CN213109787U - Unmanned aerial vehicle plotter balancing unit - Google Patents
Unmanned aerial vehicle plotter balancing unit Download PDFInfo
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- CN213109787U CN213109787U CN202021625001.2U CN202021625001U CN213109787U CN 213109787 U CN213109787 U CN 213109787U CN 202021625001 U CN202021625001 U CN 202021625001U CN 213109787 U CN213109787 U CN 213109787U
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- plotter
- unmanned aerial
- aerial vehicle
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- fixed plate
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Abstract
The utility model discloses an unmanned aerial vehicle plotter balancing unit belongs to unmanned air vehicle technical field, which comprises a fixing plate and i, the top of fixed plate is provided with installation mechanism, the rectangular channel has been seted up in the outside of fixed plate bottom, and the inside of rectangular channel is inserted and is equipped with the glass cover, fixing bolt is installed in the outside of fixed plate, and fixing bolt extends to the inside of rectangular channel, the intermediate position department of fixed plate bottom has seted up spherical groove, and the inside in spherical groove is provided with the ball, the bottom of ball is fixed with branch. The utility model discloses fixed plate top mounting mechanism's setting can be fixed the device on unmanned aerial vehicle to through the setting of glass cover, can prevent to remove the influence that in-process wind-force produced the plotter body, utilize the cooperation of plotter body top ball type groove and ball to use, make the device can take place the gravity that the in-process utilized the plotter body of slope at unmanned aerial vehicle and carry out automatic balance, ensured the effect of shooting.
Description
Technical Field
The utility model relates to a balancing unit especially relates to an unmanned aerial vehicle plotter balancing unit, belongs to unmanned air vehicle technical field.
Background
An unmanned plane is an unmanned plane which is operated by a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, and is classified into military use and civil use according to application fields. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + industry application is really just needed by the unmanned aerial vehicle, and when drawing is carried out on some areas with severe cities, the unmanned aerial vehicle is needed to be used for aerial photography for drawing convenience;
but the in-process of current unmanned aerial vehicle mapping of taking photo by plane receives external environment's influence situation that shake or slope can appear, influences the precision and the effect of mapping, consequently, the utility model provides an unmanned aerial vehicle plotter balancing unit is in order to solve the problem that exists among the prior art.
SUMMERY OF THE UTILITY MODEL
The utility model mainly aims at providing an unmanned aerial vehicle plotter balancing unit to solve the problem of the easy shake of survey and drawing process among the prior art.
The purpose of the utility model can be achieved by adopting the following technical scheme:
the utility model provides an unmanned aerial vehicle plotter balancing unit, includes the fixed plate, the top of fixed plate is provided with installation mechanism, the rectangular channel has been seted up in the outside of fixed plate bottom, and the inside of rectangular channel is inserted and is equipped with the glass cover, fixing bolt is installed in the outside of fixed plate, and fixing bolt extends to the inside of rectangular channel, the intermediate position department of fixed plate bottom has seted up spherical groove, and the inside in spherical groove is provided with the ball, the bottom of ball is fixed with branch, and the bottom of branch is fixed with the backup pad, the bottom of backup pad is provided with the support plate, and the four corners department at support plate top all is fixed with the screw rod, the screw rod all extends to the top of backup pad, the top of screw rod is provided with fixation nut, be provided with the plo.
Preferably: the installation mechanism comprises an air cavity, an installation frame and a piston, the bottom of the air cavity is fixedly connected with the fixing plate, the installation frame is fixed at the top of the air cavity, a sucker is installed at the top of the installation frame, the piston is slidably installed in the air cavity, a connecting rod is fixedly installed on the piston and extends to the outside of the air cavity, a buckling block is hinged to the connecting rod, and an air pipe is arranged between the sucker and the inside of the air cavity.
Preferably: the lateral wall of glass cover all is the plane, and the bottom of glass cover is provided with the shock pad.
Preferably: the bottom of backup pad and the top of support plate all are provided with the rubber pad, and all are provided with anti-skidding line on the rubber pad.
Preferably: the fixing bolts are provided with four groups, and the distances between the adjacent fixing bolts are the same.
Preferably: smooth coatings are arranged inside the spherical groove and outside the ball.
