CN206432809U - A kind of stable type threephase asynchronous - Google Patents
A kind of stable type threephase asynchronous Download PDFInfo
- Publication number
- CN206432809U CN206432809U CN201720166401.3U CN201720166401U CN206432809U CN 206432809 U CN206432809 U CN 206432809U CN 201720166401 U CN201720166401 U CN 201720166401U CN 206432809 U CN206432809 U CN 206432809U
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- CN
- China
- Prior art keywords
- fuselage
- head
- power transmission
- transmission shaft
- threephase asynchronous
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- 230000005540 biological transmission Effects 0.000 claims abstract description 21
- 230000002787 reinforcement Effects 0.000 claims abstract description 11
- 230000005855 radiation Effects 0.000 claims description 5
- 230000015572 biosynthetic process Effects 0.000 claims description 2
- 238000005516 engineering process Methods 0.000 abstract description 3
- 238000001149 thermolysis Methods 0.000 abstract description 3
- 230000008901 benefit Effects 0.000 abstract description 2
- 238000004804 winding Methods 0.000 description 4
- 230000005284 excitation Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 206010044565 Tremor Diseases 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
Abstract
The utility model provides a kind of stable type threephase asynchronous, belongs to motor technology field.It solves existing motor, and operationally the easy vibration of power transmission shaft causes the problem of operation stability of motor is poor.This stable type threephase asynchronous, including fuselage and the power transmission shaft being arranged in fuselage, the rear end of power transmission shaft is stretched out outside fuselage and has been fixed with the fan blade of thermolysis, the rear end of fuselage has been provided with the fan housing that protection fan blade is acted on by screw, the front end of fuselage forms the terminal pad with its integrative-structure to external expansion, the front end of fuselage is provided with head, some screws are offered on head, it is fixed between head and fuselage by hex nut in terminal pad, bearing is provided with head and power transmission shaft is passed outside head by bearing, the bottom that the both sides of head are provided with reinforcement and reinforcement is fixed with the base of integrative-structure.The utility model makes it have operation more smooth-going and the more preferable advantage of stability by being improved to its front-end architecture.
Description
Technical field
The utility model belongs to motor technology field, is related to a kind of threephase asynchronous, more particularly to a kind of stable
Type threephase asynchronous.
Background technology
Threephase motor, refers to, when the threephase stator winding of motor respectively differs 120 degree of electrical angles, be passed through three-phase alternating current
Afterwards, a rotating excitation field will be produced, the rotating excitation field cutting rotor winding, so as to produce induced-current in rotor windings, is made
The threephase asynchronous machine of motor running, the rotating speed of its rotor is less than the rotating speed of rotating excitation field, and rotor windings between magnetic field because depositing
Electromotive force and electric current are produced in relative motion, and electromagnetic torque is produced with magnetic field interaction, energy conversion is realized, with list
Phase asynchronous motor is compared, and threephase asynchronous runnability is good, and can save various materials.
Motor in life as a kind of engine convert electrical energy into mechanical energy its mainly by power transmission shaft by energy
It is transferred in working machine, both connections are typically completed by shaft coupling, the structure of current threephase asynchronous, which is mainly, determines
Rotor assembly is installed in casing, and two ends are fixed by end cap seal, and base is arranged at below casing, though this motor
Right structure is relatively easy, but operationally power transmission shaft easily trembles motor, causes the operation stability of motor poor.
The content of the invention
The purpose of this utility model is that there is provided a kind of stability is more preferable for the above-mentioned problems in the prior art
Threephase asynchronous.
The purpose of this utility model can be realized by following technical proposal：A kind of stable type threephase asynchronous, bag
Include fuselage and the power transmission shaft being arranged in fuselage, the fuselage is internally provided with rotor component, the rear end of the power transmission shaft
The fan blade of thermolysis is stretched out outside fuselage and has been fixed with, the rear end of the fuselage has been provided with protection fan blade by screw and acted on
Fan housing, it is characterised in that the front end of the fuselage is to external expansion formation and the terminal pad of its integrative-structure, before the fuselage
End, which is provided with head, described head, offers some screws, is connected between described head and fuselage by hex nut
In in terminal pad, bearing being provided with described head and power transmission shaft is passed outside head by bearing, the both sides of the head are set
The bottom for being equipped with reinforcement and reinforcement is fixed with the base of integrative-structure.
The technique effect of this stable type threephase asynchronous is：Head is fixed with the front end of fuselage, relative to tradition
Motor directly by end cap seal, can effectively reduce the vibration in the running of power transmission shaft, and head both sides are set
There is reinforcement, the base of motor is located at below head, makes head after motor installation more firm, further increase electricity
The ride comfort of motivation operation.
Further, screw is opened up on the head of this threephase asynchronous, hex nut is from the rear end of fuselage toward front end
Stretch into screw to fix head, because working machine is located in front of motor after motor installation, have impact on stretching for screwdriver
Enter, the structure can be effectively increased the space in front of nut, be more prone to the dismounting of head, the dimension in convenient motor later stage
Repair.
In above-mentioned stable type threephase asynchronous, the outer surface of the fuselage is horizontally disposed to have some rows mutually to put down
Capable radiation tooth.
In above-mentioned stable type threephase asynchronous, the side of the fuselage is provided with terminal box.
In above-mentioned stable type threephase asynchronous, mounting hole is offered on described base.
In above-mentioned stable type threephase asynchronous, the front end of the power transmission shaft is provided with flat key.
Compared with prior art, this threephase asynchronous makes it have operation more by being improved to its front-end architecture
Plus smooth-going and the more preferable advantage of stability.
