CN112162241A - Avoid angle to receive new forms of energy unmanned aerial vehicle radar auxiliary device of raindrop interference - Google Patents
Avoid angle to receive new forms of energy unmanned aerial vehicle radar auxiliary device of raindrop interference Download PDFInfo
- Publication number
- CN112162241A CN112162241A CN202011024654.XA CN202011024654A CN112162241A CN 112162241 A CN112162241 A CN 112162241A CN 202011024654 A CN202011024654 A CN 202011024654A CN 112162241 A CN112162241 A CN 112162241A
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- China
- Prior art keywords
- movable
- side wall
- aerial vehicle
- unmanned aerial
- shell
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
- G01S7/027—Constructional details of housings, e.g. form, type, material or ruggedness
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
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- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
The invention relates to the technical field of unmanned aerial vehicle radar equipment, and discloses a new-energy unmanned aerial vehicle radar auxiliary device capable of avoiding the angle from being interfered by raindrops. When like magnetic poles are arranged between the bottom side of the movable column and the side wall of the movable rod, like poles repel each other, the side wall of the movable rod can repel each other with the side wall of the movable column, the side wall of the movable column penetrates through the side wall of the movable sheet, the upward parallel angle of the movable column is reduced, and then the left end of the movable column together with the rotating shaft can penetrate through the channel under the action of the repulsive force of the movable rod, so that the connected radar can be kept at a balanced position, and the influence on the use of the radar is avoided.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle radar equipment, in particular to a new-energy unmanned aerial vehicle radar auxiliary device capable of avoiding the interference of raindrops on angles.
Background
Unmanned aerial vehicle's radar can be used for surveying remote target, can be used for various environmental monitoring's such as weather forecast, resource detection work usually, and the radar homoenergetic normal work daytime night, and do not receive the blockking of fog, cloud and rain, and radar equipment can launch the electromagnetic wave signal at the course of the work, after touchhing target object, the signal that radar equipment launched can be by the bounce, and the relevant information of this target object of feedback that can be timely.
Even the influence of the weather of thunderstorm does not receive in the thunderstorm weather of radar said, but at the flight in-process, if unmanned aerial vehicle's fuselage meets strong wind, the hail, during the thunder, these external factors still can cause the influence to unmanned aerial vehicle's outside body lateral wall department, make its vibrations, lead to its side unmanned aerial vehicle's lateral wall department to appear rocking, can cause the influence for the work of the lateral wall department of radar, the work of radar receives the influence easily, the position appears the position easily or rocks to the position of target department.
Disclosure of Invention
Technical scheme (I)
In order to solve the above problems, the present invention provides the following technical solutions: the utility model provides an avoid angle to receive new forms of energy unmanned aerial vehicle radar auxiliary device of raindrop interference, the on-line screen storage device comprises a base, the top side swing joint of base has the movable shell, the top of movable shell runs through there is the shell, the inboard of shell runs through there is the movable cover, it has the movable block to run through between the lateral wall of movable cover and the inside wall of shell, the inboard of movable cover runs through there is the mainboard, be provided with the passageway in the inside wall of mainboard, the bottom side swing joint of mainboard has the pivot, the lateral wall department swing joint of pivot has the fly leaf, the lateral wall department of pivot runs through there is the connecting axle, the lateral wall department swing joint of pivot has the activity post, the lateral wall department of fly leaf runs through there is the loose axle, the bottom side department swing joint of loose axle.
Preferably, the side wall of the movable block is slidably connected between the movable cover and the side wall interlayer of the shell, and when the movable cover and the side wall of the shell are mutually extruded, the movable block can be extruded towards the bottom end.
Preferably, the side wall of the shell is provided with a hole, so that raindrops can directly pass through the hole when hitting the shell, and the knocking force of rainwater on the side wall of the shell is reduced.
Preferably, the length of the rotating shaft is greater than that of the channel, and when the rotating shaft is in a parallel state, the rotating shaft cannot pass through the channel.
