CN209375303U - A kind of transverse flux motor of simple rotor structure - Google Patents
A kind of transverse flux motor of simple rotor structure Download PDFInfo
- Publication number
- CN209375303U CN209375303U CN201920345538.4U CN201920345538U CN209375303U CN 209375303 U CN209375303 U CN 209375303U CN 201920345538 U CN201920345538 U CN 201920345538U CN 209375303 U CN209375303 U CN 209375303U
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- China
- Prior art keywords
- set casing
- rotor structure
- fuselage cover
- pedestal
- flux motor
- 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.)
- Withdrawn - After Issue
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- 230000004907 flux Effects 0.000 title claims abstract description 22
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 35
- 230000000452 restraining effect Effects 0.000 claims abstract description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 55
- 238000003860 storage Methods 0.000 claims description 29
- 238000005192 partition Methods 0.000 claims description 14
- 230000005389 magnetism Effects 0.000 claims description 6
- 238000003466 welding Methods 0.000 claims description 6
- 239000007787 solid Substances 0.000 claims 2
- 230000000694 effects Effects 0.000 abstract description 14
- 230000017525 heat dissipation Effects 0.000 abstract description 10
- 238000012423 maintenance Methods 0.000 abstract description 5
- 239000003595 mist Substances 0.000 description 11
- 230000008859 change Effects 0.000 description 5
- 238000000034 method Methods 0.000 description 4
- 238000000889 atomisation Methods 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 230000005611 electricity Effects 0.000 description 3
- 238000011161 development Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 230000032258 transport Effects 0.000 description 1
- 238000009692 water atomization Methods 0.000 description 1
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- Iron Core Of Rotating Electric Machines (AREA)
Abstract
The utility model relates to a kind of transverse flux motors of simple rotor structure, including fuselage cover, preceding set casing, set casing and pedestal afterwards, the preceding set casing and the rear set casing are separately positioned on the fuselage cover both ends, set casing side is welded with extended loop after described, the fuselage cover is set on the extended loop, restraining position ring block is installed by bolt on the inner wall of the fuselage cover, placing groove is provided in the stop collar, rotor is provided in the placing groove, stator is equipped with by bolt in set casing after described, square pole is equipped with by bearing on the stator, coil is arranged on the square pole, the rotor side is provided with card slot, described square pole one end is fastened in the card slot, the rotor other side is equipped with shaft, placement block is equipped with by bolt on the inner wall of the extended loop, this is practical New structure is novel, and superior performance, manually adjustable output power facilitates maintenance, and heat dissipation effect is outstanding.
Description
Technical field
The utility model relates to a kind of transverse flux motors of simple rotor structure, belong to design of electrical motor technical field.
Background technique
Motor is that the core in production, conveying, transformation and the application of electric energy is set as a kind of electromechanical energy conversion device
It is standby, it is not only played an important role in national economy all trades and professions, and application in people's daily life is also increasingly wide
It is general.With electric vehicle, magnetic suspension train and naval vessel electric power push etc. high-power electricals drive technology development, people to low speed,
The requirement of high torque density, direct-driving motor is increasingly urgent to, transverse magnetic flux permanent magnet motor use unique structure, have compared with
High torque density.With the development of the relevant technologies such as correlation theory, method, material, transverse magnetic flux permanent magnet motor gradually draws
Play the extensive concern of researcher.Due to transverse magnetic flux permanent magnet motor torque density with higher, in many low speed high torques
Application field attracts attention, and is driven by electricity aspect especially suitable for means of transports such as vehicle, ships.Simultaneously relative to traditional structure electricity
Machine, transverse magnetic flux permanent magnet motor both saved material, and energy saving, therefore had important research significance.
But present transverse flux motor still remains some shortcomings, home-use motor in the utilization of real life
Output power when it is fixed, therefore require replacement motor in many cases and can just obtain desired output power, it is secondly general
Logical motor is all fixed structure, therefore needs to spend a lot of time the disassembly for completing motor when needing repairing motor, and big
Part motor is all to be radiated by the way of fan cooling to motor inside, and fan cooling effect is general, can also generate compared with
Big noise.
