Unmanned aerial vehicle motor with internal air cooling structure

Abstract

The utility model relates to the technical field of unmanned aerial vehicle motor heat dissipation, and discloses an unmanned aerial vehicle motor with an internal air cooling structure, a motor body is fixedly connected in a motor shell, an air cooling mechanism is arranged at the periphery of the motor body, a rotating shaft is fixedly connected at the top of the motor body, and a mounting mechanism is arranged at the periphery of the rotating shaft. The air cooling mechanism comprises a fixing shaft, the fixing shaft is fixedly connected to the inner side of the motor shell, rotating blades are rotationally connected to the periphery of the fixing shaft, sliding blocks are fixedly connected to the peripheries of the rotating blades, a filtering disc is arranged at the bottom of the motor shell, and mounting bolts are in threaded connection with the interior of the filtering disc. Through the rotating blades rotatably connected to the periphery of the fixed shaft, the air cooling effect is generated through air flow when the motor operates, heat dissipation of the motor body is accelerated, the heat dissipation area is further increased in combination with the heat dissipation fins, the heat dissipation efficiency is effectively improved, and performance reduction or damage caused by overheating of the motor is avoided.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned aerial vehicle motor heat dissipation technical field, concretely is a kind of unmanned aerial vehicle motor with internal air cooling structure. BACKGROUND

[0002] As a new emerging flight equipment, unmanned aerial vehicle is widely used in aerial photography, agriculture, logistics, surveying and mapping and many other fields, and the performance and reliability of unmanned aerial vehicle depend largely on the performance of its motor.

[0003] Traditional unmanned aerial vehicle motor generates a lot of heat during operation, and cannot dissipate heat in time and effectively, so the temperature of the motor continues to rise, which will lead to the efficiency of the motor to decline, the power output to be unstable, and even may cause motor failure, seriously affect the normal flight of unmanned aerial vehicle, reduce the service life and safety of unmanned aerial vehicle, so the heat dissipation of unmanned aerial vehicle motor needs to be improved. UTILITY MODEL CONTENT

[0004] The utility model aims at providing a kind of unmanned aerial vehicle motor with internal air cooling structure to solve the problems raised in the above background.

[0005] To achieve the above object, the utility model provides the following technical scheme: a kind of unmanned aerial vehicle motor with internal air cooling structure, including motor shell, the motor shell inside fixedly connected with motor body, the motor body periphery is provided with air cooling mechanism, the motor body top is fixedly connected with rotating shaft, the rotating shaft periphery is provided with mounting mechanism;

[0006] The air cooling mechanism includes fixed shaft, the fixed shaft is fixedly connected to the inner side of motor shell, rotating blade is rotatably connected to the periphery of the fixed shaft, the rotating blade periphery is fixedly connected with sliding block, the motor shell bottom is provided with filter disc, the filter disc inside is screw connected with mounting bolt, the mounting bolt is screw connected to the inner side of motor shell, the motor shell periphery bottom is rotatably connected with support, the support bottom is fixedly connected with cleaning brush, the motor body periphery is provided with heat dissipation fin, the heat dissipation fin inner side is screw connected with fixed bolt, the heat dissipation fin inner side and the periphery of motor body are mutually pasted.

[0007] Preferably, the motor shell inner side is provided with sliding slot corresponding to the sliding track of sliding block, and the sliding block is slidably connected in the sliding slot, the sliding block can rotate in the motor shell inner side through the sliding slot, and the rotating blade is limited, so that the rotating blade is more stable during rotation.

[0008] Preferably, the motor housing bottom is provided with a circular groove corresponding to the movement track of the supporting piece, and the supporting piece is slidingly connected to the inside of the circular groove.

[0009] Preferably, the cleaning brush is arranged at the bottom of the filter disc, and the top of the cleaning brush is in contact with the bottom of the filter disc.

