CN216443812U - A monitoring device for unmanned aerial vehicle - Google Patents
A monitoring device for unmanned aerial vehicle Download PDFInfo
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- CN216443812U CN216443812U CN202220106455.1U CN202220106455U CN216443812U CN 216443812 U CN216443812 U CN 216443812U CN 202220106455 U CN202220106455 U CN 202220106455U CN 216443812 U CN216443812 U CN 216443812U
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Abstract
The utility model relates to a monitoring device for unmanned aerial vehicle relates to unmanned aerial vehicle's field, its including set up in mounting panel, the rotation of unmanned aerial vehicle main part bottom connect in the shell of mounting panel bottom and through the flexible subassembly set up in the control subassembly of shell department, the mounting panel is provided with and is used for driving shell pivoted drive assembly, the control subassembly including set up in the connecting rod of flexible subassembly bottom, articulate in the hinge bar that flexible subassembly one end was kept away from to the connecting rod, set up in the control piece of hinge bar and be used for the regulating part of the angle of adjusting connecting rod and hinge bar. When the pitch angle of the monitoring piece needs to be adjusted, the angle between the hinge rod and the connecting rod is adjusted through the adjusting piece, the monitoring piece is in an inclined state, then the shell is driven to rotate through the driving assembly, the direction of the monitoring piece is adjusted, and therefore the monitoring range is enlarged.
Description
Technical Field
The application relates to the field of unmanned aerial vehicles, in particular to a monitoring device for an unmanned aerial vehicle.
Background
An unmanned aircraft, referred to as "drone", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either fully or intermittently, by an onboard computer. Unmanned aerial vehicle can be used for a plurality of fields such as security protection control, agriculture, photography, carries out security protection control through unmanned aerial vehicle at present and has alleviateed staff's work load.
In the process of implementing the application, the inventor finds that at least the following problems exist in the technology: the scope and the direction of traditional unmanned aerial vehicle control for security protection monitoring are specific, when needs adjust control range and direction, need adjust whole unmanned aerial vehicle's flight direction, can influence unmanned aerial vehicle's flight like this.
SUMMERY OF THE UTILITY MODEL
In order to facilitate adjusting the scope and the direction of control, this application provides a monitoring device for unmanned aerial vehicle.
The application provides a monitoring device for unmanned aerial vehicle adopts following technical scheme:
the utility model provides a monitoring device for unmanned aerial vehicle, including set up in mounting panel, the rotation of unmanned aerial vehicle main part bottom connect in the shell of mounting panel bottom and through flexible subassembly set up in the control subassembly of shell department, the mounting panel is provided with and is used for driving shell pivoted drive assembly, the control subassembly including set up in the connecting rod of flexible subassembly bottom, articulate in the hinge bar of flexible subassembly one end is kept away from to the connecting rod, set up in the control piece of hinge bar and be used for the regulating part of the angle of adjusting connecting rod and hinge bar.
Through adopting above-mentioned technical scheme, after the unmanned aerial vehicle main part flies the sky, the control piece can be shot the condition on ground, when the angle of pitch of control piece is adjusted to needs, adjusts the angle between hinge bar and the connecting rod through the regulating part to make the control piece be in the tilt state, then rotate through drive assembly drive shell, with the direction of adjusting the control piece, thereby improve monitoring range.
Optionally, the drive assembly comprises a drive motor arranged at the bottom of the mounting plate, a drive gear arranged at the output end of the drive motor and a gear ring arranged outside the shell, and the drive gear is meshed with the gear ring.
By adopting the technical scheme, the driving motor is started, and the driving motor can drive the shell to rotate through the driving gear and the gear ring.
Optionally, the bottom of the shell is provided with an opening, the telescopic assembly comprises a telescopic cylinder arranged in the shell and a connecting plate arranged at a piston rod of the telescopic cylinder, and the connecting rod is arranged on one side, far away from the telescopic cylinder, of the connecting plate.
Through adopting above-mentioned technical scheme, telescopic cylinder can drive the control piece and reciprocate, when need not use the control piece, heightens the height of control piece, makes the control piece be located the inside of shell completely, makes the control piece be difficult for receiving to collide with.
Optionally, the adjusting part is an adjusting cylinder, and two ends of the adjusting cylinder are hinged to the connecting plate and the hinge rod respectively.
Through adopting above-mentioned technical scheme, adjust actuating cylinder, adjust the corresponding flexible of actuating cylinder piston rod to adjust the angle between hinge bar and the connecting rod, thereby adjust the angle of hinge bar and supervision spare.
