High-altitude unmanned mounting and dismounting assembly

Abstract

The utility model relates to a high-altitude unmanned mounting and dismounting assembly. The high-altitude unmanned mounting and dismounting assembly comprises an unmanned aerial vehicle; the fixing seat is used for being arranged on a high-altitude equipment rod, and the fixing seat has a locking state and an unlocking state; the high-altitude equipment can be locked on the fixed seat in the locking state; in the unlocking state, the high-altitude equipment can be unlocked and separated from the fixed seat; the locking device is arranged on the unmanned aerial vehicle and can be used for detachably mounting high-altitude equipment; wherein the unmanned aerial vehicle has a first flight state and a second flight state; in the first flight state, the fixing base and the object locking device can be configured in the mode that high-altitude equipment arranged on the object locking device can be separated from the object locking device so as to be installed on the fixing base; in the second flight state, the fixing base and the object locking device can be configured in the mode that the high-altitude equipment arranged on the fixing base can be separated from the fixing base so as to be installed on the object locking device. And operators do not need to manually mount and dismount the high-altitude equipment, so that the safety is improved.

Description

Technical Field

[0001] The present disclosure relates to the technical field of high-altitude equipment installation and disassembly, and in particular to a high-altitude unmanned installation and disassembly component. Background Art

[0002] The replacement of high-altitude equipment such as street lights, chimney lights, radar testers, cameras, fire temperature sensors, etc. is mainly carried out by setting up scaffolding or using lifts. Installation, disassembly, and maintenance all require workers to set up scaffolding or use hydraulic lifts. These tasks require a lot of manpower and material resources, and require long periods of time to climb high, which poses a major safety hazard.

[0003] Some products have a winch installed on the base. When it needs to be replaced, the winch controls the chain to lower the equipment to the ground for replacement. Although replacement is convenient, the addition of the winch and wire rope greatly increases the overall weight. If the equipment is not well fixed on the base during the infrastructure construction period, then when it is needed to be installed later, it may fall due to insufficient bearing capacity of the existing supporting structure. The lifting motor may also be damaged, and scaffolding or hydraulic lifts may still be needed for manual repairs, which also consumes manpower and material resources.

[0004] Another existing technology is to use a magnetic lamp. The magnetic lamp is a split structure. The upper part is first installed on the base, and the lower part is the lamp. When installing, the lamp is adsorbed on the top by the suction of the magnet to achieve installation. When disassembling, it needs to be disassembled manually. The upper and lower split structures are combined together by the suction of the magnet, and live installation in low-altitude areas is achieved. However, it is difficult to dismantle due to the magnetic force. At present, it is disassembled manually, and most of it is used in low-altitude areas. Utility Model Content

[0005] In order to overcome the problems existing in the related art, the present disclosure provides a high-altitude unmanned installation and disassembly component to solve the technical problems existing in the related art.

[0006] The present invention provides a high-altitude unmanned installation and disassembly assembly, the assembly comprising:

[0007] Drones;

[0008] A fixing seat, used to be arranged on a high-altitude equipment pole, and the fixing seat has a locked state and an unlocked state;

[0009] High-altitude equipment, in the locked state, the high-altitude equipment can be locked on the fixing seat; in the unlocked state, the high-altitude equipment can be unlocked and detached from the fixing seat;

[0010] A locking device, which is provided on the drone and is capable of installing the high-altitude equipment detachably from the ground;

[0011] Wherein, the drone has a first flight state and a second flight state;

[0012] In the first flight state, the fixing seat and the locking device can be configured so that: the high-altitude equipment arranged on the locking device can be detached therefrom to be installed on the fixing seat;

[0013] In the second flight state, the fixing seat and the locking device can be constructed so that the high-altitude equipment arranged on the fixing seat can be detached therefrom to be installed on the locking device.

[0014] In some embodiments, the fixing seat includes a fixing seat body and a locking mechanism, the fixing seat body is used to be set on the high-altitude equipment pole, and the fixing seat body is formed with a mounting cavity for mounting the high-altitude equipment and having an open end; the locking mechanism is arranged on the fixing seat body;

[0015] Wherein, in the locked state, the locking mechanism can lock the high-altitude equipment in the installation cavity; in the unlocked state, the locking mechanism can disengage the high-altitude equipment from the installation cavity.

[0016] In some embodiments, the locking mechanism includes a first telescopic rod and a second telescopic rod, the first telescopic rod and the second telescopic rod are telescopically disposed on the fixing seat body along a first direction and are located at the open end, and the first telescopic rod and the second telescopic rod are disposed opposite to each other along the first direction;

[0017] In the locked state, the first telescopic rod and the second telescopic rod are in an extended state to at least partially cover the open end, and the aerial device can abut against the first telescopic rod and the second telescopic rod in a second direction to be accommodated in the installation cavity;

[0018] In the unlocked state, the first telescopic rod and the second telescopic rod are in a retracted state, and the aerial device can be detached from the installation cavity through the open end in the second direction;

[0019] The first direction is perpendicular to the second direction.