Therefore, for now, a kind of transverse flux motor of simple rotor structure is needed to help to solve above-mentioned ask
Topic.
Summary of the invention
The technical problems to be solved in the utility model overcomes existing defect, provides a kind of transverse magnetic of simple rotor structure
Three-way motor, can effectively solve the problems in background technique, the utility model structure novel, and superior performance is manually adjustable defeated
Power out, facilitates maintenance, and heat dissipation effect is outstanding.
In order to solve the above-mentioned technical problem, the utility model provides the following technical solution:
A kind of transverse flux motor of simple rotor structure, including fuselage cover, preceding set casing, rear set casing and pedestal,
The preceding set casing and the rear set casing are separately positioned on the fuselage cover both ends, and the rear set casing side, which is welded with, prolongs
Ring is stretched, the fuselage cover is set on the extended loop, restraining position ring block is installed by bolt on the inner wall of the fuselage cover,
It is provided with placing groove in the stop collar, rotor is provided in the placing groove, is equipped in the rear set casing by bolt
Stator is equipped with square pole by bearing on the stator, coil is arranged on the square pole, the rotor side is provided with
Card slot, described square pole one end are fastened in the card slot, and the rotor other side is equipped with shaft, the inner wall of the extended loop
It is upper that placement block is equipped with by bolt, transverse magnet one and transverse magnet two, the fuselage cover are arranged in the placement block
It is inside welded with partition, the preceding set casing is interior to be equipped with water storage ring by bolt, is equipped with atomization on the inner wall of the water storage ring
Piece, water storage ring side welding have Non-return air valve, and inner cavity is provided in the Non-return air valve, is passed through on the inner wall of the inner cavity
Spring one is welded with block, and the fuselage cover bottom is welded with pedestal, and notch is provided in the pedestal, and the pedestal card is set
In the notch, the notch two sides are provided with hole slot, and bayonet lock is arranged in the hole slot, and described bayonet lock one end is welded with
Connecting rod is arranged with spring two in the connecting rod, and described connecting rod one end is welded with pulling head, and the pulling head is arranged in institute
It states on the outside of pedestal, atomizing piece switch and connection plug is provided on the preceding set casing, the connection plug passes through electric wire and mist
Change piece switch connection, the atomizing piece switch is connect by electric wire with atomizing piece.
Furthermore, the fuselage cover side is provided with screw hole one, and the screw hole one is interior to be engaged with spiral shell by screw thread
Bar one.
Furthermore, screw hole two is provided on the preceding set casing, the screw hole two is interior to be engaged with screw rod by screw thread
Two.
Furthermore, it is provided with through-hole in the partition and the water storage ring, described shaft one end passes through described logical
Hole is arranged on the outside of the preceding set casing.
Furthermore, the partition side is bonded with spongy layer, and the spongy layer is corresponding with the Non-return air valve, institute
It states and is provided with stomata on spongy layer.
Furthermore, the pedestal two sides are provided with card slot hole, and described bayonet lock one end is fastened in the card slot hole.
Furthermore, the magnetism of the transverse magnet one and the magnetism of the transverse magnet two are different.
Furthermore, the water storage ring other end welding has water inlet pipe, is arranged with plug on the water inlet pipe.
Furthermore, the pedestal avris is provided with fixation hole, is imprinted with graduation mark on the extended loop.
Furthermore, the Non-return air valve avris is provided with air discharge duct, and the block avris is close to the air discharge duct.