Optionally, the lower end of the shell is hinged with a cover body used for covering the opening of the shell, one end of the cover body is provided with an extension plate, and a hinged cylinder is hinged between the cover body and the extension plate.
Through adopting above-mentioned technical scheme, when the control piece was located the shell inside completely, make articulated cylinder piston rod extension to with the lid in the lower tip of shell, further play the guard action to the control piece.
Optionally, the hinge cylinder and the driving motor are respectively located at two opposite sides outside the housing.
Through adopting above-mentioned technical scheme, the focus that makes the unmanned aerial vehicle main part is located the central point of unmanned aerial vehicle main part and puts to stationarity when improving the flight of unmanned aerial vehicle main part.
Optionally, a connecting block is arranged at the end of the piston rod of the telescopic cylinder, and the connecting block is connected with the connecting plate through a connecting screw.
Through adopting above-mentioned technical scheme, make connecting block and connecting plate can dismantle the connection, be convenient for carry out dismouting and change to the control piece.
Optionally, a buffer pad is disposed on one side of the cover body close to the housing.
Through adopting above-mentioned technical scheme, when the lid has not opened completely, if telescopic cylinder piston rod has begun the extension this moment, the blotter can cushion the control piece, reduces the damage of control piece.
In summary, the present application includes at least one of the following beneficial technical effects:
1. when the main body of the unmanned aerial vehicle flies into the sky, the monitoring part can shoot the ground, when the pitch angle of the monitoring part needs to be adjusted, the adjusting part is used for adjusting the angle between the hinge rod and the connecting rod, the monitoring part is in an inclined state, and then the driving assembly drives the shell to rotate so as to adjust the direction of the monitoring part, so that the monitoring range is enlarged;
2. when the monitoring part is not needed to be used, the height of the monitoring part is increased, so that the monitoring part is completely positioned in the shell, and the monitoring part is not easy to collide; when the monitoring part is completely positioned in the shell, the piston rod of the hinged cylinder is extended, so that the cover body covers the lower end part of the shell, and the monitoring part is further protected.
Drawings
FIG. 1 is a schematic illustration of the present application;
FIG. 2 is a schematic view of a housing and monitoring assembly of the present application.
Description of reference numerals: 1. an unmanned aerial vehicle main body; 11. a support leg; 2. mounting a plate; 21. a drive motor; 211. a drive gear; 22. a ring gear; 3. a housing; 31. a telescopic cylinder; 311. connecting blocks; 32. a connecting plate; 33. a cover body; 331. an extension plate; 332. a hinged cylinder; 333. a cushion pad; 41. a connecting rod; 42. a hinged lever; 43. an adjustment member; 44. and monitoring the control.
Detailed Description
The present application is described in further detail below with reference to figures 1-2.
The embodiment of the application discloses a monitoring device for unmanned aerial vehicle, refer to fig. 1, including mounting panel 2, shell 3 and control subassembly, 2 fixed mounting of mounting panel in unmanned aerial vehicle main part 1 bottoms, shell 3 rotates through the bearing and installs in 2 bottoms of mounting panel, and 3 internally mounted of shell have flexible subassembly, and 3 insides of shell are connected with the control subassembly through flexible subassembly. A plurality of landing legs 11 are installed to 1 bottom of unmanned aerial vehicle main part, place unmanned aerial vehicle main part 1 when subaerial, the height of 3 bottoms of shell is still higher than the height of landing leg 11 bottoms.
Referring to fig. 1 and 2, shell 3 is cylindricly, and the tip is the opening setting under shell 3, and the control subassembly includes connecting rod 41, articulated rod 42 and regulating part 43, and connecting rod 41 is vertical to be fixed in the flexible subassembly bottom, and articulated rod 42 articulates in the one end that the flexible subassembly was kept away from to connecting rod 41, and regulating part 43 installs between connecting rod 41 and articulated rod 42, and in this embodiment, regulating part 43 is adjusting cylinder, and the relative both ends of adjusting cylinder are articulated with flexible subassembly and articulated rod 42 respectively. In addition, the monitoring assembly further comprises a monitoring part 44, the monitoring part 44 is mounted at one end of the hinge rod 42 away from the connecting rod 41, and in the embodiment, the monitoring part 44 is a camera.
By adjusting the telescopic assembly, the monitoring part 44 can be adjusted to the outside of the housing 3, and then the inclination angle of the hinge rod 42 can be adjusted by the adjusting part 43 to adjust the angle of the monitoring part 44, thereby increasing the shooting range of the monitoring part 44.
