CN207884447U - A kind of unmanned plane electric machine radiator - Google Patents
A kind of unmanned plane electric machine radiator Download PDFInfo
- Publication number
- CN207884447U CN207884447U CN201820122536.4U CN201820122536U CN207884447U CN 207884447 U CN207884447 U CN 207884447U CN 201820122536 U CN201820122536 U CN 201820122536U CN 207884447 U CN207884447 U CN 207884447U
- Authority
- CN
- China
- Prior art keywords
- rotor
- short
- conducting sleeve
- circuited conducting
- unmanned plane
- 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
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Abstract
The utility model discloses a kind of unmanned plane electric machine radiators,Its structure includes body,Rotor,Stator,Latch,Clutch,Cover,Magnetic shoe,Radiator,Body is located on the left of rotor,Rotor is parallel with stator,Clutch is located on the right side of stator,Cover is set on the right side of clutch,Rotor includes short-circuited conducting sleeve,Trim ring,Shaft,Second short-circuited conducting sleeve,Conducting bar,Rotor core,Thermovent,Short-circuited conducting sleeve is connected with rotor core front end,Trim ring insertion is installed in the second short-circuited conducting sleeve,Shaft is installed on trim ring outer surface of cupular part,Radiator is equipped in structure,Heat conductor carried out in heat conduction to cooling fin to the hot gas of internal rotor,Cooling fin carries out heat dissipation work to hot gas,Then fan turning handle hot gas is discharged from thermovent,Heat dissipation effect when rotor setting in motion in its motor to rotor is set to further increase,The right angle service life of rotor.
Description
Technical field
The utility model is a kind of unmanned plane electric machine radiator, belongs to motor radiating technical field.
Background technology
Motor is indicated with letter M (old plant D) in circuit, its main function is to generate driving torque, as
The power source of electrical appliance or various machineries, generator indicate that its main function is converted using electric energy with letter G in circuit
For mechanical energy.
Prior art discloses application No. is：Motor component described in a kind of electric machine radiator of CN201410366390.4
Including motor front end cover, motor housing, motor stator, rotor, motor transmission shaft, back end cover for motor；The motor stator
It surrounds to form air gap with rotor；There is air admission hole on the motor front end cover；The motor rear end is covered with venthole；
The motor front end cover is connect with motor housing；The rear and front end of the motor transmission shaft is respectively by after motor front end cover and motor
The bearing installed in end cap is fixed and is supported；The back end cover for motor is fixedly connected with motor housing bolt；The motor stator,
Rotor, motor housing, motor transmission shaft and back end cover for motor surround to form motor inner space, but the prior art exists
The service life of rotor is reduced to the heat dissipation effect unobvious of rotor when rotor setting in motion in motor.
Utility model content
In view of the deficienciess of the prior art, the utility model aim is to provide a kind of unmanned plane electric machine radiator, with
Solve it is existing in motor when rotor setting in motion to the heat dissipation effect unobvious of rotor, the service life of rotor is asked in reduction
Topic.
To achieve the goals above, the utility model is to realize by the following technical solutions：A kind of unmanned plane motor
Radiator, structure include body, rotor, stator, latch, clutch, cover, magnetic shoe, radiator, and the body is located at
On the left of rotor, the rotor is parallel with stator, and the clutch is located on the right side of stator, and the cover is set on the right side of clutch,
The radiator insertion is installed in rotor, and the rotor includes short-circuited conducting sleeve, trim ring, shaft, the second short-circuited conducting sleeve, conducting bar, turns
Sub- iron core, thermovent, the short-circuited conducting sleeve are connected with rotor core front end, and the trim ring insertion is installed in the second short-circuited conducting sleeve,
The shaft is installed on trim ring outer surface of cupular part, and second short-circuited conducting sleeve is connected with rotor core rear end, the conducting bar installation
On the left of the second short-circuited conducting sleeve, the thermovent is welded in short-circuited conducting sleeve bottom, and the radiator includes fan, cooling fin, thermal conductivity
Body, muffler, balancer, the fan are set on the left of cooling fin, and the cooling fin fits with heat conductor, the thermal conductivity position
On the right side of muffler, the balancer is installed on fan both sides.
Further, a diameter of 10cm of the heat conductor.
Further, the latch is set at the top of stator inner ring.
Further, the fan fits with rotor top.
Further, the shaft is cylindrical structure.
Further, the heat conductor is fabricated from iron.
