CN116620588B - Security monitoring equipment with support structure - Google Patents
Security monitoring equipment with support structure Download PDFInfo
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- CN116620588B CN116620588B CN202310921387.3A CN202310921387A CN116620588B CN 116620588 B CN116620588 B CN 116620588B CN 202310921387 A CN202310921387 A CN 202310921387A CN 116620588 B CN116620588 B CN 116620588B
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- 238000012544 monitoring process Methods 0.000 title claims abstract description 51
- 238000012806 monitoring device Methods 0.000 claims abstract description 38
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- 230000000149 penetrating effect Effects 0.000 claims description 2
- 230000000694 effects Effects 0.000 abstract description 12
- 238000010586 diagram Methods 0.000 description 6
- 238000005516 engineering process Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 3
- 238000005265 energy consumption Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- WSNMPAVSZJSIMT-UHFFFAOYSA-N COc1c(C)c2COC(=O)c2c(O)c1CC(O)C1(C)CCC(=O)O1 Chemical compound COc1c(C)c2COC(=O)c2c(O)c1CC(O)C1(C)CCC(=O)O1 WSNMPAVSZJSIMT-UHFFFAOYSA-N 0.000 description 1
- 208000025174 PANDAS Diseases 0.000 description 1
- 208000021155 Paediatric autoimmune neuropsychiatric disorders associated with streptococcal infection Diseases 0.000 description 1
- 240000000220 Panda oleosa Species 0.000 description 1
- 235000016496 Panda oleosa Nutrition 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000011900 installation process Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
- B64U20/87—Mounting of imaging devices, e.g. mounting of gimbals
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
- B64U10/16—Flying platforms with five or more distinct rotor axes, e.g. octocopters
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/30—Constructional aspects of UAVs for safety, e.g. with frangible components
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U60/00—Undercarriages
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
- B64U2101/31—UAVs specially adapted for particular uses or applications for imaging, photography or videography for surveillance
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Studio Devices (AREA)
Abstract
The invention provides security monitoring equipment with a support structure, and particularly relates to the technical field of security equipment, comprising an unmanned aerial vehicle body, wherein a movable module for adjusting the position of a monitoring assembly is arranged at the lower end of the unmanned aerial vehicle body, the movable module is detachably connected with a fixed module, and the fixed module is fixedly connected on a support or a wall; the monitoring assembly comprises a first monitoring device and a second monitoring device, the movable module comprises a first adjusting structure for enabling the first monitoring device to horizontally rotate and a second adjusting structure for enabling the second monitoring device to vertically rotate, and the first adjusting structure is connected with the second adjusting structure in a linkage mode. The security monitoring equipment with the support structure provided by the invention enables the position of the existing security equipment to be adjusted according to the actual situation when the existing security equipment is installed and adjusted, and achieves the multifunctional technical effect.
Description
Technical Field
The invention belongs to the technical field of monitoring, and particularly relates to security monitoring equipment with a support structure.
Background
With the development of economy and communication technology, security is getting more and more attention. The video monitoring is characterized by visual, accurate, timely and rich information content, is a safety monitoring method which is most widely applied at present, integrates a computer technology, a network technology, an image processing technology and a data transmission technology, can acquire relevant information of a target scene in real time by installing a camera on the target scene for two-dimensional shooting, and is widely applied to places such as factory workshops, home interiors, outdoor worksites and the like.
Taking a common household as an example, in order to ensure safety, a video monitoring camera or an alarm device is generally installed in the household, and a smoke detector, a water intrusion sensor and an infrared detector are connected with a wireless alarm host through connecting the video monitoring camera such as a dome camera and a panda camera with a wireless router in the household, and then the wireless alarm host is connected to the wireless router, so that a household security monitoring system is formed. The user accesses the wireless router by using the mobile terminal, such as a mobile phone, so as to acquire the security information of the home in real time and realize the monitoring of the home.
