Hydrogen energy power inspection unmanned aerial vehicle

Abstract

The application provides a camera-enabled hydrogen energy power inspection unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicles. The unmanned aerial vehicle comprises an unmanned aerial vehicle, a hollow rod one is arranged at the lower part of the unmanned aerial vehicle, one side of the bottom of the hollow rod one is provided with an assembly column, the other side of the assembly column is fixedly connected with an outer protective shell, an isolation unit is arranged at the joint of the outer protective shell and the assembly column, an outer cover shell is embedded in the outer protective shell, and a camera is arranged on the outer cover shell. The application solves the problems of complex assembly and disassembly processes, lack of efficient constraint and release structures, consumption of a large amount of time during maintenance, complex reassembly operation, influence on inspection efficiency, interruption of work due to power consumption during the camera shooting process, and influence on camera shooting.

Description

TECHNICAL FIELD

[0001] The application belongs to the technical field of unmanned aerial vehicles, and particularly relates to a hydrogen energy power inspection unmanned aerial vehicle capable of taking pictures. BACKGROUND

[0002] With the expansion of the scale of the power system and the upgrading of the inspection demand, the unmanned aerial vehicle becomes one of the core devices for power inspection due to its flexible maneuvering, wide coverage and the advantage of replacing manual work to enter complex and dangerous areas, wherein the picture taking function is a key carrier for the unmanned aerial vehicle to realize the inspection operation, and is required to capture the running state of the power transmission line and tower equipment in real time, record the hidden danger information such as line aging, component failure and foreign matter winding, and provide visual basis for subsequent maintenance.

[0003] The existing picture taking module has a complex assembly and disassembly process, lacks an efficient constraint and release structure, and requires a lot of time for maintenance, and the subsequent reassembly also needs complex operation, which affects the inspection efficiency, and in the picture taking process, the camera may be interrupted due to power consumption, which affects the picture taking, and therefore the hydrogen energy power inspection unmanned aerial vehicle capable of taking pictures is proposed. SUMMARY

[0004] This section aims to summarize some aspects of the embodiments of the application and briefly introduce some preferred embodiments. Some simplifications or omissions may be made in this section and the abstract and title of the specification to avoid obscuring the purpose of this section, abstract and title, and such simplifications or omissions cannot be used to limit the scope of the application.

[0005] In view of the following technical problems in the prior art: the assembly and disassembly process is complex, lacks an efficient constraint and release structure, requires a lot of time for maintenance, and the subsequent reassembly also needs complex operation, which affects the inspection efficiency, and in the picture taking process, the camera may be interrupted due to power consumption, which affects the picture taking.

[0006] To solve the above technical problems, the application provides the following technical scheme: a hydrogen energy power inspection unmanned aerial vehicle capable of taking pictures, comprising an unmanned aerial vehicle, a hollow rod one is arranged at the lower part of the unmanned aerial vehicle, one side of an assembly column is arranged at the bottom of the hollow rod one, an outer protective shell is fixedly connected to the other side of the assembly column, an isolation unit is arranged at the joint of the outer protective shell and the assembly column, an outer cover shell is arranged outside the outer protective shell, a camera is arranged on the outer cover shell, an inner circular shell is arranged in the outer protective shell, and an inner rotating part is arranged inside the inner circular shell.

[0007] By adopting the above technical scheme, the unmanned aerial vehicle provides flight power and inspection basic support as the main body, the hollow rod together with the transition support effect connecting the unmanned aerial vehicle and the assembly column, the outer protective shell of the assembly column ensures the stability of the connection, the isolation unit can isolate external impurities to ensure that the camera is not polluted during assembly, the outer cover is connected outside the outer protective shell to ensure the stability of the camera during inspection, and the inner circular shell serves as a guide to ensure the rotation of the inner rotating part.

[0008] Further, the isolation unit includes a charging base connected to the assembly column, a rotating seat rotatably connected to the charging base, a plurality of guide grooves reserved on the rotating seat, a guide rod slidingly connected in the guide groove, and a plurality of evenly distributed isolation pieces arranged between the charging base and the rotating seat, each guide rod being fixedly connected to a corresponding isolation piece.