[0020] In some embodiments, the first telescopic rod includes a first rod body, a first spring and a first electromagnet, the first rod body and the first spring both extend along the first direction, and the first spring is connected to the first rod body; when the first electromagnet loses power, the first spring can drive the first rod body to extend, and when the first electromagnet is energized, the first electromagnet can drive the first rod body to retract by overcoming the elastic force of the first spring; wherein the end of the first rod body is formed with a first guiding slope that can guide the aerial device into the installation cavity;

[0021] The second telescopic rod includes a second rod body, a second spring and a second electromagnet, the second rod body and the second spring both extend along the first direction, and the second spring is connected to the second rod body; when the second electromagnet loses power, the second spring can drive the second rod body to extend, and when the second electromagnet is energized, the second electromagnet can drive the second rod body to retract by overcoming the elastic force of the second spring; wherein, a second guiding slope is formed at the end of the second rod body, which can guide the aerial equipment into the installation cavity.

[0022] In some embodiments, the locking mechanism further includes a proximity switch and a push switch, the proximity switch, the push switch, the first electromagnet, and the second electromagnet are connected in series to form a series circuit, and the proximity switch and the push switch are both disposed in the mounting cavity and can be disposed opposite to the high-altitude equipment in the second direction;

[0023] When the proximity switch is powered and detects that the distance to the aerial device in the second direction is not greater than the first distance, the proximity switch is in an on state, and the series circuit is turned on to retract the first rod body and the second rod body, wherein the first distance is the size of the installation cavity in the second direction;

[0024] When the proximity switch detects that the distance from the aerial equipment in the second direction (B) is greater than the first distance, the proximity switch is in an off state, and the series circuit loses power to extend the first rod body and the second rod body.

[0025] In some embodiments, a first contact terminal is provided on the inner wall of the installation cavity, and a second contact terminal and an indicator light are provided on the outer surface of the high-altitude equipment. When the high-altitude equipment is locked in the installation cavity, the first contact terminal can contact the second contact terminal to supply power to the high-altitude equipment, and when the first contact terminal and the second contact terminal are in contact, the indicator light can be lit.

[0026] In some embodiments, the locking device includes a locking bracket and a locking device, wherein the locking bracket is used to be connected to the drone, and the locking device is arranged on the locking bracket and is provided with a receiving cavity, wherein the receiving cavity is formed with an open opening, and the high-altitude equipment can enter the receiving cavity through the open opening;

[0027] The high-altitude unmanned installation and disassembly component also includes an elastic card block, one of the inner wall of the accommodating cavity and the outer wall of the high-altitude equipment is provided with the elastic card block, and the other is provided with a card slot, the elastic card block is used to be engaged in the card slot to connect the high-altitude equipment and the lock, and when the high-altitude equipment is subjected to a force moving away from the lock greater than a first force, the elastic card block can be detached from the card slot.

[0028] In some embodiments, the locking device further comprises a driving mechanism, the locking device is rotatably disposed on the locking bracket, and the driving mechanism is used to drive the locking device to rotate.

[0029] In some embodiments, the driving mechanism includes a driving motor, a driving gear, a brake and a rack, wherein the driving motor is disposed on the lock bracket, the driving gear is transmission-connected to the driving motor, the rack is transmission-connected to the driving gear, and the brake is disposed on the lock bracket to limit the rotation of the driving gear;

[0030] The locker is rotatably disposed on the lock bracket via a first rotating shaft, and the bottom wall of the locker is configured as an arc-shaped bottom wall, and the rack is disposed in contact with the arc-shaped bottom wall and arranged around the first rotating shaft.

[0031] In some embodiments, the driving mechanism further includes a wireless control transmitting module, a wireless control receiving module, a buffer pad and a limit block;

[0032] The wireless control transmitting module is wirelessly connected to the wireless control receiving module, the wireless control receiving module is electrically connected to the driving motor, the buffer pad is arranged on the inner wall of the accommodating cavity, and the limit block is arranged on the end of the rack.

[0033] The technical solution provided by the embodiments of the present disclosure may include the following beneficial effects: when it is necessary to install high-altitude equipment, the high-altitude equipment is set on a locking device, and the locking device is set on a drone, and by operating the drone to fly to a first flight state, the high-altitude equipment set on the locking device can be detached therefrom, and then installed on a fixed seat set on a high-altitude equipment pole. When it is necessary to dismantle the high-altitude equipment set on the fixed seat, by operating the drone to fly to a second flight state, the high-altitude equipment set on the fixed seat can be detached therefrom, and then installed on the locking device on the drone. That is, by providing the high-altitude unmanned installation and disassembly component, there is no need for operators to climb high to manually install and disassemble the high-altitude equipment, which reduces the consumption of manpower and material resources while improving safety.

