CN211618107U - Unmanned aerial vehicle's electromagnetic protection structure - Google Patents
Unmanned aerial vehicle's electromagnetic protection structure Download PDFInfo
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- CN211618107U CN211618107U CN202020154062.9U CN202020154062U CN211618107U CN 211618107 U CN211618107 U CN 211618107U CN 202020154062 U CN202020154062 U CN 202020154062U CN 211618107 U CN211618107 U CN 211618107U
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- aerial vehicle
- unmanned aerial
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- cavity
- board
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Abstract
The utility model relates to an unmanned air vehicle technique field just discloses an unmanned aerial vehicle's electromagnetism protective structure, including casing, wing, supporting leg and the control mainboard of setting inside the casing, the fixed board that places that is equipped with in left side of the bottom inner wall of casing and being located the control mainboard, the upper surface of placing the board is equipped with the protection casing, the left side wall of protection casing passes through the hinge and articulates the setting with the left side wall of placing the board, a plurality of evenly distributed's card wire casing has all been seted up to both sides around the protection casing, the fixed cardboard that is equipped with of right side wall of protection casing, the inside of placing the board just is located the right side and has seted up the cavity, the inside of cavity is equipped with the chucking mechanism that is used. The utility model discloses the effectual electromagnetic field interference that reduces the electric energy transmission line and produce has ensured mooring unmanned aerial vehicle's security, and the staff of also being convenient for simultaneously overhauls mooring unmanned aerial vehicle.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle's electromagnetic protection structure.
Background
Mooring unmanned aerial vehicle has had extensive application in a plurality of fields, and mooring unmanned aerial vehicle need connect unmanned aerial vehicle in real time through transmission cable in order to supply power for unmanned aerial vehicle at the during operation to drive unmanned aerial vehicle and realize various operations aloft.
However, the principle of electromagnetism shows that, as the voltage is greatly increased, a strong electromagnetic field is generated in the process of electric energy transmission, the electromagnetic wave in the electromagnetic field can greatly influence the unmanned aerial vehicle flying in the sky to receive the flight control signal sent by the ground workstation, so that the unmanned aerial vehicle is insensitive to control and cannot complete the predetermined task, certain potential safety hazard can be generated in the safety performance, and the working efficiency of mooring the unmanned aerial vehicle is influenced.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving among the prior art mooring unmanned aerial vehicle can produce very strong electromagnetic field at power transmission's in-process, causes mooring unmanned aerial vehicle's the insensitive problem of control, and the unmanned aerial vehicle's that proposes electromagnetic protection structure.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides an unmanned aerial vehicle's electromagnetic protection structure, includes casing, wing, supporting leg and sets up at the inside control mainboard of casing, the fixed board of placing that is equipped with in left side that the bottom inner wall of casing just is located the control mainboard, the upper surface of placing the board is equipped with the protection casing, the left side wall of protection casing passes through the hinge and articulates the setting with the left side wall of placing the board, a plurality of evenly distributed's card wire casing has all been seted up to both sides around the protection casing, the fixed cardboard that is equipped with of right side wall of protection casing, the inside of placing the board just is located the right side and has seted up the cavity, the inside of cavity is equipped with the chucking mechanism.
Preferably, chucking mechanism includes square slide bar, slider, spring, connecting rod and fixture block, square slide bar transversely is located the inside of cavity and both ends respectively with the left and right sides fixed connection of cavity, the slider is located the inside of cavity and the pole wall sliding connection of lateral wall through square slide hole and square slide bar, the spring activity cup joints on the pole wall of square slide bar and is located the right side of slider, the left end of spring and the right side wall fixed connection of slider, the right-hand member of spring and the right side wall fixed connection of cavity, the bar hole has been seted up at the top of cavity, the vertical inside and the lower extreme that are located the bar hole of connecting rod and the upside fixed connection of slider, the upper end left side and the fixture block fixed connection of connecting rod, the fixture block sets up with the cardboard joint.
Preferably, the fixture block is a wedge-shaped block, and one side of the inclined plane is arranged upwards.
Preferably, a plurality of clamping pads are fixedly arranged in the clamping groove.
Preferably, finger grooves are formed in the tops of the front side and the rear side of the protective cover.
Preferably, the left side and the right side of the placing plate are both fixedly provided with mounting seats, and the mounting seats are both provided with mounting bolts.
Preferably, the placing plate and the protective cover are both made of aluminum alloy materials.