Preferably, the side wall of the movable column is slidably connected to the side wall of the movable plate, and when the top side of the movable column is squeezed, the side wall of the movable column can move downwards and penetrate through the side wall of the movable plate.
Preferably, like magnetic poles are attached between the bottom side of the movable column and the top side of the movable rod, and like poles repel each other, so that the movable column is repelled by the movable rod to be upwardly offset.
Preferably, the outer side walls of the two ends of the rotating shaft are movably connected to the channel, and when one end of the rotating shaft is supported and tilted, the rotating shaft can penetrate through the side wall of the channel and extend into the channel, so that the radar can be kept parallel integrally.
(II) advantageous effects
Compared with the prior art, the invention provides a new energy unmanned aerial vehicle radar auxiliary device for avoiding the interference of raindrops on the angle, which has the following beneficial effects:
1. this avoid angle to receive new forms of energy unmanned aerial vehicle radar auxiliary device of raindrop interference, when the rainwater strikes in the top side of shell, extrude each other between the lateral wall of shell and the movable cover, extrude the movable block from the top side between the lateral wall of shell and movable cover to the bottom and be close to movable shell department, extrude the lateral wall of movable shell to base department downwards, the top side of base receives the extrusion dynamics and extrudes downwards, can reduce the power of beating of rainwater to unmanned aerial vehicle lateral wall department.
2. This avoid angle to receive new forms of energy unmanned aerial vehicle radar auxiliary device of raindrop interference, when mutual extrusion between the lateral wall of shell and the movable cover, the inside wall department of movable cover collides each other at the inside wall of mainboard, when the lateral wall of mainboard receives the collision, the movable post is pressed downwards to the bottom side of mainboard, because wind-force and rain force are to the inhomogeneous of beating of the dynamics of shell, the lateral wall of mainboard can appear crooked rocking, can follow unmanned aerial vehicle's lateral wall department with the rainwater and flow away in the same direction as the slipstream, and the dynamics that utilizes the rainwater comes to aerify to unmanned aerial vehicle's inside, but the energy saving.
3. This avoid angle to receive new forms of energy unmanned aerial vehicle radar auxiliary device of raindrop interference, be provided with like polarity magnetic pole between the bottom side of activity post and the lateral wall of movable rod, like polarity repels, the lateral wall of movable rod can with the lateral wall of activity post between the repulsion each other, the lateral wall of activity post runs through between the lateral wall of activity piece, the last parallel angle of activity post reduces, the repulsion force that receives the movable rod again, can run through the left end of activity post with the pivot together to passageway department, can guarantee that the radar that connects keeps on balanced position, avoid influencing the use of radar.
4. This avoid angle to receive new forms of energy unmanned aerial vehicle radar auxiliary device of raindrop interference, through the rainwater through following in shell and the movable cover can directly the roll-off, contained angle department between shell and the movable cover is pressed the movable block downwards, can be directly when pressing the lateral wall of movable block downwards, the in-process of activity about the movable block, can press gas to the inside wall department of movable cover, can make the lateral wall of movable cover receive gaseous extrusion and become elastic, avoid unmanned aerial vehicle's inner structure to receive the impact and be beaten and damage.
Drawings
FIG. 1 is a schematic front view of the overall external structure of the present invention;
FIG. 2 is a schematic view of the connection between the housing and the internal related structures of the present invention;
fig. 3 is a schematic view of the structural connection between the main plate and the movable post according to the present invention.