[0009] By adopting the above technical scheme, the charging base is fixedly connected to the assembly column to achieve positioning, and can provide a charging interface for the camera-related components. During rotation of the rotating seat around the charging base, the guide rod slides in the guide groove. Since the guide rod is fixedly connected to the isolation piece, the sliding guide rod will pull the isolation piece to change the orientation, allowing the isolation pieces to approach each other or separate from each other. This allows the corresponding charging base to be opened and closed during assembly or disassembly of the camera. Meanwhile, the guide groove can constrain the movement trajectory of the guide rod to prevent the isolation piece from being misaligned.

[0010] Further, the inner rotating part includes an inner rotating shell, one side of the inner rotating shell being fixedly connected to the edge portion of the rotating seat, and one side of the inner circular shell being fixedly connected to the assembly column.

[0011] By adopting the above technical scheme, the inner circular shell is fixedly connected to the assembly column to form a stable support frame. During insertion of the guide rod into the guide cavity, the inner rotating shell will rotate due to the fit with the guide cavity, thereby pulling the rotation of the rotating seat.

[0012] Further, a pair of guide cavities are reserved on the inner rotating shell, and a pair of guide cavities are reserved on the inner circular shell.

[0013] By adopting the above technical scheme, the guide cavity provides a channel for the displacement of the guide rod into the inner circular shell, facilitating component assembly and positioning. During insertion, the guide cavity will fit with the constraint unit II. After the guide rod is inserted through the guide cavity, it can be embedded in the guide cavity. By applying force on the guide cavity, the inner rotating shell will rotate, thereby rotating the connected rotating seat.

[0014] Further, the outer shell and the outer protective shell are both provided with a restraint unit one, which comprises a guide bar fixed on the two sides of the outer shell and an assembly cavity reserved on the two sides of the outer protective shell, one side of the guide bar is connected with an embedded rod, the assembly cavity is connected with a release table, the two sides of the release table are fixed with displacement bars, the two sides of the assembly cavity are reserved with displacement cavities, and the displacement bars and the displacement cavities are matched with each other.

[0015] By adopting the above technical scheme, during the assembly of the outer shell, the guide bars on the two sides of the outer shell are inserted into the guide cavities on the two sides of the inner shell, the embedded rods connected with the guide bars are displaced into the guide cavities, during the displacement to the release table area, the embedded rods will be automatically swung into the assembly cavity, the restraint action is performed, the outer shell and the outer protective shell are restrained, the stability during the connection is ensured, during the disassembly of the camera, after the pressure is applied to the release table, the release table will be linearly displaced through the cooperation of the displacement bars and the displacement cavities, the release table will be pressed to make the embedded rods swing and reset into the guide bars, so that the outer shell can be displaced.

[0016] Further, the guide bars are reserved with accommodating cavities, the specifications of the embedded rods are matched with the size of the assembly cavity, and the embedded rods are provided with a reset member three at the pin connection position of the embedded rods and the guide bars.

[0017] By adopting the above technical scheme, the accommodating cavities on the guide bars can accommodate the embedded rods during the insertion of the embedded rods, preventing the embedded rods from protruding and affecting the insertion of the guide bars into the assembly cavity, the specifications of the embedded rods are matched with the size of the assembly cavity, ensuring that the embedded rods can be accurately inserted into the assembly cavity to achieve stable restraint, and the reset member three is assembled at the pin connection position of the embedded rods and the guide bars, when the embedded rods are displaced to the assembly cavity, the reset member three is reset to make the embedded rods swing into the assembly cavity to constitute the restraint.

[0018] Further, the guide bars are matched with the guide cavities and the guide cavities, and the guide cavities are divided into guide sections on the two sides and a rotating section in the middle.