[0034] It is to be understood that the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the present disclosure. BRIEF DESCRIPTION OF THE DRAWINGS

[0035] The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments consistent with the present disclosure and, together with the description, serve to explain the principles of the present disclosure.

[0036] Figure 1 It is a schematic structural diagram of a fixing base and high-altitude equipment according to an embodiment of the present invention.

[0037] Figure 2 It is a schematic structural diagram of a fixing base and high-altitude equipment according to an embodiment of the present invention.

[0038] Figure 3 and Figure 4 It is a schematic structural diagram of a locking device according to an embodiment of the present invention.

[0039] Description of Reference Numerals

[0040] 1. Fixing seat; 11. Fixing seat body; 110. Mounting cavity; 1101. First contact terminal; 12. Locking mechanism; 121. First telescopic rod; 1211. First rod body; 1212. First spring; 1213. First guiding slope; 122. Second telescopic rod; 1221. Second rod body; 1222. Second spring; 1223. Second guiding slope; 123. Proximity switch; 124. Press switch; 125. Rectifier module; 126. Battery; 127. Power cord; 13. Support spring;

[0041] 2. High altitude equipment; 21. Second contact terminal; 22. Indicator light; 23. Elastic card block; 25. Cover plate;

[0042] 3. Locking device; 31. Locking bracket; 311. Locking member; 32. Locking device; 320. Accommodating chamber; 3201. Card slot; 321. First rotating shaft; 33. Driving mechanism; 331. Driving motor; 332. Driving gear; 333. Brake; 334. Rack; 335. Wireless control receiving module; 336. Buffer pad; 337. Limiting block; 338. Power socket. DETAILED DESCRIPTION

[0043] Exemplary embodiments will be described in detail herein, examples of which are shown in the accompanying drawings. When the following description refers to the drawings, the same numbers in different drawings represent the same or similar elements unless otherwise indicated. The embodiments described in the following exemplary embodiments do not represent all embodiments consistent with the present disclosure. Instead, they are merely examples of devices and methods consistent with some aspects of the present disclosure as detailed in the appended claims.

[0044] In the present disclosure, unless otherwise stated, directional words such as "first direction, second direction" may refer to Figure 1 As shown; the directional words used such as "inside and outside" refer to the inside and outside of the specific structural outline; the terms used such as "first and second" are only used to distinguish one element from another element, and do not have order and importance.

[0045] Reference Figures 1 to 4 As shown, the present disclosure provides a high-altitude unmanned installation and disassembly assembly, the assembly comprising:

[0046] Drones (not shown);

[0047] A fixing base 1 is used to be arranged on a high-altitude equipment pole (not shown), and the fixing base 1 has a locked state and an unlocked state;

[0048] The high-altitude equipment 2 can be locked on the fixing seat 1 in the locked state; and can be unlocked and detached from the fixing seat 1 in the unlocked state.

[0049] The locking device 3 is provided on the drone and can be used to install the high-altitude equipment 2 detachably from the ground;

[0050] Wherein, the UAV has a first flight state and a second flight state;

[0051] In the first flight state, the fixing seat 1 and the locking device 3 can be configured so that: the high-altitude equipment 2 arranged on the locking device 3 can be detached therefrom to be installed on the fixing seat 1;

[0052] In the second flight state, the fixing seat 1 and the locking device 3 can be constructed so that the high-altitude equipment 2 arranged on the fixing seat 1 can be detached therefrom to be installed on the locking device 3 .

[0053] In the above technical solution, when it is necessary to install the high-altitude equipment 2, the high-altitude equipment 2 is set on the locking device 3, and the locking device 3 is set on the drone. By operating the drone to fly to the first flight state, the high-altitude equipment 2 set on the locking device 3 can be detached from it, and then installed on the fixing seat 1 set on the high-altitude equipment pole. When it is necessary to disassemble the high-altitude equipment 2 set on the fixing seat 1, by operating the drone to fly to the second flight state, the high-altitude equipment 2 set on the fixing seat 1 can be detached from it, and then installed on the locking device 3 on the drone. That is, by setting the high-altitude unmanned installation and disassembly component, there is no need for the operator to climb up manually to install and disassemble the high-altitude equipment 2, which reduces the consumption of manpower and material resources and improves safety. In addition, the above-mentioned fixing seat 1 is not limited to being set on the high-altitude equipment pole, and can also be set on a high-altitude building, and the present disclosure does not limit this.

[0054] It should be noted that the above-mentioned high-altitude equipment 2 can be street lights, chimney lights, radar testers, cameras, fire temperature sensors and other equipment installed at high places. The present disclosure does not limit the specific structural type of the high-altitude equipment 2.