The utility model the utility model has the advantages that
1, the motor magnetic circuit of the utility model is obviously shortened compared to traditional magnetic circuit, thus can increase motor use when
Efficiency, and enhance the performance of motor；
2, the utility model can be by adjusting the distance between the position change stator of rear set casing and rotor, therefore can
Change the length of magnetic circuit, so as to play the effect for adjusting output power, therefore compared to common motor, the utility model
Using more flexible；
3, in the utility model due to preceding set casing and rear set casing fuselage cover both ends are fixed on by screw rod,
And it is fixedly connected between the pedestal of fuselage cover bottom and pedestal by bayonet lock, therefore when needing repairing or replacing motor
It can be easily accomplished disassembly, therefore compared to traditional motor, the utility model can be easy to repair when damaging；
4, atomizing piece is installed due to being provided with water storage ring in preceding set casing, and in water storage ring in the utility model, because
This so as to radiate for fuselage interior, therefore can be compared at work by atomizing piece by the water atomization in water storage ring
In traditional fan cooling mode, the radiating mode effect is more preferable, and the noise generated is smaller；
5, the utility model is big in the water mist of atomization due to being bonded with spongy layer on partition when being radiated
Particle droplet can be attached on spongy layer, therefore moist spongy layer can also play heat dissipation effect, therefore heat dissipation effect is more
Add outstanding；
6, the utility model structure novel, superior performance, manually adjustable output power facilitate maintenance, and heat dissipation effect goes out
It is many.
Detailed description of the invention
Attached drawing is used to provide a further understanding of the present invention, and constitutes part of specification, practical with this
Novel embodiment is used to explain the utility model together, does not constitute limitations of the present invention.
Fig. 1 is the utility model front view.
Fig. 2 is the utility model section view.
Fig. 3 is set casing cross section view after the utility model.
Fig. 4 is the unidirectional valve head cross section view of the utility model.
Fig. 5 is the utility model pedestal top view.
Fig. 6 is set casing front view before the utility model.
Figure label: 1, fuselage cover；2, preceding set casing；3, rear set casing；4, pedestal；5, extended loop；6, stop collar；7,
Rotor；8, stator；9, bearing；10, square pole；11, coil；12, shaft；13, block is placed；14, transverse magnet one；15, laterally
Magnet two；16, partition；17, water storage ring；18, atomizing piece；19, Non-return air valve；20, spring one；21, block；22, pedestal；23,
Bayonet lock；24, connecting rod；25, spring two；26, head is pulled；27, atomizing piece switchs；28, connection plug；29, screw rod one；30, spiral shell
Bar two；31, spongy layer；32, water inlet pipe；33, plug；34, fixation hole；35, graduation mark；36, air discharge duct.
Specific embodiment
It is illustrated below in conjunction with preferred embodiment of the attached drawing to the utility model, it should be understood that described herein excellent
It selects embodiment to be only used for describing and explaining the present invention, is not used to limit the utility model.
As shown in figures 1 to 6, a kind of transverse flux motor of simple rotor structure, including fuselage cover 1, preceding set casing 2, after
Set casing 3 and pedestal 4, it is characterised in that: preceding set casing 2 and rear set casing 3 are separately positioned on 1 both ends of fuselage cover, rear fixed
3 side of shell is welded with extended loop 5, and fuselage cover 1 is set on extended loop 5, is equipped on the inner wall of fuselage cover 1 by bolt
Stop collar 6 is provided with placing groove in stop collar 6, and rotor 7 is provided in placing groove, is equipped with calmly in rear set casing 3 by bolt
Son 8 is equipped with square pole 10 by bearing 9 on stator 8, coil 11 is arranged on square pole 10,7 side of rotor is provided with card
Slot, 10 one end of square pole are fastened in card slot, and 7 other side of rotor is equipped with shaft 12, are pacified on the inner wall of extended loop 5 by bolt
Equipped with block 13 is placed, places in block 13 and be arranged with transverse magnet 1 and transverse magnet 2 15, be welded with partition in fuselage cover 1
16, preceding set casing 2 is interior to be equipped with water storage ring 17 by bolt, and atomizing piece 18, water storage ring 17 are equipped on the inner wall of water storage ring 17
Side welding has Non-return air valve 19, and inner cavity is provided in Non-return air valve 19, passes through spring 1 on the inner wall of inner cavity and is welded with gear
Block 21,1 bottom of fuselage cover are welded with pedestal 22, and notch is provided in pedestal 4, and pedestal 22 is fastened in notch, notch two sides
It is provided with hole slot, bayonet lock 23 is arranged in hole slot, 23 one end of bayonet lock is welded with connecting rod 24, is arranged with spring in connecting rod 24
2 25,24 one end of connecting rod, which is welded with, pulls head 26, and the setting of head 26 is pulled to be provided with atomization on 4 outside of pedestal, preceding set casing 2
Piece switch 27 and connection plug 28, connection plug 28 are connect by electric wire with atomizing piece switch 27, and atomizing piece switch 27 passes through electricity
Line is connect with atomizing piece 18.
