CN219740073U - Heat radiation structure of unmanned aerial vehicle motor - Google Patents
Heat radiation structure of unmanned aerial vehicle motor Download PDFInfo
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- CN219740073U CN219740073U CN202320868202.2U CN202320868202U CN219740073U CN 219740073 U CN219740073 U CN 219740073U CN 202320868202 U CN202320868202 U CN 202320868202U CN 219740073 U CN219740073 U CN 219740073U
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- aerial vehicle
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- 230000005855 radiation Effects 0.000 title claims abstract description 7
- 238000009434 installation Methods 0.000 claims description 13
- 230000017525 heat dissipation Effects 0.000 claims description 12
- 230000000694 effects Effects 0.000 abstract description 10
- 238000000034 method Methods 0.000 description 12
- 230000008569 process Effects 0.000 description 9
- 238000005457 optimization Methods 0.000 description 6
- 238000001816 cooling Methods 0.000 description 4
- 230000009471 action Effects 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 238000011900 installation process Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a heat radiation structure of an unmanned aerial vehicle motor, which comprises a motor shell and a bottom plate, wherein the front side and the rear side of the top of the bottom plate are respectively provided with a mounting groove, the front side and the rear side of the motor shell are respectively fixedly connected with an embedded plate, the embedded plates are embedded in the mounting grooves, the two sides of the top of the bottom plate are respectively provided with a guide assembly, the front side and the rear side of the top of the bottom plate are respectively fixedly connected with a mounting box, and the inside of the mounting box is connected with a mounting plate in a sliding manner. According to the utility model, the mounting groove is formed, the mosaic plate is firstly inlaid in the mounting groove, and then the mounting plate is pushed to move to the top of the mosaic plate to prevent the mounting plate from moving upwards, so that the motor casing is fixed, the problem that the motor casing is too complex to mount and is usually fixed in the unmanned aerial vehicle by using bolts is solved, the mounting efficiency is reduced, the using effect is reduced, and the effect of being convenient for fixing the motor casing is achieved.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a heat radiation structure of an unmanned aerial vehicle motor.
Background
The power of unmanned aerial vehicle rotor comes from the motor, in unmanned aerial vehicle long-time work, because the working current of motor is great, and the motor can produce a large amount of heat, makes motor temperature rise, and in addition, the electricity transfers also can produce a large amount of heat, consequently, need to cool down unmanned aerial vehicle motor and electricity.
The list is as the application number: the utility model discloses a motor heat dissipation mechanism for an unmanned aerial vehicle, which comprises a motor casing and a motor arm connecting piece, wherein the motor arm connecting piece is fixedly connected with the motor casing and the motor arm respectively, the motor casing is in a hollow cylinder shape, an air inlet is formed in the bottom surface of the motor casing, an air outlet is formed in the side wall of the motor casing, and a heat dissipation air channel is formed by the air inlet, the inner cavity of the motor casing and the air outlet. Compared with the traditional fan and cooling fin structure, the structure of the utility model cools the motor and the electric regulator in a natural air cooling mode, fully utilizes the self air draft structure of the cooling mechanism, has the outstanding advantages of good cooling effect, simple structure, small weight, convenient maintenance and the like, and enhances the flight stability of the unmanned aerial vehicle.
Based on the retrieval of the above patent and the discovery of the equipment in the combination prior art, the equipment can solve the technical problems of poor heat dissipation effect, complex structure, inconvenient maintenance, increased load of the unmanned aerial vehicle and the like of the existing unmanned aerial vehicle heat dissipation structure when in use, and the motor casing is excessively complex to install in the use process, and the motor casing is fixed in the unmanned aerial vehicle by using bolts generally, so that the installation efficiency is reduced, and the use effect is reduced.
Disclosure of Invention
In order to solve the problems in the prior art, the utility model aims to provide a heat dissipation structure of an unmanned aerial vehicle motor, which has the advantage of being convenient for fixing a motor casing, and solves the problems that the installation of the motor casing is too complex, the motor casing is usually fixed in the unmanned aerial vehicle by using bolts, the installation efficiency is reduced, and the use effect is reduced.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides a heat radiation structure of unmanned aerial vehicle motor, includes motor casing and bottom plate, the mounting groove has all been seted up to the front side and the rear side at bottom plate top, the equal fixedly connected with mosaic plate of front side and rear side of motor casing, mosaic plate inlays the inside at the mounting groove, guide assembly has all been seted up to the both sides at bottom plate top, the equal fixedly connected with mounting box of front side and rear side at bottom plate top, the inside sliding connection of mounting box has the mounting panel, the outside fixedly connected with spring of mounting panel, the spring is provided with a plurality of and is the equidistance and distributes, the one end and the outside fixedly connected with of mounting box inner wall of mounting panel are kept away from to the spring, the equal fixedly connected with spacing subassembly in the outside of mounting panel both sides.