[0055] In one embodiment, referring to Figure 1 and Figure 2 As shown, the fixing seat 1 includes a fixing seat body 11 and a locking mechanism 12. The fixing seat body 11 is used to be set on the high-altitude equipment pole, and the fixing seat body 11 is formed with a mounting cavity 110 for mounting the high-altitude equipment 2 and having an open end; the locking mechanism 12 is arranged on the fixing seat body 11; wherein, in the locked state, the locking mechanism 12 can lock the high-altitude equipment 2 in the mounting cavity 110; in the unlocked state, the locking mechanism 12 can make the high-altitude equipment 2 detach from the mounting cavity 110. The fixing seat body 11 can be constructed as any appropriate structure, and the locking mechanism 12 can also be constructed as any appropriate structure, and the present disclosure does not limit this.

[0056] Optionally, refer to Figure 1 and Figure 2As shown, the locking mechanism 12 may include a first telescopic rod 121 and a second telescopic rod 122, and the first telescopic rod 121 and the second telescopic rod 122 are telescopically arranged on the fixing seat body 11 along the first direction A and are located at the open end, and the first telescopic rod 121 and the second telescopic rod 122 are arranged relatively to each other along the first direction A; in the locked state, the first telescopic rod 121 and the second telescopic rod 122 are in an extended state to at least partially block the open end, and the aerial equipment 2 can be abutted against the first telescopic rod 121 and the second telescopic rod 122 in the second direction B to be accommodated in the installation cavity 110; in the unlocked state, the first telescopic rod 121 and the second telescopic rod 122 are in a retracted state, and the aerial equipment 2 can be detached from the installation cavity 110 through the open end in the second direction B; wherein the first direction A is perpendicular to the second direction B.

[0057] That is, in this embodiment, by providing the first telescopic rod 121 and the second telescopic rod 122, and utilizing the characteristics that the first telescopic rod 121 and the second telescopic rod 122 can be telescoped in the first direction A, the high-altitude equipment 2 can be locked and unlocked in the installation cavity 110 of the fixing seat 1. The first telescopic rod 121 and the second telescopic rod 122 can also be constructed as any appropriate structure, and the present disclosure does not limit this.

[0058] For example, refer to Figure 1 and Figure 2 As shown, the first telescopic rod 121 includes a first rod body 1211, a first spring 1212 and a first electromagnet. The first rod body 1211 and the first spring 1212 both extend in the first direction A, and the first spring 1212 is connected to the first rod body 1211; when the first electromagnet loses power, the first spring 1212 can drive the first rod body 1211 to extend, and when the first electromagnet is energized, the first electromagnet can drive the first rod body 1211 to retract by overcoming the elastic force of the first spring 1212; wherein, the end of the first rod body 1211 is formed with a first guiding slope 1213 that can guide the aerial equipment 2 to enter the installation cavity 110. The second telescopic rod 122 includes a second rod body 1221, a second spring 1222 and a second electromagnet. The second rod body 1221 and the second spring 1222 both extend along the first direction A, and the second spring 1222 is connected to the second rod body 1221. When the second electromagnet loses power, the second spring 1222 can drive the second rod body 1221 to extend. When the second electromagnet is energized, the second electromagnet can drive the second rod body 1221 to retract by overcoming the elastic force of the second spring 1222. The end of the second rod body 1221 is formed with a second guiding slope 1223 that can guide the aerial equipment 2 to enter the installation cavity 110.

[0059] In this embodiment, when the first electromagnet is energized, the first electromagnet can drive the first rod 1211 to retract against the elastic force of the first spring 1212, and when the second electromagnet is energized, the second electromagnet can drive the second rod 1221 to retract against the elastic force of the second spring 1222, so that the open end of the installation cavity 110 is in an open state, and the aerial device 2 can pass through the open end to enter the installation cavity 110. In addition, when the first electromagnet is de-energized, the first spring 1212 can drive the first rod 1211 to extend, and when the second electromagnet is de-energized, the second spring 1222 can drive the second rod 1221 to extend, so that the aerial device 2 can be locked in the installation cavity 110. For example, referring to Figure 2 As shown, the aerial device 2 is provided with a cover plate 25 , and the cover plate 25 can abut against the first rod body 1211 and the second rod body 1221 in the second direction B, thereby preventing the aerial device 2 from being separated from the installation cavity 110 .

[0060] In another embodiment, referring to Figure 1 and Figure 2 As shown, the locking mechanism 12 also includes a proximity switch 123 and a push switch 124, the proximity switch 123, the push switch 124, the first electromagnet and the second electromagnet are connected in series to form a series circuit, and the proximity switch 123 and the push switch 124 are both arranged in the installation cavity 110 and can be arranged relative to the high-altitude equipment 2 in the second direction B. When the high-altitude equipment 2 moves toward the push switch 124 along the second direction B and pushes against the action of the push switch 124, the series circuit is turned on to retract the first rod body 1211 and the second rod body 1221. When the proximity switch 123 detects that the distance from the high-altitude equipment 2 in the second direction B is not greater than the first distance, the proximity switch 123 is in a conducting state. When the proximity switch 123 detects that the distance from the high-altitude equipment 2 in the second direction B is greater than the first distance, the proximity switch 123 is in a disconnected state, and the series circuit loses power to extend the first rod body 1211 and the second rod body 1221. Wherein, the first distance is not less than the size of the installation cavity 110 in the second direction B.

