CN211663451U - Rotor unmanned aerial vehicle communication platform - Google Patents
Rotor unmanned aerial vehicle communication platform Download PDFInfo
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- CN211663451U CN211663451U CN202020196376.5U CN202020196376U CN211663451U CN 211663451 U CN211663451 U CN 211663451U CN 202020196376 U CN202020196376 U CN 202020196376U CN 211663451 U CN211663451 U CN 211663451U
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Abstract
The utility model discloses a rotor unmanned aerial vehicle communication platform, through the rotor rotates, drives unmanned aerial vehicle and removes, mounting platform keeps away from the moving direction based on inertia orientation and slides, mounting platform drives the slide bar is in mounting platform with part between the first chock plug is flexible, and then extrudees expanding spring, expanding spring will do all can the power and transmit first chock plug, first chock plug is in slide in the expansion cylinder to receive the reaction force that the cylinder brought, and reverse transmission arrives expanding spring makes expanding spring is right mounting platform exerts reaction force, reduces mounting platform's horizontal slip, and then reduces mounting platform receives vibrations, avoids mounting platform's internal element damages in vibrations.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle communication field especially relates to a rotor unmanned aerial vehicle communication platform.
Background
Drones are currently unmanned aircraft that are operated by radio remote control devices and self-contained program control devices or are operated autonomously, either completely or intermittently, by an on-board computer. Compared with manned driving, the unmanned aerial vehicle has a wider application range, is applied to the fields of aerial photography, plant protection, miniature self-shooting, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, electric power inspection, disaster relief, movie and television shooting, romantic manufacturing and the like at present, greatly expands the application of the unmanned aerial vehicle, and developed countries actively expand the industrial application and develop the unmanned aerial vehicle technology.
Because unmanned aerial vehicle communicates with external terminal through installing at inside communication platform, receive external terminal's control signal, can know unmanned aerial vehicle's communication platform from this is whole unmanned aerial vehicle's brain, current communication platform receives unmanned aerial vehicle huge traction force at unmanned aerial vehicle flight in-process, makes communication platform and unmanned aerial vehicle bump, influences the normal operating of communication platform internal elements, and then influences communication platform's information transfer.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a rotor unmanned aerial vehicle communication platform aims at solving current communication platform among the prior art and receives unmanned aerial vehicle huge traction force at unmanned aerial vehicle flight in-process, makes communication platform and unmanned aerial vehicle bump, influences the normal operating of communication platform inner member, and then influences communication platform's information transfer's technical problem.
In order to achieve the purpose, the utility model discloses a rotor unmanned aerial vehicle communication platform, including organism, rotor, mounting platform and damping device, the organism has a standing groove, the standing groove is located the surface of the organism, and the opening is towards the top of the organism, and stretch into the inside of the organism, the rotor rotates with the organism to be connected, and is located the organism and is close to one side of the standing groove opening, the mounting platform with the organism pass through the damping device with the mounting platform is connected, and is located the inside of the standing groove, the damping device with the organism fixed connection, and with the mounting platform butt; the damping device comprises a sliding rod and a damping component, one end of the sliding rod is fixedly connected with the mounting platform, the other end of the sliding rod is connected with the machine body through the damping component, the damping component is positioned on the periphery of the mounting platform and faces the machine body, the damping component is fixedly connected with the machine body and is connected with the sliding rod in a sliding manner, and the damping component is positioned at one end of the sliding rod, which is far away from the mounting platform; damping subassembly includes first chock plug, telescopic cylinder and expanding spring, first chock plug with slide bar fixed connection, and be located the slide bar is kept away from mounting platform's one end, telescopic cylinder with organism fixed connection, and with first chock plug sliding connection, and be located the periphery of first chock plug, expanding spring with first chock plug butt, and with the mounting platform butt, and be located the periphery of slide bar.