The utility model has the advantages that:
the utility model provides a pair of unmanned aerial vehicle plotter balancing unit, fixed plate top installation mechanism's setting, can fix the device on unmanned aerial vehicle, and through the setting of glass cover, can prevent to remove the influence that in-process wind-force produced the plotter body, utilize the cooperation of plotter body top ball type groove and ball to use, make the device can carry out automatic balance at the gravity that unmanned aerial vehicle took place to utilize the plotter body at the in-process that the slope, the effect of shooting has been ensured, through the air cavity, a mounting bracket, a piston, the connecting rod, the knot piece, the sucking disc, the setting of the installation mechanism that the trachea is constituteed, make the installation and the dismantlement of device more convenient, the practicality is higher, screw rod and fixation nut's setting between backup pad and the support plate, can conveniently install fixedly to the plotter body.
Drawings
Fig. 1 is a front sectional view of the present invention;
fig. 2 is a mounting mechanism diagram of the present invention;
fig. 3 is a view of the glass cover of the present invention.
In the figure: 1. a fixing plate; 2. an installation mechanism; 3. a rectangular groove; 4. a glass cover; 5. fixing the bolt; 6. a spherical groove; 7. a ball bearing; 8. a strut; 9. a support plate; 10. a carrier plate; 11. a screw; 12. fixing a nut; 13. a plotter body; 14. an air cavity; 15. a mounting frame; 16. a piston; 17. a connecting rod; 18. buckling blocks; 19. a suction cup; 20. the trachea.
Detailed Description
In order to make the technical solutions of the present invention clearer and clearer for those skilled in the art, the present invention will be described in further detail with reference to the following embodiments and drawings, but the embodiments of the present invention are not limited thereto.
As shown in fig. 1-3, the present embodiment provides a balancing device for an unmanned plane plotter, which comprises a fixing plate 1, a mounting mechanism 2 disposed on the top of the fixing plate 1, a rectangular groove 3 disposed on the outer side of the bottom of the fixing plate 1, a glass cover 4 is inserted in the rectangular groove 3, a fixing bolt 5 is arranged on the outer side of the fixing plate 1, the fixing bolt 5 extends into the rectangular groove 3, a spherical groove 6 is arranged in the middle of the bottom of the fixing plate 1, and the ball 7 is arranged in the ball groove 6, the bottom of the ball 7 is fixed with a support rod 8, the bottom of the support rod 8 is fixed with a support plate 9, the bottom of the support plate 9 is provided with a support plate 10, and the four corners of the top of the carrier plate 10 are all fixed with screws 11, the screws 11 all extend to the top of the support plate 9, the top of the screws 11 is provided with fixing nuts 12, and a plotter body 13 is arranged between the support plate 9 and the carrier plate 10.
In this embodiment, as shown in fig. 2, the installation mechanism 2 includes an air cavity 14, an installation frame 15 and a piston 16, the bottom of the air cavity 14 is fixedly connected with the fixing plate 1, the installation frame 15 is fixed at the top of the air cavity 14, a suction cup 19 is installed at the top of the installation frame 15, the piston 16 is slidably installed inside the air cavity 14, a connecting rod 17 is fixedly installed on the piston 16, the connecting rod 17 extends to the outside of the air cavity 14, a buckle block 18 is hinged to the connecting rod 17, an air pipe 20 is arranged between the suction cup 19 and the inside of the air cavity 14, in the fixing process, the suction cup 19 is sucked at the bottom of the unmanned aerial vehicle, then the buckle block 18 is rotated, the piston 16 is stretched through the connecting rod 17 in the overturning process of the buckle block 18, it.
In this embodiment, as shown in fig. 3, the lateral wall of glass cover 4 is the plane all, and the bottom of glass cover 4 is provided with the shock pad, avoids the harm that unmanned aerial vehicle caused glass cover 4 when the accident appears.
In the embodiment, as shown in fig. 1, the bottom of the supporting plate 9 and the top of the carrier 10 are both provided with rubber pads, and the rubber pads are both provided with anti-slip patterns, so as to improve the fixing effect on the plotter body 13 and prevent the plotter body 13 from being damaged due to the extrusion of the supporting plate 9 and the carrier 10.
In the present embodiment, as shown in fig. 1, four sets of fixing bolts 5 are provided, and the distances between adjacent fixing bolts 5 are the same, which improves the stability of fixing the glass cover 4.
In the present embodiment, as shown in fig. 1, the ball grooves 6 and the balls 7 are both provided with a smooth coating on the inside thereof, so as to reduce the friction force applied to the balls 7 during rotation, thereby ensuring the leveling of the plotter body 13.
