CN210191834U - Unmanned aerial vehicle's motor mounting structure - Google Patents
Unmanned aerial vehicle's motor mounting structure Download PDFInfo
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- CN210191834U CN210191834U CN201920945129.8U CN201920945129U CN210191834U CN 210191834 U CN210191834 U CN 210191834U CN 201920945129 U CN201920945129 U CN 201920945129U CN 210191834 U CN210191834 U CN 210191834U
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- aerial vehicle
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- 238000009434 installation Methods 0.000 claims description 25
- 238000009423 ventilation Methods 0.000 claims description 8
- 230000006978 adaptation Effects 0.000 claims description 2
- 238000003466 welding Methods 0.000 claims 1
- 230000002349 favourable effect Effects 0.000 abstract description 2
- 230000000694 effects Effects 0.000 description 5
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a motor mounting structure of an unmanned aerial vehicle, which comprises a body, a plurality of wings are arranged on the circumferential outer wall of the body, one end of the wings, which is far away from the body, is provided with a mounting box, a plurality of positioning plates are arranged on the circumferential inner wall of the mounting box, positioning holes are arranged on the top outer wall of the positioning plates, a first mounting plate is arranged on the circumferential inner wall of the mounting box, which is close to the top, a circular hole is arranged on the inner part of the first mounting plate, which is close to the central position, a plurality of first mounting holes are also arranged on the top outer wall of the first mounting plate, a motor is arranged inside the mounting box, a plurality of positioning columns are fixed on the bottom outer wall of the motor through bolts, a second mounting plate is fixed on the circumferential outer wall of the motor, a, be favorable to the stable flight of unmanned aerial vehicle.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle's motor mounting structure.
Background
The unmanned aircraft is an unmanned aerial vehicle for short, and is also called UAV in short, and the UAV is an unmanned aircraft operated by utilizing a radio remote control device and a self-contained program control device, and is widely applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, electric power inspection, disaster relief, film and television shooting, romantic manufacturing and the like. Unmanned aerial vehicle's flight mainly relies on motor drive, and the stability of the good or bad flight that will directly decide unmanned aerial vehicle of motor installation, however, current unmanned aerial vehicle motor installation is direct to fix it through the bolt more, and stability is lower, and fixed effect is relatively poor in view of this, we provide an unmanned aerial vehicle's motor mounting structure.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle's motor mounting structure to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme:
an unmanned aerial vehicle motor mounting structure comprises a machine body, wherein a plurality of wings are arranged on the circumferential outer wall of the machine body, a mounting box is arranged at one end, away from the machine body, of each wing, a plurality of positioning plates are arranged on the circumferential inner wall of the mounting box close to the bottom, positioning holes are formed in the top outer wall of each positioning plate, a first mounting plate is arranged on the circumferential inner wall of the mounting box close to the top, a circular hole is formed in the first mounting plate close to the center, a plurality of first mounting holes are formed in the top outer wall of the first mounting plate, a motor is arranged in the mounting box, a plurality of positioning columns are fixed on the bottom outer wall of the motor through bolts, a second mounting plate is fixed on the circumferential outer wall of the motor close to the top through bolts, a plurality of second mounting holes are formed in the top outer wall of the second mounting plate, and the end part of an output, the top of install bin is equipped with the case lid, the top outer wall of case lid is close to central point and puts the department and has seted up the dead eye, and is equipped with the bearing in the dead eye, still seted up a plurality of ventilation holes on the top outer wall of case lid.
Preferably, the number of the positioning columns is equal to that of the positioning plates, the shapes and the sizes of the positioning columns are matched with the positioning holes, and the positioning columns and the positioning holes are in clamping fit.
Preferably, the positioning plate is tightly welded with the installation box, and the first installation plate is fixedly welded with the installation box.
Preferably, the body, the wings and the mounting box are of an integrally formed structure.
Preferably, the shape and the size of the box cover are matched with those of the mounting box, and the box cover and the mounting box are in threaded connection.
Preferably, the first mounting panel with the shape and the size of the second mounting panel are the same, first mounting hole with be equipped with the gim peg between the second mounting hole, just the gim peg with first mounting hole with be threaded connection between the second mounting hole.
Preferably, the number of the vent holes is 8-14, and the vent holes are arranged at equal intervals.