As the preferable mode of the utility model, the guide assembly comprises a guide block, guide grooves are formed in two sides of the top of the bottom plate, and the inner walls of the guide grooves are in sliding connection with the surfaces of the guide block.
As the preferable one of the utility model, the limit component comprises a limit block, both sides of the inner wall of the installation box are provided with limit grooves, and the inner wall of each limit groove is in sliding connection with the surface of the limit block.
As the preferable mode of the utility model, the top of the mounting box is provided with a sliding groove, the outer side of the top of the mounting plate is fixedly connected with a T-shaped plate, and the surface of the T-shaped plate is in sliding connection with the inner wall of the sliding groove.
As the preferable choice of the utility model, the top of the mosaic plate is provided with a plurality of mosaic grooves which are equidistantly distributed, the inner wall of the mosaic groove is embedded with rubber balls, and the top of the rubber balls is fixedly connected with the inner side of the bottom of the mounting plate.
As the preferable mode of the utility model, the top of the T-shaped plate is fixedly connected with a stress plate, and the width of the stress plate is larger than that of the T-shaped plate.
As the preferable mode of the utility model, the front side and the rear side of the top of the bottom plate are fixedly connected with first corresponding strips, and the inner side of the right side of the mounting plate is fixedly connected with second corresponding strips.
Compared with the prior art, the utility model has the following beneficial effects:
1. according to the utility model, the mounting groove is formed, the mosaic plate is firstly inlaid in the mounting groove, and then the mounting plate is pushed to move to the top of the mosaic plate to prevent the mounting plate from moving upwards, so that the motor casing is fixed, the problem that the motor casing is too complex to mount and is usually fixed in the unmanned aerial vehicle by using bolts is solved, the mounting efficiency is reduced, the using effect is reduced, and the effect of being convenient for fixing the motor casing is achieved.
2. According to the utility model, the guide assembly is arranged, so that a user can conveniently and firstly correspond the guide blocks on the two sides of the motor casing to the guide grooves and move downwards, and the motor casing can drive the mosaic plates to be inlaid in the installation grooves, and the mosaic plates cannot be rapidly inlaid in the installation grooves due to the deviation in the installation process can be prevented.
3. According to the utility model, the limiting assembly is arranged, so that a user can limit the mounting plate up and down and left and right by utilizing the sliding fit of the limiting block and the limiting groove in the moving process of the mounting plate, and the phenomenon that the mounting plate cannot resist the mosaic plate and the mosaic plate is separated from the mounting groove due to the fact that the deviation of the mounting plate occurs in the moving process of the mounting plate is avoided.
Drawings
FIG. 1 is a schematic perspective view of the present utility model;
FIG. 2 is an exploded view of a cross-sectional part of the base plate of the present utility model;
fig. 3 is an enlarged schematic view of the structure of fig. 2 a according to the present utility model.
In the figure: 1. a motor housing; 2. a bottom plate; 3. a mounting groove; 4. mosaic plates; 5. a guide assembly; 51. a guide block; 52. a guide groove; 6. a mounting box; 7. a mounting plate; 8. a spring; 9. a limit component; 91. a limiting block; 92. a limit groove; 10. a chute; 11. a T-shaped plate; 12. embedding grooves; 13. rubber balls; 14. a force-bearing plate; 15. a first corresponding bar; 16. and a second corresponding bar.
Description of the embodiments
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
As shown in fig. 1 to 3, the heat dissipation structure of the unmanned aerial vehicle motor provided by the utility model comprises a motor shell 1 and a bottom plate 2, wherein the front side and the rear side of the top of the bottom plate 2 are respectively provided with a mounting groove 3, the front side and the rear side of the motor shell 1 are respectively fixedly connected with a mosaic plate 4, the mosaic plates 4 are inlaid in the mounting grooves 3, both sides of the top of the bottom plate 2 are respectively provided with a guide assembly 5, the front side and the rear side of the top of the bottom plate 2 are respectively fixedly connected with a mounting box 6, the inside of the mounting box 6 is slidably connected with a mounting plate 7, the outer sides of the mounting plates 7 are fixedly connected with springs 8, the springs 8 are distributed at equal intervals, one ends of the springs 8 far away from the mounting plates 7 are fixedly connected with the outer sides of the inner walls of the mounting boxes 6, and the outer sides of the two sides of the mounting plates 7 are respectively fixedly connected with a limiting assembly 9.