[0019] By adopting the above technical scheme, the guide bars are matched with the guide cavities, ensuring that the guide bars can be smoothly displaced into the inner shell through the guide cavities, and the guide bars are matched with the guide cavities, so that the guide bars can be inserted into the guide cavities, and during the continuous insertion process, the guide bars will press on the cavity wall of the guide cavities, after the guide bars are displaced to the rotating section of the guide cavities, the inner rotating shell will be rotated, and then the rotating seat will be rotated.

[0020] Further, the opening of the introduction cavity is reserved with a constraint unit two, the constraint unit two comprises a avoiding cavity one reserved on the inner circular shell, the avoiding cavity one is slidably connected with a constraint platform one, the side of the constraint platform one is slidably connected with a constraint platform two, the cavity wall of the avoiding cavity one is provided with a reset member one between the constraint platform one, the constraint platform one is reserved with a avoiding cavity two matched with the constraint platform two, the cavity wall of the avoiding cavity two is provided with a reset member two between the constraint platform two, and the outer wall of the inner rotating part is reserved with an embedding entrance matched with the constraint platform two.

[0021] By adopting the above technical scheme, during the introduction of the strip plug into the introduction cavity, that is, in the guide section of the guide cavity, the outer slope surface of the constraint platform one is pressed outward, so that the constraint platform one is displaced into the avoiding cavity one, the reset member one is compressed, and the constraint platform two on the side of the constraint platform one is synchronously displaced with the constraint platform one during sliding of the constraint platform one, so that the constraint platform two can be moved out of the embedding entrance, so that the rotation of the inner rotating shell is not hindered, and during disassembly of the outer cover shell, the inner rotating shell is reset, the embedding entrance of the outer wall is aligned with the constraint platform two, at this time, the constraint platform two is slid from the avoiding cavity two and embedded into the embedding entrance under the action of the reset member two, so that the constraint platform two is positioned and constrained with the inner rotating part and the inner circular shell, the inner rotating part is prevented from rotating at will, and the subsequent assembly of the outer cover shell is facilitated.

[0022] Further, the side of the constraint platform one that protrudes outward is provided with a slope surface.

[0023] By adopting the above technical scheme, the slope surface structure of the constraint platform one outward can make the constraint platform one more smoothly displace along the avoiding cavity one during the introduction of the strip plug into the introduction cavity.

[0024] Further, the side of the constraint platform two that protrudes into the embedding entrance is provided with a slope surface.

[0025] By adopting the above technical scheme, the slope surface structure of the constraint platform two that protrudes into the embedding entrance can make the constraint platform two more smoothly displace from the embedding entrance during displacement of the constraint platform two.

[0026] The beneficial effects of the present application are:

[0027] 1、The unmanned aerial vehicle, the hollow rod one, the assembly column and the outer protective shell are connected to form a stable core frame, so that the connection of various parts during the inspection process is firm, the isolation unit at the connection of the outer protective shell and the assembly column is connected with the guide rod and the isolation piece through the rotating seat, so that the opening and closing of the charging base is achieved during assembly and disassembly of the camera, external impurities are effectively blocked, the outer cover shell is arranged outside the outer protective shell, conditions for stable assembly of the camera are provided, the stability of the camera during the inspection is ensured, and shaking during shooting is prevented to affect the shooting effect.

[0028] 2、The present application is through the fixed design of the inner rotating shell and the rotating seat, in cooperation with the guide bar and the guide cavity, the guide cavity, so that the guide bar can be smoothly pulled during the insertion period, and the inner rotating shell is rotated, and then the synchronous rotation of the rotating seat is realized, the constraint unit is through the cooperation of the embedded rod and the assembly cavity, the effect of the reset piece three, and the corresponding change of the reset piece one and the reset piece two in the constraint unit two, the slope design of the constraint platform two and the constraint platform one, realize the rapid assembly and disassembly of the outer cover shell, and after disassembly, the inner rotating part can be positioned and constrained through the constraint platform two and the embedding entrance, and a precise insertion channel is reserved for subsequent assembly.