Compared with the prior art, the beneficial effects of the utility model are that: according to the motor mounting structure of the unmanned aerial vehicle, the motor can be positioned firstly through the positioning columns, the positioning plates and the positioning holes, and then the motor can be further mounted and fixed through the arrangement of the first mounting plate, the second mounting plate and the fixing bolts, so that the fixing effect is enhanced, and the stability of the device is improved; through case lid and install bin threaded connection, be convenient for open the case lid and maintain the motor, through the setting in ventilation hole, can strengthen the ventilation effect in the install bin, be favorable to the stable work of motor, prolong its life.
Drawings
Fig. 1 is a schematic overall top view structure of the present invention;
FIG. 2 is a schematic structural view of the mounting box and the box cover of the present invention;
FIG. 3 is a schematic view of a partial cross-sectional structure of the mounting box and the wing of the present invention;
fig. 4 is a schematic structural diagram of the motor of the present invention;
FIG. 5 is a schematic view of the bottom structure of the box cover of the present invention;
fig. 6 is a schematic view of a partial sectional structure of the middle mounting box of the present invention.
In the figure: 1. a body; 2. an airfoil; 3. installing a box; 30. a first mounting plate; 300. a circular hole; 301. a first mounting hole; 302. a fixing bolt; 31. positioning a plate; 310. positioning holes; 4. a box cover; 40. a bearing bore; 41. a vent hole; 5. a motor; 50. a rotating shaft; 51. a positioning column; 52. a second mounting plate; 520. and a second mounting hole.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and to simplify the description, but do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore should not be construed as limiting the present invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically limited otherwise.
Referring to fig. 1-6, the present invention provides a technical solution:
a motor mounting structure of an unmanned aerial vehicle comprises a machine body 1, a plurality of wings 2 are arranged on the circumferential outer wall of the machine body 1, a mounting box 3 is arranged at one end, away from the machine body 1, of each wing 2, a plurality of positioning plates 31 are arranged on the circumferential inner wall of the mounting box 3 close to the bottom, positioning holes 310 are formed in the top outer wall of each positioning plate 31, a first mounting plate 30 is arranged on the circumferential inner wall of the mounting box 3 close to the top, a circular hole 300 is formed in the first mounting plate 30 close to the center, a plurality of first mounting holes 301 are formed in the top outer wall of the first mounting plate 30, a motor 5 is arranged in the mounting box 3, a plurality of positioning columns 51 are fixed on the bottom outer wall of the motor 5 through bolts, a second mounting plate 52 is fixed on the circumferential outer wall of the motor 5 close to the top through bolts, a plurality of second mounting holes 520 are formed in the top outer wall of the second, the top of install bin 3 is equipped with case lid 4, and the top outer wall of case lid 4 is close to central point and puts the department and has seted up dead eye 40, and is equipped with the bearing in the dead eye 40, has still seted up a plurality of ventilation holes 41 on the top outer wall of case lid 4.
In this embodiment, the number of the positioning columns 51 is equal to that of the positioning plates 31, the shapes and sizes of the positioning columns 51 are matched with those of the positioning holes 310, and the positioning columns 51 are clamped and matched with the positioning holes 310, so that the positioning columns 51 are stably placed in the positioning holes 310, and the motor 5 can be positioned.
It should be noted that, the positioning plate 31 and the mounting box 3 are tightly welded, and the first mounting plate 30 and the mounting box 3 are welded and fixed, so that the positioning plate 31 and the first mounting plate 30 are stably fixed in the mounting box 3.
In this embodiment, the body 1, the wings 2 and the installation box 3 are of an integrally formed structure, so that the connection among the body 1, the wings 2 and the installation box 3 is tighter, and the stability of the device is enhanced.
It is supplementary to need, the shape and the size of the case lid 4 and the install bin 3 looks adaptation, and be threaded connection between the two, be convenient for open and close case lid 4 to be convenient for top install the motor 5 in the case 3 and maintain.
Further, the first mounting plate 30 and the second mounting plate 52 have the same shape and size, the fixing bolt 302 is disposed between the first mounting hole 301 and the second mounting hole 520, and the fixing bolt 302 and the first mounting hole 301 and the second mounting hole 520 are both in threaded connection, so that the motor 5 is stably mounted on the first mounting plate 30.
In addition, the number of the vent holes 41 is 8-14, preferably 10 in the embodiment, and the vent holes are arranged at equal intervals, so that the ventilation effect in the installation box 3 is enhanced, and the stable work of the motor 5 is facilitated.
It should be noted that the motor 5 may be a motor of the type CREATION 2407 manufactured by yoketai motor technologies ltd, and its associated circuitry and power supply may also be provided by the manufacturer; furthermore, the present invention relates to the motor 5 being the prior art, and the technical personnel in the field can completely realize the present invention without extra description, and the protection of the present invention does not relate to the improvement of the structure and the working principle of the motor 5.