Drive assembly is installed to 2 bottoms of mounting panel, and drive assembly includes driving motor 21, drive gear 211 and ring gear 22, and driving motor 21 fixed connection is in 2 bottoms of mounting panel, and driving motor 21 is vertical downwards, and drive gear 211 key-type is connected in driving motor 21 output shaft, and the shell 3 outside is located to the fixed cover of ring gear 22, and drive gear 211 and the meshing of ring gear 22.
The hinge rod 42 is adjusted to be in an inclined state through the adjusting piece 43, the monitoring piece 44 is enabled to be in an inclined state, then the driving motor 21 is started, the driving motor 21 drives the shell 3 to rotate through the driving gear 211 and the gear ring 22, the monitoring piece 44 is driven to rotate, the direction of the monitoring piece 44 is adjusted, and the shooting range of the monitoring piece 44 is further enlarged.
The telescopic assembly comprises a telescopic cylinder 31 and a connecting plate 32, the telescopic cylinder 31 is fixedly connected to the inner top surface of the shell 3, the telescopic cylinder 31 is vertically downward, a connecting block 311 is fixedly connected to the end part of a piston rod of the telescopic cylinder 31, the connecting plate 32 is connected to the bottom of the connecting block 311, the connecting block 311 is connected with the connecting plate 32 through a connecting screw, in addition, the connecting rod 41 is fixedly connected to one side, away from the telescopic cylinder 31, of the connecting plate 32, and the adjusting piece 43 is hinged to one side, away from the connecting plate 32, of the connecting plate 32.
The telescopic cylinder 31 is adjusted, the end part of the piston rod of the telescopic cylinder 31 can drive the connecting plate 32 and the monitoring part 44 to move up and down, and when the monitoring part 44 needs to be used, the height of the monitoring part 44 is reduced, so that the monitoring part 44 extends out of the shell 3, and the monitoring part 44 is convenient to monitor; when the monitoring part 44 is not needed, the height of the monitoring part 44 is increased, so that the monitoring part 44 is completely positioned in the shell 3, the monitoring part 44 is stored, the monitoring part 44 is protected, and the monitoring part 44 is not easy to collide with. In addition, by arranging the connection screw, the connection block 311 and the connection plate 32 are detachably connected, so that the monitoring part 44 can be conveniently detached and replaced.
In order to further protect the monitoring part 44, the lower end of the housing 3 is hinged to a cover 33, the cover 33 is used for covering the opening at the bottom of the housing 3, the cover 33 is arranged in a circular shape, an extending plate 331 is fixedly connected to one end of the cover 33 close to the hinged point, a hinge cylinder 332 is installed between the extending plate 331 and the cover 33, and two opposite ends of the hinge cylinder 332 are respectively hinged to the outside of the housing 3 and the extending plate 331. When the monitoring part 44 is not needed, the telescopic cylinder 31 is adjusted to enable the piston rod of the telescopic cylinder 31 to contract so as to drive the connecting plate 32 and the monitoring part 44 to move and contract into the shell 3, then the hinged cylinder 332 is adjusted to enable the piston rod of the hinged cylinder 332 to extend, so that the cover body 33 covers the lower end part of the shell 3 and seals the opening of the shell 3, and the monitoring part 44 is further protected. In addition, in order to reduce the shielding of the monitoring part 44 by the cover 33, the cover 33 is made of an acrylic material and has good light transmittance.
Further, a buffer 333 is installed on one side of the cover 33, when the cover 33 covers the bottom of the housing 3, the buffer 333 is located on the top of the cover 33, and the buffer 333 is made of transparent rubber material, has certain elasticity, and has good light transmittance. When the cover 33 is not completely opened, if the piston rod of the telescopic cylinder 31 begins to extend, the cushion 333 can cushion the monitoring element 44 to reduce the damage to the monitoring element 44 until the cover 33 is opened.
In order to improve the stability of unmanned aerial vehicle main part 1 when flying, driving motor 21 and articulated cylinder 332 are located the outer relative both sides of shell 3 respectively, make the focus of unmanned aerial vehicle main part 1 be located the central point of unmanned aerial vehicle main part 1 and put to stability when improving unmanned aerial vehicle main part 1 and fly.