[0029] Other features and advantages of the present application will be set forth in the following description, and in part will become apparent to those skilled in the art from the description, or can be learned by practice of the present application. The objects and other advantages of the present application can be achieved and obtained by the structure specifically pointed out in the description and drawings. BRIEF DESCRIPTION OF DRAWINGS

[0030] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings needed in the embodiment description will be briefly introduced below. Obviously, the drawings in the following description are only some embodiments of the present application, and those skilled in the art can also obtain other drawings according to these drawings without creative labor. Among them:

[0031] Figure 1 It is the overall structure schematic diagram of the embodiment of the present application;

[0032] Figure 2 It is the assembly column and outer cover shell structure schematic diagram of the embodiment of the present application;

[0033] Figure 3 It is the outer protective shell part sectional view structure schematic diagram of the embodiment of the present application;

[0034] Figure 4 It is the Figure 3 Inner X structure schematic diagram of the embodiment of the present application;

[0035] Figure 5 It is the Figure 4 Inner Y structure schematic diagram of the embodiment of the present application;

[0036] Figure 6 It is the outer protective shell structure schematic diagram of the embodiment of the present application;

[0037] Figure 7 It is the Figure 6 Inner Z structure schematic diagram of the embodiment of the present application;

[0038] Figure 8 It is the isolation unit closed structure schematic diagram of the embodiment of the present application;

[0039] Figure 9 Figure 1 is a schematic diagram of an open structure of an isolation unit according to an embodiment of the present application;

[0040] Reference signs: 100, unmanned aerial vehicle; 200, hollow rod one; 300, assembly column; 400, outer protective shell; 500, outer cover shell; 600, restraint unit one; 601, lead-in strip; 602, embedded rod; 603, release platform; 604, displacement cavity; 605, displacement strip; 606, assembly cavity; 800, inner circular shell; 801, lead-in cavity; 900, restraint unit two; 901, restraint platform one; 902, avoidance cavity one; 903, reset member one; 904, avoidance cavity two; 905, restraint platform two; 906, reset member two; 907, embedding entrance; 1000, camera; 1100, assembly seat; 1200, inner rotating member; 1201, inner rotating shell; 1202, guide cavity; 1300, isolation unit; 1301, charging base; 1302, rotating seat; 1303, guide groove; 1304, guide rod; 1305, isolation sheet. DETAILED DESCRIPTION

[0041] In order to make the above objectives, features and advantages of the present application more apparent, the specific embodiments of the present application will be described in detail below with reference to the accompanying drawings.

[0042] In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present application. However, it will be apparent to one skilled in the art that the present application can be practiced without the specific details given herein, that the present application can be practiced with other than the described embodiments and that variations from the particular embodiments described herein can be made and still be within the scope of the present application.

[0043] Secondly, the "one embodiment" or "an embodiment" referred to herein means that a specific feature, structure, or characteristic described can be included in at least one implementation of the present application. The "in one embodiment" appearing in different places in the specification does not all refer to the same embodiment, nor is it an alternative or selective embodiment mutually exclusive with other embodiments.

[0044] Thirdly, the present application is described in detail in conjunction with the schematic diagram, and in the detailed description of the embodiments of the present application, the sectional view of the device structure is partially enlarged without the general proportion for the convenience of description, and the schematic diagram is only an example, which should not limit the scope of protection of the present application herein. In addition, the three-dimensional spatial dimensions of length, width and depth should be included in actual manufacture.

[0045] Reference Figures 1-9The embodiment of the present application provides a kind of camera hydrogen energy power inspection unmanned aerial vehicle, including unmanned aerial vehicle 100, the lower part of unmanned aerial vehicle 100 is equipped with hollow stick one 200, the bottom of hollow stick one 200 is equipped with one side of assembly column 300, the other side of assembly column 300 is fixedly connected with outer protective shell 400, the junction of outer protective shell 400 and assembly column 300 is equipped with isolation unit 1300, outer protective shell 400 is equipped with outer cover shell 500 outside, camera 1000 is equipped with via assembly seat 1100 on outer cover shell 500, outer protective shell 400 is equipped with inner circular shell 800, inner rotating part 1200 is equipped with inside inner circular shell 800, unmanned aerial vehicle 100 provides flight power and inspection basic support as main body, hollow stick one 200 plays the transition support effect of connecting unmanned aerial vehicle 100 and assembly column 300, assembly column 300 assembles outer protective shell 400 to ensure the stability of connection, isolation unit 1300 can isolate external impurity interference to ensure that camera 1000 is not assembled during blocking impurity interface pollution, outer cover shell 500 is covered in outer protective shell 400, to ensure that camera 1000 is stably connected during inspection, inner circular shell 800 is as a guide, to ensure that the rotation of inner rotating part 1200 is carried out.