The damping device further comprises a buffer pad and a buffer spring, wherein the buffer pad is connected with the sliding rod in a sliding mode, is abutted against the telescopic spring and is positioned on one side, close to the mounting platform, of the telescopic spring; the buffer spring is abutted with the mounting platform, abutted with the cushion pad and positioned between the cushion pad and the mounting platform.
The unmanned rotorcraft communication platform further comprises a shock insulation pad, wherein the shock insulation pad is fixedly connected with the mounting platform and is located on one side of the body, close to the mounting platform, and far away from the opening direction of the placing groove.
The communication platform of the unmanned rotorcraft further comprises a telescopic supporting rod and a resisting component, wherein the telescopic supporting rod is fixedly connected with the mounting platform, is positioned on one side, close to the shock insulation pad, of the mounting platform and is positioned on the periphery of the shock insulation pad; the resisting component is fixedly connected with the machine body, is connected with the telescopic supporting rod in a sliding mode, and is located at one end, far away from the mounting platform, of the telescopic supporting rod.
The second plug head is fixedly connected with the telescopic supporting rod and is positioned at one end of the telescopic supporting rod, which is far away from the mounting platform; the resisting cylinder is fixedly connected with the machine body, is connected with the second plug head in a sliding mode and is located on the periphery of the second plug head.
The resisting assembly further comprises a resisting spring, the resisting spring is abutted with the second plug head, abutted with the mounting platform and located on the periphery of the telescopic supporting rod.
The unmanned rotorcraft communication platform further comprises a first ball and a second ball, wherein the first ball is fixedly connected with the telescopic cylinder, is rotatably connected with the airframe, and is positioned on one side, away from the mounting platform, of the telescopic cylinder; the second ball is fixedly connected with the resisting cylinder, is rotatably connected with the machine body and is positioned on one side, far away from the mounting platform, of the resisting cylinder.
The utility model discloses a rotor unmanned aerial vehicle communication platform, through the rotor rotates, drives unmanned aerial vehicle and removes, mounting platform keeps away from the moving direction based on inertia orientation and slides, mounting platform drives the slide bar is in mounting platform with part between the first chock plug is flexible, and then extrudees expanding spring, expanding spring will do all can the power transmission first chock plug, first chock plug is in slide in the expanding cylinder to receive the reaction force that the cylinder brought, and reverse transmission arrives expanding spring makes expanding spring is right mounting platform applys the reaction force, reduces mounting platform's horizontal slip, and then reduces mounting platform receives vibrations, avoids mounting platform's internal element damages in vibrations.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a schematic view of the connection structure of the body and the rotor of the present invention.
Fig. 2 is a schematic view of the connection structure between the mounting platform and the machine body of the present invention.
Fig. 3 is a schematic structural diagram of the damping assembly of the present invention.
Fig. 4 is a schematic view of the connection structure of the telescopic support rod and the mounting platform of the present invention.
Fig. 5 is a schematic structural view of the resisting assembly of the present invention.
In the figure: 1-body, 2-rotor, 3-mounting platform, 4-damping device, 5-vibration isolation cushion, 6-telescopic supporting rod, 7-resisting component, 8-first ball, 9-second ball, 11-placing groove, 41-sliding rod, 42-damping component, 43-buffer pad, 44-buffer spring, 71-second plug head, 72-resisting cylinder, 73-resisting spring, 100-rotor unmanned aerial vehicle communication platform, 421-first plug head, 422-telescopic cylinder and 423-telescopic spring.
Detailed Description
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary and intended to be used for explaining the present invention, and should not be construed as limiting the present invention.
In the description of the present invention, it is to be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on those shown in the drawings, and are merely for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention. In addition, in the description of the present invention, "a plurality" means two or more unless specifically limited otherwise.
