffer pad 23 is arranged at the bottom of the lifting tray 2. A guardrail 22 is arranged at the edge of the lifting tray 2. The fixed frame 1 is provided with an in-place detection component 12 and a buffer limit block 13.

[0037] At least one fixed frame 1 is provided with a driving mechanism 3 for driving the lifting tray 2 to rise and fall, and the driving mechanism 3 includes a screw rod 31 and a motor and a reducer 33; the screw rod 31 is connected to the fixed frame 1 through a bearing seat 34, and the nut seat 32 on the screw rod 31 is connected to the lifting tray 2; the driving shaft of the motor and the reducer 33 is connected to the screw rod 31.

[0038] See also Figure 2 and Figure 3 As shown, the embodiment of the utility model also provides an unmanned inspection vehicle, including a chassis 4 and a car box 5 arranged on the chassis 4, wherein the car box 5 is provided with the above-mentioned drone cabin lifting mechanism, and the cabin 7 and the drone 71 are arranged on the lifting tray 2. Specifically, side doors 51 are respectively arranged on both sides of the car box 5, and the top of the side door 51 is connected to the car box 5 through a hinge 52. An energy storage module 55 is arranged inside the car box 5, and a main radar 53 and a camera 54 are arranged on the top of the car box 5.

[0039] See also Figure 4 and Figure 5As shown, a skylight mechanism 6 is provided on the top of the vehicle box 5, and the skylight mechanism 6 includes a skylight frame 61 and two skylight slide plates 65; a guide shaft 62 is provided on the skylight frame 61, and the two skylight slide plates 65 are respectively slidably provided on the guide shaft 62 through linear bearings 63. Specifically, the skylight mechanism 6 also includes a driving motor 67, a rack 66 is provided on the bottom surface of the skylight slide plate 65, and a gear 68 meshing with the rack 66 is provided on the driving shaft of the driving motor 67. A waterproof enclosure 64 is provided around the window 69 in the skylight frame 61.

[0040] The working principle of the utility model is:

[0041] The utility model controls the unmanned vehicle to drive to the designated location through the mobile phone APP, and then controls the skylight to open. Then the lifting structure lifts the drone nest, and the weather station on the top of the nest obtains weather information. After determining that the take-off conditions are met, the drone takes off and starts inspection, and the same method is used to recover the drones in turn.

[0042] In the description of the specification, the description with reference to the terms "one embodiment", "preferably", "example", "specific example" or "some examples" means that the specific features, structures, materials or characteristics described in conjunction with the embodiment or example are included in at least one embodiment or example of the utility model, and the schematic expressions of the above terms in this specification do not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials or characteristics described may be combined in any one or more embodiments or examples in a suitable manner.

[0043] Through the description of the above structure and principle, technicians in the relevant technical field should understand that the present invention is not limited to the above-mentioned specific implementation methods. Improvements and substitutions based on the present invention using the known technology in the field all fall within the protection scope of the present invention and should be defined by the claims.

Claims

1. A UAV cabin lifting mechanism, comprising two oppositely arranged fixing frames (1); characterized in that: It also comprises a lifting tray (2), and the opposite surfaces of the two fixed frames (1) are provided with slide rails (11), the lifting tray (2) is arranged between the two fixed frames (1), and the two sides of the lifting tray (2) are respectively connected to the slide rails (11) through sliders (21); At least one fixed frame (1) is provided with a driving mechanism (3) for driving the lifting tray (2) to rise and fall, the driving mechanism (3) comprising a screw rod (31) and a motor and a reducer (33); the screw rod (31) is connected to the fixed frame (1) via a bearing seat (34), and a nut seat (32) on the screw rod (31) is connected to the lifting tray (2); the driving shaft of the motor and the reducer (33) is connected to the screw rod (31).

2. The UAV cabin lifting mechanism according to claim 1, characterized in that: A vibration-damping pad (14) is provided at the bottom of the fixing frame (1), and a buffer pad (23) is provided at the bottom of the lifting tray (2).

3. The UAV cabin lifting mechanism according to claim 1, characterized in that: A guardrail (22) is provided at the edge of the lifting tray (2).

4. The UAV cabin lifting mechanism according to claim 1, characterized in that: The fixing frame (1) is provided with an in-place detection component (12) and a buffer limit block (13).

5. An unmanned inspection vehicle, comprising a chassis (4) and a vehicle box (5) arranged on the chassis (4), characterized in that: The vehicle box (5) is provided with a UAV cabin lifting mechanism as claimed in any one of claims 1 to 4, and a cabin (7) and a UAV (71) are provided on the lifting tray (2).

6. The unmanned inspection vehicle according to claim 5, characterized in that: A sunroof mechanism (6) is arranged on the top of the vehicle box (5), and the sunroof mechanism (6) comprises a sunroof frame (61) and two sunroof slide plates (65); a guide shaft (62) is arranged on the sunroof frame (61), and the two sunroof slide plates (65) are slidably arranged on the guide shaft (62) through linear bearings (63) respectively.

7. The unmanned inspection vehicle according to claim 6, characterized in that: The sunroof mechanism (6) further comprises a driving motor (67), a rack (66) is provided on the bottom surface of the sunroof slide plate (65), and a driving shaft of the driving motor (67) is provided with a gear (68) meshing with the rack (66).

8. The unmanned inspection vehicle according to claim 6, characterized in that: A waterproof enclosure (64) is arranged around the window (69) in the skylight frame (61).

9. The unmanned inspection vehicle according to claim 5, characterized in that: Side doors (51) are respectively arranged on both sides of the vehicle box (5), and the tops of the side doors (51) are connected to the vehicle box (5) via hinges (52).

10. The unmanned inspection vehicle according to claim 5, characterized in that: An energy storage module (55) is arranged inside the vehicle box (5), and a main radar (53) and a camera (54) are arranged on the top of the vehicle box (5).