[0046] Isolation unit 1300 includes charging base 1301, charging base 1301 is connected with assembly column 300, rotating seat 1302 is rotatably connected on charging base 1301, a plurality of guide grooves 1303 are reserved on rotating seat 1302, guide rod 1304 is slidably connected in guide groove 1303, a plurality of uniformly distributed isolation sheets 1305 are equipped between charging base 1301 and rotating seat 1302, each guide rod 1304 is fixedly connected with corresponding isolation sheet 1305, charging base 1301 is fixedly connected with assembly column 300 on one hand to realize positioning, and on the other hand can provide charging interface for related components of camera 1000, during the rotation of rotating seat 1302 around charging base 1301, guide rod 1304 synchronously slides in guide groove 1303, because guide rod 1304 is fixedly connected with isolation sheet 1305, sliding guide rod 1304 will drag isolation sheet 1305 to change direction, so that isolation sheet 1305 approaches each other or separates from each other, so that the corresponding opening and closing of charging base 1301 can be realized during assembling or disassembling camera 1000, and guide groove 1303 can constrain the movement track of guide rod 1304 to prevent isolation sheet 1305 from being misaligned.

[0047] Inner rotating part 1200 includes inner rotating shell 1201, one side of inner rotating shell 1201 is fixedly connected with the edge portion of rotating seat 1302, one side of inner circular shell 800 is fixedly connected with assembly column 300, inner circular shell 800 is fixedly connected with assembly column 300, to form a stable support frame, during the insertion of lead-in strip 601 into guide cavity 1202, inner rotating shell 1201 is rotated via the adhesion with guide cavity 1202, and then the rotation of rotating seat 1302 is dragged.

[0048] A pair of guide cavities 1202 are reserved on the inner rotating shell 1201, and a pair of guide cavities 801 are reserved on the inner circular shell 800, which provide a path for the guide bars 601 to move into the inner circular shell 800, facilitating the assembly and positioning of the components, and will be in close contact with the constraint unit two 900 during the insertion. The guide cavities 1202 are reserved on the inner rotating shell 1201, and after the guide bars 601 are inserted through the guide cavities 801, they can be embedded in the guide cavities 1202. By applying force on the guide cavities 1202, the inner rotating shell 1201 will rotate, thereby rotating the rotating seat 1302 connected to it.

[0049] The constraint unit one 600 is installed on both sides of the outer shell 500 and the outer protective shell 400. The constraint unit one 600 includes the guide bars 601 fixed on both sides of the outer shell 500 and the assembly cavities 606 reserved on both sides of the outer protective shell 400. One side of the embedded rod 602 is pinned to the guide bar 601. The dismounting table 603 is slidably connected in the assembly cavity 606. The displacement bars 605 are fixed on both sides of the dismounting table 603. The displacement cavities 604 are reserved on both sides of the assembly cavity 606. The displacement bars 605 and the displacement cavities 604 are matched with each other. During the assembly of the outer shell 500, the guide bars 601 on both sides of the outer shell 500 are inserted into the guide cavities 801 on both sides of the inner circular shell 800. The embedded rod 602 pinned to the guide bar 601 moves into the guide cavity 801. During the displacement to the dismounting table 603 area, the embedded rod 602 will actively swing into the assembly cavity 606 to perform a constraint action, so that the outer shell 500 and the outer protective shell 400 are constrained, ensuring stability during connection. When the camera 1000 needs to be removed, pressure is applied to the dismounting table 603. The dismounting table 603 will slide linearly through the cooperation of the displacement bars 605 and the displacement cavities 604. The dismounting table 603 slides and presses the embedded rod 602, causing the embedded rod 602 to swing back to the guide bar 601 around the pin joint. In this way, the outer shell 500 can be displaced.