Brief description of the drawings
Fig. 1 is the structural representation of this threephase asynchronous.
In figure, 1, fuselage；2nd, power transmission shaft；3rd, fan housing；4th, terminal pad；5th, head；6th, screw；7th, reinforcement；8th, base；9、
Radiation tooth；10th, terminal box；11st, mounting hole；12nd, flat key.
Embodiment
The following is specific embodiment of the utility model and with reference to accompanying drawing, further is made to the technical solution of the utility model
Description, but the utility model is not limited to these embodiments.
As shown in figure 1, this stable type threephase asynchronous, including fuselage 1 and the power transmission shaft 2 being arranged in fuselage 1, machine
The fan blade for being internally provided with outside rotor component, the rear end stretching fuselage 1 of power transmission shaft 2 and being fixed with thermolysis of body 1, machine
The rear end of body 1 has been provided with the fan housing 3 that protection fan blade is acted on by screw, and the front end of fuselage 1 is formed and its one to external expansion
The terminal pad 4 of structure, the front end of fuselage 1, which is provided with head 5, head 5, offers some screws 6, between head 5 and fuselage 1
It is fixed on by hex nut in terminal pad 4, bearing is provided with head 5 and power transmission shaft 2 is passed outside head 5 by bearing, machine
The bottom that first 5 both sides are provided with reinforcement 7 and reinforcement 7 is fixed with the base 8 of integrative-structure.
Further describe in detail, in order to increase the radiating effect of motor, the outer surface of fuselage 1 is horizontally disposed there are some rows mutual
Parallel radiation tooth 9, the side of fuselage 1, which is provided with terminal box 10, base 8, offers mounting hole 11, and the front end of power transmission shaft 2 is set
It is equipped with flat key 12.
Specific embodiment described herein is only to the utility model spirit explanation for example.The utility model institute
Category those skilled in the art can make various modifications or supplement or using similar to described specific embodiment
Mode substitute, but without departing from spirit of the present utility model or surmount scope defined in appended claims.
Although more used herein fuselage 1, power transmission shaft 2, fan housing 3, terminal pad 4, head 5, screw 6, reinforcement 7,
The terms such as base 8, radiation tooth 9, terminal box 10, mounting hole 11, flat key 12, but it is not precluded from the possibility using other terms.
It is used for the purpose of more easily describing and explaining essence of the present utility model using these terms；It is construed as any one
Additional limitation is all disagreed with the utility model spirit.
Claims (5)
1. a kind of stable type threephase asynchronous, including fuselage（1）Be arranged in fuselage（1）Interior power transmission shaft（2）, the machine
Body（1）Be internally provided with rotor component, the power transmission shaft（2）Rear end stretch out fuselage（1）It is outer and be fixed with radiating work
Fan blade, the fuselage（1）Rear end by screw be provided with protection fan blade act on fan housing（3）, it is characterised in that institute
State fuselage（1）Front end to external expansion formation and the terminal pad of its integrative-structure（4）, the fuselage（1）Front end set it is organic
Head（5）, described head（5）On offer some screws（6）, described head（5）With fuselage（1）Between pass through hex nut
It is fixed on terminal pad（4）On, described head（5）Inside it is provided with bearing and power transmission shaft（2）Head is passed by bearing（5）Outside,
The head（5）Both sides be provided with reinforcement（7）And reinforcement（7）Bottom be fixed with the base of integrative-structure（8）.
2. a kind of stable type threephase asynchronous according to claim 1, it is characterised in that the fuselage（1）It is outer
Surface is horizontally disposed the radiation tooth that some rows are parallel to each other（9）.
3. a kind of stable type threephase asynchronous according to claim 1 or 2, it is characterised in that the fuselage（1）'s
Side is provided with terminal box（10）.
4. a kind of stable type threephase asynchronous according to claim 1, it is characterised in that described base（8）On
Offer mounting hole（11）.
5. a kind of stable type threephase asynchronous according to claim 1, it is characterised in that the power transmission shaft（2）'s
Front end is provided with flat key（12）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720166401.3U CN206432809U (en) | 2017-02-23 | 2017-02-23 | A kind of stable type threephase asynchronous |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720166401.3U CN206432809U (en) | 2017-02-23 | 2017-02-23 | A kind of stable type threephase asynchronous |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206432809U true CN206432809U (en) | 2017-08-22 |
Family
ID=59590199
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720166401.3U Expired - Fee Related CN206432809U (en) | 2017-02-23 | 2017-02-23 | A kind of stable type threephase asynchronous |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206432809U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107659044A (en) * | 2017-10-31 | 2018-02-02 | 方大电机股份有限公司 | A kind of motor rotating shaft |
-
2017
- 2017-02-23 CN CN201720166401.3U patent/CN206432809U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107659044A (en) * | 2017-10-31 | 2018-02-02 | 方大电机股份有限公司 | A kind of motor rotating shaft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder | ||
| CP01 | Change in the name or title of a patent holder |
Address after: The town of Wenling City Industrial Park, Taizhou City, Zhejiang province 317500 Patentee after: FANGDA ELECTRIC MACHINE CO.,LTD. Address before: The town of Wenling City Industrial Park, Taizhou City, Zhejiang province 317500 Patentee before: FANGDA ELECTRIC MOTOR Co.,Ltd. |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Stable form three -phase asynchronous motor Effective date of registration: 20181109 Granted publication date: 20170822 Pledgee: Zhejiang Tyrone commercial bank Limited by Share Ltd. Taizhou Wenling branch Pledgor: FANGDA ELECTRIC MACHINE CO.,LTD. Registration number: 2018330000377 |
|
| 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: 20170822 |