In a first example of the present embodiment:
referring to fig. 1 to 3, the utility model provides a rotor unmanned aerial vehicle communication platform 100, including organism 1, rotor 2, mounting platform 3 and damping device 4, organism 1 has a standing groove 11, standing groove 11 is located the surface of organism 1, and the opening is towards the top of organism 1, and stretch into the inside of organism 1, rotor 2 rotates with organism 1 to be connected, and is located organism 1 near one side of standing groove 11 opening, mounting platform 3 with organism 1 through damping device 4 with mounting platform 3 is connected, and is located the inside of standing groove 11, damping device 4 with organism 1 fixed connection, and with mounting platform 3 butt; the damping device 4 comprises a sliding rod 41 and a damping component 42, one end of the sliding rod 41 is fixedly connected with the mounting platform 3, the other end of the sliding rod is connected with the machine body 1 through the damping component 42, the damping component 42 is positioned on the periphery of the mounting platform 3 and faces the direction of the machine body 1, the damping component 42 is fixedly connected with the machine body 1 and is connected with the sliding rod 41 in a sliding manner, and the damping component is positioned at one end of the sliding rod 41, which is far away from the mounting platform 3; damping component 42 includes first chock plug 421, telescopic cylinder 422 and expanding spring 423, first chock plug 421 with slide bar 41 fixed connection, and be located slide bar 41 is kept away from mounting platform 3's one end, telescopic cylinder 422 with organism 1 fixed connection, and with first chock plug 421 sliding connection, and be located the periphery of first chock plug 421, expanding spring 423 with first chock plug 421 butt, and with mounting platform 3 butt, and be located slide bar 41's periphery.
Further, the damping device 4 further includes a buffer pad 43 and a buffer spring 44, wherein the buffer pad 43 is slidably connected to the sliding rod 41, abuts against the extension spring 423, and is located on one side of the extension spring 423 close to the mounting platform 3; the buffer spring 44 abuts against the mounting platform 3, abuts against the buffer pad 43, and is located between the buffer pad 43 and the mounting platform 3.
In this embodiment, the machine body 1 is a rectangular body, the top of the machine body is provided with the placement groove 11 extending into the machine body 1, the placement groove 11 is a rectangular groove, the bottom of the placement groove 11 is provided with a power supply, four end portions of the machine body 1 are respectively connected with the rotor wings 2 through bracket threads, the rotor wings 2 are driven by a motor to rotate and drive the machine body 1 to move through the rotation of the four rotor wings 2, the telescopic cylinder 422 is installed on the side wall of the machine body 1 in the placement groove 11 in a threaded manner and is horizontally inverted towards the direction of the mounting platform 3, the slide rod 41 is a telescopic rod and is provided with a fixed section and a telescopic section, the telescopic rod is telescopic through the sliding of the fixed section and the telescopic section, one end of the slide rod 41 is fixed with the first plug 421 in a threaded manner, the other end of the slide rod is connected with the mounting platform 3 in a threaded manner, the slide rod 41 is slidably connected with the telescopic cylinder 422 through, and extrudes the first stopper 421 extends into the inside of the telescopic cylinder 422, the telescopic cylinder 422 receives the gas reaction force, the periphery of the slide rod 41 is sleeved with the cushion pad 43, the cushion pad 43 is in the shape of a hollow circular ring, the front side and the rear side of the cushion pad 43 are respectively abutted with the cushion spring 44 and the telescopic spring 423, the cushion spring 44 and the telescopic spring 423 are respectively sleeved on the periphery of the slide rod 41, one end of the cushion spring 44 is abutted with the mounting platform 3, the other end of the cushion spring is abutted with the cushion pad 43 and transmits the elastic force, one end of the telescopic spring 423 is abutted with the body 1, the other end of the telescopic spring is abutted with the cushion pad 43 and receives the elastic force of the cushion spring 44, the number of the damping devices 4 is four, and the damping devices are respectively mounted around the mounting platform 3, so, the rotor 2 rotates, the unmanned aerial vehicle is driven to move, the mounting platform 3 slides towards a far-away moving direction based on inertia, the mounting platform 3 drives the sliding rod 41 to partially stretch and contract between the mounting platform 3 and the first plug head 421 so as to extrude the telescopic spring 423 and the buffer spring 44, the buffer spring 44 transmits force to the buffer cushion 43 when being extruded by the mounting platform 3, the buffer cushion 43 applies pressure to the telescopic spring 423, the telescopic spring 423 transmits force to the first plug head 421, the first plug head 421 slides in the telescopic cylinder 422, receives reaction force brought by the cylinder and reversely transmits the reaction force to the buffer spring 44, so that the buffer spring 44 applies reaction force to the mounting platform 3, the horizontal sliding of the mounting platform 3 is reduced, and the vibration received by the mounting platform 3 is reduced, the interior of the mounting platform 3 is protected.