In the figure: 1. a base; 2. a movable shell; 3. a movable block; 4. a movable cover; 5. a housing; 6. a main board; 7. a channel; 8. a rotating shaft; 9. a movable plate; 10. a connecting shaft; 11. a movable rod; 12. a movable post; 13. a movable plate; 14. a movable shaft.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Please refer to fig. 1-3, a new energy unmanned aerial vehicle radar auxiliary device for avoiding angle interference by raindrops, comprising a base 1, a movable shell 2 movably connected to a top side of the base 1, a housing 5 penetrated through a top end of the movable shell 2, a movable cover 4 penetrated through an inner side of the housing 5, a movable block 3 penetrated through between an outer side wall of the movable cover 4 and an inner side wall of the housing 5, a main plate 6 penetrated through an inner side of the movable cover 4, a channel 7 arranged in the inner side wall of the main plate 6, a rotating shaft 8 movably connected to a bottom side of the main plate 6, a movable plate 9 movably connected to a side wall of the rotating shaft 8, a connecting shaft 10 penetrated through a side wall of the rotating shaft 8, a movable column 12 movably connected to a side wall of the rotating shaft 8, a movable shaft 14 penetrated through a side wall of the movable plate 9, a movable plate 13 movably connected to a bottom side wall of the movable shaft 14.
Wherein, the lateral wall sliding connection of movable block 3 is between the lateral wall intermediate layer of movable cover 4 and shell 5, when extrudeing each other between the lateral wall of movable cover 4 and shell 5, can extrude movable block 3 to the bottom.
The side wall of the shell 5 is provided with a hole, so that raindrops can directly pass through the hole when hitting the shell 5, and the knocking force of rainwater on the side wall of the shell 5 is reduced.
The length of the rotating shaft 8 is larger than that of the channel 7, and when the rotating shaft 8 is in a parallel state, the rotating shaft cannot pass through the channel 7.
Wherein, the lateral wall of the movable column 12 is slidably connected to the lateral wall of the movable plate 13, and when the top side of the movable column 12 is pressed, the lateral wall of the movable column 12 can move downwards and penetrate through the lateral wall of the movable plate 13.
Like magnetic poles are attached between the bottom side of the movable column 12 and the top side of the movable rod 11, and like poles repel each other, so that the movable column 12 is repelled by the movable rod 11 to be upwardly offset.
The outer side walls of the two ends of the rotating shaft 8 are movably connected to the channel 7, and when one end of the rotating shaft 8 is supported and tilted, the rotating shaft can penetrate through the side wall of the channel 7 and extend into the channel, so that the radar can be kept parallel integrally.
The working principle is as follows: when the unmanned aerial vehicle is used, in the running process of the unmanned aerial vehicle, when rainwater strikes the top side of the shell 5, the side wall of the shell 5 and the movable cover 4 are mutually extruded, the movable block 3 is extruded to the position, close to the movable shell 2, of the bottom end from the top side between the shell 5 and the side wall of the movable cover 4, the side wall of the movable shell 2 is downwards extruded to the position of the base 1, and the top side of the base 1 is downwards extruded by the extrusion force;
as shown in fig. 2, when the side wall of the housing 5 and the movable cover 4 are squeezed together, the inner side wall of the movable cover 4 collides with the inner side wall of the main board 6, and when the side wall of the main board 6 is collided, the bottom side of the main board 6 presses the movable column 12 downward, and because the wind force and the rain force are not uniform in striking the housing 5, the side wall of the main board 6 may skew and rock, so that the heights of the two sides of the movable column 12 pressed downward are different, when the left side of the movable column 12 is pressed downward, the side wall of the movable column 12 may cross to the side wall of the movable plate 13 (as shown in fig. 3), and at this time, the side wall of the rotating shaft 8 may be close to the left end of the side wall of the movable shaft 14;
when like magnetic poles are arranged between the bottom side of the movable column 12 and the side wall of the movable rod 11, like poles repel each other, the side wall of the movable rod 11 and the side wall of the movable column 12 repel each other, the upward parallel angle of the movable column 12 is reduced after the side wall of the movable column 12 penetrates through the side wall of the movable sheet 13, and the left end of the movable column 12 with the rotating shaft 8 can penetrate to the channel 7 together under the repulsive force of the movable rod 11, so that the connected radar can be kept at a balanced position;