1 side of fuselage cover is provided with screw hole one, and screw hole one is interior to be engaged with screw rod 1 by screw thread, therefore can facilitate
Set casing 3 after disassembly, and facilitate the exposed length for adjusting extended loop 5, to play the mesh of adjustment stator 8 and 7 spacing of rotor
's；Screw hole two is provided on preceding set casing 2, screw hole two is interior to be engaged with screw rod 2 30 by screw thread, therefore easy to disassemble preceding fixed
Shell 2, and also facilitate maintenance water storage ring 17 and Non-return air valve 19；Through-hole, shaft 12 are provided in partition 16 and water storage ring 17
One end passes through through-hole and is arranged in preceding 2 outside of set casing, which can guarantee that partition 16 and water storage ring 17 will not influence shaft 12
Normal rotation；16 side of partition is bonded with spongy layer 31, and spongy layer 31 is corresponding with Non-return air valve 19, therefore in water storage ring 17
It can be directed at 1 internal structure of fuselage cover when the interior discharge water mist by Non-return air valve 19, and spongy layer 31 can be by bulky grain
Droplet absorption, so that spongy layer 31 be made to get wet profit, further enhances heat dissipation effect, and stomata, therefore side are provided on spongy layer 31
Just water mist passes through, so as to play preferable heat dissipation effect inside fuselage cover；22 two sides of pedestal are provided with card slot hole,
23 one end of bayonet lock is fastened in card slot hole, fuselage cover can be fixed on pedestal with being fixedly connected for card slot hole by bayonet lock
It is interior；The magnetism of transverse magnet 1 and the magnetism of transverse magnet 2 15 are different, so as to achieve the effect that transverse magnet, and make
Coil and square pole drive shaft rotation；17 other end welding of water storage ring has water inlet pipe 32, and plug 33 is arranged on water inlet pipe 32,
It is filled the water by water inlet pipe into water storage ring to convenient, can guarantee the water in water storage ring shaking not using plug
It can spill；4 avris of pedestal is provided with fixation hole 34, therefore can facilitate the fixation of pedestal 4, is imprinted with scale on extended loop 5
Line 35, to facilitate distance when observing at a distance from adjustment stator is between rotor between the two；19 avris of Non-return air valve is set
It is equipped with air discharge duct 36, therefore discharge can be facilitated when water mist gradually increases, 21 avris of block is close to air discharge duct 36, therefore only
Water mist can be discharged when air pressure increases in water storage ring 17, so as to prevent the water in water storage ring 17 under normal circumstances from flowing out,
And it can prevent extraneous gas and dust from entering in water storage ring 17.