[0010] Preferably, the mounting mechanism comprises a hollow disc, the hollow disc is slidingly connected to the periphery of the rotating shaft, the inside of the hollow disc is fixedly connected with a sliding block, the outside of the hollow disc is fixedly connected with a propeller, and the inside of the hollow disc is threadedly connected with a limiting bolt.

[0011] Preferably, the rotating shaft is provided with a circular hole corresponding to the position of the limiting bolt, and the limiting bolt is threadedly connected to the inside of the circular hole.

[0012] Preferably, the inside of the rotating shaft is provided with a limiting groove corresponding to the movement track of the sliding block, and the sliding block is slidingly connected to the inside of the limiting groove.

[0013] Compared with the prior art, the unmanned aerial vehicle motor with the internal air cooling structure has the following beneficial effects:

[0014] 1. The unmanned aerial vehicle motor with the internal air cooling structure, the rotating blades connected to the periphery of the fixing shaft are rotated, air flow is utilized to generate the air cooling effect when the motor is running, the heat dissipation of the motor body is accelerated, the heat dissipation area is further increased by the heat dissipation fins, the heat dissipation efficiency is effectively improved, and the performance decline or damage of the motor due to overheating is avoided.

[0015] 2. The unmanned aerial vehicle motor with the internal air cooling structure, the hollow disc of the mounting mechanism is slidingly connected to the limiting groove in the inside of the rotating shaft through the sliding block, can be conveniently moved in the periphery of the rotating shaft, and then the limiting bolt is threadedly connected to the circular hole in the inside of the rotating shaft, so that the propeller and the rotating shaft are quickly mounted and dismounted, and the propeller or the motor can be conveniently replaced or maintained and repaired. BRIEF DESCRIPTION OF DRAWINGS

[0016] In order to more clearly illustrate the technical scheme in the embodiments of the present application, the drawings needed to be used in the following embodiment description will be briefly introduced, obviously, the drawings in the following description are only some embodiments of the present application, and for the ordinary skilled in the art, other drawings can be obtained according to these drawings without creative labor.

[0017] Figure 1 It is a front view structural schematic diagram of the present application;

[0018] Figure 2 It is a sectional view structural schematic diagram of the motor shell;

[0019] Figure 3 It is a structural schematic diagram of the air cooling mechanism;

[0020] Figure 4 It is a structural schematic diagram of the fixing bolt, the heat dissipation fin and the sliding block;

[0021] Figure 5 It is a structural schematic diagram of the mounting mechanism.

[0022] In the drawings: 1, motor shell; 2, rotating shaft; 3, mounting mechanism; 31, limiting bolt; 32, sliding block; 33, propeller; 34, hollow disc; 4, air cooling mechanism; 41, cleaning brush; 42, mounting bolt; 43, filter disc; 44, rotating blade; 45, sliding block; 46, fixed shaft; 47, support; 48, fixing bolt; 49, heat dissipation fin; 5, motor body. DETAILED DESCRIPTION

[0023] The technical scheme in the embodiments of the present application will be described clearly and completely in combination with the drawings in the embodiments of the present application, obviously, the described embodiments are only some embodiments of the present application, but not all the embodiments. Based on the embodiments in the present application, all the other embodiments obtained by the ordinary skilled in the art without creative labor are within the protection scope of the present application.

[0024] In the present application, unless otherwise explicitly specified and limited, the terms "mounting", "connecting", "connecting", "fixing" and the like should be understood broadly, for example, it can be fixedly connected, or it can be detachably connected, or it can be integrated; it can be mechanically connected, or it can be electrically connected; it can be directly connected, or it can be indirectly connected through an intermediate medium; it can be the communication inside two elements or the interaction relationship between two elements. For the ordinary skilled in the art, the specific meaning of the above terms in the present application can be understood according to the specific circumstances.