[0061] In this embodiment, when it is necessary to disassemble the high-altitude equipment 2 set on the fixing seat 1, the operator can first operate the drone to approach the high-altitude equipment 2 and realize the connection between the locking device 3 and the high-altitude equipment 2, and then the drone drives the high-altitude equipment 2 to move toward the pressing switch 124 along the second direction B and presses against the pressing switch 124 to operate, thereby realizing the conduction of the series circuit. As can be seen from the above, when the first electromagnet and the second electromagnet are energized, the first rod 1211 and the second rod 1221 can be retracted, and the drone can drive the high-altitude equipment 2 to move in the second direction B in the direction away from the fixing seat 1, so that the high-altitude equipment 2 is separated from the installation cavity 110. In addition, by setting the proximity switch 123, when it is detected that the distance from the high-altitude equipment 2 is greater than the first distance, the proximity switch 123 is in the disconnected state, the series circuit loses power, and the first rod 1211 and the second rod 1221 are reset to the extended state.

[0062] In other embodiments, referring to Figure 1 and Figure 2 As shown, the inner wall of the installation cavity 110 is provided with a first contact terminal 1101, and the outer surface of the aerial device 2 is provided with a second contact terminal 21 and an indicator light 22. When the aerial device 2 is locked in the installation cavity 110, the first contact terminal 1101 can contact the second contact terminal 21 to supply power to the aerial device 2, and when the first contact terminal 1101 and the second contact terminal 21 are in contact, the indicator light 22 can light up, indicating that the aerial device 2 has been installed in place. The first contact terminal 1101 and the second contact terminal 21 can be constructed as metal conductors such as copper sheets, but the present disclosure does not limit the specific types of the first contact terminal 1101 and the second contact terminal 21.

[0063] For example, the first direction A mentioned above may be a horizontal direction, and the second direction B may be a vertical direction, which is not limited in the present disclosure.

[0064] 1) For the embodiment of installing from top to bottom (refer to Figure 1 shown):

[0065] When the aerial equipment 2 needs to be installed, the locking device 3 is first set on the drone, and then the aerial equipment 2 is set on the locking device 3. As the drone continues to move upward, the aerial equipment 2 is subjected to a continuous upward force, which presses against the first guide slope 1213 of the first rod body 1211 and the second guide slope 1223 of the second rod body 1221, overcoming the elastic force of the first spring 1212 and the second spring 1222, so that the first rod body 1211 and the second rod body 1221 move from the extended state to the retracted state. At the same time, the aerial equipment 2 also enters the installation cavity 110. When the second contact terminal 21 of the aerial equipment 2 is conductively connected to the first contact terminal 1101 on the inner wall of the installation cavity 110, the indicator light 22 lights up, indicating that the aerial equipment 2 is installed in place. At this time, the first rod body 1211 and the second rod body 1221 are also reset to the extended state under the action of the spring elastic force and support the cover plate 25 of the aerial equipment 2 to prevent the aerial equipment 2 from detaching from the installation cavity 110. After being installed in place, the drone moves downward, so that the high-altitude equipment 2 is separated from the locking device 3 (the specific implementation method is referred to below), thereby completing the installation of the high-altitude equipment 2.

[0066] Among them, the first flight state includes a first flight stage of flying upward to realize the installation of the high-altitude equipment 2 on the fixing seat 1, and a second flight stage of flying downward to realize the separation of the high-altitude equipment 2 from the locking device 3.

[0067] 2) For the embodiment of disassembly from top to bottom (refer to Figure 1 shown):

[0068] When the aerial equipment 2 needs to be disassembled, the drone continues to rise to achieve the connection between the aerial equipment 2 and the locking device 3 (see below for details), and then the drone continues to rise. Since the proximity switch 123, the push switch 124, the first electromagnet and the second electromagnet form a series circuit, when the aerial equipment 2 hits the push switch 124, the series circuit is energized, and the first rod 1211 and the second rod 1221 continue to remain in a retracted state. When the proximity switch 123 detects that the distance from the aerial equipment 2 in the second direction B is greater than the first distance, that is, the aerial equipment 2 is completely detached from the installation cavity 110, the proximity switch 123 loses power, the series circuit loses power, the first rod 1211 and the second rod 1221 are reset to the extended state, and the aerial equipment 2 slowly falls with the drone to complete the disassembly.

