CN207045754U - A kind of unmanned plane motor cabinet and the unmanned plane including the motor cabinet - Google Patents
A kind of unmanned plane motor cabinet and the unmanned plane including the motor cabinet Download PDFInfo
- Publication number
- CN207045754U CN207045754U CN201721035397.3U CN201721035397U CN207045754U CN 207045754 U CN207045754 U CN 207045754U CN 201721035397 U CN201721035397 U CN 201721035397U CN 207045754 U CN207045754 U CN 207045754U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- motor cabinet
- wall
- motor
- annular outer
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 4
- 229910052782 aluminium Inorganic materials 0.000 claims description 4
- 239000004411 aluminium Substances 0.000 claims description 4
- 239000000463 material Substances 0.000 claims description 3
- 239000007787 solid Substances 0.000 claims description 2
- 230000017525 heat dissipation Effects 0.000 abstract description 6
- 238000009423 ventilation Methods 0.000 abstract description 6
- 229910001095 light aluminium alloy Inorganic materials 0.000 abstract description 3
- 230000005611 electricity Effects 0.000 description 5
- 229920000049 Carbon (fiber) Polymers 0.000 description 3
- 239000004917 carbon fiber Substances 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000005183 dynamical system Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
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- Toys (AREA)
Abstract
The utility model discloses a kind of unmanned plane motor cabinet and the unmanned plane including the motor cabinet, belong to unmanned plane field, including for supporting the circumferentially disposed annular outer wall of loading plate described in the loading plate and ring of motor, the loading plate is arranged on the middle part of the annular outer wall, the mounting hole for fixing the motor is provided with the loading plate, the annular outer wall side is outwards provided with the fixing pipe of clamping device, the clamping device is used for the horn being clamped and installed in the fixing pipe, the fixed mechanism being installed on unmanned aerial vehicle body is provided with the annular outer wall.The utility model, as flexible locking mechanism, makes the locking to horn relatively reliable, the holding area that gain tabletting further increases horn as rigid locking mechanism makes clamping relatively reliable using clamping device；The design of heat emission hole can provide heat dissipation ventilation passage for motor；Using aircraft aluminum matter, own wt can be mitigated on the premise of proof strength.
Description
Technical field
Unmanned plane field is the utility model is related to, more particularly to a kind of unmanned plane motor cabinet and the nothing including the motor cabinet
It is man-machine.
Background technology
In professional unmanned plane demand, using on the premise of more and more extensive, electricity exposed outside to solve propeller motor
Machine does not have an outer protection, it is exposed outside control line, power line the problem of, for the dynamical system of preferably protection multi-rotor unmanned aerial vehicle
System, and make product appearance more both artistic and practical, it is necessary to a kind of unmanned plane motor cabinet is provided.
Utility model content
The purpose of this utility model is to provide the nothing of a kind of effectively protection multi-rotor unmanned aerial vehicle motor and appearance looks elegant practicality
Man-machine motor cabinet and the unmanned plane including the motor cabinet.
To achieve the above object, the utility model adopts the following technical scheme that：
On the one hand, the utility model provides a kind of unmanned plane motor cabinet, including for supporting loading plate and the ring institute of motor
The circumferentially disposed annular outer wall of loading plate is stated, the loading plate is arranged on the middle part of the annular outer wall, set on the loading plate
The mounting hole for fixing the motor is equipped with, the annular outer wall side is outwards provided with the fixing pipe of clamping device, institute
The horn that clamping device is used to be clamped and installed in the fixing pipe is stated, is provided with the annular outer wall and is installed to unmanned plane machine
Fixed mechanism with it.
Further, the fixing pipe and the horn are interference fits, and tolerance is in 0.05-0.1mm.
Further, the axial side wall of the external part of the fixing pipe is provided with side opening, the both sides point of the side opening
The grip unit of bolt fastening is not provided with, and the grip unit and bolt form the clamping device.