However, the following technical problems generally exist in the use and installation process of the existing security equipment:
(1) The most widely used security equipment is monitoring security equipment, is mainly applied to monitoring video of places, can find and record security problems at the first time, but most of the current monitoring security equipment is fixedly installed, and is inconvenient to adjust, so that the monitoring range is smaller, the omnibearing coverage of places and environments is difficult to achieve, and the monitoring efficiency is lower;
(2) According to the continuous change of the use requirement, although the movable monitoring security equipment appears in the prior art, the movable monitoring security equipment can be movably monitored on the ground or mounted on the guide rail, but the influence of weather is great, for example, when snowing occurs, snow can remain on the guide rail, thick snow can be formed in the environment with low temperature, so that the movable monitoring security equipment can be blocked when moving on the guide rail, and can not continuously move for monitoring, so that the movable monitoring security equipment is difficult to adapt to the outdoor complex environment, and the monitoring effect of the movable monitoring security equipment is influenced;
(3) The security monitoring support of supervisory equipment, when installing supervisory equipment on the security monitoring support, when installing the control to the eminence, still need install with the help of rising the frame, have certain danger to the staff, inconvenient installation.
Therefore, how to enable the prior security equipment to carry out position adjustment according to the actual situation during installation and adjustment.
Disclosure of Invention
The invention aims to provide security monitoring equipment with a support structure, solves the technical problem of how to enable the existing security equipment to be capable of adjusting the position according to the actual situation when being installed and adjusted, and achieves the multifunctional technical effect.
The security monitoring equipment with the support structure comprises an unmanned aerial vehicle body, wherein a movable module for adjusting the position of a monitoring assembly is arranged at the lower end of the unmanned aerial vehicle body, the movable module is detachably connected with a fixed module, and the fixed module is fixedly connected to a support or a wall; the monitoring assembly comprises a first monitoring device and a second monitoring device, the movable module comprises a first adjusting structure for enabling the first monitoring device to horizontally rotate and a second adjusting structure for enabling the second monitoring device to vertically rotate, and the first adjusting structure is in linkage connection with the second adjusting structure.
The first adjusting structure comprises a vertical column, a horizontal rod, two vertical shafts and a second circular plate, wherein the top end of the vertical column is fixedly arranged at the bottom end of the unmanned aerial vehicle body, the lateral part of the horizontal rod is horizontally fixed at the bottom end of the vertical column, the two vertical shafts are respectively connected to the two ends of the horizontal rod in a rotating mode, the second circular plate is coaxially connected with the bottom end of the vertical shaft, and the second monitoring device is fixedly arranged at the edge position of the upper end face of the second circular plate; the top end of the vertical shaft is connected with the second adjusting structure through a bevel gear assembly.
The second adjusting structure comprises a rotating shaft which horizontally penetrates through and is rotationally connected to the side part of the vertical column, two wheel shafts, a rotating wheel and an angle adjusting structure, wherein one end of the two wheel shafts is respectively rotationally connected to two ends of the rotating shaft, the rotating wheel is coaxially and fixedly connected to the other end of the wheel shaft, the angle adjusting structure is connected with the inner side part of the rotating wheel, the angle adjusting structure is also connected with the side part of the rotating shaft, and the side part of the rotating shaft is connected with the bevel gear assembly; the lateral part of pivot is connected with the motor through the drive belt, the motor is fixed to be set up on the horizon bar.
The bevel gear assembly comprises a bevel gear II coaxially arranged on the rotating shaft and a bevel gear I coaxially arranged on the vertical shaft, and the bevel gear I is in meshed connection with the bevel gear II.
The rotating wheel comprises a circular plate I and a cone coaxially fixed on the inner side surface of the circular plate I, the bottom surface of the cone is consistent with the upper bottom surface and the lower bottom surface of the circular plate I in size and is tightly attached to the circular plate I, and the conical surface of the cone is inclined towards the rotating shaft; the rotating shaft penetrates through the first circular plate and the center of the cone.