Referring to fig. 2, the guide assembly 5 includes a guide block 51, guide grooves 52 are formed on two sides of the top of the bottom plate 2, and an inner wall of the guide groove 52 is slidably connected with a surface of the guide block 51.
As a technical optimization scheme of the utility model, through arranging the guide component 5, a user can conveniently and firstly correspond the guide blocks 51 on the two sides of the motor casing 1 with the guide grooves 52 and move downwards, so that the motor casing 1 can drive the mosaic plates 4 to be inlaid in the installation grooves 3, and the mosaic plates 4 cannot be rapidly inlaid in the installation grooves 3 due to the deviation in the installation process can be prevented.
Referring to fig. 2, the limiting component 9 includes a limiting block 91, both sides of the inner wall of the mounting box 6 are provided with limiting grooves 92, and the inner wall of the limiting groove 92 is slidably connected with the surface of the limiting block 91.
As a technical optimization scheme of the utility model, by arranging the limiting component 9, a user can limit the mounting plate 7 up and down and left and right by utilizing the sliding fit of the limiting block 91 and the limiting groove 92 in the moving process of the mounting plate 7, and the phenomenon that the mounting plate 7 cannot resist the mosaic plate 4 and the mosaic plate 4 is separated from the mounting groove 3 due to the fact that the deviation of the mounting plate 7 occurs in the moving process is prevented.
Referring to fig. 2, a chute 10 is provided at the top of the mounting box 6, a T-shaped plate 11 is fixedly connected to the outer side of the top of the mounting plate 7, and the surface of the T-shaped plate 11 is slidably connected with the inner wall of the chute 10.
As a technical optimization scheme of the utility model, through the arrangement of the sliding chute 10 and the T-shaped plate 11, a user can conveniently push the T-shaped plate 11 to drive the mounting plate 7 to move along the opening path of the sliding chute 10 when the mounting plate 7 cannot be completely pushed to move by the elastic force of the spring 8.
Referring to fig. 3, the top of the mosaic plate 4 is provided with mosaic grooves 12, the mosaic grooves 12 are provided with a plurality of equidistant distribution grooves, the inner wall of the mosaic groove 12 is embedded with rubber balls 13, and the top of the rubber balls 13 is fixedly connected with the inner side of the bottom of the mounting plate 7.
As a technical optimization scheme of the utility model, the embedded groove 12 and the rubber ball 13 are arranged, so that the rubber ball 13 can deform in the process of moving the mounting plate 7 to the top of the embedded plate 4, and the rubber ball 13 can be restored and embedded in the embedded groove 12 until the rubber ball 13 corresponds to the embedded groove 12, so that the fixing effect of the mounting plate 7 on the motor casing 1 can be improved.
Referring to fig. 2, a force plate 14 is fixedly connected to the top of the T-shaped plate 11, and the width of the force plate 14 is greater than that of the T-shaped plate 11.
As a technical optimization scheme of the utility model, through the arrangement of the stress plate 14, the width of the stress plate 14 is larger than that of the T-shaped plate 11, so that a user can conveniently drive the T-shaped plate 11 to move through the stress plate 14 when the user needs to push the T-shaped plate 11 to apply force, the force application area of the user when the user needs to apply force is improved, and the use effect is improved.
Referring to fig. 3, the front side and the rear side of the top of the bottom plate 2 are fixedly connected with a first corresponding strip 15, and the inner side of the right side of the mounting plate 7 is fixedly connected with a second corresponding strip 16.
As a technical optimization scheme of the utility model, by arranging the first corresponding strip 15 and the second corresponding strip 16, the second corresponding strip 16 is driven to move in the moving process of the mounting plate 7, and when the second corresponding strip 16 moves to the top of the first corresponding strip 15, the current rubber ball 13 is embedded in the embedded groove 12, so that a user can observe that the rubber ball 13 is released and embedded in the embedded groove 12 conveniently.