[0050] The guide bar 601 is reserved with a containing cavity, the embedded rod 602 is matched with the size of the assembly cavity 606, and the pin joint between the embedded rod 602 and the guide bar 601 is provided with a reset member three. The reset member three is a spiral beryllium copper wire that can generate an opposite torsion force when it is deformed and restored. The containing cavity on the guide bar 601 can accommodate the embedded rod 602 during insertion, preventing the embedded rod 602 from protruding and affecting the insertion of the guide bar 601 into the assembly cavity 606. The embedded rod 602 is matched with the size of the assembly cavity 606, ensuring that the embedded rod 602 can be accurately embedded in the assembly cavity 606 for stable constraint. The reset member three is assembled at the pin joint between the embedded rod 602 and the guide bar 601. When the embedded rod 602 moves to the assembly cavity 606, the reset member three resets, causing the embedded rod 602 to swing into the assembly cavity 606 to form a constraint.

[0051] The introduction bar 601 is adapted to the introduction cavity 801 and the guide cavity 1202, the guide cavity 1202 is divided into guide sections at both sides and a rotating section in the middle, the introduction bar 601 is adapted to the introduction cavity 801, which ensures that the introduction bar 601 can smoothly displace to the inside of the inner circular shell 800 through the introduction cavity 801, and the introduction bar 601 is adapted to the guide cavity 1202, so that the introduction bar 601 can be embedded in the guide cavity 1202. During the continuous insertion process, the introduction bar 601 will press on the cavity wall of the guide cavity 1202, and after the introduction bar 601 displaces to the rotating section of the guide cavity 1202, the inner rotating shell 1201 will rotate, thereby dragging the rotating seat 1302 to rotate.

[0052] The openings of the introduction cavity 801 are reserved for the constraint unit two 900, which includes the avoidance cavity one 902 reserved on the inner circular shell 800, the avoidance cavity one 902 is slidably connected with the constraint platform one 901, the side of the constraint platform one 901 is slidably connected with the constraint platform two 905, the cavity wall of the avoidance cavity one 902 is provided with the reset member one 903 between the constraint platform one 901, the constraint platform one 901 is reserved with the avoidance cavity two 904 adapted to the constraint platform two 905, the cavity wall of the avoidance cavity two 904 is provided with the reset member two 906 between the constraint platform two 905, the reset member one and the reset member two are both springs, the outer wall of the inner rotating part 1200 is reserved with the embedding entrance 907 adapted to the constraint platform two 905, during the insertion of the introduction bar 601 into the introduction cavity 801, that is, in the guide section of the guide cavity 1202, the constraint platform one 901 will be pressed towards the outer slope surface, so that the constraint platform one 901 displaces into the avoidance cavity one, and the reset member one 903 is compressed. During the sliding of the constraint platform one 901, the constraint platform two 905 on the side of the constraint platform one 901 synchronously displaces with the constraint platform one 901, so that the constraint platform two 905 can move out of the embedding entrance 907, so as not to hinder the rotation of the inner rotating shell 1201. During the disassembly of the outer cover shell 500, the inner rotating shell 1201 is reset, the embedding entrance 907 of the outer wall is aligned with the constraint platform two 905, at this time, the constraint platform two 905 slides out of the avoidance cavity two 904 and is embedded into the embedding entrance 907 under the action of the reset member two 906, so as to achieve the positioning and constraint of the inner rotating part 1200 and the inner circular shell 800, prevent the inner rotating part 1200 from rotating randomly, and facilitate the subsequent assembly of the outer cover shell 500.

[0053] The outwardly protruding side of the constraint platform one 901 is provided with a slope surface, and the outwardly protruding slope surface structure of the constraint platform one 901 can make the constraint platform one 901 more smoothly displace along the avoidance cavity one 902 during the insertion of the introduction bar 601 into the introduction cavity 801.

