Aircraft real-time monitoring device based on low-altitude gridding service platform and use method of aircraft real-time monitoring device

Abstract

The invention discloses an aircraft real-time monitoring device based on a low-altitude gridding service platform and a using method thereof, and relates to the technical field of aircraft monitoring, the aircraft real-time monitoring device comprises an aircraft body, a fixing plate is arranged at the bottom of the aircraft body, the front end and the rear end of each of the two sides of the fixing plate are fixedly connected with supporting legs, and the supporting legs are fixedly connected with the aircraft body. A movable plate is arranged at the bottom of the fixed plate, and a high-definition camera body is arranged at the bottom of the movable plate. The high-definition camera body is arranged to monitor the low-altitude condition, the monitoring direction and angle of the high-definition camera body can be adjusted by arranging the adjusting mechanism, so that the monitoring range of the high-definition camera body is further enlarged, and the cleaning mechanism is arranged to clean the high-definition camera body when impurities are attached to the surface of the high-definition camera body. And impurities are cleaned, so that the definition of a camera picture of the high-definition camera body is ensured, a worker can see a monitoring picture more clearly, and misjudgment caused by picture blurring is prevented.

Description

Technical Field

[0001] The present invention relates to the technical field of aircraft monitoring, and in particular to a real-time aircraft monitoring device based on a low-altitude grid service platform and a method for using the same. Background Art

[0002] The low-altitude grid service platform is a system used to manage and monitor low-altitude airspace. It mainly involves the operation of low-altitude aircraft, and usually includes functions such as airspace management, data sharing, early warning system, and data analysis. The low-altitude grid service platform combines aircraft for real-time monitoring and can provide efficient, flexible, and comprehensive monitoring solutions.

[0003] When using an aircraft for real-time monitoring, it is usually necessary to select suitable sensors and equipment, such as high-definition cameras, thermal imagers, lidars, etc., and configure them according to specific monitoring needs. When performing monitoring operations, the aircraft needs to fly outdoors for a long time. As the air quality is getting worse and worse, there are more and more impurities such as dust and haze in the air. During the flight of the aircraft, impurities are easy to adhere to the surface of the camera, affecting the clarity of the camera, making the monitoring screen viewed by the staff blurred, affecting the judgment of the real-time situation. Summary of the invention

[0004] The purpose of the present invention is to provide an aircraft real-time monitoring device based on a low-altitude grid service platform and a method of using the device, which has the advantages of adjustable monitoring angle and dust removal, and solves the problem that due to the increasingly poor air quality, there are more and more impurities such as dust and haze in the air. During the flight of the aircraft, impurities are easily attached to the surface of the camera, affecting the clarity of the camera, making the monitoring screen viewed by the staff blurred, and affecting the judgment of the real-time situation.

[0005] To achieve the above-mentioned purpose, the present invention provides the following technical solutions: a real-time monitoring device for an aircraft based on a low-altitude grid service platform and a method for using the same, comprising an aircraft body, a fixed plate is provided at the bottom of the aircraft body, the front end and the rear end of both sides of the fixed plate are fixedly connected with legs, a movable plate is provided at the bottom of the fixed plate, a high-definition camera body is provided at the bottom of the movable plate, an adjustment mechanism is provided on the surface of the high-definition camera body, a cleaning mechanism is provided at the bottom of the movable plate, the adjustment mechanism comprises a supporting sheet, the supporting sheet is located at both sides of the bottom of the movable plate and is fixedly connected to the movable plate, a fixed sleeve is provided on the surface of the high-definition camera body, both sides of the fixed sleeve are fixedly connected with rotating columns, one end of the rotating column away from the fixed sleeve is movably connected to one side of the supporting sheet through a bearing, the cleaning mechanism comprises a mounting groove, the mounting groove is opened at the bottom of the movable plate, the inner cavity of the mounting groove is detachably connected with a disassembly plate, and the bottom of the disassembly plate is fixedly connected with a cleaning pad.

[0006] Preferably, a first motor is fixedly connected to the right side of the right support plate, and the output shaft of the first motor passes through the right support plate and is transmission-connected to the right end of the right rotating column, and a second motor is fixedly connected to the top of the fixed plate, and the output shaft of the second motor passes through the bottom of the fixed plate and is transmission-connected to the top of the movable plate, and the output shaft of the second motor is movably connected to the inner cavity of the fixed plate via a bearing.