As shown in fig. 1 to fig. 3, the present embodiment provides an operation process of the balancing device for the plotter of the unmanned aerial vehicle as follows:
step 1: before use, the suction cup 19 is sucked at the bottom of the unmanned aerial vehicle, then the buckling block 18 is rotated, the piston 16 is stretched through the connecting rod 17 in the overturning process of the buckling block 18, the interior of the suction cup 19 is ensured to be in a negative pressure state, and the device is fixed;
step 2: then, placing the plotter body 13 between the support plate 9 and the support plate 10, screwing the fixing nut 12 to fix the plotter body 13, and then inserting the top of the glass cover 4 into the rectangular groove 3 to protect the plotter body 13;
and step 3: in the use, utilize glass cover 4 to block the windage, under the condition of unmanned aerial vehicle ware slope, receive the influence of plotter body 13 gravity, ball 7 takes place relative rotation in the inside of ball-type groove 6, ensures the steady of plotter body 13.
The above description is only a further embodiment of the present invention, but the scope of protection of the present invention is not limited thereto, and any person skilled in the art can replace or change the technical solution and the concept of the present invention within the scope of the present invention.
Claims (6)
1. The utility model provides an unmanned aerial vehicle plotter balancing unit which characterized in that: comprises a fixed plate (1), wherein an installation mechanism (2) is arranged at the top of the fixed plate (1), a rectangular groove (3) is arranged at the outer side of the bottom of the fixed plate (1), a glass cover (4) is inserted in the rectangular groove (3), a fixing bolt (5) is installed at the outer side of the fixed plate (1), the fixing bolt (5) extends into the rectangular groove (3), a spherical groove (6) is arranged at the middle position of the bottom of the fixed plate (1), a ball (7) is arranged in the spherical groove (6), a support rod (8) is fixed at the bottom of the ball (7), a support plate (9) is fixed at the bottom of the support rod (8), a support plate (10) is arranged at the bottom of the support plate (9), screw rods (11) are fixed at four corners of the top of the support plate (10), and the screw rods (11) all extend to the top of the support plate (9), the top of the screw rod (11) is provided with a fixing nut (12), and a plotter body (13) is arranged between the support plate (9) and the support plate (10).
2. The unmanned aerial vehicle plotter balancing device of claim 1, characterized in that: installation mechanism (2) include air cavity (14), mounting bracket (15) and piston (16), the bottom and fixed plate (1) fixed connection of air cavity (14), the top of air cavity (14) is fixed with mounting bracket (15), and sucking disc (19) are installed at the top of mounting bracket (15), the inside slidable mounting of air cavity (14) has piston (16), and fixed mounting has connecting rod (17) on piston (16), connecting rod (17) extend to the outside of air cavity (14), articulated on connecting rod (17) have detain piece (18), be provided with trachea (20) between sucking disc (19) and air cavity (14) inside.
3. The unmanned aerial vehicle plotter balancing device of claim 1, characterized in that: the side wall of the glass cover (4) is a plane, and a shock pad is arranged at the bottom of the glass cover (4).
4. The unmanned aerial vehicle plotter balancing device of claim 1, characterized in that: the bottom of the supporting plate (9) and the top of the carrier plate (10) are both provided with rubber pads, and the rubber pads are both provided with anti-skid lines.
5. The unmanned aerial vehicle plotter balancing device of claim 1, characterized in that: the four groups of fixing bolts (5) are arranged, and the distances between the adjacent fixing bolts (5) are the same.
6. The unmanned aerial vehicle plotter balancing device of claim 1, characterized in that: smooth coatings are arranged inside the spherical groove (6) and outside the ball (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021625001.2U CN213109787U (en) | 2020-08-07 | 2020-08-07 | Unmanned aerial vehicle plotter balancing unit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021625001.2U CN213109787U (en) | 2020-08-07 | 2020-08-07 | Unmanned aerial vehicle plotter balancing unit |
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| Publication Number | Publication Date |
|---|---|
| CN213109787U true CN213109787U (en) | 2021-05-04 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202021625001.2U Active CN213109787U (en) | 2020-08-07 | 2020-08-07 | Unmanned aerial vehicle plotter balancing unit |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113932138A (en) * | 2021-11-11 | 2022-01-14 | 贵州水利水电职业技术学院 | Unmanned aerial vehicle measures drawing device |
-
2020
- 2020-08-07 CN CN202021625001.2U patent/CN213109787U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113932138A (en) * | 2021-11-11 | 2022-01-14 | 贵州水利水电职业技术学院 | Unmanned aerial vehicle measures drawing device |
| CN113932138B (en) * | 2021-11-11 | 2023-02-21 | 贵州水利水电职业技术学院 | Unmanned aerial vehicle measures drawing device |
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