CN215554086U - Be applied to unmanned aerial vehicle's novel butterfly structure device of stopping - Google Patents
Be applied to unmanned aerial vehicle's novel butterfly structure device of stopping Download PDFInfo
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- CN215554086U CN215554086U CN202122102520.1U CN202122102520U CN215554086U CN 215554086 U CN215554086 U CN 215554086U CN 202122102520 U CN202122102520 U CN 202122102520U CN 215554086 U CN215554086 U CN 215554086U
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- butterfly
- unmanned aerial
- aerial vehicle
- plate body
- butterfly brake
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, and particularly discloses a novel butterfly brake structure device applied to an unmanned aerial vehicle, which comprises an unmanned aerial vehicle body, wherein two sides of the unmanned aerial vehicle body are respectively provided with a gliding side plate, the surface of the gliding side plate is provided with a mounting groove, a butterfly brake mounting sleeve is arranged in the mounting groove, and a butterfly brake plate body is arranged in an inner cavity of the butterfly brake mounting sleeve; this design can effectually make this design possess simple structure, convenient to use and clear characteristics of arrangement, when using, can move the screw rod through twisting to quick the butterfly is stopped the installation cover and is taken out the butterfly and is stopped the plate body, and then quick realization butterfly is stopped the maintenance of plate body and the purpose of changing, and after installing new butterfly and is stopped the plate body, can guarantee again that the butterfly stops the fastness of plate body in the butterfly is stopped the installation cover, can guarantee the butterfly and stop the normal operating of plate body, the normal speed reduction of unmanned aerial vehicle body has been guaranteed.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a novel butterfly brake structure device applied to an unmanned aerial vehicle.
Background
The unmanned plane is called unmanned plane for short, and is an unmanned aerial vehicle operated by radio remote control equipment and a self-contained program control device.
The butterfly that installs usually on current unmanned aerial vehicle's the gliding curb plate is stopped, through the deflection that the butterfly stopped to realize unmanned aerial vehicle speed reduction and descending. But current butterfly is stopped the structure and is passed through integratively, stops when breaking down or damaging when the butterfly, just needs to stop whole butterfly and dismantle from unmanned aerial vehicle, and the part that the dismantlement process is comparatively loaded down with trivial details and dismantle is more, is unfavorable for the quick maintenance that the butterfly stopped.
SUMMERY OF THE UTILITY MODEL
Aiming at the defects of the prior art, the utility model provides the novel butterfly brake structure device applied to the unmanned aerial vehicle, the design scheme has the advantages of convenience in maintenance and simple and rapid maintenance process, and the problems of inconvenient maintenance and complex process of the conventional device are solved.
The novel butterfly brake structure device applied to the unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein two sides of the unmanned aerial vehicle body are respectively provided with a gliding side plate, the surface of each gliding side plate is provided with a mounting groove, a butterfly brake mounting sleeve is arranged in each mounting groove, and a butterfly brake plate body is arranged in an inner cavity of each butterfly brake mounting sleeve; the top of the butterfly brake plate body is provided with extrusion grooves at equal intervals from left to right, and the bottom of the butterfly brake plate body is provided with a plurality of groups of limiting clamping grooves at equal intervals from left to right; the butterfly brake mounting sleeve is characterized in that grooves are formed in the bottom of an inner cavity of the butterfly brake mounting sleeve and in positions corresponding to each group of limiting clamping grooves, a plurality of springs are fixed in each groove, a limiting clamping plate is fixed between the tops of the springs, and limiting clamping blocks are integrally formed on the tops of the limiting clamping plates.
As a further improvement of the utility model, a screw rod is connected to the top of the butterfly brake plate body in a threaded manner at a position corresponding to each extrusion groove, and a pressing block is connected to the bottom of the screw rod through a bearing.
Above-mentioned technical scheme, through the press block of design, can effectually promote the butterfly and stop the plate body and move down to stop the plate body fastening power for the butterfly through the screw rod.
As a further improvement of the utility model, the top of the screw is fixedly connected with a screwing block.
Above-mentioned technical scheme plays the effect of conveniently twisting the screw rod.
As a further improvement of the utility model, the size of the pressing block is matched with the size of the extrusion groove.
According to the technical scheme, the pressing block enters the extrusion groove.
As a further improvement of the butterfly brake plate, each group of limiting clamping grooves comprises three groove bodies, the size of each groove body is matched with that of the limiting clamping block, and the limiting clamping block is clamped in the limiting clamping groove at the bottom of the butterfly brake plate body.
Above-mentioned technical scheme through spacing fixture block and spacing draw-in groove, can stop the better of plate body fastening to the butterfly, can avoid the butterfly to stop the plate body and stop the activity in the installation cover at the butterfly.
As a further improvement of the butterfly brake mounting sleeve, the left side and the right side of the butterfly brake plate body are attached to the inner wall of the butterfly brake mounting sleeve.
Above-mentioned technical scheme can promote the butterfly and brake the stability of plate body in the butterfly installation cover of stopping.