Further, the cooling fin is made of aluminium alloy.
Advantageous effect
A kind of unmanned plane electric machine radiator of the utility model, is equipped with radiator in structure, and heat conductor is carried out to turning
In sub internal hot gas progress heat conduction to cooling fin, cooling fin carries out heat dissipation work to hot gas, then fan turning handle hot gas from
Thermovent is discharged, and heat dissipation effect when rotor setting in motion in its motor to rotor is made to further increase, right angle the making of rotor
Use the service life.
Description of the drawings
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model
Sign, objects and advantages will become more apparent upon：
Fig. 1 is a kind of structural schematic diagram of unmanned plane electric machine radiator of the utility model；
Fig. 2 is a kind of construction for heat radiating device schematic diagram of unmanned plane electric machine radiator of the utility model；
Fig. 3 is a kind of rotor structure schematic diagram of unmanned plane electric machine radiator of the utility model.
In figure：It is body -1, rotor -2, stator -3, latch -4, clutch -5, cover -6, magnetic shoe -7, radiator -8, short
Road ring -201, trim ring -202, shaft -203, the second short-circuited conducting sleeve -204, conducting bar -205, rotor core -206, thermovent -207, wind
Fan -801, cooling fin -802, heat conductor -803, muffler -804, balancer -805.
Specific implementation mode
To make the technical means, creative features, achievement of purpose, and effectiveness of the utility model be easy to understand, below
In conjunction with specific implementation mode, the utility model is expanded on further.
It please refers to Fig.1, Fig. 2, Fig. 3, the utility model provides a kind of unmanned plane electric machine radiator technical solution：Its structure
Including body 1, rotor 2, stator 3, latch 4, clutch 5, cover 6, magnetic shoe 7, radiator 8, the body 1 is located at rotor 2
Left side, the rotor 2 is parallel with stator 3, and the latch 4 is set at the top of 3 inner ring of stator, and it is right that the clutch 5 is located at stator 3
Side, the cover 6 are set to 5 right side of clutch, and the insertion of the radiator 8 is installed in rotor 2, and the rotor 2 includes short circuit
Ring 201, trim ring 202, shaft 203, the second short-circuited conducting sleeve 204, conducting bar 205, rotor core 206, thermovent 207, the short-circuited conducting sleeve
201 are connected with 206 front end of rotor core, and the insertion of the trim ring 202 is installed in the second short-circuited conducting sleeve 204, and the shaft 203 is pacified
Loaded on 202 outer surface of cupular part of trim ring, second short-circuited conducting sleeve 204 is connected with 206 rear end of rotor core, and the conducting bar 205 is pacified
Loaded on 204 left side of the second short-circuited conducting sleeve, the thermovent 207 is welded in 201 bottom of short-circuited conducting sleeve, and the radiator 8 includes fan
801, cooling fin 802, heat conductor 803, muffler 804, balancer 805, the fan 801 is set to 802 left side of cooling fin, described
Cooling fin 802 fits with heat conductor 803, and the heat conductor 803 is located at 804 right side of muffler, and the balancer 805 is installed on
801 both sides of fan, a diameter of 10cm of the heat conductor 803, institute's latch 4 are set at the top of 3 inner ring of stator, the fan
801 fit with 2 top of rotor, and the shaft 203 is cylindrical structure, and the heat conductor 803 is fabricated from iron, the cooling fin
802 are made of aluminium alloy.
Cooling fin 802 described in this patent is a kind of device to the easy heat-generating electronic elements heat dissipation in electric appliance, mostly by aluminium
Alloy, brass or bronze make plate, sheet, splintery etc., as cpu central processing unit will use sizable heat dissipation in computer
Piece, power supply pipe in television set, row pipe, the power tube in amplifirer will use cooling fin, and general cooling fin in use will be
Electronic component applies last layer heat-conducting silicone grease with radiating rib contact surface, and the heat that component is sent out is made more effectively to be transmitted to cooling fin
On, then be dispersed into surrounding air through cooling fin, flywheel of 5 clutch of the clutch between engine and gearbox
In shell, clutch assembly is fixed in the rear plane of flywheel with screw, the output shaft of clutch is exactly the input shaft of gearbox.