The angle adjusting structure comprises a hinging seat fixedly arranged on the side part of the rotating shaft, an electric push rod, a sliding block and monitoring equipment I, wherein the bottom end of the electric push rod is rotatably connected with the hinging seat, the sliding block is movably arranged at the free end of the electric push rod, the monitoring equipment I is fixedly arranged on the sliding block, and the side surface of the sliding block is hinged with the free end of the electric push rod; the conical surface is provided with a chute, and the central line of the chute and the central line of the rotating shaft are both positioned on the rotating surface of the central line of the wheel shaft.
The outer side of the vertical shaft is provided with a plurality of second propellers in a circular array.
The fixing module comprises a vertical plate, two upper horizontal rods which are parallel to each other and are respectively fixed at two ends of the vertical plate, lifting rods which are arranged right below the upper horizontal rods in parallel, connecting rods with two ends respectively and vertically fixedly connected with the lifting rods, and lifting cylinders with free ends vertically connected with the bottom surfaces of the connecting rods; the bottom end of the vertical plate is horizontally provided with a lower horizontal rod, the two lower horizontal rods are connected through a supporting rod, and the bottom end of the lifting cylinder is fixed on the supporting rod; the bottom surface of going up the horizon bar is provided with half slot one, the up end of lifter is provided with half slot two, half slot one with half slot two detachable butt joint to form the round hole.
The outer end of the lower horizontal rod is provided with a magnet plate.
The beneficial effects of the invention are as follows:
(1) The scheme is provided with a first adjusting structure, and has the following technical effects:
the first circular plate II can drive the second monitoring equipment to horizontally rotate, so that the second monitoring equipment is positioned in different angle directions, and shooting and photographing are carried out; the second circular plate falls above the magnet plate when the second circular plate is stationary, and plays a role in supporting and fixing the whole device; third, be provided with screw two on the vertical scroll, when the unmanned aerial vehicle body drove whole device and take off, the vertical scroll can rotate under the effect of external force, and then makes screw two rotate, and screw two's rotation helps improving the lift, reduces the energy consumption of unmanned aerial vehicle body.
(2) The scheme is provided with a second adjusting structure, and has the following technical effects:
the first circular plate can drive the first monitoring equipment to rotate up and down, so that the first monitoring equipment is positioned in different angle directions and performs shooting and photographing; secondly, when the unmanned aerial vehicle body is in a take-off state, the circular plate I is in a vertical state, and the bottom of the outer side of the circular plate I is contacted with the ground, so that the effect of wheels can be achieved; and thirdly, under the action of the angle adjusting structure, the first circular plate can be in a horizontal state, so that the first circular plate has a shielding effect, and is beneficial to protecting the first monitoring equipment in rainy and snowy days.
(3) The angle adjusting structure is arranged in the scheme, and has the following technical effects:
firstly, the inclination angle of the first circular plate can be adjusted, and the first circular plate can be adjusted according to actual situations; secondly, help adjusting supervisory equipment one's position, the convenience is shot and is made a video recording to the shooting of vertical direction different angles.
(4) According to the scheme, the security equipment, the support and the unmanned aerial vehicle are designed in a modularized mode, so that the security equipment is designed in a movable mode, and under the action of the unmanned aerial vehicle, only a plurality of fixed modules are required to be arranged, so that the movable modules can be switched among different fixed modules, and the monitoring range is enlarged; in addition, can be applied to the weather of sleet, help protecting the camera, finally, because fixed module and movable module can nimble dock, therefore very big convenience is installed the automatic adjustment process of dismantling.
Drawings
Fig. 1 is a schematic structural diagram of a security monitoring device in an embodiment of the present invention.
Fig. 2 is a front view of a security monitoring device in an embodiment of the present invention.
Fig. 3 is a schematic structural diagram of an active module according to an embodiment of the invention.
Fig. 4 is a schematic diagram of a connection structure between an angle adjusting structure and a first circular plate in an embodiment of the invention.
