CN206850618U - A kind of energy-saving motor - Google Patents
A kind of energy-saving motor Download PDFInfo
- Publication number
- CN206850618U CN206850618U CN201720457053.5U CN201720457053U CN206850618U CN 206850618 U CN206850618 U CN 206850618U CN 201720457053 U CN201720457053 U CN 201720457053U CN 206850618 U CN206850618 U CN 206850618U
- Authority
- CN
- China
- Prior art keywords
- connecting plate
- cavity
- body fuselage
- front shroud
- water pipe
- 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
- 238000004804 winding Methods 0.000 claims abstract description 9
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 38
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims 2
- 229910052742 iron Inorganic materials 0.000 claims 1
- 238000001816 cooling Methods 0.000 abstract description 2
- 210000003739 Neck Anatomy 0.000 description 5
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000005674 electromagnetic induction Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Abstract
The utility model discloses a kind of energy-saving motor, including body fuselage, front shroud and connecting plate, the connecting plate is arranged between body fuselage and front shroud, side of the front shroud away from connecting plate is equiped with belt pulley, the inside of the body fuselage is provided with dividing plate, the dividing plate is equiped with fan in the side side wall away from connecting plate, the dividing plate close to the side of connecting plate from top to bottom, stator core is sequentially provided with from outer to inner, stator winding group and rotor, the both sides of the rotor are provided with rotor winding group, the middle part of the rotor is provided with rotary shaft, one end of the rotary shaft is connected by bearing with fan, the other end of the rotary shaft connects through connecting plate with belt pulley.The cooling mechanism that the utility model is carried in itself by motor can be radiated, if heat is excessive, can also preferably be radiated by installing connecting plate, it is not necessary to if connecting plate, can also assemble front shroud and body fuselage.
Description
Technical field
It the utility model is related to technical field of motors, more particularly to a kind of energy-saving motor.
Background technology
Motor (English:Electric machinery, it is commonly called as " motor ") refer to realize electric energy according to the law of electromagnetic induction
Conversion or a kind of calutron transmitted.Represented in circuit with alphabetical M (old plant D).Its main function is to produce drive
Dynamic torque, as electrical appliance or various mechanical power sources.Generator is represented with alphabetical G in circuit.Its main function is
Be converted into mechanical energy using electric energy, current motor be all mostly it is single a fan is installed in rear shell to be radiated,
But many times, motor still can cause to overheat because of working long hours, and have impact on the work of motor internal stator and rotor
Efficiency, in some instances it may even be possible to damage the internal structure of motor.
Utility model content
The purpose of this utility model is and a kind of energy-saving electric proposed in order to solve shortcoming present in prior art
Machine.
To achieve these goals, the utility model employs following technical scheme:
A kind of energy-saving motor, including body fuselage, front shroud and connecting plate, the connecting plate are arranged on body fuselage
Between front shroud, side of the front shroud away from connecting plate is equiped with belt pulley, the inside of the body fuselage be provided with every
Plate, the dividing plate are equiped with fan in the side side wall away from connecting plate, the dividing plate close to the side of connecting plate from top to bottom,
It is sequentially provided with stator core, stator winding group and rotor from outer to inner, the both sides of the rotor are provided with rotor winding group, described turn
The middle part of son is provided with rotary shaft, and one end of the rotary shaft is connected by bearing with fan, and the other end of the rotary shaft runs through
Connecting plate connects with belt pulley, and the inside of the connecting plate is provided with cavity, and the middle part in the cavity is equiped with water pipe, and water pipe
Both ends be respectively positioned on the outside of connecting plate, the madial wall of the cavity is provided with heat-conducting plate, between the heat-conducting plate and water pipe
Upper side wall is equiped with fixed round platform, is provided with ball float in the cavity on the downside of the fixed round platform, the upper side wall of the connecting plate is provided with
Some ventholes connected with cavity.
Preferably, it is equiped with fan housing in side side wall of the body fuselage away from front shroud.
Preferably, the front shroud is equal close to the side upper and lower ends of body fuselage close to the side of connecting plate, connecting plate
Provided with fixture block, and the lateral wall of connecting plate and body fuselage is provided with the neck to match with fixture block.
Preferably, the middle part of the fixed round platform is provided with through hole, and the diameter of through hole is less than the diameter of ball float.