Utility model works principle: being connect by bearing 9 with stator 8 in the utility model due to 10 one end of square pole,
The other end is fastened in rotor 7, and coil 11 is arranged on square pole 10, therefore in transverse magnet 1 and transverse magnet two
Square pole 10 can be driven to rotate among 15 two opposite polarity magnets, to drive shaft 9 to rotate, when needing to adjust according to demand
When the output power of abridged edition utility model, Unscrew 1 first, therefore rear set casing 3 can be pulled out, side at this time
10 other end of shape bar can pull out partial-length out of card slot, and the distance between stator 8 and rotor 7 increase, therefore the length of magnetic circuit
Degree is also increasing, and so as to change output power, due to being imprinted with graduation mark 35 on extended loop 5, can observe scale
The length of line 35 judges pull distance, and since the length of magnetic path is affected to output power, pull distance should be shorter as far as possible,
Screw rod 1 is tightened after adjustment, when needing to use the utility model for a long time, water can be added to radiate, it is logical first
It crosses water inlet pipe 32 and injects suitable quantity of water into water storage ring 17, then stopper water inlet pipe 32 using plug 33, connection plug 28 is accessed
External power supply presses atomizing piece switch 27, therefore pass through the harmonic high frequency of atomizing piece 18 so as to provide electric energy for atomizing piece 18
Vibration, aqueous water minor structure can be broken up and generate the elegant water mist of nature, when water mist gradually increases, gas in water storage ring 17
Pressure is also gradually increasing and is entering in Non-return air valve 19, therefore block can be provided spring 1 and inwardly squeezed by air pressure, water mist
It can be escaped and enter in fuselage cover 1 from the air discharge duct 36 of 19 avris of Non-return air valve, due to being provided with through-hole on partition 16, because
This water mist can pass through through-hole and drift in fuselage cover 1, and the heat that the utility model generates can be absorbed by water mist, so as to
Heat dissipation effect is enough played, due to being bonded with spongy layer 31 on partition 16, spongy layer 31 can adsorb bulky grain droplet, from
And can play a protective role, and spongy layer 31 can also become dampness, so as to further function as heat dissipation effect,
When need repairing the utility model when, due between fuselage cover 1 and preceding set casing 2 and rear set casing 3 pass through screw rod 2 30 and
Screw rod 1 is fixedly connected, therefore is backed out screw rod 1 and screw rod 2 30 and can be removed preceding set casing 2 and rear set casing 3, will
When fuselage cover 1 is removed from pedestal 4, the pulling head 26 of two sides is pulled out simultaneously first, therefore bayonet lock 23 can be inside
Spring 2 25 is squeezed, while 23 other end of bayonet lock can be drawn into hole slot, then pulls out fuselage cover 1 upwards, this
Utility model structure novel, superior performance, manually adjustable output power facilitate maintenance, and heat dissipation effect is outstanding.
The above are the preferable embodiment of the utility model, the utility model those skilled in the art can also be to upper
It states embodiment to change and modify, therefore, the utility model is not limited to above-mentioned specific embodiment, all abilities
Field technique personnel made any conspicuous improvement, replacement or modification on the basis of the utility model belong to practical
Novel protection scope.
Claims (10)
1. a kind of transverse flux motor of simple rotor structure, including fuselage cover (1), preceding set casing (2), rear set casing (3)
With pedestal (4), it is characterised in that: the preceding set casing (2) and the rear set casing (3) are separately positioned on the fuselage cover
(1) both ends, described rear set casing (3) side are welded with extended loop (5), and the fuselage cover (1) is set in the extended loop (5)
On, restraining position ring block (6) are installed by bolt on the inner wall of the fuselage cover (1), are provided with placement in the stop collar (6)
Slot is provided with rotor (7) in the placing groove, is equipped with stator (8), the stator by bolt in set casing (3) after described
(8) it is equipped with square pole (10), is arranged with coil (11) on the square pole (10), the rotor (7) one by bearing (9) on
Side is provided with card slot, and described square pole (10) one end is fastened in the card slot, and rotor (7) other side is equipped with shaft
(12), it is equipped on the inner wall of the extended loop (5) by bolt and places block (13), be arranged with transverse direction in the placement block (13)
Magnet one (14) and transverse magnet two (15), the fuselage cover (1) is interior to be welded with partition (16), in the preceding set casing (2)
It is equipped with water storage ring (17), is equipped with atomizing piece (18) on the inner wall of the water storage ring (17), the water storage ring by bolt
(17) side welding has Non-return air valve (19), is provided with inner cavity in the Non-return air valve (19), passes through on the inner wall of the inner cavity
Spring one (20) is welded with block (21), and fuselage cover (1) bottom is welded with pedestal (22), setting in the pedestal (4)
There is notch, the pedestal (22) is fastened in the notch, and the notch two sides are provided with hole slot, are arranged in the hole slot
Bayonet lock (23), described bayonet lock (23) one end are welded with connecting rod (24), are arranged with spring two (25), institute on the connecting rod (24)
It states connecting rod (24) one end and is welded with pulling head (26), pulling head (26) setting is solid before described on the outside of the pedestal (4)
Determine to be provided with atomizing piece switch (27) and connection plug (28) on shell (2), the connection plug (28) passes through electric wire and atomizing piece
(27) connection is switched, the atomizing piece switch (27) is connect by electric wire with atomizing piece (18).