Fig. 5 is a schematic structural diagram of a fixing module according to an embodiment of the invention.
Fig. 6 is a schematic diagram of a connection structure between the angle adjusting structure and the first circular plate in the embodiment of the invention.
Fig. 7 is a schematic structural diagram of a unmanned aerial vehicle system according to an embodiment of the present invention.
Wherein, the reference numerals are as follows: 1. an unmanned aerial vehicle body; 2. a first propeller; 3. a fixed module; 31. a vertical plate; 32. a horizontal rod is arranged; 321. a semicircular groove I; 33. a lifting rod; 331. a semicircular groove II; 34. a first bolt; 35. a lower horizontal rod; 36. a magnet plate; 37. a lifting cylinder; 38. a support rod; 39. a second bolt; 4. an angle adjusting structure; 41. a hinge base; 42. an electric push rod; 43. a sliding block; 44. monitoring equipment I; 5. a circular plate I; 51. a chute; 52. conical surface; 6. a wheel axle; 7. a rotating shaft; 8. monitoring equipment II; 9. a circular plate II; 10. a second propeller; 11. a vertical shaft; 12. a horizontal bar; 13. a vertical column; 14. bevel gears I; 15. bevel gears II; 17. a transmission belt; 18. a motor; 19. an adjusting structure I; 20. an adjusting structure II; 21. bevel gear assembly.
Detailed Description
In order to more clearly describe the technical characteristics of the present solution, the present solution is described below by means of specific embodiments.
Referring to fig. 1-7, a security monitoring device with a bracket structure comprises an unmanned aerial vehicle body 1, wherein a movable module for adjusting the position of a monitoring component is arranged at the lower end of the unmanned aerial vehicle body 1, the movable module is detachably connected with a fixed module 3, and the fixed module 3 is fixedly connected on a bracket or a wall; the monitoring assembly comprises a first monitoring device 44 and a second monitoring device 8, and the movable module comprises a first adjusting structure 19 for enabling the first monitoring device 44 to horizontally rotate and a second adjusting structure 20 for enabling the second monitoring device 8 to vertically rotate, wherein the first adjusting structure 19 is in linkage connection with the second adjusting structure 20.
A first propeller 2 is arranged on the unmanned aerial vehicle body 1.
The first adjusting structure 19 comprises a vertical column 13, a horizontal rod 12, two vertical shafts 11, a second circular plate 9 and a second monitoring device 8, wherein the top end of the vertical column 13 is fixedly arranged at the bottom end of the unmanned aerial vehicle body 1, the lateral part of the horizontal rod is horizontally fixed at the bottom end of the vertical column 13, the two vertical shafts 11 are respectively connected at two ends of the horizontal rod 12 in a rotating mode, the second circular plate 9 is coaxially connected with the bottom end of the vertical shaft 11, and the second monitoring device 8 is fixedly arranged at the edge position of the upper end face of the second circular plate 9; the top end of the vertical shaft 11 is connected with the second adjusting structure 20 through a bevel gear assembly 21.
The second adjusting structure 20 comprises a rotating shaft 7 horizontally penetrating through and rotationally connected to the side part of the vertical column 13, two wheel shafts 6 with one ends respectively rotationally connected to two ends of the rotating shaft 7, a rotating wheel coaxially and fixedly connected to the other end of the wheel shaft 6, and an angle adjusting structure 4 connected with the inner side part of the rotating wheel, wherein the angle adjusting structure 4 is also connected with the side part of the rotating shaft 7, and the side part of the rotating shaft 7 is connected with the bevel gear assembly 21; the side part of the rotating shaft 7 is connected with a motor 18 through a transmission belt 17, and the motor 18 is fixedly arranged on the horizontal rod 12.
The bevel gear assembly 21 comprises a bevel gear II 15 coaxially arranged on the rotating shaft 7 and a bevel gear I14 coaxially arranged on the vertical shaft 11, wherein the bevel gear I14 is in meshed connection with the bevel gear II 15.