[0007] Preferably, a support ring is movably connected to the surface of the second motor output shaft and located at the bottom of the fixed plate through a bearing, the top of the support ring is fixedly connected to the bottom of the fixed plate, both sides of the bottom of the aircraft body are fixedly connected to a mounting frame, both sides of the top of the fixed plate are fixedly connected to an insertion plate, the top of the insertion plate extends to the inner cavity of the mounting frame and is detachably connected to the inner cavity of the mounting frame, a nut is fixedly connected to the back side of the inner cavity of the mounting frame, a positioning bolt is provided on the front side of the mounting frame, the rear end of the positioning bolt extends to the inner cavity of the nut and is threadedly connected to the inner cavity of the nut.

[0008] Preferably, positioning grooves are provided on both sides of the inner cavity of the installation groove, positioning blocks are fixedly connected to both sides of the disassembly plate, one side of the positioning block extends to the inner cavity of the positioning groove and is slidably connected to the inner cavity of the positioning groove, and an auxiliary groove is provided at the bottom of the disassembly plate.

[0009] Preferably, a fixing groove is provided on the side away from the inner cavity of the two positioning grooves, the inner cavity of the fixing groove is slidably connected with a clamping block, one side of the clamping block is fixedly connected with a spring, and the end of the spring away from the clamping block is fixedly connected to the inner wall of the fixing groove.

[0010] Preferably, a sliding groove is provided on the side of the positioning block away from the disassembly plate, one end of the clamping block extends to the inner cavity of the sliding groove and is movably connected with the inner cavity of the sliding groove, the inner cavity of the sliding groove is provided with a clamping groove, and the clamping block is engaged with the inner cavity of the clamping groove.

[0011] Preferably, the method of use is as follows:

[0012] A. When the aircraft body drives the high-definition camera body to fly and the high-definition camera body monitors the low-altitude conditions in real time, if the monitoring angle of the high-definition camera body needs to be adjusted, the first motor is started. When the first motor is running, it can cooperate with the fixing sleeve and the rotating column to drive the high-definition camera body to rotate, so as to adjust the monitoring angle of the high-definition camera body. When the monitoring direction of the high-definition camera body needs to be adjusted, the second motor is started. The output shaft of the second motor drives the movable plate to rotate. The movable plate then cooperates with the supporting plate, the fixing sleeve and the rotating column to drive the high-definition camera body to rotate, so that the monitoring direction of the high-definition camera body can be adjusted. By disassembling the fixing plate, it can be removed from the bottom of the aircraft body, so as to inspect and repair multiple components on its surface. When disassembling the fixing plate, first rotate the positioning bolt so that the rear end of the positioning bolt is moved out of the inner cavity of the nut. After being moved out, it can be pulled out from the inner cavity of the mounting frame. After being pulled out, the positioning effect of the positioning bolt on the insertion plate disappears. At this time, the insertion plate can be pulled out from the inner cavity of the mounting frame, thereby achieving the purpose of disassembling the fixing plate;

[0013] B. When the staff observes that the monitoring image becomes blurred and needs to clean the surface of the high-definition camera body, the first motor is also started. The first motor cooperates with the fixed sleeve and the rotating column to drive the high-definition camera body to rotate, so that the high-definition camera body makes a complete circular motion. When the high-definition camera body rotates to the top, its surface can rub against the bottom of the cleaning pad, so that the cleaning pad can wipe off the impurities attached to the surface, thereby improving the clarity of the camera image. When the cleaning pad needs to be disassembled and cleaned, first use fingernails to hold the auxiliary groove and pull the disassembly plate outward. At this time, the card block in the inner cavity of the card slot will be subjected to pressure generated by the pulling force. The pressure causes the inner wall of the card slot to squeeze the card block, causing it to slide into the inner cavity of the fixed slot. When the card block completely slides out of the inner cavity of the card slot, the disassembly plate can be pulled out from the inner cavity of the mounting slot to clean the cleaning pad.