In a second example of the present embodiment:
referring to fig. 1 to 5, the utility model provides a rotor unmanned aerial vehicle communication platform 100, including organism 1, rotor 2, mounting platform 3 and damping device 4, organism 1 has a standing groove 11, standing groove 11 is located the surface of organism 1, and the opening is towards the top of organism 1, and stretch into the inside of organism 1, rotor 2 rotates with organism 1 to be connected, and is located organism 1 near one side of standing groove 11 opening, mounting platform 3 with organism 1 through damping device 4 with mounting platform 3 is connected, and is located the inside of standing groove 11, damping device 4 with organism 1 fixed connection, and with mounting platform 3 butt; the damping device 4 comprises a sliding rod 41 and a damping component 42, one end of the sliding rod 41 is fixedly connected with the mounting platform 3, the other end of the sliding rod is connected with the machine body 1 through the damping component 42, the damping component 42 is positioned on the periphery of the mounting platform 3 and faces the direction of the machine body 1, the damping component 42 is fixedly connected with the machine body 1 and is connected with the sliding rod 41 in a sliding manner, and the damping component is positioned at one end of the sliding rod 41, which is far away from the mounting platform 3; damping component 42 includes first chock plug 421, telescopic cylinder 422 and expanding spring 423, first chock plug 421 with slide bar 41 fixed connection, and be located slide bar 41 is kept away from mounting platform 3's one end, telescopic cylinder 422 with organism 1 fixed connection, and with first chock plug 421 sliding connection, and be located the periphery of first chock plug 421, expanding spring 423 with first chock plug 421 butt, and with mounting platform 3 butt, and be located slide bar 41's periphery.
Further, rotor unmanned aerial vehicle communication platform 100 still includes shock insulation pad 5, shock insulation pad 5 with mounting platform 3 fixed connection, and be located mounting platform 3 is close to one side of organism 1, and keeps away from the opening direction of standing groove 11.
Further, the unmanned rotorcraft communication platform 100 further comprises a telescopic support rod 6 and a resisting component 7, wherein the telescopic support rod 6 is fixedly connected with the mounting platform 3, is positioned on one side of the mounting platform 3 close to the vibration isolation pad 5, and is positioned on the periphery of the vibration isolation pad 5; the resisting component 7 is fixedly connected with the machine body 1, is connected with the telescopic supporting rod 6 in a sliding mode, and is located at one end, far away from the mounting platform 3, of the telescopic supporting rod 6.
Further, the resisting assembly 7 comprises a second plug head 71 and a resisting cylinder 72, wherein the second plug head 71 is fixedly connected with the telescopic support rod 6 and is located at one end of the telescopic support rod 6 far away from the mounting platform 3; the resisting cylinder 72 is fixedly connected with the machine body 1, is connected with the second plug head 71 in a sliding manner, and is positioned on the periphery of the second plug head 71.
Further, the resisting assembly 7 further comprises a resisting spring 73, and the resisting spring 73 is abutted with the second plug head 71 and the mounting platform 3 and is located on the periphery of the telescopic support rod 6.
Further, the unmanned rotorcraft communication platform 100 further comprises a first ball 8 and a second ball 9, wherein the first ball 8 is fixedly connected with the telescopic cylinder 422, is rotatably connected with the airframe 1, and is located on one side of the telescopic cylinder 422, which is far away from the installation platform 3; the second ball 9 is fixedly connected with the resisting cylinder 72, is rotatably connected with the machine body 1, and is located on one side of the resisting cylinder 72 away from the mounting platform 3.