The rotating wheel comprises a circular plate I5 and a cone coaxially fixed on the inner side surface of the circular plate I5, the bottom surface of the cone is consistent with the upper bottom surface and the lower bottom surface of the circular plate I5 in size and is tightly attached, and the conical surface 52 of the cone is inclined towards the rotating shaft 7; the rotating shaft 7 passes through the center of the circular plate 5 and the cone.
The angle adjusting structure 4 comprises a hinging seat 41 fixedly arranged on the side part of the rotating shaft 7, an electric push rod 42 with the bottom end rotationally connected with the hinging seat 41, a sliding block 43 movably arranged at the free end of the electric push rod 42, and monitoring equipment I44 fixedly arranged on the sliding block 43, wherein the side surface of the sliding block 43 is hinged with the free end of the electric push rod 42; the conical surface 52 is provided with a chute 51, and the central line of the chute 51 and the central line of the rotating shaft 7 are both positioned on the rotating surface of the central line of the wheel shaft 6.
The outer side of the vertical shaft 11 is provided with a plurality of second propellers 10 in a circular array.
The fixed module 3 comprises a vertical plate 31, two upper horizontal rods 32 which are parallel to each other and are respectively fixed at two ends of the vertical plate 31, lifting rods 33 which are arranged right below the upper horizontal rods 32 in parallel, connecting rods with two ends respectively and vertically fixedly connected with the two lifting rods 33, and lifting cylinders 37 with free ends vertically connected with the bottom surfaces of the connecting rods;
the bottom end of the vertical plate 31 is horizontally provided with a lower horizontal rod 35, the two lower horizontal rods 35 are connected through a supporting rod 38, and the bottom end of the lifting cylinder 37 is fixed on the supporting rod 38; the bottom surface of the upper horizontal rod 32 is provided with a half groove I321, the upper end surface of the lifting rod 33 is provided with a half groove II 331, and the half groove I321 and the half groove II 331 are detachably connected to form a round hole.
A first bolt 34 and a second bolt 39 are arranged on the side of the vertical plate 31, and the first bolt 34 and the second bolt 39 are fixed on a bracket or a wall body.
The outer end of the lower horizontal bar 35 is provided with a magnet plate 36.
The specific working process of the invention comprises the following steps:
the security monitoring equipment in this scheme, including these two parts of fixed module 3 and movable module, fixed module 3 can be provided with a plurality ofly, installs on the wall, on the support, on the wire pole, on the track etc. through the bolt respectively.
Under the driving action of the unmanned aerial vehicle body 1, the butt joint of the fixed module 3 and the movable module is realized, and it is to be noted that the unmanned aerial vehicle body 1 can be designed in a path, namely, the path from one fixed module 3 to the other fixed module 3 is determined, and the operation is easy for a person skilled in the art.
When the movable module is in butt joint with the fixed module 3, the lifting cylinder 37 drives the lifting rod 33 to descend, the semicircular groove I321 and the semicircular groove II 331 are temporarily separated, the unmanned aerial vehicle body 1 drives the rotating shaft 7, the rotating shaft 7 stretches into the space between the semicircular groove I321 and the semicircular groove II 331 (when the circular plate II 9 reaches the upper part of the magnet plate 36), then the lifting cylinder 37 enables the lifting rod 33 to be in contact with the upper horizontal rod 32, the rotating shaft 7 is clamped, and the bottom surface of the circular plate II 9 is in contact with the upper end surface of the magnet plate 36 to be attracted, so that the positioning of the circular plate II 9 is realized.
When the positions of the first monitoring device 44 and the second monitoring device 8 need to be adjusted, under the action of the motor 18, the rotating shaft 7 rotates, and the vertical shaft 11 is driven to rotate through the first bevel gear 14 and the second bevel gear 15, so that the first circular plate 5 and the second circular plate 9 rotate, and the shooting angles of the first monitoring device 44 and the second monitoring device 8 are adjusted.