[0014] Compared with the prior art, the present invention has the following beneficial effects:

[0015] The present invention provides an aircraft body to support the components on the bottom and drive them to fly, so as to improve the monitoring range of the high-definition camera body; provides a fixing plate and supporting legs, wherein the fixing plate is used to support the components on the surface, and the supporting legs are used to support the entire device when it falls; provides a high-definition camera body to monitor low-altitude conditions; provides an adjusting mechanism to adjust the monitoring direction and angle of the high-definition camera body, thereby further increasing the monitoring range of the high-definition camera body; provides a cleaning mechanism to clean impurities when they are attached to the surface of the high-definition camera body, thereby ensuring the clarity of the image captured by the high-definition camera body, enabling staff to see the monitoring image more clearly and preventing wrong judgments due to blurred images. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 It is a schematic diagram of the main plane structure of the present invention;

[0017] Figure 2 It is a schematic structural diagram of the installation frame and the insert plate of the present invention in a separated state;

[0018] Figure 3 It is a bottom view structural schematic diagram of the movable plate of the present invention;

[0019] Figure 4 It is a schematic diagram of the structure of the mounting groove and the disassembly plate of the present invention in a separated state when viewed from above;

[0020] Figure 5 It is a partial cross-sectional structural schematic diagram of the movable plate of the present invention;

[0021] Figure 6 It is a structural schematic diagram of the separated state of the card block and the card slot of the present invention.

[0022] In the figure: 1. Aircraft body; 2. Fixed plate; 3. Outrigger; 4. Movable plate; 5. High-definition camera body; 6. Adjustment mechanism; 601. Support plate; 602. Fixed sleeve; 603. Rotating column; 604. First motor; 605. Second motor; 606. Support ring; 7. Cleaning mechanism; 701. Mounting slot; 702. Disassembly plate; 703. Cleaning pad; 704. Positioning slot; 705. Positioning block; 706. Auxiliary slot; 707. Fixed slot; 708. Block; 709. Spring; 710. Slide slot; 711. Slot; 8. Mounting frame; 9. Insert plate; 10. Nut; 11. Positioning bolt. DETAILED DESCRIPTION

[0023] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0024] The aircraft body 1, fixed plate 2, supporting leg 3, movable plate 4, high-definition camera body 5, adjusting mechanism 6, supporting plate 601, fixing sleeve 602, rotating column 603, first motor 604, second motor 605, supporting ring 606, cleaning mechanism 7, mounting groove 701, disassembly plate 702, cleaning pad 703, positioning groove 704, positioning block 705, auxiliary groove 706, fixing groove 707, clamping block 708, spring 709, slide groove 710, clamping groove 711, mounting frame 8, insertion plate 9, nut 10, and positioning bolt 11 of the present invention are all universal standard parts or parts known to those skilled in the art, and their structures and principles can be known to those skilled in the art through technical manuals or through conventional experimental methods.

[0025] Example 1

[0026] like Figure 1-6 As shown, it is the first embodiment of the present invention, which provides an aircraft real-time monitoring device based on a low-altitude grid service platform and a method of using the same, comprising an aircraft body 1, a fixed plate 2 is arranged at the bottom of the aircraft body 1, the front and rear ends of both sides of the fixed plate 2 are fixedly connected with legs 3, a movable plate 4 is arranged at the bottom of the fixed plate 2, a high-definition camera body 5 is arranged at the bottom of the movable plate 4, an adjustment mechanism 6 is arranged on the surface of the high-definition camera body 5, a cleaning mechanism 7 is arranged at the bottom of the movable plate 4, and the adjustment mechanism 6 includes a support sheet 601 The support sheet 601 is located on both sides of the bottom of the movable plate 4 and is fixedly connected to the movable plate 4. A fixed sleeve 602 is provided on the surface of the high-definition camera body 5. A rotating column 603 is fixedly connected to both sides of the fixed sleeve 602. One end of the rotating column 603 away from the fixed sleeve 602 is movably connected to one side of the support sheet 601 through a bearing. The cleaning mechanism 7 includes a mounting groove 701. The mounting groove 701 is opened at the bottom of the movable plate 4. The inner cavity of the mounting groove 701 is detachably connected to a disassembly plate 702. The bottom of the disassembly plate 702 is fixedly connected to a cleaning pad 703.