The working principle and the using flow of the utility model are as follows: when the user needs to carry out fixed installation with motor casing 1, the user is at first with the guide block 51 of motor casing 1 both sides and guide slot 52 correspond upward and the downwardly moving, thereby can make motor casing 1 drive mosaic plate 4 inlay the inside of mounting groove 3, prevent to appear the skew and lead to mosaic plate 4 unable quick inlay the inside of mounting groove 3 in the installation, thereby the user utilizes spring 8's elasticity promotion mounting panel 7 to remove the top of mosaic plate 4 and prevent mounting panel 7 upward movement, thereby fix motor casing 1, and utilize the sliding fit of stopper 91 and spacing groove 92 thereby can carry out spacing about mounting panel 7, prevent that mounting panel 7 from appearing the phenomenon of skew at the in-process that removes, lead to mounting panel 7 can't resist mosaic plate 4 and lead to the fact mosaic plate 4 break away from the phenomenon of mounting groove 3, the ability that has been convenient for fix motor casing 1 has been possessed.
To sum up: this unmanned aerial vehicle motor's heat radiation structure, through setting up mounting groove 3, inlay the inside of mounting groove 3 with mosaic plate 4 at first, promote mounting panel 7 afterwards and remove the top of mosaic plate 4 and prevent mounting panel 7 upward movement to fix motor casing 1, solved the installation of motor casing too complicated, generally used the bolt to fix the motor casing in unmanned aerial vehicle's inside, reduced installation effectiveness, reduced the problem of result of use.
It is noted that relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The utility model provides a heat radiation structure of unmanned aerial vehicle motor, includes motor casing (1) and bottom plate (2), its characterized in that: the utility model discloses a motor cabinet, including motor cabinet (1), mounting plate (2), mounting plate (7), spring (8), mounting plate (7) are all offered with the rear side to the front side at bottom plate (2) top, mounting plate (3) are all offered with the rear side, front side and rear side of motor cabinet (1) are all fixedly connected with mosaic plate (4), mosaic plate (4) inlay in the inside of mounting plate (3), guide assembly (5) have all been offered in the both sides at bottom plate (2) top, the equal fixedly connected with mounting box (6) of front side and rear side at bottom plate (2) top, the inside sliding connection of mounting box (6) has mounting plate (7), the outside fixedly connected with spring (8), spring (8) are provided with a plurality of and are the equidistance and distribute, the one end and the outside fixedly connected with of mounting box (6) inner wall of mounting plate (7) are kept away from to spring (8), the equal fixedly connected with spacing subassembly (9) in the outside of mounting plate (7) both sides.
2. The heat dissipation structure of an unmanned aerial vehicle according to claim 1, wherein: the guide assembly (5) comprises a guide block (51), guide grooves (52) are formed in two sides of the top of the bottom plate (2), and the inner walls of the guide grooves (52) are connected with the surfaces of the guide block (51) in a sliding mode.
3. The heat dissipation structure of an unmanned aerial vehicle according to claim 1, wherein: limiting components (9) are including stopper (91), spacing groove (92) have all been seted up to the both sides of mounting box (6) inner wall, the inner wall of spacing groove (92) and the surface sliding connection of stopper (91).
4. The heat dissipation structure of an unmanned aerial vehicle according to claim 1, wherein: the top of installation box (6) has seted up spout (10), the outside fixedly connected with T shaped plate (11) at mounting panel (7) top, the surface and the inner wall sliding connection of spout (10) of T shaped plate (11).
5. The heat dissipation structure of an unmanned aerial vehicle according to claim 1, wherein: mosaic grooves (12) are formed in the top of the mosaic plate (4), a plurality of mosaic grooves (12) are formed in the mosaic grooves and are distributed at equal distances, rubber balls (13) are inlaid in the inner walls of the mosaic grooves (12), and the top of each rubber ball (13) is fixedly connected with the inner side of the bottom of the mounting plate (7).
6. The heat dissipation structure of an unmanned aerial vehicle according to claim 4, wherein: the top fixedly connected with atress board (14) of T shaped plate (11), the width of atress board (14) is greater than the width of T shaped plate (11).
7. The heat dissipation structure of an unmanned aerial vehicle according to claim 1, wherein: the front side and the rear side at the top of the bottom plate (2) are fixedly connected with first corresponding strips (15), and the inner side at the right side of the mounting plate (7) is fixedly connected with second corresponding strips (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320868202.2U CN219740073U (en) | 2023-04-18 | 2023-04-18 | Heat radiation structure of unmanned aerial vehicle motor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320868202.2U CN219740073U (en) | 2023-04-18 | 2023-04-18 | Heat radiation structure of unmanned aerial vehicle motor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219740073U true CN219740073U (en) | 2023-09-22 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320868202.2U Active CN219740073U (en) | 2023-04-18 | 2023-04-18 | Heat radiation structure of unmanned aerial vehicle motor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219740073U (en) |
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2023
- 2023-04-18 CN CN202320868202.2U patent/CN219740073U/en active Active
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