As a further improvement of the utility model, one side of the butterfly brake mounting sleeve, which is far away from the butterfly brake plate body, is connected with a driving structure arranged in the unmanned aerial vehicle body.
Above-mentioned technical scheme can drive butterfly plate body deflection of stopping.
Compared with the prior art, the utility model has the following beneficial effects:
according to the butterfly brake mounting sleeve, the butterfly brake plate body, the screw rod, the pressing block, the spring, the limiting clamping plate, the limiting clamping block and the like, the butterfly brake mounting sleeve is simple in structure, convenient to use and clear in arrangement, when the butterfly brake mounting sleeve is used, the butterfly brake plate body can be taken out of the butterfly brake mounting sleeve rapidly by screwing the screw rod, the butterfly brake plate body is maintained and replaced rapidly, after a new butterfly brake plate body is mounted, firmness of the butterfly brake plate body in the butterfly brake mounting sleeve can be guaranteed, normal operation of the butterfly brake plate body can be guaranteed, and normal deceleration of an unmanned aerial vehicle body is guaranteed.
Drawings
The accompanying drawings, which are included to provide a further understanding of the application and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the application and together with the description serve to explain the application and not to limit the application. In the drawings:
Fig. 1 is a schematic front view of an unmanned aerial vehicle body according to the present invention;
FIG. 2 is a schematic side view of the butterfly brake mounting sleeve of the present invention;
fig. 3 is a partially enlarged structural schematic view of the butterfly brake mounting sleeve of the utility model.
In the figure: 1. an unmanned aerial vehicle body; 2. a glide side plate; 3. mounting grooves; 4. a butterfly brake mounting sleeve; 5. a butterfly brake plate body; 501. extruding a groove; 502. a limiting clamping groove; 6. a screw; 7. twisting the block; 8. a pressing block; 9. a groove; 10. a spring; 11. a limiting clamping plate; 12. and a limiting clamping block.
Detailed Description
In the following description, for purposes of explanation, numerous implementation details are set forth in order to provide a thorough understanding of the various embodiments of the present invention. It should be understood, however, that these implementation details are not to be interpreted as limiting the utility model. That is, in some embodiments of the utility model, such implementation details are not necessary. In addition, some conventional structures and components are shown in simplified schematic form in the drawings.
In addition, the descriptions related to the first, the second, etc. in the present invention are only used for description purposes, do not particularly refer to an order or sequence, and do not limit the present invention, but only distinguish components or operations described in the same technical terms, and are not understood to indicate or imply relative importance or implicitly indicate the number of indicated technical features. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In addition, technical solutions between various embodiments may be combined with each other, but must be realized by a person skilled in the art, and when the technical solutions are contradictory or cannot be realized, such a combination should not be considered to exist, and is not within the protection scope of the present invention.
Referring to fig. 1-3, the novel butterfly brake structure device applied to the unmanned aerial vehicle of the utility model comprises an unmanned aerial vehicle body 1, wherein two sides of the unmanned aerial vehicle body 1 are both provided with a gliding side plate 2, the surface of the gliding side plate 2 is provided with a mounting groove 3, a butterfly brake mounting sleeve 4 is arranged in the mounting groove 3, and a butterfly brake plate body 5 is arranged in the inner cavity of the butterfly brake mounting sleeve 4; the top of the butterfly brake plate body 5 is provided with extrusion grooves 501 at equal intervals from left to right, and the bottom of the butterfly brake plate body 5 is provided with a plurality of groups of limiting clamping grooves 502 at equal intervals from left to right; the butterfly is stopped the inner chamber bottom of installing sleeve 4 and is all seted up fluted 9 with the position department that every group spacing draw-in groove 502 corresponds, all is fixed with a plurality of springs 10 in every recess 9, is fixed with spacing cardboard 11 between the top of a plurality of springs 10, and spacing cardboard 11's top integrated into one piece has spacing fixture block 12.
The top of the butterfly brake plate body 5 and the position corresponding to each extrusion groove 501 are in threaded connection with a screw 6, and the bottom of the screw 6 is connected with a pressing block 8 through a bearing; through the pressing block 8 of design, can effectually promote the butterfly and stop plate body 5 and move down to stop plate body 5 fastening power for the butterfly through screw rod 6.
The top of the screw 6 is fixedly connected with a twisting block 7; the effect of conveniently screwing the screw 6 is achieved.
The size of the pressing block 8 is matched with that of the extrusion groove 501; facilitating the entry of the press block 8 into the pressing channel 501.
Each group of limiting clamping grooves 502 comprises three groove bodies, the size of each groove body is matched with that of the limiting clamping block 12, and the limiting clamping block 12 is clamped in the limiting clamping groove 502 at the bottom of the butterfly brake plate body 5; through spacing fixture block 12 and spacing draw-in groove 502, can stop the better of plate body 5 fastening to the butterfly, can avoid the butterfly to stop the plate body 5 and stop the activity in the installation cover 4 at the butterfly.
The left side and the right side of the butterfly brake plate body 5 are both attached to the inner wall of the butterfly brake mounting sleeve 4; the stability of butterfly brake plate body 5 in butterfly brake mounting sleeve 4 can be promoted.