Preferably, the external part end face of the fixing pipe is provided with outwardly gain tabletting.
Further, prefabricated horn positioning hole is provided with the fixing pipe.
Preferably, the through hole mutually run through with the fixing pipe is provided with the annular outer wall, the through hole is provided with
Limit the stopping means that the horn moves to through hole.
Further, the fixed mechanism be arranged on below the annular outer wall at least three be used for be fixed on fuselage
On fixed angles.
Preferably, some thermal vias are provided with the annular outer wall.
Further, the material of the unmanned plane motor cabinet is aviation aluminium, and the loading plate is designed using hollow out.
On the other hand, there is provided a kind of unmanned plane, including described unmanned plane motor cabinet, the motor cabinet are fixed on the nothing
Man-machine upper for supporting motor, the fixing pipe of the motor cabinet is used to clamp horn.
Further, the motor is TM MN52 serial motors.
Due at least there is advantages below using above-mentioned technical proposal, the utility model：
(1) the utility model makes the locking to horn relatively reliable, gain using clamping device as flexible locking mechanism
The holding area that tabletting further increases horn as rigid locking mechanism makes clamping relatively reliable；The design of heat emission hole can be
Motor provides heat dissipation ventilation passage；Using aircraft aluminum matter, own wt can be mitigated on the premise of proof strength；To motor
Semi-surrounding is designed, and motor radiating has also been taken into account while motor is protected；
(2) the utility model is simple in construction, and the position arrangement for adjusting motor and electricity is more reasonable, controllable, is especially suitable for TM
MN52 series unmanned plane motors.
Brief description of the drawings
Above-mentioned is only the general introduction of technical solutions of the utility model, in order to better understand technology hand of the present utility model
Section, below in conjunction with accompanying drawing, the utility model is described in further detail with embodiment.
Fig. 1 is the structural representation of one embodiment of unmanned plane motor cabinet of the present utility model；
Fig. 2 is the structural representation of another angle of Fig. 1 unmanned plane motor cabinet.
Embodiment
The utility model provides a kind of one embodiment of unmanned plane motor cabinet, as shown in Figure 1 and Figure 2, including for supporting
The loading plate 3 of motor and the annular outer wall 1 of the axial direction of ring loading plate 3, loading plate 3 are arranged on the middle part of annular outer wall 1, loading plate 3
On be provided with mounting hole 2 for fixing motor, the side of annular outer wall 1 is outwards provided with the fixing pipe 13 of clamping device 11,
Clamping device 11 is used for the horn being clamped and installed in fixing pipe 13, is provided with and is installed on unmanned aerial vehicle body on annular outer wall 1
Fixed mechanism 4.
The utility model can be by taking MS1000 unmanned planes as an example, and its motor is TM MN5212 motors, and the utility model is using
When, it is arranged on fuselage, motor is arranged on loading plate 3 by mounting hole 2, by carbon fiber pipe horn by fixed mechanism 4
It is installed in fixing pipe 13, the clamping degree of horn can be adjusted for clamping device 11, and loading plate 3 is formed with annular outer wall 1
The semi-surrounding shape of motor is protected, mounting hole 2 also there is certain heat dissipation ventilation to act on.
Horn can be 25mm carbon fiber pipes.
Further, fixing pipe 13 and horn can be interference fits, and tolerance is in 0.05-0.1mm.
As an improvement can be provided with side opening in the side wall of the external part of fixing pipe 13, the both sides of side opening can be with
The grip unit fastened by bolt 10 is respectively arranged with, grip unit and bolt 10 form clamping device 11.In grip unit
It is provided with the fixing hole being adapted with bolt 10.Make that two grip units are close so that fixing pipe 13 is pressed from both sides by tightening bolt 10
Tight horn.
In order to increase the holding area of fixing pipe and horn, the external part end face of fixing pipe 13 is provided with outwardly gain
Tabletting 8.