When the unmanned aerial vehicle's of this embodiment motor mounting structure is installed, unscrew case lid 4 earlier, open case lid 4, put into install bin 3 with motor 5 from circular port 300 in, make corresponding reference column 51 joint in locating hole 310, rethread gim peg 302 is together fixed with first mounting panel 30 and second mounting panel 52, thereby fix motor 5 installation, fix again through fixing a position earlier motor 5, make more firm of its installation, after the installation, cover case lid 4, ventilation effect through a plurality of ventilation holes 41 can strengthen install bin 3, be convenient for the stable work of motor 5, prolong its life.
The foregoing shows and describes the general principles, essential features, and advantages of the invention. It should be understood by those skilled in the art that the present invention is not limited by the above embodiments, and the description in the above embodiments and the description is only preferred examples of the present invention, and is not intended to limit the present invention, and that the present invention can have various changes and modifications without departing from the spirit and scope of the present invention, and these changes and modifications all fall into the scope of the claimed invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (7)
1. The utility model provides an unmanned aerial vehicle's motor mounting structure, includes organism (1), its characterized in that: the aircraft is characterized in that a plurality of wings (2) are arranged on the circumferential outer wall of the aircraft body (1), an installation box (3) is arranged at one end, far away from the aircraft body (1), of each wing (2), a plurality of positioning plates (31) are arranged on the circumferential inner wall of the installation box (3) close to the bottom, positioning holes (310) are formed in the top outer wall of each positioning plate (31), a first installation plate (30) is arranged on the circumferential inner wall of the installation box (3) close to the top, a circular hole (300) is formed in the position, close to the center, of the interior of the first installation plate (30), a plurality of first installation holes (301) are further formed in the top outer wall of the first installation plate (30), a motor (5) is arranged in the interior of the installation box (3), a plurality of positioning columns (51) are fixed on the bottom outer wall of the motor (5) through bolts, and a second installation plate (52) is, a plurality of second mounting holes (520) have been seted up on the top outer wall of second mounting panel (52), the output shaft end connection of motor (5) has pivot (50), the top of install bin (3) is equipped with case lid (4), the top outer wall of case lid (4) is close to central point and puts the department and has seted up dead eye (40), and is equipped with the bearing in dead eye (40), still seted up a plurality of ventilation holes (41) on the top outer wall of case lid (4).
2. The unmanned aerial vehicle's motor mounting structure of claim 1, characterized in that: the quantity of reference column (51) with the quantity of locating plate (31) equals, the shape and the size of dimensions of reference column (51) with locating hole (310) looks adaptation, and the joint cooperation between the two.
3. The unmanned aerial vehicle's motor mounting structure of claim 1, characterized in that: the positioning plate (31) and the installation box (3) are welded tightly, and the first installation plate (30) and the installation box (3) are fixed by welding.
4. The unmanned aerial vehicle's motor mounting structure of claim 1, characterized in that: the airplane body (1), the wings (2) and the mounting box (3) are of an integrally formed structure.
5. The unmanned aerial vehicle's motor mounting structure of claim 1, characterized in that: the shape and the size of the box cover (4) are matched with those of the installation box (3), and the box cover and the installation box are in threaded connection.
6. The unmanned aerial vehicle's motor mounting structure of claim 1, characterized in that: the shape and the size of the first mounting plate (30) are the same as those of the second mounting plate (52), a fixing bolt (302) is arranged between the first mounting hole (301) and the second mounting hole (520), and the fixing bolt (302) is in threaded connection with the first mounting hole (301) and the second mounting hole (520).
7. The unmanned aerial vehicle's motor mounting structure of claim 1, characterized in that: the number of the vent holes (41) is 8-14, and the vent holes are arranged at equal intervals.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920945129.8U CN210191834U (en) | 2019-06-22 | 2019-06-22 | Unmanned aerial vehicle's motor mounting structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920945129.8U CN210191834U (en) | 2019-06-22 | 2019-06-22 | Unmanned aerial vehicle's motor mounting structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210191834U true CN210191834U (en) | 2020-03-27 |
Family
ID=69872065
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920945129.8U Expired - Fee Related CN210191834U (en) | 2019-06-22 | 2019-06-22 | Unmanned aerial vehicle's motor mounting structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210191834U (en) |
-
2019
- 2019-06-22 CN CN201920945129.8U patent/CN210191834U/en not_active Expired - Fee Related
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200327 Termination date: 20210622 |