[0027] like Figure 1-6 As shown, the aircraft body 1 is used to support the components at the bottom and can drive it to fly, so as to improve the monitoring range of the high-definition camera body 5, the fixing plate 2 is used to support the components on the surface, the legs 3 are used to support the entire device when it falls, the high-definition camera body 5 is used to monitor the low-altitude conditions, the adjustment mechanism 6 can adjust the monitoring direction and angle of the high-definition camera body 5, so as to further increase the monitoring range of the high-definition camera body 5, and the cleaning mechanism 7 can clean the impurities when impurities are attached to the surface of the high-definition camera body 5, so as to ensure the clarity of the camera picture of the high-definition camera body 5, so that the staff can see the monitoring picture more clearly and prevent wrong judgment due to blurred picture.

[0028] Example 2

[0029] Reference Figure 2 and 3 , which is the second embodiment of the present invention, and this embodiment is based on the previous embodiment.

[0030] In this embodiment, a first motor 604 is fixedly connected to the right side of the right support plate 601, and the output shaft of the first motor 604 passes through the right support plate 601 and is transmission-connected to the right end of the right rotating column 603. A second motor 605 is fixedly connected to the top of the fixed plate 2, and the output shaft of the second motor 605 passes through the bottom of the fixed plate 2 and is transmission-connected to the top of the movable plate 4. The output shaft of the second motor 605 is movably connected to the inner cavity of the fixed plate 2 via a bearing.

[0031] A support ring 606 is movably connected to the surface of the output shaft of the second motor 605 and located at the bottom of the fixed plate 2 through a bearing, and the top of the support ring 606 is fixedly connected to the bottom of the fixed plate 2. The two sides of the bottom of the aircraft body 1 are fixedly connected to the mounting frame 8, and the two sides of the top of the fixed plate 2 are fixedly connected to the insertion plate 9. The top of the insertion plate 9 extends to the inner cavity of the mounting frame 8 and is detachably connected to the inner cavity of the mounting frame 8. A nut 10 is fixedly connected to the back side of the inner cavity of the mounting frame 8, and a positioning bolt 11 is arranged on the front side of the mounting frame 8. The rear end of the positioning bolt 11 extends to the inner cavity of the nut 10 and is threadedly connected to the inner cavity of the nut 10.

[0032] like Figure 2 and 3 As shown, in the process where the aircraft body 1 drives the high-definition camera body 5 to fly and the high-definition camera body 5 monitors the low-altitude conditions in real time, when it is necessary to adjust the monitoring angle of the high-definition camera body 5, the first motor 604 is started. When the first motor 604 is running, it can cooperate with the fixed sleeve 602 and the rotating column 603 to drive the high-definition camera body 5 to rotate, so as to adjust the monitoring angle of the high-definition camera body 5. When it is necessary to adjust the monitoring direction of the high-definition camera body 5, the second motor 605 is started, and the output shaft of the second motor 605 drives the movable plate 4 to rotate, and the movable plate 4 cooperates with the support plate 601 and the fixed sleeve 603 to rotate. 602 and the rotating column 603 drive the high-definition camera body 5 to rotate, so that the monitoring direction of the high-definition camera body 5 can be adjusted. By disassembling the fixing plate 2, it can be removed from the bottom of the aircraft body 1 so as to inspect and repair multiple components on its surface. When disassembling the fixing plate 2, first rotate the positioning bolt 11 to move the rear end of the positioning bolt 11 out of the inner cavity of the nut 10. After moving out, it can be pulled out from the inner cavity of the mounting frame 8. After being pulled out, the positioning effect of the positioning bolt 11 on the insertion plate 9 disappears. At this time, the insertion plate 9 can be pulled out from the inner cavity of the mounting frame 8, thereby achieving the purpose of disassembling the fixing plate 2.

[0033] Example 3

[0034] Reference Figure 4 and 5 , which is the third embodiment of the present invention, and this embodiment is based on the previous two embodiments.