[0054] The side of the constraint platform two 905 protruding into the embedding entrance 907 is provided with a slope surface, and the slope surface structure of the side of the constraint platform two 905 protruding into the embedding entrance 907 can make the constraint platform two 905 more smoothly displace during the displacement of the constraint platform two 905.

[0055] The charging base 1301 is provided with a plurality of charging contacts I connected to the battery of the unmanned aerial vehicle 100 via wires, and the inside of the outer shell 500 is provided with a fitting column, and the side of the fitting column close to the assembly column 300 is provided with charging contacts II electrically connected to the camera 1000. During assembly, the charging contacts II are fitted with the charging contacts I, so that the camera 1000 in the camera can be charged, preventing the camera 1000 from running out of power and affecting work.

[0056] The embodiment is specific:

[0057] During the assembly of connecting the camera 1000 and the unmanned aerial vehicle 100, the lead-in strip 601 is inserted into the lead-in cavity 801 and the guide cavity 1202 of the inner rotating shell 1201. During the continuous insertion of the lead-in strip 601, it touches and exerts force on the guide cavity 1202, and rotates the inner rotating shell 1201 through the fitting of the rotating section of the guide cavity 1202. The inner rotating shell 1201 rotates the fixed rotating seat 1302 together, and the rotating seat 1302 rotates around the charging base 1301, dragging the guide rod 1304 to slide along the guide groove 1303, and then the guide rod 1304 drags the isolation sheet 1305 to unfold, thereby controlling the opening of the charging base 1301 to be connected with the camera 1000, and synchronously moving the restraint unit I 600. The embedded rod 602 on the lead-in strip 601 is first actively swung to the assembly cavity 606 during the lead-in process, and is fixed by the restraint of the reset member III to fix the outer shell 500. If disassembly is required, the embedded rod 602 is first pressed towards the release platform 603, and the release platform 603 slides along the displacement cavity 604 through the displacement strip 605, thereby compressing the embedded rod 602 to reset and release the restraint to enable displacement and disassembly, and the isolation sheet 1305 is closed to block impurities during disassembly;

[0058] During the insertion of the lead-in strip 601 into the lead-in cavity 801, the slope of the restraint platform I 901 is first pressed, the restraint platform I 901 slides along the avoidance cavity I 902 and compresses the reset member I 903, synchronously dragging the restraint platform II 905 out of the embedded port 907 of the inner rotating member 1200, avoiding hindering the rotation of the inner rotating shell 1201, and the slope structure of the restraint platform II 905 makes the movement out of the action more smooth. After the outer shell 500 is disassembled, the inner rotating shell 1201 is first reset, so that the embedded port 907 is aligned with the restraint platform II 905, and the reset member II 906 then embeds the restraint platform II 905 into the embedded port 907, thereby restraining the inner rotating member 1200 from rotating at will, so as to facilitate subsequent reconnection. Finally, through the trajectory restraint and reset of each component, the whole process of assembly and disassembly is continuous and smooth.

[0059] It is to be understood that the development of the particular implementations described herein was motivated by the desire to solve real-world problems, and as such the claimed implementations can be susceptible to further implementation while still being generically consistent with the descriptions provided herein. Specifically, although many of the examples provided herein describe one or more implementations with any particular feature, an individual feature can be replaced by alternative features within the scope of the application. Thus, features discussed in one example can be interchanged with features in another example. Any implementation of more than one feature disclosed herein is specifically referenced within the scope of the application.

[0060] It should be noted that the above examples are merely intended to illustrate the technical solutions of the present application but not to limit the present application. Although the present application is described in detail with reference to the preferred embodiments, those skilled in the art should understand that the technical solutions of the present application can be modified or equivalently replaced without departing from the spirit and scope of the present application, and all modifications and equivalent replacements should be included in the scope of the claims of the present application.