[0069] The second flight state includes a third flight stage in which the high-altitude device 2 abuts against the pressing switch 124 to trigger the series circuit to be energized by flying upward, and a fourth flight stage in which the high-altitude device 2 is separated from the fixing seat 1 by flying downward.

[0070] 3) For the embodiment of installation from bottom to top (refer to Figure 2 shown):

[0071] The structure is basically similar to the embodiment of first-up and then-down installation, and the fixing base 1 is in an inverted state. The difference is that the fixing base 1 is provided with a support spring 13 for supporting the high-altitude equipment 2. Because the gravity factor needs to be considered, the function of the support spring 13 is to ensure that the high-altitude equipment 2 is supported under normal circumstances. And the gravity of the high-altitude equipment 2 is not enough to overcome the elastic force of the support spring 13 to press the switch 124, so that the series circuit is in a power-off state, and the first rod body 1211 and the second rod body 1221 are continuously in an extended state. The specific installation steps are similar to the embodiment of first-up and then-down, and the present disclosure will not be repeated here.

[0072] 4) For the embodiment of disassembly from bottom to top (refer to Figure 2 shown):

[0073] It is basically similar to the up-first-down embodiment, except that the drone continues to apply downward pressure, so that the aerial equipment 2 overcomes the elastic force of the support spring 13, presses against the press switch 124, so that the series circuit is energized, the first rod 1211 and the second rod 1221 retract, and the drone pulls the aerial equipment 2 upward. When the proximity switch 123 detects that the distance to the aerial equipment 2 in the second direction B is greater than the first distance, that is, when the aerial equipment 2 is completely detached from the installation cavity 110, the proximity switch 123 loses power, the series circuit loses power, and the first rod 1211 and the second rod 1221 are reset to the extended state, completing the disassembly of the aerial equipment 2.

[0074] In addition, the above-mentioned fixing base 1 can also include a rectifier module 125, a battery 126 and a power line 127. The power line 127 charges the battery 126 through the rectifier module 125. When the power line 127 is powered off, the fixing base 1 can also use the battery 126 to work.

[0075] Optionally, refer to Figure 3 and Figure 4 As shown, the above-mentioned locking device 3 may include a locking bracket 31 and a locking device 32. The locking bracket 31 is used to be connected to the drone. The locking device 32 is arranged on the locking bracket 31 and is provided with a receiving cavity 320. The receiving cavity 320 is formed with an open mouth, and the high-altitude equipment 2 can enter the receiving cavity 320 through the open mouth. The high-altitude unmanned installation and disassembly assembly also includes an elastic card block 23. One of the inner wall of the receiving cavity 320 and the outer wall of the high-altitude equipment 2 is provided with an elastic card block 23, and the other is provided with a card slot 3201. The elastic card block 23 is used to be connected to the card slot 3201 to connect the high-altitude equipment 2 and the locking device 32, and when the high-altitude equipment 2 is subjected to a force away from the locking device 32 greater than the first force, the elastic card block 23 can be detached from the card slot 3201.

[0076] In this embodiment, the lock bracket 31 can be constructed into any appropriate shape and structure, which is not limited by the present disclosure. For example, the lock bracket 31 can be connected to the drone through the lock 311. The lock 32 can also be constructed into any appropriate shape and structure, which is not limited by the present disclosure. The setting of the accommodating chamber 320 can effectively protect the high-altitude equipment 2 and prevent the high-altitude equipment 2 from shaking. The matching design of the elastic block 23 and the slot 3201 realizes the detachable installation of the high-altitude equipment 2 and the lock 32.

[0077] Reference Figure 3 and Figure 4 As shown, the lock device 3 further includes a driving mechanism 33, and the lock 32 is rotatably disposed on the lock bracket 31, and the driving mechanism 33 is used to drive the lock 32 to rotate. The driving mechanism 33 includes a driving motor 331, a driving gear 332, a brake 333 and a rack 334, the driving motor 331 is disposed on the lock bracket 31, the driving gear 332 is transmission-connected to the driving motor 331, the rack 334 is transmission-connected to the driving gear 332, and the brake 333 is disposed on the lock bracket 31 to limit the rotation of the driving gear 332; the lock 32 is rotatably disposed on the lock bracket 31 through the first rotating shaft 321, and the bottom wall of the lock 32 is configured as an arc bottom wall, and the rack 334 is disposed in contact with the arc bottom wall and arranged around the first rotating shaft 321.

[0078] In this embodiment, the driving motor 331 drives the driving gear 332 to rotate, and the driving gear 332 and the rack 334 transmit, so that the lock 32 rotates around the first rotating shaft 321, thereby adjusting the angle of the high-altitude equipment 2 set in the lock 32, so as to achieve the installation and removal of the high-altitude equipment 2 at different angles. In addition, by setting a brake 333, the rotation of the driving gear 332 is controlled to maintain the high-altitude equipment 2 at a corresponding angle.