In this embodiment, the cushion pad 43 is bonded to the bottom of the mounting platform 3, the cushion pad 43 is located between the mounting platform 3 and the machine body 1 and respectively abuts against the mounting platform 3 and the machine body 1, and the cushion pad 43 is made of a high-resilience material and has a plurality of through holes inside, so that the cushion pad 43 has good resilience; the side of the mounting platform 3 close to the cushion pad 43, the periphery of the mounting platform 3 is respectively fixed with the telescopic support rods 6 by screw threads, the number of the telescopic support rods 6 is four, and the telescopic support rods 6 are respectively towards the machine body 1 and at the bottom of the placing groove 11, the telescopic support rods 6 are sliding telescopic rods and are connected with the machine body 1 and the mounting platform 3, the side of the telescopic support rods 6 far away from the mounting platform 3 is fixed with the second plug head 71 by screw threads, the second plug head 71 extends into the resisting cylinder 72, the resisting cylinder 72 is installed at the bottom of the placing groove 11 by screw threads, the telescopic support rods 6 and the second plug head 71 extend into the resisting cylinder 72, the resisting spring 73 is arranged between the second plug head 71 and the mounting platform 3, and the resisting spring 73 is arranged around the periphery of the telescopic support rods 6, the second plug 71 is pressed by the mounting platform 3 and is transmitted to the second plug 71, the second plug 71 is subjected to the reaction force of the resisting cylinder 72, so that the second plug 71 reacts against the resisting spring 73, and the resisting spring 73 exerts the reaction force on the mounting platform 3 to slow down the movement of the mounting platform 3; the first ball 8 is integrally fixed on one side of the telescopic cylinder 422 close to the machine body 1, a part of the first ball 8 horizontally extends into the machine body 1 and rotates with the machine body 1 around the center of the first ball 8, the second ball 9 is integrally fixed on one side of the resisting cylinder 72 close to the machine body 1, and a part of the second ball 9 extends into the bottom of the vertical machine body 1 and rotates with the machine body 1, so that the horizontal sliding of the mounting platform 3 drives the telescopic support rod 6 to horizontally slide and simultaneously receives the pulling force of the telescopic support and drives the resisting cylinder 72 to rotate on the second ball 9, and the stress direction is always on the central axis of the telescopic support rod 6; when 3 vertical sliding of mounting platform, drive slide bar 41 vertical sliding, and drive first ball 8 rotates, makes slide bar 41 is flexible to the atress direction is in on 41's the center axis of slide bar, so when unmanned aerial vehicle rises and descends, reduce the vibration that mounting platform 3 received avoids communication platform to remove the in-process at unmanned aerial vehicle and damages.
While the invention has been described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the spirit and scope of the invention.
Claims (7)
1. A rotor unmanned aerial vehicle communication platform is characterized by comprising a machine body, a rotor, a mounting platform and a damping device,
the body is provided with a placing groove, the placing groove is positioned on the surface of the body, the opening of the placing groove faces the upper side of the body and extends into the body, the rotor wing is rotatably connected with the body and positioned on one side of the body close to the opening of the placing groove, the mounting platform and the body are connected with the mounting platform through the damping device and positioned in the placing groove, and the damping device is fixedly connected with the body and abutted against the mounting platform;
the damping device comprises a sliding rod and a damping component, one end of the sliding rod is fixedly connected with the mounting platform, the other end of the sliding rod is connected with the machine body through the damping component, the damping component is positioned on the periphery of the mounting platform and faces the machine body, the damping component is fixedly connected with the machine body and is connected with the sliding rod in a sliding manner, and the damping component is positioned at one end of the sliding rod, which is far away from the mounting platform;
damping subassembly includes first chock plug, telescopic cylinder and expanding spring, first chock plug with slide bar fixed connection, and be located the slide bar is kept away from mounting platform's one end, telescopic cylinder with organism fixed connection, and with first chock plug sliding connection, and be located the periphery of first chock plug, expanding spring with first chock plug butt, and with the mounting platform butt, and be located the periphery of slide bar.