[0025] The present application provides the following technical scheme:

[0026] Embodiment one

[0027] Please refer to Figures 1-5 The utility model provides a technical scheme: a kind of unmanned aerial vehicle motor with internal air cooling structure, including motor shell 1, motor shell 1 inside fixedly connected with motor body 5, motor body 5 periphery is provided with air cooling mechanism 4, motor body 5 top is fixedly connected with rotating shaft 2, rotating shaft 2 periphery is provided with mounting mechanism 3;

[0028] Air cooling mechanism 4 includes fixed shaft 46, fixed shaft 46 is fixedly connected to motor shell 1 inner side, rotating blade 44 is rotatably connected on the periphery of fixed shaft 46, sliding block 45 is fixedly connected on the periphery of rotating blade 44, filter disc 43 is arranged at the bottom of motor shell 1, mounting bolt 42 is screw-connected in the inside of filter disc 43, mounting bolt 42 is screw-connected to the inner side of motor shell 1, supporting member 47 is rotatably connected on the periphery bottom of motor shell 1, cleaning brush 41 is fixedly connected to the bottom of supporting member 47, heat dissipation fin 49 is provided on the periphery of motor body 5, fixed bolt 48 is screw-connected to the inner side of heat dissipation fin 49, and the inner side of heat dissipation fin 49 and the periphery of motor body 5 are mutually attached.

[0029] Further, the sliding groove corresponding to the movement track of the sliding block 45 is formed in the inner side of the motor shell 1, and the sliding block 45 is slidably connected in the sliding groove. By forming the sliding groove, the sliding block 45 can rotate in the inner side of the motor shell 1, and the rotating blade 44 is limited, so that the rotating blade 44 is more stable during rotation.

[0030] Further, the circular groove corresponding to the movement track of the supporting member 47 is formed at the bottom of the motor shell 1, and the supporting member 47 is slidably connected in the circular groove. By forming the circular groove, the supporting member 47 can rotate at the bottom of the motor shell 1, and the supporting member 47 can support the cleaning brush 41, so that the cleaning brush 41 is more stable during rotation.

[0031] Further, the cleaning brush 41 is arranged at the bottom of the filter disc 43, and the top of the cleaning brush 41 and the bottom of the filter disc 43 are in contact with each other. By arranging the cleaning brush 41, the bottom of the filter disc 43 can be cleaned, so that the filter disc 43 is not easy to be blocked.

[0032] Embodiment two

[0033] Please refer to Figures 1-5 And on the basis of embodiment one, further obtain that the mounting mechanism 3 includes hollow disc 34, the hollow disc 34 is slidably connected on the periphery of the rotating shaft 2, the sliding block 32 is fixedly connected to the inner side of the hollow disc 34, the propeller 33 is fixedly connected to the outer side of the hollow disc 34, and the limiting bolt 31 is screw-connected to the inner side of the hollow disc 34.

[0034] Further, the rotating shaft 2 is internally provided with a circular hole corresponding to the position of the limiting bolt 31, and the limiting bolt 31 is threadedly connected to the inside of the circular hole. Through the circular hole, the limiting bolt 31 can be threadedly connected to the inside of the rotating shaft 2, so that the hollow disc 34 can be installed to the periphery of the rotating shaft 2.

[0035] Further, the rotating shaft 2 is internally provided with a circular hole corresponding to the position of the limiting bolt 31, and the limiting bolt 31 is threadedly connected to the inside of the circular hole. Through the circular hole, the limiting bolt 31 can be threadedly connected to the inside of the rotating shaft 2, so that the hollow disc 34 can be installed to the periphery of the rotating shaft 2.

[0036] In actual operation, when the device is used, the sliding block 32 inside the hollow disc 34 is inserted into the rotating shaft 2, and the limiting bolt 31 is threadedly connected to the inside of the hollow disc 34 and the rotating shaft 2, so that the hollow disc 34 can be installed to the periphery of the rotating shaft 2. When the motor body 5 rotates, the hollow disc 34 and the propeller 33 can be driven to rotate by the rotating shaft 2. When the motor body 5 is used, the unmanned aerial vehicle can be lifted. By using air flow, the rotating blade 44 is driven to rotate, so that the air flow inside the motor body 5 is driven to flow, and the heat of the motor body 5 can be dissipated through the heat dissipation fins 49. The hot air around the motor body 5 is quickly taken away, and the cold air is continuously supplemented, forming a good air circulation to produce a wind cooling effect, accelerating the heat dissipation of the motor body 5. The wind entering the motor housing 1 is filtered by the filter disc 43. When the filter disc 43 is blocked, the cleaning brush 41 is manually rotated to clean the surface of the filter disc 43, so that the filter disc 43 is not easily blocked, and the heat dissipation effect of the motor body 5 is better.