[0079] Optionally, the driving mechanism 33 may also include a wireless control transmitting module, a wireless control receiving module 335, a buffer pad 336 and a limit block 337; the wireless control transmitting module is wirelessly connected to the wireless control receiving module 335, the wireless control receiving module 335 is electrically connected to the driving motor 331, the buffer pad 336 is arranged on the inner wall of the accommodating cavity 320, and the limit block 337 is arranged at the end of the rack 334.

[0080] In this embodiment, a command is sent to the wireless control receiving module 335 through the wireless control transmitting module, and the wireless control receiving module 335 controls the drive motor 331 to rotate to execute the corresponding command to achieve the purpose of adjustment. The drive motor 331 can be configured as a stepper motor to improve the accuracy of control. By providing a buffer pad 336, the high-altitude equipment 2 can be effectively protected. For example, the buffer pad 336 can be configured as a sponge pad. In addition, the setting of the limit block 337 can limit the rotation angle of the lock 32. In addition, a power socket 338 can be provided on the lock device 3, and the power socket 338 can be powered by the drone to power the wireless control receiving module 335 and the drive motor 331.

[0081] Those skilled in the art will readily appreciate other embodiments of the present disclosure after considering the specification and practicing the present disclosure. This application is intended to cover any variations, uses or adaptations of the present disclosure, which follow the general principles of the present disclosure and include common knowledge or customary technical means in the art that are not disclosed in the present disclosure. The specification and examples are to be considered as exemplary only, and the true scope and spirit of the present disclosure are indicated by the following claims.

[0082] It should be understood that the present disclosure is not limited to the exact structures that have been described above and shown in the drawings, and that various modifications and changes may be made without departing from the scope thereof. The scope of the present disclosure is limited only by the appended claims.

Claims

1. A high-altitude unmanned installation and disassembly assembly, characterized in that: The components include: Drones; A fixing seat (1) is used to be arranged on a pole of a high-altitude device, and the fixing seat (1) has a locked state and an unlocked state; A high-altitude device (2), in the locked state, the high-altitude device (2) can be locked on the fixing seat (1); in the unlocked state, the high-altitude device (2) can be unlocked and detached from the fixing seat (1); A locking device (3) is provided on the drone and is capable of installing the high-altitude equipment (2) detachably from the ground; Wherein, the drone has a first flight state and a second flight state; In the first flight state, the fixing seat (1) and the locking device (3) can be constructed so that: the high-altitude equipment (2) arranged on the locking device (3) can be detached therefrom to be installed on the fixing seat (1); In the second flight state, the fixing seat (1) and the locking device (3) can be constructed so that the high-altitude equipment (2) arranged on the fixing seat (1) can be detached therefrom so as to be installed on the locking device (3).

2. The high altitude unmanned installation and disassembly assembly according to claim 1, characterized in that: The fixing seat (1) comprises a fixing seat body (11) and a locking mechanism (12); the fixing seat body (11) is used to be arranged on a high-altitude equipment pole, and the fixing seat body (11) is formed with a mounting cavity (110) for mounting the high-altitude equipment (2) and having an open end; the locking mechanism (12) is arranged on the fixing seat body (11); Wherein, in the locked state, the locking mechanism (12) can lock the aerial device (2) in the installation cavity (110); in the unlocked state, the locking mechanism (12) can disengage the aerial device (2) from the installation cavity (110).

3. The high altitude unmanned installation and disassembly assembly according to claim 2, characterized in that: The locking mechanism (12) comprises a first telescopic rod (121) and a second telescopic rod (122), the first telescopic rod (121) and the second telescopic rod (122) being telescopically arranged on the fixing seat body (11) along a first direction (A) and being located at the open end, and the first telescopic rod (121) and the second telescopic rod (122) being arranged opposite to each other along the first direction (A); In the locked state, the first telescopic rod (121) and the second telescopic rod (122) are in an extended state to at least partially cover the open end, and the aerial device (2) can abut against the first telescopic rod (121) and the second telescopic rod (122) in a second direction (B) to be accommodated in the installation cavity (110); In the unlocked state, the first telescopic rod (121) and the second telescopic rod (122) are in a retracted state, and the aerial device (2) can be detached from the installation cavity (110) through the open end in the second direction (B); Wherein, the first direction (A) is perpendicular to the second direction (B).