One side of the butterfly brake mounting sleeve 4, which is far away from the butterfly brake plate body 5, is connected with a driving structure arranged in the unmanned aerial vehicle body 1; the butterfly brake plate body 5 can be driven to deflect.
When the butterfly brake plate body 5 needs to be replaced by using the butterfly brake plate body replacement device (working principle), a worker firstly holds the twisting block 7 to unscrew the four screw rods 6, so that the pressing block 8 is driven by the screw rods 6 to withdraw from the extrusion groove 501, the butterfly brake plate body 5 is further lifted by the return of the spring 10, then the worker can hold the butterfly brake plate body 5 and can easily take out the butterfly brake plate body 5 from the butterfly brake mounting sleeve 4 by pulling outwards, when a new butterfly brake plate body 5 is installed, the worker only needs to insert the butterfly brake plate body 5 into the butterfly brake mounting sleeve 4 to clamp the limiting clamping groove 502 at the bottom of the butterfly brake plate body 5 and the limiting clamping block 12 at the top of the limiting clamping plate 11 together, then sequentially screws the four screw rods 6, pushes the pressing block 8 into the extrusion groove 501 through the screw rods 6, and continuously applies downward thrust to the butterfly brake plate body 5, and finally compresses and shortens the spring 10, the limiting clamping plate 11 enters the groove 9, and the butterfly brake plate body 5 is mounted again until the butterfly brake plate body is screwed down.
The above description is only an embodiment of the present invention, and is not intended to limit the present invention. Various modifications and alterations to this invention will become apparent to those skilled in the art. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention should be included in the scope of the claims of the present invention.
Claims (7)
1. The utility model provides a be applied to novel butterfly of unmanned aerial vehicle and stop structure device, includes unmanned aerial vehicle body (1), its characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), and is characterized in that gliding side plates (2) are arranged on two sides of the unmanned aerial vehicle body (1), mounting grooves (3) are formed in the surfaces of the gliding side plates (2), butterfly brake mounting sleeves (4) are arranged in the mounting grooves (3), and butterfly brake plate bodies (5) are arranged in inner cavities of the butterfly brake mounting sleeves (4);
the top of the butterfly brake plate body (5) is provided with extrusion grooves (501) at equal intervals from left to right, and the bottom of the butterfly brake plate body (5) is provided with a plurality of groups of limiting clamping grooves (502) at equal intervals from left to right;
the butterfly is stopped the inner chamber bottom of installing sleeve (4) and is all seted up recess (9) with the position department that every group spacing draw-in groove (502) correspond, every all be fixed with a plurality of springs (10) in recess (9), it is a plurality of be fixed with spacing cardboard (11) between the top of spring (10), the top integrated into one piece of spacing cardboard (11) has spacing fixture block (12).
2. The novel butterfly brake structure device applied to the unmanned aerial vehicle as claimed in claim 1, wherein: the butterfly is stopped the top of plate body (5) and is located equal threaded connection with every extrusion groove (501) corresponding position and have screw rod (6), the bottom of screw rod (6) is connected with through the bearing and presses briquetting (8).
3. The novel butterfly brake structure device applied to the unmanned aerial vehicle as claimed in claim 2, wherein: the top of the screw rod (6) is fixedly connected with a twisting block (7).
4. The novel butterfly brake structure device applied to the unmanned aerial vehicle as claimed in claim 2, wherein: the size of the pressing block (8) is matched with that of the extrusion groove (501).
5. The novel butterfly brake structure device applied to the unmanned aerial vehicle as claimed in claim 1, wherein: each group of limiting clamping grooves (502) comprises three groove bodies, the size of each groove body is matched with that of each limiting clamping block (12), and each limiting clamping block (12) is clamped in the corresponding limiting clamping groove (502) in the bottom of the butterfly brake plate body (5).
6. The novel butterfly brake structure device applied to the unmanned aerial vehicle as claimed in claim 1, wherein: the left side and the right side of the butterfly brake plate body (5) are attached to the inner wall of the butterfly brake mounting sleeve (4).
7. The novel butterfly brake structure device applied to the unmanned aerial vehicle as claimed in claim 1, wherein: the butterfly brake mounting sleeve (4) is far away from one side of the butterfly brake plate body (5) and is connected with a driving structure arranged in the unmanned aerial vehicle body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122102520.1U CN215554086U (en) | 2021-09-02 | 2021-09-02 | Be applied to unmanned aerial vehicle's novel butterfly structure device of stopping |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122102520.1U CN215554086U (en) | 2021-09-02 | 2021-09-02 | Be applied to unmanned aerial vehicle's novel butterfly structure device of stopping |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215554086U true CN215554086U (en) | 2022-01-18 |
Family
ID=79845874
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122102520.1U Active CN215554086U (en) | 2021-09-02 | 2021-09-02 | Be applied to unmanned aerial vehicle's novel butterfly structure device of stopping |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215554086U (en) |
-
2021
- 2021-09-02 CN CN202122102520.1U patent/CN215554086U/en active Active
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