Compared with the prior art, the utility model provides an unmanned aerial vehicle's electromagnetic protection structure possesses following beneficial effect:
1. this unmanned aerial vehicle's electromagnetic protection structure through setting up at inside board and the protection casing of placing of casing, can keep apart the inside electric energy transmission line of casing to the electromagnetic field interference that can effectual reduction electric energy transmission line produced has improved mooring unmanned aerial vehicle's security, also can get up the orderly range of electric energy transmission line simultaneously, and easily staff overhauls.
2. This unmanned aerial vehicle's electromagnetic protection structure, through setting up cardboard, square slide bar, slider, spring, connecting rod and the fixture block placing between board and the protection casing, the staff of being convenient for processes the protection casing and opens and close.
The part that does not relate to in the device all is the same with prior art or can adopt prior art to realize, the utility model discloses the effectual electromagnetic field interference that reduces the electric energy transmission line and produce has ensured mooring unmanned aerial vehicle's security, and the staff of also being convenient for simultaneously overhauls mooring unmanned aerial vehicle.
Drawings
Fig. 1 is a schematic structural view of an electromagnetic protection structure of an unmanned aerial vehicle according to the present invention;
FIG. 2 is a schematic view of the internal structure of the housing of FIG. 1;
FIG. 3 is an enlarged view of a portion A of FIG. 2;
FIG. 4 is an enlarged view of the junction of portion B of FIG. 3;
fig. 5 is a schematic structural view of the shield of fig. 3.
In the figure: the device comprises a shell 1, wings 2, supporting legs 3, a control main board 4, a placing board 5, a protective cover 6, a wire clamping groove 7, a clamping pad 8, a clamping board 9, a square sliding rod 10, a sliding block 11, a spring 12, a connecting rod 13, a clamping block 14, a finger groove 15 and a mounting seat 16.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only 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 therefore, should not be construed as limiting the present invention.
Referring to fig. 1-5, an unmanned aerial vehicle's electromagnetic protection structure, which comprises a housing 1, wing 2, supporting leg 3 and the control mainboard 4 of setting in casing 1 inside, casing 1's bottom inner wall just is located the fixed board 5 that places that is equipped with in left side of control mainboard 4, the upper surface of placing board 5 is equipped with protection casing 6, the left side wall of protection casing 6 passes through the hinge and articulates the setting with the left side wall of placing board 5, a plurality of evenly distributed's card wire casing 7 has all been seted up to both sides around protection casing 6, put into the inside at protection casing 6 with power transmission line and make card wire casing 7 compress tightly power transmission line, the electromagnetic field interference that effectual reduction power transmission line produced, the fixed cardboard 9 that is equipped with of right side wall of protection casing 6, place the inside of board 5 and be located the right side and seted up the cavity, the inside of cavity.
The clamping mechanism comprises a square sliding rod 10, a sliding block 11, a spring 12, a connecting rod 13 and a clamping block 14, the square sliding rod 10 is transversely positioned in the cavity, two ends of the square sliding rod 10 are respectively and fixedly connected with the left side and the right side of the cavity, the sliding block 11 is positioned in the cavity, the side wall of the sliding block 11 is in sliding connection with the rod wall of the square sliding rod 10 through a square sliding hole, the spring 12 is movably sleeved on the rod wall of the square sliding rod 10 and positioned on the right side of the sliding block 11, the left end of the spring 12 is fixedly connected with the right side wall of the sliding block 11, the right end of the spring 12 is fixedly connected with the right side wall of the cavity, a strip-shaped hole is formed in the top of the cavity, the connecting rod 13 is vertically positioned in the strip-shaped hole, the lower end of the connecting rod 13 is fixedly connected with the upper side of the sliding block 11, the clamping block 14, so that the clamping block 14 is separated from the clamping plate 9, and the protective cover 6 can be opened in a hinge mode.
The clamping block 14 is a wedge-shaped block, and one side of the inclined plane faces upwards to be provided with an electric energy transmission line which is compressed and fixed on the surface of the placing plate 5.
The inside of a plurality of card wire casing 7 all is fixed and is equipped with chucking pad 8.
The left side and the right side of the placing plate 5 are both fixedly provided with mounting seats 16, mounting bolts are arranged on the mounting seats 16, and the placing plate 5 can be mounted inside the shell 1.
The placing plate 5 and the protective cover 6 are both made of aluminum alloy materials, and interference of an electromagnetic field can be effectively reduced.