4. The high altitude unmanned installation and disassembly assembly according to claim 3, characterized in that: The first telescopic rod (121) comprises a first rod body (1211), a first spring (1212) and a first electromagnet, wherein the first rod body (1211) and the first spring (1212) both extend along the first direction (A), and the first spring (1212) is connected to the first rod body (1211); when the first electromagnet loses power, the first spring (1212) can drive the first rod body (1211) to extend, and when the first electromagnet is energized, the first electromagnet can drive the first rod body (1211) to retract by overcoming the elastic force of the first spring (1212); wherein a first guiding inclined surface (1213) capable of guiding the aerial device (2) to enter the installation cavity (110) is formed at the end of the first rod body (1211); The second telescopic rod (122) comprises a second rod body (1221), a second spring (1222) and a second electromagnet, wherein the second rod body (1221) and the second spring (1222) both extend along the first direction (A), and the second spring (1222) is connected to the second rod body (1221); when the second electromagnet loses power, the second spring (1222) can drive the second rod body (1221) to extend, and when the second electromagnet is energized, the second electromagnet can drive the second rod body (1221) to retract by overcoming the elastic force of the second spring (1222); wherein a second guiding inclined surface (1223) capable of guiding the aerial device (2) to enter the installation cavity (110) is formed at the end of the second rod body (1221).

5. The high altitude unmanned installation and disassembly assembly according to claim 4, characterized in that: The locking mechanism (12) further comprises a proximity switch (123) and a push switch (124); the proximity switch (123), the push switch (124), the first electromagnet and the second electromagnet are connected in series to form a series circuit; the proximity switch (123) and the push switch (124) are both arranged in the installation cavity (110) and can be arranged relative to the aerial device (2) in the second direction (B); When the aerial device (2) moves toward the push switch (124) along the second direction (B) and abuts against the push switch (124), the proximity switch (123) is energized and detects that the distance from the aerial device (2) in the second direction (B) is not greater than a first distance, the proximity switch (123) is in an on state, and the series circuit is turned on to retract the first rod body (1211) and the second rod body (1221), wherein the first distance is the size of the installation cavity (110) in the second direction (B); When the proximity switch (123) detects that the distance from the aerial device (2) in the second direction (B) is greater than the first distance, the proximity switch (123) is in an off state, and the series circuit loses power to allow the first rod body (1211) and the second rod body (1221) to extend.

6. The high altitude unmanned installation and removal assembly according to any one of claims 2 to 5, characterized in that: The inner wall of the installation cavity (110) is provided with a first contact terminal (1101), and the outer surface of the aerial device (2) is provided with a second contact terminal (21) and an indicator light (22); when the aerial device (2) is locked in the installation cavity (110), the first contact terminal (1101) can contact the second contact terminal (21) to supply power to the aerial device (2), and when the first contact terminal (1101) and the second contact terminal (21) are in contact, the indicator light (22) can light up.

7. The high altitude unmanned installation and disassembly assembly according to any one of claims 1 to 5, characterized in that: The locking device (3) comprises a locking bracket (31) and a locking device (32), wherein the locking bracket (31) is used to be connected to the drone, and the locking device (32) is arranged on the locking bracket (31) and is provided with a receiving cavity (320), wherein the receiving cavity (320) is formed with an open opening, and the high-altitude equipment (2) can enter the receiving cavity (320) through the open opening; The high-altitude unmanned installation and disassembly component also includes an elastic card block (23), one of the inner wall of the accommodating cavity (320) and the outer wall of the high-altitude equipment (2) is provided with the elastic card block (23), and the other is provided with a card slot (3201), the elastic card block (23) is used to be engaged in the card slot (3201) to connect the high-altitude equipment (2) and the lock (32), and when the high-altitude equipment (2) is subjected to a force that is greater than a first force away from the lock (32), the elastic card block (23) can be detached from the card slot (3201).

8. The high altitude unmanned installation and disassembly assembly according to claim 7, characterized in that: The locking device (3) further comprises a driving mechanism (33); the locking device (32) is rotatably arranged on the locking bracket (31); and the driving mechanism (33) is used to drive the locking device (32) to rotate.

9. The high altitude unmanned installation and disassembly assembly according to claim 8, characterized in that: The driving mechanism (33) comprises a driving motor (331), a driving gear (332), a brake (333) and a rack (334); the driving motor (331) is arranged on the locking bracket (31); the driving gear (332) is transmission-connected to the driving motor (331); the rack (334) is transmission-connected to the driving gear (332); and the brake (333) is arranged on the locking bracket (31) to limit the rotation of the driving gear (332); The lock (32) is rotatably arranged on the lock bracket (31) via a first rotating shaft (321), and the bottom wall of the lock (32) is constructed as an arc-shaped bottom wall, and the rack (334) is arranged in contact with the arc-shaped bottom wall and arranged around the first rotating shaft (321).

10. The high altitude unmanned installation and disassembly assembly according to claim 9, characterized in that: The driving mechanism (33) further comprises a wireless control transmitting module, a wireless control receiving module (335), a buffer pad (336) and a limit block (337); The wireless control transmitting module is wirelessly connected to the wireless control receiving module (335), the wireless control receiving module (335) is electrically connected to the driving motor (331), the buffer pad (336) is arranged on the inner wall of the accommodating cavity (320), and the limit block (337) is arranged at the end of the rack (334).

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