Specifically, the second circular plate 9 can drive the second monitoring device 8 to horizontally rotate, so that the second monitoring device 8 is positioned in different angular directions for shooting and photographing, and the first circular plate 5 can drive the first monitoring device 44 to vertically rotate, so that the first monitoring device 44 is positioned in different angular directions and shooting and photographing are performed.
When unmanned aerial vehicle body 1 takes off under the route of design, take off and shift, lift cylinder 37 moves down lifter 33, and pivot 7 breaks away from half slot one 321 and half slot two 331, is provided with screw two 10 on vertical scroll 11, and when unmanned aerial vehicle body 1 drove whole device and takes off, vertical scroll 11 can rotate under the effect of external force, and then makes screw two 10 rotate, and the rotation of screw two 10 helps improving the lift, reduces unmanned aerial vehicle body 1's energy consumption.
When the unmanned aerial vehicle body 1 is in the state of taking off, in order to save energy, the first circular plate 5 is in a vertical state, and the bottom of the outer side of the first circular plate is in contact with the ground, so that the effect of wheels can be achieved.
In addition, under the action of the angle adjusting structure 4, namely, the electric push rod 42 is retracted to drive the sliding block 43 to slide, so that the sliding block 43 drives the first circular plate 5 to be in a horizontal state, and the first circular plate 5 has a shielding effect, thereby being beneficial to protecting the first monitoring equipment 44 in rainy and snowy weather.
According to the scheme, the security equipment, the support and the unmanned aerial vehicle are designed in a modularized mode, so that the security equipment is designed in a movable mode, and under the action of the unmanned aerial vehicle, only a plurality of fixed modules 3 are required to be arranged, so that the movable modules can be switched among different fixed modules 3, and the monitoring range is enlarged; in addition, can be applied to the weather of sleet, help protecting the camera, finally, because fixed module 3 and movable module can nimble dock, therefore very big convenience is installed the automatic adjustment process of dismantling.
The technical features of the present invention that are not described in the present invention may be implemented by or using the prior art, and are not described in detail herein, but the above description is not intended to limit the present invention, and the present invention is not limited to the above examples, but is also intended to be within the scope of the present invention by those skilled in the art.
Claims (7)
1. The security monitoring equipment with the support structure comprises an unmanned aerial vehicle body (1), and is characterized in that a movable module for adjusting the position of a monitoring assembly is arranged at the lower end of the unmanned aerial vehicle body (1), the movable module is detachably connected with a fixed module (3), and the fixed module (3) is fixedly connected to a support or a wall;
the monitoring assembly comprises a first monitoring device (44) and a second monitoring device (8), the movable module comprises a first adjusting structure (19) for enabling the second monitoring device (8) to horizontally rotate and a second adjusting structure (20) for enabling the first monitoring device (44) to vertically rotate, and the first adjusting structure (19) and the second adjusting structure (20) are in linkage connection;
the first adjusting structure (19) comprises a vertical column (13) with the top end fixedly arranged at the bottom end of the unmanned aerial vehicle body (1), a horizontal rod (12) with the side part horizontally fixed at the bottom end of the vertical column (13), two vertical shafts (11) respectively connected with the two ends of the horizontal rod (12) in a rotating mode, a second circular plate (9) coaxially connected with the bottom end of the vertical shaft (11), and a second monitoring device (8) is fixedly arranged at the edge position of the upper end face of the second circular plate (9);
the top end of the vertical shaft (11) is connected with the second adjusting structure (20) through a bevel gear assembly (21);
the second adjusting structure (20) comprises a rotating shaft (7) horizontally penetrating through and rotatably connected to the side part of the vertical column (13), two wheel shafts (6) with one ends respectively rotatably connected to two ends of the rotating shaft (7), a rotating wheel coaxially and fixedly connected to the other end of the wheel shaft (6), and an angle adjusting structure (4) connected with the inner side part of the rotating wheel, wherein the angle adjusting structure (4) is also connected with the side part of the rotating shaft (7), and the side part of the rotating shaft (7) is connected with the bevel gear assembly (21);
the side part of the rotating shaft (7) is connected with a motor (18) through a transmission belt (17), and the motor (18) is fixedly arranged on the horizontal rod (12).