Preferably, prefabricated horn positioning hole 7 can be provided with fixing pipe 13.
Preferably, the through hole 6 run through with the phase of fixing pipe 13 is provided with annular outer wall 1, restricted horn is set at through hole 6
The stopping means 9 moved to through hole 6.
For mount on fuselage, fixed mechanism 4 is to be arranged at least three of the lower section of annular outer wall 1 to be used to be fixed on machine
Fixed angles 4 with it.Fixed angles 4 can be installed on the carbon plate on fuselage.
In order that the radiating effect of motor is more preferable, some thermal vias 12 can be provided with annular outer wall 1.Thermal vias
12 can provide heat dissipation ventilation passage for motor electricity tune.
Preferably, the motor being mutually applicable can be TM MN52 serial motors.The utility model has preferable versatility,
Be particularly suitable for use in TM MN52 serial motors.
In order to reduce the load-carrying of unmanned plane as far as possible in the case of proof strength, the material of unmanned plane motor cabinet is aviation
Aluminium, can be 7075 aviation aluminium, and loading plate 3 can also further reduce load-carrying using hollow out design.
Preferably, annular outer wall 1 and loading plate 3 can form semi-surrounding design of electrical motor.Taken into account while motor is protected
Motor radiating.
On the other hand, there is provided a kind of unmanned plane, including above-mentioned unmanned plane motor cabinet, motor cabinet are fixed on unmanned plane and used
In support motor, the fixing pipe 13 of motor cabinet is used to clamp horn.
Further, motor can be TM MN52 serial motors.
The utility model can be by taking MS1000 unmanned planes as an example, and its motor is TM MN5212 motors, and the utility model is using
When, motor is arranged on loading plate 3 by mounting hole 2, carbon fiber pipe horn is installed in fixing pipe 13, passes through precasting machine
Arm positioning hole 7 adjusts horn position, and stopping means 9 limits horn and moved to through hole 6, makes clamp system 11 by tightening bolt 10
Nip part nips so that fixing pipe 13 clamps horn, gain tabletting 8 further fixes to clamp horn, then by solid
Determine angle 4 to be installed on the carbon plate of fuselage, mounting hole 2 also there is certain heat dissipation ventilation to act on, the thermal vias on annular outer wall 1
12 further can provide radiating for motor electricity tune.
It is of the present utility model to use clamping device to make the locking to horn relatively reliable, gain as flexible locking mechanism
The holding area that tabletting further increases horn as rigid locking mechanism makes clamping relatively reliable；The design of heat emission hole can be
Motor provides heat dissipation ventilation passage；Using aircraft aluminum matter, own wt can be mitigated on the premise of proof strength；To motor
Semi-surrounding is designed, and motor radiating has also been taken into account while motor is protected；The utility model is simple in construction, adjusts motor and electricity
Position arrangement it is more reasonable, controllable, be especially suitable for TM MN52 series unmanned plane motors.
It is described above, only it is preferred embodiment of the present utility model, not the utility model is made any formal
Limitation, those skilled in the art make a little simple modification, equivalent variations or modification using the technology contents of the disclosure above,
Fall in the scope of protection of the utility model.
Claims (10)
1. a kind of unmanned plane motor cabinet, it is characterised in that including for supporting loading plate described in the loading plate and ring of motor circumferential
The annular outer wall of setting, the loading plate are arranged on the middle part of the annular outer wall, are provided with the loading plate for fixing
The mounting hole of the motor, the annular outer wall side are outwards provided with the fixing pipe of clamping device, and the clamping device is used
In being provided with the fixation machine that is installed on unmanned aerial vehicle body on the horn being clamped and installed in the fixing pipe, the annular outer wall
Structure.
2. unmanned plane motor cabinet according to claim 1, it is characterised in that the axial side wall of the external part of the fixing pipe
Be provided with side opening, the both sides of the side opening are respectively arranged with the grip unit being fastened by bolts, the grip unit and
Bolt forms the clamping device.