2. The rotary-wing drone communication platform of claim 1,
the damping device further comprises a buffer pad and a buffer spring, the buffer pad is connected with the sliding rod in a sliding mode, is abutted against the telescopic spring and is positioned on one side, close to the mounting platform, of the telescopic spring; the buffer spring is abutted with the mounting platform, abutted with the cushion pad and positioned between the cushion pad and the mounting platform.
3. The rotary-wing drone communication platform of claim 1,
rotor unmanned aerial vehicle communication platform still includes the shock insulation pad, the shock insulation pad with mounting platform fixed connection to be located mounting platform is close to one side of organism, and keeps away from the opening direction of standing groove.
4. The rotary-wing drone communication platform of claim 3,
the communication platform of the unmanned rotorcraft further comprises a telescopic supporting rod and a resisting component, wherein the telescopic supporting rod is fixedly connected with the mounting platform, is positioned on one side of the mounting platform, which is close to the shock insulation pad, and is positioned on the periphery of the shock insulation pad; the resisting component is fixedly connected with the machine body, is connected with the telescopic supporting rod in a sliding mode, and is located at one end, far away from the mounting platform, of the telescopic supporting rod.
5. The rotary-wing drone communication platform of claim 4,
the second plug head is fixedly connected with the telescopic supporting rod and is positioned at one end of the telescopic supporting rod, which is far away from the mounting platform; the resisting cylinder is fixedly connected with the machine body, is connected with the second plug head in a sliding mode and is located on the periphery of the second plug head.
6. The rotary-wing drone communication platform of claim 5,
the resisting assembly further comprises a resisting spring, the resisting spring is abutted with the second plug head, abutted with the mounting platform and located on the periphery of the telescopic supporting rod.
7. The rotary-wing drone communication platform of claim 6,
the rotor unmanned aerial vehicle communication platform further comprises a first ball and a second ball, wherein the first ball is fixedly connected with the telescopic cylinder, is rotatably connected with the machine body and is positioned on one side, away from the mounting platform, of the telescopic cylinder; the second ball is fixedly connected with the resisting cylinder, is rotatably connected with the machine body and is positioned on one side, far away from the mounting platform, of the resisting cylinder.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020196376.5U CN211663451U (en) | 2020-02-21 | 2020-02-21 | Rotor unmanned aerial vehicle communication platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020196376.5U CN211663451U (en) | 2020-02-21 | 2020-02-21 | Rotor unmanned aerial vehicle communication platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211663451U true CN211663451U (en) | 2020-10-13 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020196376.5U Expired - Fee Related CN211663451U (en) | 2020-02-21 | 2020-02-21 | Rotor unmanned aerial vehicle communication platform |
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| Country | Link |
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| CN (1) | CN211663451U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112696601A (en) * | 2020-12-23 | 2021-04-23 | 国家电网有限公司 | Terminal processing device for wireless communication |
| CN112829927A (en) * | 2020-12-30 | 2021-05-25 | 江苏斯匹德精密机械科技有限公司 | Control method and device for oil-driven unmanned aerial vehicle |
-
2020
- 2020-02-21 CN CN202020196376.5U patent/CN211663451U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112696601A (en) * | 2020-12-23 | 2021-04-23 | 国家电网有限公司 | Terminal processing device for wireless communication |
| CN112696601B (en) * | 2020-12-23 | 2022-09-09 | 国家电网有限公司 | Terminal processing device for wireless communication |
| CN112829927A (en) * | 2020-12-30 | 2021-05-25 | 江苏斯匹德精密机械科技有限公司 | Control method and device for oil-driven unmanned aerial vehicle |
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Granted publication date: 20201013 Termination date: 20210221 |