In the utility model, when in use, the worker pushes the fixture block 14 by hand to make the connecting rod 13 drive the slider 11 to slide on the rod wall of the square sliding rod 10 and extrude the spring 12, so that the fixture block 14 is separated from the clamping plate 9, thereby the protective cover 6 can be opened in a hinge manner, then the power transmission line is placed in the protective cover 6 and the clamping groove 7 is tightly pressed on the power transmission line, finally the protective cover 6 is closed, the clamping plate 9 can extrude the fixture block 14 to move in the closing process, when the fixture block 14 crosses the clamping plate 9, the spring 12 which is extruded at the moment applies external force to the slider 11 and moves leftwards, thereby the fixture block 14 can clamp the clamping plate 9, further the protective cover 6 can fix the surface of the placing plate 5 and cover the power transmission line, the electromagnetic field interference generated by the power transmission line is effectively reduced, and the safety of the mooring unmanned aerial vehicle is improved, meanwhile, the electric energy transmission lines can be orderly arranged, so that the electric energy transmission line is easy to overhaul.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (7)
1. The utility model provides an unmanned aerial vehicle's electromagnetic protection structure, includes casing (1), wing (2), supporting leg (3) and sets up at inside control mainboard (4) of casing (1), its characterized in that, the fixed board (5) of placing that is equipped with in left side of the bottom inner wall of casing (1) and is located control mainboard (4), the upper surface of placing board (5) is equipped with protection casing (6), the left side wall of protection casing (6) is through the hinge with place the articulated setting of the left side wall of board (5), a plurality of evenly distributed's card wire casing (7) have all been seted up to both sides around protection casing (6), the fixed cardboard (9) that is equipped with of right side wall of protection casing (6), the inside of placing board (5) just is located the right side and has seted up the cavity, the inside of cavity is equipped with the chucking mechanism that is used for cardboard (9) joint.
2. The electromagnetic protection structure of the unmanned aerial vehicle as claimed in claim 1, wherein the clamping mechanism comprises a square slide bar (10), a slide block (11), a spring (12), a connecting rod (13) and a clamping block (14), the square slide bar (10) is transversely positioned in the cavity, two ends of the square slide bar are respectively fixedly connected with the left side and the right side of the cavity, the slide block (11) is positioned in the cavity, the side wall of the slide block is slidably connected with the rod wall of the square slide bar (10) through a square slide hole, the spring (12) is movably sleeved on the rod wall of the square slide bar (10) and positioned on the right side of the slide block (11), the left end of the spring (12) is fixedly connected with the right side wall of the slide block (11), the right end of the spring (12) is fixedly connected with the right side wall of the cavity, a strip-shaped hole is formed in the top of the cavity, the connecting rod (13) is vertically positioned in the strip-shaped hole, and, the upper end left side and fixture block (14) fixed connection of connecting rod (13), fixture block (14) and cardboard (9) joint set up.
3. The electromagnetic protection structure of the unmanned aerial vehicle of claim 2, characterized in that the fixture block (14) is a wedge-shaped block, and one side of the inclined plane is arranged upward.
4. The electromagnetic protection structure of the unmanned aerial vehicle of claim 1, characterized in that a plurality of chucking cushions (8) are fixed in the chucking grooves (7).
5. The electromagnetic protection structure of the unmanned aerial vehicle of claim 1, characterized in that finger grooves (15) are formed in the top of the front side and the back side of the protection cover (6).
6. The electromagnetic protection structure of the unmanned aerial vehicle of claim 1, wherein the left and right sides of the placing plate (5) are both fixedly provided with mounting seats (16), and the mounting seats (16) are both provided with mounting bolts.
7. The electromagnetic protection structure of unmanned aerial vehicle of claim 1, characterized in that, place board (5) and protection casing (6) and all adopt aluminum alloy material to make.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020154062.9U CN211618107U (en) | 2020-02-06 | 2020-02-06 | Unmanned aerial vehicle's electromagnetic protection structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020154062.9U CN211618107U (en) | 2020-02-06 | 2020-02-06 | Unmanned aerial vehicle's electromagnetic protection structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211618107U true CN211618107U (en) | 2020-10-02 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020154062.9U Expired - Fee Related CN211618107U (en) | 2020-02-06 | 2020-02-06 | Unmanned aerial vehicle's electromagnetic protection structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211618107U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112550743A (en) * | 2020-12-17 | 2021-03-26 | 桂林航天工业学院 | Unmanned aerial vehicle target detection device |
-
2020
- 2020-02-06 CN CN202020154062.9U patent/CN211618107U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112550743A (en) * | 2020-12-17 | 2021-03-26 | 桂林航天工业学院 | Unmanned aerial vehicle target detection device |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20201002 Termination date: 20220206 |