[0035] In this embodiment, positioning grooves 704 are provided on both sides of the inner cavity of the installation groove 701, and positioning blocks 705 are fixedly connected to both sides of the disassembly plate 702. One side of the positioning block 705 extends to the inner cavity of the positioning groove 704 and is slidably connected to the inner cavity of the positioning groove 704. An auxiliary groove 706 is provided at the bottom of the disassembly plate 702.

[0036] A fixing groove 707 is provided on the side away from the inner cavity of the two positioning grooves 704. The inner cavity of the fixing groove 707 is slidably connected with a clamping block 708. One side of the clamping block 708 is fixedly connected with a spring 709. The end of the spring 709 away from the clamping block 708 is fixedly connected to the inner wall of the fixing groove 707.

[0037] A slide groove 710 is provided on the side of the positioning block 705 away from the disassembly plate 702. One end of the clamping block 708 extends to the inner cavity of the slide groove 710 and is movably connected with the inner cavity of the slide groove 710. A clamping groove 711 is provided in the inner cavity of the slide groove 710, and the clamping block 708 is engaged with the inner cavity of the clamping groove 711.

[0038] like Figure 4 and 5 As shown, when the staff observes that the monitoring image becomes blurred and needs to clean the surface of the high-definition camera body 5, the first motor 604 is also started. The first motor 604 cooperates with the fixing sleeve 602 and the rotating column 603 to drive the high-definition camera body 5 to rotate, so that the high-definition camera body 5 makes a complete circular motion. When the high-definition camera body 5 rotates to the top, its surface can rub against the bottom of the cleaning pad 703, so that the cleaning pad 703 wipes off the impurities attached to the surface, thereby improving the clarity of the camera image. When the cleaning pad 703 needs to be disassembled and cleaned, first use your fingernails to hold the auxiliary groove 706 and pull the disassembly plate 702 outward. At this time, the block 708 in the inner cavity of the groove 711 will be subjected to pressure generated by the pulling force. The pressure causes the inner wall of the groove 711 to squeeze the block 708 and make it slide into the inner cavity of the fixed groove 707. When the block 708 completely slides out of the inner cavity of the groove 711, the disassembly plate 702 can be pulled out from the inner cavity of the installation groove 701 to clean the cleaning pad 703.

[0039] A method for using an aircraft real-time monitoring device based on a low-altitude grid service platform and a method for using the same, the method for using the device comprising the following steps:

[0040] In the process that the aircraft body 1 drives the high-definition camera body 5 to fly and the high-definition camera body 5 monitors the low-altitude conditions in real time, when it is necessary to adjust the monitoring angle of the high-definition camera body 5, the first motor 604 is started. When the first motor 604 is running, it can cooperate with the fixing sleeve 602 and the rotating column 603 to drive the high-definition camera body 5 to rotate, so as to adjust the monitoring angle of the high-definition camera body 5. When it is necessary to adjust the monitoring direction of the high-definition camera body 5, the second motor 605 is started, and the output shaft of the second motor 605 drives the movable plate 4 to rotate. The movable plate 4 then cooperates with the supporting sheet 601, the fixing sleeve 602 and the rotating column 603 to drive the high-definition camera body 5 to rotate, so that the monitoring direction of the high-definition camera body 5 can be adjusted. By disassembling the fixing plate 2, it can be removed from the bottom of the aircraft body 1 so as to inspect and repair multiple components on its surface. When disassembling the fixing plate 2, first rotate the positioning bolt 11 so that the rear end of the positioning bolt 11 is moved out of the inner cavity of the nut 10. After being moved out, it can be pulled out from the inner cavity of the mounting frame 8. After being pulled out, the positioning effect of the positioning bolt 11 on the insertion plate 9 disappears. When the staff observes that the monitoring picture becomes blurred and needs to clean the surface of the high-definition camera body 5, the first motor 604 is also started. The first motor 604 cooperates with the fixing sleeve 602 and the rotating column 603 to drive the high-definition camera body 5 to rotate, so that the high-definition camera body 5 makes a complete circular motion. When the high-definition camera body 5 rotates to the top, its surface can rub against the bottom of the cleaning pad 703, so that the cleaning pad 703 can wipe off the dirt attached to the high-definition camera body 5. To remove impurities on the surface and improve the clarity of the camera image, when the cleaning pad 703 needs to be disassembled and cleaned, first use your fingernails to hold the auxiliary groove 706 and pull the disassembly plate 702 outward. At this time, the block 708 in the inner cavity of the slot 711 will be subjected to pressure generated by the pulling force. The pressure causes the inner wall of the slot 711 to squeeze the block 708, causing it to slide into the inner cavity of the fixed slot 707. When the block 708 completely slides out of the inner cavity of the slot 711, the disassembly plate 702 can be pulled out from the inner cavity of the mounting slot 701 to clean the cleaning pad 703.