It is preferably located in the side wall of the water pipe in cavity and is uniformly provided with some apopores, the bottom wall of the cavity
For to recessed curved slot arrangement, and the bottom wall of cavity and the junction of water pipe also are provided with apopore.
, can be good by front shroud, connecting plate and body fuselage by the cooperation of fixture block and neck in the utility model
It is installed together, and can also dismantles, the workpiece installed on body fuselage and front shroud works as usual, into connecting plate
Water pipe water filling, water can be full of in cavity by the apopore on water pipe, and setting by ball float and fixed round platform
Put, water overfill can be prevented and overflowed, the heat and heat-conducting plate contact, a part of heat in body fuselage are absorbed, another portion
Divide and be only absorbed by the water, if the too high generation steam of temperature, can be discharged by the through hole on fixed round platform, and then pass through venthole again
Discharge, when the water inlet end for after hours, closing water pipe, then get the outlet of water pipe, the bottom that the water in cavity passes through arc
Wall and apopore discharge water pipe, and the setting of fan housing and fan, can carry out certain radiating, the utility model makes to motor
Use convenient and swift, the cooling mechanism carried in itself by motor can be radiated, if heat is excessive, can also pass through peace
Load fishplate bar is preferably radiated, it is not necessary to if connecting plate, can also be assembled front shroud and body fuselage, very
It is convenient.
Brief description of the drawings
Fig. 1 be the utility model proposes a kind of energy-saving motor structural representation;
Fig. 2 be the utility model proposes a kind of energy-saving motor part A structural representation.
In figure:1 body fuselage, 2 front shrouds, 3 connecting plates, 4 dividing plates, 5 bearings, 6 fans, 7 rotors, 8 stator cores, 9 are determined
Round platform, 14 ball floats, 15 ventholes, 16 necks, 17 cards are fixed in sub- coiling group, 10 rotor winding groups, 11 water pipes, 12 heat-conducting plates, 13
Block.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole
Embodiment.
Reference picture 1-2, a kind of energy-saving motor, including body fuselage 1, front shroud 2 and connecting plate 3, connecting plate 3 are set
Between body fuselage 1 and front shroud 2, front shroud 2 is close to the side of connecting plate 3, connecting plate 3 close to the side of body fuselage 1
Upper and lower ends are equipped with fixture block 17, and the lateral wall of connecting plate 3 and body fuselage 1 is provided with the neck to match with fixture block 17
16, side of the front shroud 2 away from connecting plate 3 is equiped with belt pulley, and body fuselage 1 is installed in the side side wall away from front shroud 2
There is fan housing, the inside of body fuselage 1 is provided with dividing plate 4, and dividing plate 4 is equiped with fan 6, dividing plate 4 in the side side wall away from connecting plate 3
Stator core 8, stator winding group 9 and rotor 7, rotor 7 are sequentially provided with from top to bottom, from outer to inner close to the side of connecting plate 3
Both sides be provided with rotor winding group 10, the middle part of rotor 7 is provided with rotary shaft, and one end of rotary shaft is connected by bearing 5 and fan 6
Connect, the other end of rotary shaft connects through connecting plate 3 with belt pulley, and the inside of connecting plate 3 is provided with cavity, the middle part dress in cavity
Both ends provided with water pipe 11, and water pipe 11 are respectively positioned on the outside of connecting plate 3, and the madial wall of cavity is provided with heat-conducting plate 12, heat conduction
Upper side wall between plate 12 and water pipe 11 is equiped with fixed round platform 13, and ball float 14 is provided with the cavity of the fixed downside of round platform 13, and
The middle part of fixed round platform 13 is provided with through hole, and the diameter of through hole is less than the diameter of ball float 14, and the upper side wall of connecting plate 3 is provided with some
The venthole 15 connected with cavity, some apopores, the bottom wall of cavity are uniformly provided with the side wall of the water pipe 11 in cavity
For to recessed curved slot arrangement, and the junction of the bottom wall of cavity and water pipe 11 also is provided with apopore.