When being used when preparing unmanned plane during flying, start unmanned plane, the rotor 2 and stator 3 in motor coordinate work
Make the conversion of realization electric energy and mechanical energy and mechanical energy and electric energy, rotor 2 starts rotation work and drives unmanned plane during flying, rotor 2
A large amount of hot gas are will produce in rotation, at this moment, the heat conductor 803 in radiator carries out carrying out heat conduction to the hot gas of internal rotor
Onto cooling fin 802, cooling fin 802 carries out heat dissipation work to hot gas, and then 801 turning handle hot gas of fan is from 207 row of thermovent
Go out, the balancer 805 on fan does balancing work to fan, and muffler 804 carries out noise reduction to the noise generated when heat dissipation work
Work.
To the heat dissipation effect unobvious of rotor when the utility model solves the rotor setting in motion in motor, turn in reduction
The service life of son, the utility model are combined with each other by above-mentioned component, and radiator is equipped in structure, and heat conductor carries out
The hot gas of internal rotor is carried out in heat conduction to cooling fin, cooling fin 802 carries out heat dissipation work to hot gas, then fan turning handle
Hot gas is discharged from thermovent, so that heat dissipation effect when rotor setting in motion in its motor to rotor is further increased, and right angle turns
The service life of son, it is described in detail below:
The radiator 8 includes fan 801, cooling fin 802, heat conductor 803, muffler 804, balancer 805, described
Fan 801 is set to 802 left side of cooling fin, and the cooling fin 802 fits with heat conductor 803, and the heat conductor 803 is located at noise reduction
804 right side of device, the balancer 805 are installed on 801 both sides of fan.
The advantages of basic principles and main features and the utility model of the utility model have been shown and described above, for
For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this
In the case of the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute
Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent requirements of the claims
All changes are embraced therein.Any reference numeral in claim should not be considered as to the involved right of limitation
It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiment being appreciated that.
Claims (5)
1. a kind of unmanned plane electric machine radiator, it is characterised in that：Its structure includes body (1), rotor (2), stator (3), card
Tooth (4), clutch (5), cover (6), magnetic shoe (7), radiator (8), the body (1) are located on the left of rotor (2), described turn
Sub (2) are parallel with stator (3), and the clutch (5) is located on the right side of stator (3), and it is right that the cover (6) is set to clutch (5)
Side, the radiator (8) is embedded to be installed in rotor (2), and the rotor (2) includes short-circuited conducting sleeve (201), trim ring (202), turns
Axis (203), the second short-circuited conducting sleeve (204), conducting bar (205), rotor core (206), thermovent (207), the short-circuited conducting sleeve (201) with
Rotor core (206) front end is connected, and the trim ring (202) is embedded to be installed in the second short-circuited conducting sleeve (204), the shaft
(203) it is installed on trim ring (202) outer surface of cupular part, second short-circuited conducting sleeve (204) is connected with rotor core (206) rear end,
The conducting bar (205) is installed on the left of the second short-circuited conducting sleeve (204), and the thermovent (207) is welded in short-circuited conducting sleeve (201) bottom,
The radiator (8) includes fan (801), cooling fin (802), heat conductor (803), muffler (804), balancer (805),
The fan (801) is set on the left of cooling fin (802), and the cooling fin (802) fits with heat conductor (803), the thermal conductivity
Body (803) is located on the right side of muffler (804), and the balancer (805) is installed on fan (801) both sides.
2. a kind of unmanned plane electric machine radiator according to claim 1, it is characterised in that：The heat conductor (803)
A diameter of 10cm.
3. a kind of unmanned plane electric machine radiator according to claim 1, it is characterised in that：The fan (801) with turn
It fits at the top of sub (2).
4. a kind of unmanned plane electric machine radiator according to claim 1, it is characterised in that：The latch (4) is set to fixed
At the top of sub (3) inner ring.
5. a kind of unmanned plane electric machine radiator according to claim 1, it is characterised in that：The shaft (203) is circle
Column structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820122536.4U CN207884447U (en) | 2018-01-25 | 2018-01-25 | A kind of unmanned plane electric machine radiator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820122536.4U CN207884447U (en) | 2018-01-25 | 2018-01-25 | A kind of unmanned plane electric machine radiator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207884447U true CN207884447U (en) | 2018-09-18 |
Family
ID=63508173
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820122536.4U Expired - Fee Related CN207884447U (en) | 2018-01-25 | 2018-01-25 | A kind of unmanned plane electric machine radiator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207884447U (en) |
-
2018
- 2018-01-25 CN CN201820122536.4U patent/CN207884447U/en not_active Expired - Fee Related
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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: 20180918 Termination date: 20200125 |