2. a kind of transverse flux motor of simple rotor structure according to claim 1, it is characterised in that: outside the fuselage
Shell (1) side is provided with screw hole one, and the screw hole one is interior to be engaged with screw rod one (29) by screw thread.
3. a kind of transverse flux motor of simple rotor structure according to claim 1, it is characterised in that: fixed before described
Screw hole two is provided on shell (2), the screw hole two is interior to be engaged with screw rod two (30) by screw thread.
4. a kind of transverse flux motor of simple rotor structure according to claim 1, it is characterised in that: the partition
(16) and in the water storage ring (17) it is provided with through-hole, described shaft (12) one end passes through the through-hole and is arranged described preceding solid
Determine on the outside of shell (2).
5. a kind of transverse flux motor of simple rotor structure according to claim 1, it is characterised in that: the partition
(16) side is bonded with spongy layer (31), and the spongy layer (31) is corresponding with the Non-return air valve (19), the spongy layer
(31) stomata is provided on.
6. a kind of transverse flux motor of simple rotor structure according to claim 1, it is characterised in that: the pedestal
(22) two sides are provided with card slot hole, and described bayonet lock (23) one end is fastened in the card slot hole.
7. a kind of transverse flux motor of simple rotor structure according to claim 1, it is characterised in that: the transverse magnetic
The magnetism of body one (14) and the magnetism of the transverse magnet two (15) are different.
8. a kind of transverse flux motor of simple rotor structure according to claim 1, it is characterised in that: the water storage ring
(17) other end welding has water inlet pipe (32), is arranged with plug (33) on the water inlet pipe (32).
9. a kind of transverse flux motor of simple rotor structure according to claim 1, it is characterised in that: the pedestal
(4) avris is provided with fixation hole (34), is imprinted with graduation mark (35) on the extended loop (5).
10. a kind of transverse flux motor of simple rotor structure according to claim 1, it is characterised in that: described unidirectional
Air valve (19) avris is provided with air discharge duct (36), and block (21) avris is close to the air discharge duct (36).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920345538.4U CN209375303U (en) | 2019-03-19 | 2019-03-19 | A kind of transverse flux motor of simple rotor structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920345538.4U CN209375303U (en) | 2019-03-19 | 2019-03-19 | A kind of transverse flux motor of simple rotor structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209375303U true CN209375303U (en) | 2019-09-10 |
Family
ID=67824168
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920345538.4U Withdrawn - After Issue CN209375303U (en) | 2019-03-19 | 2019-03-19 | A kind of transverse flux motor of simple rotor structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209375303U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109756050A (en) * | 2019-03-19 | 2019-05-14 | 苏州欧比特机械有限公司 | A kind of transverse flux motor of simple rotor structure |
-
2019
- 2019-03-19 CN CN201920345538.4U patent/CN209375303U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109756050A (en) * | 2019-03-19 | 2019-05-14 | 苏州欧比特机械有限公司 | A kind of transverse flux motor of simple rotor structure |
| CN109756050B (en) * | 2019-03-19 | 2024-04-05 | 苏州欧比特机械有限公司 | Transverse flux motor with simple rotor structure |
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| GR01 | Patent grant | ||
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| AV01 | Patent right actively abandoned | ||
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| AV01 | Patent right actively abandoned |
Granted publication date: 20190910 Effective date of abandoning: 20240405 |
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| AV01 | Patent right actively abandoned |
Granted publication date: 20190910 Effective date of abandoning: 20240405 |