, can be by front shroud 2, connecting plate 3 and body fuselage 1 by the cooperation of fixture block 17 and neck 16 in the utility model
It is installed together, and can also dismantles well, the workpiece installed on body fuselage 1 and front shroud 2 works as usual, to
The water filling of water pipe 11 in connecting plate 3, water can be full of in cavity by the apopore on water pipe 11, and pass through ball float 14
With the setting of fixed round platform 13, water overfill can be prevented and overflowed, the heat and heat-conducting plate 12 in body fuselage 1 contact, one
Heat is divided to be absorbed, another part is only absorbed by the water, if the too high generation steam of temperature, can pass through the through hole on fixed round platform 13
Discharge, and then is discharged by venthole 15 again, when after hours, closing the water inlet end of water pipe 11, then get water pipe 11
Export, the water in cavity discharges water pipe 11, and the setting of fan housing and fan by the bottom wall and apopore of arc, can be to electricity
Machine carries out certain radiating.
It is described above, the only preferable embodiment of the utility model, but the scope of protection of the utility model is not
This is confined to, any one skilled in the art is in the technical scope that the utility model discloses, according to this practicality
New technical scheme and its utility model design are subject to equivalent substitution or change, should all cover in protection model of the present utility model
Within enclosing.
Claims (5)
1. a kind of energy-saving motor, including body fuselage (1), front shroud (2) and connecting plate (3), the connecting plate (3) is set
Between body fuselage (1) and front shroud (2), it is characterised in that install side of the front shroud (2) away from connecting plate (3)
There is belt pulley, the inside of the body fuselage (1) is provided with dividing plate (4), side side wall of the dividing plate (4) away from connecting plate (3)
On be equiped with fan (6), the dividing plate (4) is sequentially provided with stator iron from top to bottom, from outer to inner close to the side of connecting plate (3)
Core (8), stator winding group (9) and rotor (7), the both sides of the rotor (7) are provided with rotor winding group (10), the rotor (7)
Middle part be provided with rotary shaft, one end of the rotary shaft passes through bearing (5) and fan (6) connects, the other end of the rotary shaft
Connected through connecting plate (3) with belt pulley, the inside of the connecting plate (3) is provided with cavity, and the middle part in the cavity is equiped with
Water pipe (11), and the both ends of water pipe (11) are respectively positioned on the outside of connecting plate (3), the madial wall of the cavity is provided with heat-conducting plate
(12), the upper side wall between the heat-conducting plate (12) and water pipe (11) is equiped with fixed round platform (13), the fixed round platform (13)
Ball float (14) is provided with the cavity of downside, the upper side wall of the connecting plate (3) is provided with some ventholes (15) connected with cavity.
2. a kind of energy-saving motor according to claim 1, it is characterised in that the body fuselage (1) is away from protecgulum
Fan housing is equiped with the side side wall of plate (2).
3. a kind of energy-saving motor according to claim 1, it is characterised in that the front shroud (2) is close to connecting plate
(3) side, connecting plate (3) are equipped with fixture block (17) close to the side upper and lower ends of body fuselage (1), and connecting plate (3) and
The lateral wall of body fuselage (1) is provided with the neck (16) to match with fixture block (17).
4. a kind of energy-saving motor according to claim 1, it is characterised in that set in the middle part of the fixed round platform (13)
There is through hole, and the diameter of through hole is less than the diameter of ball float (14).
A kind of 5. energy-saving motor according to claim 1, it is characterised in that the water pipe (11) in cavity
Side wall on be uniformly provided with some apopores, the bottom wall of the cavity be to recessed curved slot arrangement, and the bottom wall of cavity with
The junction of water pipe (11) also is provided with apopore.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201720457053.5U CN206850618U (en) | 2017-04-27 | 2017-04-27 | A kind of energy-saving motor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201720457053.5U CN206850618U (en) | 2017-04-27 | 2017-04-27 | A kind of energy-saving motor |
Publications (1)
Publication Number | Publication Date |
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CN206850618U true CN206850618U (en) | 2018-01-05 |
Family
ID=60794357
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201720457053.5U Expired - Fee Related CN206850618U (en) | 2017-04-27 | 2017-04-27 | A kind of energy-saving motor |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN206850618U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108923584A (en) * | 2018-06-29 | 2018-11-30 | 安徽孟凌精密电子有限公司 | A kind of automobile micro machine of perfect heat-dissipating |
-
2017
- 2017-04-27 CN CN201720457053.5U patent/CN206850618U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108923584A (en) * | 2018-06-29 | 2018-11-30 | 安徽孟凌精密电子有限公司 | A kind of automobile micro machine of perfect heat-dissipating |
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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: 20180105 Termination date: 20190427 |