[0041] The standard parts used in this application document can all be purchased from the market and can be customized according to the description in the specification and drawings. The specific connection methods of each part adopt conventional means such as mature bolts, rivets, welding, etc. in the prior art. The machinery, parts and equipment all adopt conventional models in the prior art. The control method is automatic control through a controller. The control circuit of the controller can be implemented through simple programming by technicians in this field, which is common knowledge in the field. This application is mainly used to protect mechanical devices, so this application no longer explains the control method and circuit connection in detail.

[0042] It should be noted that, in this article, relational terms such as first and second, etc. are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device. In the absence of further restrictions, the elements defined by the sentence "comprise a ..." do not exclude the existence of other identical elements in the process, method, article or device including the elements.

[0043] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A real-time monitoring device for an aircraft based on a low-altitude grid service platform, comprising an aircraft body (1), characterized in that: A fixed plate (2) is provided at the bottom of the aircraft body (1), and the front and rear ends of both sides of the fixed plate (2) are fixedly connected with supporting legs (3), a movable plate (4) is provided at the bottom of the fixed plate (2), a high-definition camera body (5) is provided at the bottom of the movable plate (4), an adjustment mechanism (6) is provided on the surface of the high-definition camera body (5), and a cleaning mechanism (7) is provided at the bottom of the movable plate (4), and the adjustment mechanism (6) includes a supporting sheet (601), and the supporting sheet (601) is located on both sides of the bottom of the movable plate (4) and is fixed to the movable plate (4). The surface of the high-definition camera body (5) is provided with a fixed sleeve (602), and both sides of the fixed sleeve (602) are fixedly connected with rotating columns (603), and one end of the rotating column (603) away from the fixed sleeve (602) is movably connected to one side of the support plate (601) through a bearing, and the cleaning mechanism (7) includes a mounting groove (701), and the mounting groove (701) is opened at the bottom of the movable plate (4), and the inner cavity of the mounting groove (701) is detachably connected with a disassembly plate (702), and the bottom of the disassembly plate (702) is fixedly connected with a cleaning pad (703).

2. The real-time aircraft monitoring device based on a low-altitude grid service platform according to claim 1 is characterized in that: A first motor (604) is fixedly connected to the right side of the right support plate (601), and an output shaft of the first motor (604) passes through the right support plate (601) and is transmission-connected to the right end of the right rotating column (603). A second motor (605) is fixedly connected to the top of the fixed plate (2), and an output shaft of the second motor (605) passes through the bottom of the fixed plate (2) and is transmission-connected to the top of the movable plate (4). The output shaft of the second motor (605) is movably connected to the inner cavity of the fixed plate (2) via a bearing.

3. The real-time aircraft monitoring device based on a low-altitude grid service platform according to claim 2 is characterized in that: A support ring (606) is movably connected to the surface of the output shaft of the second motor (605) and is located at the bottom of the fixing plate (2) through a bearing, and the top of the support ring (606) is fixedly connected to the bottom of the fixing plate (2). Both sides of the bottom of the aircraft body (1) are fixedly connected to a mounting frame (8), and both sides of the top of the fixing plate (2) are fixedly connected to an insertion plate (9), the top of the insertion plate (9) extends to the inner cavity of the mounting frame (8) and is detachably connected to the inner cavity of the mounting frame (8), the back side of the inner cavity of the mounting frame (8) is fixedly connected to a nut (10), and the front side of the mounting frame (8) is provided with a positioning bolt (11), the rear end of the positioning bolt (11) extends to the inner cavity of the nut (10) and is threadedly connected to the inner cavity of the nut (10).