The implementation principle of the monitoring device for the unmanned aerial vehicle is as follows: after unmanned aerial vehicle main part 1 flies to the sky, control piece 44 can shoot the condition on ground, when the pitch angle of supervision control piece 44 was adjusted to needs, the adjusting cylinder piston rod is flexible to adjust the pitch angle of supervision control piece 44 through articulated rod 42, in order to increase the shooting scope of supervision control piece 44. When the monitoring piece 44 is in an inclined state, the driving motor 21 is started, and the driving motor 21 drives the housing 3 to rotate through the driving gear 211 and the gear ring 22 so as to drive the hinge rod 42 and the monitoring piece 44 to rotate, so that the orientation of the monitoring piece 44 is adjusted, and the shooting range of the monitoring piece 44 is further improved. When the monitoring part 44 is not needed, the piston rod of the telescopic cylinder 31 extends and retracts, the monitoring part 44 is completely accommodated in the shell 3, then the hinged cylinder 332 is adjusted, the piston rod of the hinged cylinder 332 extends, the cover body 33 covers the bottom of the shell 3, and the monitoring part 44 is further protected.
The above embodiments are preferred embodiments of the present application, and the protection scope of the present application is not limited by the above embodiments, so: all equivalent changes made according to the structure, shape and principle of the present application shall be covered by the protection scope of the present application.
Claims (8)
1. A monitoring device for unmanned aerial vehicle, its characterized in that: including set up in mounting panel (2), the rotation of unmanned aerial vehicle main part (1) bottom connect in shell (3) of mounting panel (2) bottom and through flexible subassembly set up in the control subassembly of shell (3) department, mounting panel (2) are provided with and are used for driving shell (3) pivoted drive assembly, the control subassembly including set up in connecting rod (41) of flexible subassembly bottom, articulate in articulated mast (42) of flexible subassembly one end are kept away from in connecting rod (41), set up in control piece (44) of articulated mast (42) and be used for adjusting regulating adjusting part (43) of the angle of connecting rod (41) and articulated mast (42).
2. A monitoring device for unmanned aerial vehicles according to claim 1, wherein: drive assembly including set up in driving motor (21) of mounting panel (2) bottom, set up in drive gear (211) of driving motor (21) output and set up in ring gear (22) in shell (3) outside, drive gear (211) and ring gear (22) meshing.
3. A monitoring device for unmanned aerial vehicles according to claim 2, wherein: the bottom of the shell (3) is provided with an opening, the telescopic assembly comprises a telescopic cylinder (31) arranged in the shell (3) and a connecting plate (32) arranged at the position of a piston rod of the telescopic cylinder (31), and the connecting rod (41) is arranged on one side, away from the telescopic cylinder (31), of the connecting plate (32).
4. A monitoring device for unmanned aerial vehicles according to claim 3, wherein: the adjusting piece (43) is an adjusting cylinder, and two ends of the adjusting cylinder are respectively hinged with the connecting plate (32) and the hinge rod (42).
5. A monitoring device for unmanned aerial vehicles according to claim 3, wherein: the lower end of the shell (3) is hinged with a cover body (33) used for covering the opening of the shell (3), one end of the cover body (33) is provided with an extension plate (331), and a hinged cylinder (332) is hinged between the cover body (33) and the extension plate (331).
6. A monitoring device for unmanned aerial vehicle according to claim 5, wherein: the hinged air cylinder (332) and the driving motor (21) are respectively positioned at two opposite sides outside the shell (3).
7. A monitoring device for unmanned aerial vehicles according to claim 3, wherein: the end part of the piston rod of the telescopic cylinder (31) is provided with a connecting block (311), and the connecting block (311) is connected with the connecting plate (32) through a connecting screw.
8. A monitoring device for unmanned aerial vehicle according to claim 5, wherein: a buffer cushion (333) is arranged on one side of the cover body (33) close to the shell (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220106455.1U CN216443812U (en) | 2022-01-15 | 2022-01-15 | A monitoring device for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220106455.1U CN216443812U (en) | 2022-01-15 | 2022-01-15 | A monitoring device for unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN216443812U true CN216443812U (en) | 2022-05-06 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202220106455.1U Active CN216443812U (en) | 2022-01-15 | 2022-01-15 | A monitoring device for unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117533538A (en) * | 2024-01-09 | 2024-02-09 | 山西省地球物理化学勘查院有限公司 | Laser scanning's adjustment mechanism for unmanned aerial vehicle |
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2022
- 2022-01-15 CN CN202220106455.1U patent/CN216443812U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117533538A (en) * | 2024-01-09 | 2024-02-09 | 山西省地球物理化学勘查院有限公司 | Laser scanning's adjustment mechanism for unmanned aerial vehicle |
| CN117533538B (en) * | 2024-01-09 | 2024-04-16 | 山西省地球物理化学勘查院有限公司 | Laser scanning's adjustment mechanism for unmanned aerial vehicle |
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