Claims

1. A camera-enabled hydrogen energy power inspection unmanned aerial vehicle, comprising an unmanned aerial vehicle (100), characterized in that, The lower part of the unmanned aerial vehicle (100) is provided with a hollow rod (200), one side of the bottom of the hollow rod (200) is provided with an assembly column (300), the other side of the assembly column (300) is fixedly connected with an outer protective shell (400), the joint between the outer protective shell (400) and the assembly column (300) is provided with an isolation unit (1300), the outer protective shell (400) is provided with an outer cover shell (500) outside, the outer cover shell (500) is provided with a camera (1000), the inner part of the outer protective shell (400) is provided with an inner circular shell (800), and the inner part of the inner circular shell (800) is provided with an inner rotating part (1200). The isolation unit (1300) comprises a charging base (1301) connected with the assembly column (300), a rotating seat (1302) rotatably connected with the charging base (1301), a plurality of guide grooves (1303) reserved on the rotating seat (1302), a guide rod (1304) slidably connected in the guide groove (1303), and a plurality of uniformly distributed isolation sheets (1305) arranged between the charging base (1301) and the rotating seat (1302), each guide rod (1304) being fixedly connected with a corresponding isolation sheet (1305). The inner rotating part (1200) comprises an inner rotating shell (1201), one side of the inner rotating shell (1201) is fixedly connected with the edge of the rotating seat (1302), and one side of the inner circular shell (800) is fixedly connected with the assembly column (300). A pair of guide cavities (1202) are reserved on the inner rotating shell (1201), and a pair of import cavities (801) are reserved on the inner circular shell (800). Both sides of the outer cover shell (500) and the outer protective shell (400) are provided with a constraint unit (600), the constraint unit (600) comprises an import strip (601) fixedly connected to both sides of the outer cover shell (500) and an assembly cavity (606) reserved on both sides of the outer protective shell (400), one side of the import strip (601) is pinned with an embedded rod (602), the assembly cavity (606) is slidably connected with a release table (603), both sides of the release table (603) are fixedly connected with a displacement strip (605), both sides of the assembly cavity (606) are provided with a displacement cavity (604), and the displacement strip (605) and the displacement cavity (604) are matched with each other.

2. The camera-capable hydrogen energy power inspection unmanned aerial vehicle according to claim 1, characterized in that: The import strip (601) is provided with a containing cavity, the specification of the embedded rod (602) is matched with the size of the assembly cavity (606), and the pin joint between the embedded rod (602) and the import strip (601) is provided with a reset part three.

3. The imageable hydrogen energy power inspection unmanned aerial vehicle according to claim 2, characterized in that: The import strip (601) is matched with the import cavity (801) and the guide cavity (1202), and the guide cavity (1202) is divided into a guide section on both sides and a rotating section in the middle.

4. The imageable hydrogen energy power inspection unmanned aerial vehicle according to claim 3, characterized in that: The openings of the introduction cavities (801) are reserved with restraint units two (900), the restraint units two (900) contain avoidance cavities one (902) reserved on the inner circular shell (800), the avoidance cavities one (902) are slidably connected with restraint platforms one (901), the side of the restraint platforms one (901) is slidably connected with restraint platforms two (905), the cavity wall of the avoidance cavities one (902) and the restraint platforms one (901) are provided with reset units one (903), the restraint platforms one (901) are reserved with avoidance cavities two (904) matched with the restraint platforms two (905), the cavity wall of the avoidance cavities two (904) and the restraint platforms two (905) are provided with reset units two (906), and the outer wall of the inner rotating part (1200) is reserved with embedding entrances (907) matched with the restraint platforms two (905).

5. The imageable hydrogen energy power inspection unmanned aerial vehicle according to claim 4, characterized in that: The outwardly protruding side of the restraint platforms one (901) is provided with a slope.

6. The imageable hydrogen energy power inspection unmanned aerial vehicle according to claim 5, characterized in that: The side of the restraint platforms two (905) embedded in the embedding entrances (907) is provided with a slope, and the inner wall of the outer cover shell (500) and the peripheral wall of the outer protective shell (400) are matched in size.

Images