3. unmanned plane motor cabinet according to claim 2, it is characterised in that the external part end face of the fixing pipe is provided with
Outwardly gain tabletting.
4. unmanned plane motor cabinet according to claim 1, it is characterised in that prefabricated horn is provided with the fixing pipe and is determined
Position hole.
5. unmanned plane motor cabinet according to claim 1, it is characterised in that be provided with the annular outer wall with it is described solid
The through hole that fixed tube mutually runs through, the through hole set the stopping means that the restricted horn moves to through hole.
6. unmanned plane motor cabinet according to claim 1, it is characterised in that the fixed mechanism is to be arranged on the annular
At least three fixed angles for being fixed on fuselage below outer wall.
7. unmanned plane motor cabinet according to any one of claims 1 to 6, it is characterised in that be provided with the annular outer wall
Some thermal vias.
8. unmanned plane motor cabinet according to any one of claims 1 to 6, it is characterised in that the material of the unmanned plane motor cabinet
Matter is aviation aluminium, and the loading plate is designed using hollow out.
9. a kind of unmanned plane, it is characterised in that including any described unmanned plane motor cabinet of claim 1 to 8, the motor cabinet
It is fixed on the unmanned plane and is used to support motor, the fixing pipe of the motor cabinet is used to clamp horn.
10. unmanned plane according to claim 9, it is characterised in that the motor is TMMN52 serial motors.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721035397.3U CN207045754U (en) | 2017-08-18 | 2017-08-18 | A kind of unmanned plane motor cabinet and the unmanned plane including the motor cabinet |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721035397.3U CN207045754U (en) | 2017-08-18 | 2017-08-18 | A kind of unmanned plane motor cabinet and the unmanned plane including the motor cabinet |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207045754U true CN207045754U (en) | 2018-02-27 |
Family
ID=61503863
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721035397.3U Expired - Fee Related CN207045754U (en) | 2017-08-18 | 2017-08-18 | A kind of unmanned plane motor cabinet and the unmanned plane including the motor cabinet |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207045754U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110920885A (en) * | 2018-09-19 | 2020-03-27 | 漳浦比速光电科技有限公司 | Remote control type air lighting device and using method thereof |
| CN110972474A (en) * | 2018-11-30 | 2020-04-07 | 深圳市大疆创新科技有限公司 | Protective housing, motor element, horn subassembly and unmanned aerial vehicle |
| WO2020107551A1 (en) * | 2018-11-30 | 2020-06-04 | 深圳市大疆创新科技有限公司 | Protective shell, motor assembly, arm assembly and unmanned aerial vehicle |
| WO2022078092A1 (en) * | 2020-10-16 | 2022-04-21 | 深圳市道通智能航空技术股份有限公司 | Unmanned aerial vehicle |
-
2017
- 2017-08-18 CN CN201721035397.3U patent/CN207045754U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110920885A (en) * | 2018-09-19 | 2020-03-27 | 漳浦比速光电科技有限公司 | Remote control type air lighting device and using method thereof |
| CN110972474A (en) * | 2018-11-30 | 2020-04-07 | 深圳市大疆创新科技有限公司 | Protective housing, motor element, horn subassembly and unmanned aerial vehicle |
| WO2020107551A1 (en) * | 2018-11-30 | 2020-06-04 | 深圳市大疆创新科技有限公司 | Protective shell, motor assembly, arm assembly and unmanned aerial vehicle |
| WO2022078092A1 (en) * | 2020-10-16 | 2022-04-21 | 深圳市道通智能航空技术股份有限公司 | Unmanned aerial vehicle |
| EP4206074A4 (en) * | 2020-10-16 | 2024-05-15 | Autel Robotics Co., Ltd. | Unmanned aerial vehicle |
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Legal Events
| 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: 20180227 Termination date: 20210818 |