rainwater passing through the shell 5 and the movable cover 4 can directly slide out, the movable block 3 is pressed downwards at an included angle between the shell 5 and the movable cover 4, when the side wall of the movable block 3 is directly pressed downwards, the movable block 3 can move up and down and can press gas to the inner side wall of the movable cover 4, the side wall of the movable cover 4 can be made to be extruded by the gas to become elastic, and the extruded top surface of the side wall can be recovered as soon as possible.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The utility model provides an avoid angle to receive new forms of energy unmanned aerial vehicle radar auxiliary device of raindrop interference, includes base (1), its characterized in that: the top side of the base (1) is movably connected with a movable shell (2), the top end of the movable shell (2) penetrates through a shell (5), the inner side of the shell (5) penetrates through a movable cover (4), a movable block (3) penetrates between the outer side wall of the movable cover (4) and the inner side wall of the shell (5), a main board (6) penetrates through the inner side of the movable cover (4), a channel (7) is arranged in the inner side wall of the main board (6), the bottom side of the main board (6) is movably connected with a rotating shaft (8), the side wall of the rotating shaft (8) is movably connected with a movable plate (9), the side wall of the rotating shaft (8) penetrates through a connecting shaft (10), and the side wall of the rotating shaft (8) is movably connected with a movable, a movable shaft (14) penetrates through the side wall of the movable plate (9), a movable sheet (13) is movably connected to the bottom side wall of the movable shaft (14), and a movable rod (11) is movably connected to the bottom side of the movable sheet (13).
2. The radar auxiliary device for the new energy unmanned aerial vehicle capable of avoiding the angle interference by raindrops as claimed in claim 1, wherein: the side wall of the movable block (3) is connected between the side wall interlayers of the movable cover (4) and the shell (5) in a sliding mode.
3. The radar auxiliary device for the new energy unmanned aerial vehicle capable of avoiding the angle interference by raindrops as claimed in claim 1, wherein: the side wall of the shell (5) is provided with a hole.
4. The radar auxiliary device for the new energy unmanned aerial vehicle capable of avoiding the angle interference by raindrops as claimed in claim 1, wherein: the length of the rotating shaft (8) is larger than that of the channel (7).
5. The radar auxiliary device for the new energy unmanned aerial vehicle capable of avoiding the angle interference by raindrops as claimed in claim 1, wherein: the side wall of the movable column (12) is connected to the side wall of the movable sheet (13) in a sliding manner.
6. The radar auxiliary device for the new energy unmanned aerial vehicle capable of avoiding the angle interference by raindrops as claimed in claim 1, wherein: like magnetic poles are attached between the bottom side of the movable column (12) and the top side of the movable rod (11).
7. The radar auxiliary device for the new energy unmanned aerial vehicle capable of avoiding the angle interference by raindrops as claimed in claim 1, wherein: the outer side walls of the two ends of the rotating shaft (8) are movably connected to the channel (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011024654.XA CN112162241A (en) | 2020-09-25 | 2020-09-25 | Avoid angle to receive new forms of energy unmanned aerial vehicle radar auxiliary device of raindrop interference |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011024654.XA CN112162241A (en) | 2020-09-25 | 2020-09-25 | Avoid angle to receive new forms of energy unmanned aerial vehicle radar auxiliary device of raindrop interference |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112162241A true CN112162241A (en) | 2021-01-01 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011024654.XA Withdrawn CN112162241A (en) | 2020-09-25 | 2020-09-25 | Avoid angle to receive new forms of energy unmanned aerial vehicle radar auxiliary device of raindrop interference |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112162241A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113844379A (en) * | 2021-12-01 | 2021-12-28 | 枣庄智博智能科技有限公司 | Get rid of barrier and improve efficient multi-angle car radar subassembly |
-
2020
- 2020-09-25 CN CN202011024654.XA patent/CN112162241A/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113844379A (en) * | 2021-12-01 | 2021-12-28 | 枣庄智博智能科技有限公司 | Get rid of barrier and improve efficient multi-angle car radar subassembly |
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| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20210101 |
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| WW01 | Invention patent application withdrawn after publication |