4. The real-time aircraft monitoring device based on a low-altitude grid service platform according to claim 1 is characterized in that: Positioning grooves (704) are provided on both sides of the inner cavity of the installation groove (701), and positioning blocks (705) are fixedly connected to both sides of the disassembly plate (702), one side of the positioning block (705) extends to the inner cavity of the positioning groove (704) and is slidably connected to the inner cavity of the positioning groove (704), and an auxiliary groove (706) is provided at the bottom of the disassembly plate (702).

5. The real-time aircraft monitoring device based on the low-altitude grid service platform according to claim 4 is characterized by: A fixing groove (707) is provided on one side of the inner cavity of the two positioning grooves (704) away from each other, and a clamping block (708) is slidably connected to the inner cavity of the fixing groove (707), and a spring (709) is fixedly connected to one side of the clamping block (708), and one end of the spring (709) away from the clamping block (708) is fixedly connected to the inner wall of the fixing groove (707).

6. The real-time aircraft monitoring device based on the low-altitude grid service platform according to claim 5 is characterized by: A sliding groove (710) is provided on a side of the positioning block (705) away from the disassembly plate (702); one end of the clamping block (708) extends to the inner cavity of the sliding groove (710) and is movably connected to the inner cavity of the sliding groove (710); a clamping groove (711) is provided in the inner cavity of the sliding groove (710); and the clamping block (708) is clamped with the inner cavity of the clamping groove (711).

7. The method for using the aircraft real-time monitoring device based on the low-altitude grid service platform according to any one of claims 1 to 6, characterized in that: The steps for using it are as follows: A. When the aircraft body (1) drives the high-definition camera body (5) to fly and the high-definition camera body (5) monitors the low-altitude situation in real time, if the monitoring angle of the high-definition camera body (5) needs to be adjusted, the first motor (604) is started. When the first motor (604) is running, it can cooperate with the fixed sleeve (602) and the rotating column (603) to drive the high-definition camera body (5) to rotate, so as to adjust the monitoring angle of the high-definition camera body (5). When the monitoring direction of the high-definition camera body (5) needs to be adjusted, the second motor (605) is started. The output shaft of the second motor (605) drives the movable plate (4) to rotate. The movable plate (4) then cooperates with the support plate (601) and the fixed sleeve (602) to rotate. 602) and the rotating column (603) drive the high-definition camera body (5) to rotate, so that the monitoring direction of the high-definition camera body (5) can be adjusted. By disassembling the fixing plate (2), it can be removed from the bottom of the aircraft body (1) so as to inspect and repair multiple components on its surface. When disassembling the fixing plate (2), first rotate the positioning bolt (11) so that the rear end of the positioning bolt (11) moves out of the inner cavity of the nut (10). After moving out, it can be pulled out from the inner cavity of the installation frame (8). After being pulled out, the positioning effect of the positioning bolt (11) on the insertion plate (9) disappears. At this time, the insertion plate (9) can be pulled out from the inner cavity of the installation frame (8), thereby achieving the purpose of disassembling the fixing plate (2); B. When the staff observes that the monitoring image becomes blurred and needs to clean the surface of the high-definition camera body (5), the first motor (604) is also started. The first motor (604) cooperates with the fixing sleeve (602) and the rotating column (603) to drive the high-definition camera body (5) to rotate, so that the high-definition camera body (5) performs a complete circular motion. When the high-definition camera body (5) rotates to the top, its surface can rub against the bottom of the cleaning pad (703), so that the impurities attached to the surface are wiped off by the cleaning pad (703), thereby improving the clarity of the camera image. When the cleaning pad (703) is disassembled for cleaning, the auxiliary groove (706) is first held with fingernails, and the disassembly plate (702) is pulled outward. At this time, the block (708) in the inner cavity of the groove (711) is subjected to pressure due to the pulling force. The pressure causes the inner wall of the groove (711) to squeeze the block (708) so that it slides into the inner cavity of the fixed groove (707). When the block (708) completely slides out of the inner cavity of the groove (711), the disassembly plate (702) can be pulled out of the inner cavity of the installation groove (701) so as to clean the cleaning pad (703).

Images