[0037] It should be noted that in this text, relational terms such as first and second are used only to distinguish one entity or operation from another, and do not necessarily require or imply that there is any such actual relationship or order between these entities or operations. Moreover, the terms "include", "contain" or any other variants thereof are intended to cover non-exclusive inclusion, so that the process, method, article or equipment including a series of elements not only includes those elements, but also includes other elements not explicitly listed or inherent to such process, method, article or equipment. Without more limitations, the element defined by the statement "including a" does not exclude the presence of another identical element in the process, method, article or equipment including the element.

Claims

1. A UAV motor with an internal air-cooled structure, comprising a motor housing (1), characterized in that: The motor housing (1) is fixedly connected to the motor body (5), the motor body (5) is provided with a wind cooling mechanism (4) on the periphery, the top of the motor body (5) is fixedly connected to a rotating shaft (2), and the rotating shaft (2) is provided with a mounting mechanism (3) on the periphery. The air-cooling mechanism (4) includes a fixed shaft (46), which is fixedly connected to the inner side of the motor housing (1). Rotating blades (44) are rotatably connected to the outer side of the fixed shaft (46). A slider (45) is fixedly connected to the outer side of the rotating blades (44). A filter disc (43) is provided at the bottom of the motor housing (1). A mounting bolt (42) is threaded inside the filter disc (43). The mounting bolt (42) is threaded to the inner side of the motor housing (1). A support member (47) is rotatably connected to the bottom of the outer side of the motor housing (1). A cleaning brush (41) is fixedly connected to the bottom of the support member (47). A heat dissipation fin (49) is provided on the outer side of the motor body (5). A fixing bolt (48) is threaded on the inner side of the heat dissipation fin (49). The inner side of the heat dissipation fin (49) is in close contact with the outer side of the motor body (5).

2. The UAV motor with an internal air-cooled structure according to claim 1, characterized in that: The inner side of the motor housing (1) is provided with a groove corresponding to the movement trajectory of the slider (45), and the slider (45) is slidably connected inside the groove.

3. A UAV motor with an internal air-cooled structure according to claim 1, characterized in that: The bottom of the motor housing (1) is provided with a circular groove corresponding to the movement trajectory of the support member (47), and the support member (47) is slidably connected inside the circular groove.

4. A UAV motor with an internal air-cooled structure according to claim 1, characterized in that: The cleaning brush (41) is located at the bottom of the filter plate (43), and the top of the cleaning brush (41) is in contact with the bottom of the filter plate (43).

5. A UAV motor with an internal air-cooled structure according to claim 1, characterized in that: The installation mechanism (3) includes a hollow disc (34), which is slidably connected to the periphery of the rotating shaft (2). A sliding block (32) is fixedly connected to the inner side of the hollow disc (34), and a propeller (33) is fixedly connected to the outer side of the hollow disc (34). A limit bolt (31) is threadedly connected to the inner side of the hollow disc (34).

6. A UAV motor with an internal air-cooled structure according to claim 5, characterized in that: The rotating shaft (2) has a circular hole inside that corresponds to the position of the limiting bolt (31), and the limiting bolt (31) is threaded into the inside of the circular hole.

7. A UAV motor with an internal air-cooled structure according to claim 5, characterized in that: The inner side of the rotating shaft (2) is provided with a limiting groove corresponding to the movement trajectory of the sliding block (32), and the sliding block (32) is slidably connected inside the limiting groove.

Images