2. The security monitoring device with a support structure according to claim 1, wherein the bevel gear assembly (21) comprises a bevel gear two (15) coaxially arranged on the rotating shaft (7), and a bevel gear one (14) coaxially arranged on the vertical shaft (11), and the bevel gear one (14) is in meshed connection with the bevel gear two (15).
3. The security monitoring device with the support structure according to claim 1, wherein the rotating wheel comprises a circular plate one (5) and a cone coaxially fixed on the inner side surface of the circular plate one (5), the bottom surface of the cone is consistent with the upper bottom surface and the lower bottom surface of the circular plate one (5) in size and is tightly attached, and the conical surface (52) of the cone is inclined towards the rotating shaft (7);
the rotating shaft (7) passes through the circular plate I (5) and the center of the cone.
4. The security monitoring device with the support structure according to claim 3, wherein the angle adjusting structure (4) comprises a hinging seat (41) fixedly arranged at the side part of the rotating shaft (7), an electric push rod (42) with the bottom end rotationally connected with the hinging seat (41), a sliding block (43) movably arranged at the free end of the electric push rod (42), and a monitoring device I (44) fixedly arranged on the sliding block (43), and the side surface of the sliding block (43) is hinged with the free end of the electric push rod (42);
a chute (51) is formed in the conical surface (52), and the central line of the chute (51) and the central line of the rotating shaft (7) are both positioned on the rotating surface of the central line of the wheel shaft (6).
5. A security monitoring device with a support structure according to claim 3, characterized in that the outside of the vertical shaft (11) is provided with a plurality of propellers (10) in a circular array.
6. The security monitoring device with the support structure according to claim 1, wherein the fixing module (3) comprises a vertical plate (31), two upper horizontal rods (32) which are parallel to each other and are respectively fixed at two ends of the vertical plate (31), lifting rods (33) which are arranged right below the upper horizontal rods (32) in parallel, connecting rods with two ends respectively and vertically fixedly connected with the two lifting rods (33), and lifting cylinders (37) with free ends vertically connected with the bottom surfaces of the connecting rods;
a lower horizontal rod (35) is horizontally arranged at the bottom end of the vertical plate (31), the two lower horizontal rods (35) are connected through a supporting rod (38), and the bottom end of the lifting cylinder (37) is fixed on the supporting rod (38);
the bottom surface of going up horizon bar (32) is provided with half slot one (321), the up end of lifter (33) is provided with half slot two (331), half slot one (321) with half slot two (331) detachable butt joint to form the round hole.
7. The security monitoring device with a bracket structure according to claim 6, wherein the outer end of the lower horizontal rod (35) is provided with a magnet plate (36).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310921387.3A CN116620588B (en) | 2023-07-26 | 2023-07-26 | Security monitoring equipment with support structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310921387.3A CN116620588B (en) | 2023-07-26 | 2023-07-26 | Security monitoring equipment with support structure |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN116620588A CN116620588A (en) | 2023-08-22 |
| CN116620588B true CN116620588B (en) | 2023-09-29 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202310921387.3A Active CN116620588B (en) | 2023-07-26 | 2023-07-26 | Security monitoring equipment with support structure |
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| CN (1) | CN116620588B (en) |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
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| KR20230036637A (en) * | 2021-09-07 | 2023-03-15 | 정하익 | Construction, works, cleaning, treatment, material, products, equipment, facility, drone, 3D printer, mobility |
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| KR101654799B1 (en) * | 2015-08-31 | 2016-09-06 | 고성우 | drone |
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| CN116620588A (en) | 2023-08-22 |
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