CN202550787U - Flywheel battery - Google Patents
Flywheel battery Download PDFInfo
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- CN202550787U CN202550787U CN 201120527533 CN201120527533U CN202550787U CN 202550787 U CN202550787 U CN 202550787U CN 201120527533 CN201120527533 CN 201120527533 CN 201120527533 U CN201120527533 U CN 201120527533U CN 202550787 U CN202550787 U CN 202550787U
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- flywheel
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- flying wheel
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/16—Mechanical energy storage, e.g. flywheels or pressurised fluids
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Abstract
The invention relates to a flywheel energy storage device, in particular to a flywheel battery with a rapid charging and discharging function. The flywheel battery comprises a flywheel device and a driving device which drives the flywheel to rotate. The flywheel device comprises a flywheel, a flywheel rotating shaft and magnetic suspension bearings at the two ends of the flywheel rotating shaft. The periphery of the flywheel device is provided with a vacuum enclosed hood which is in an interference fit with the magnetic suspension bearings. The flywheel is made of a magnetic material or internal magnets are fixedly arranged on the flywheel. The driving device comprises a transmission shaft and a rotor. One end of the transmission shaft is fixedly connected with the rotor, and the other end of the transmission shaft is connected with a motor or an engine. The rotor is made of the magnetic material or external magnets are arranged on the rotor. A gap is reserved between the rotor of the driving device and the flywheel device. The axis of the rotor is parallel to or overlapped with the axis of the flywheel rotating shaft. The flywheel and the rotor drive each other through a magnetic force. By the flywheel battery, energy storage capacity can be improved and service lifetime can be prolonged; and the flywheel battery is easy to produce in batches and maintain.
Description
Technical field
The utility model relates to a kind of energy accumulation device for fly wheel, relates in particular to a kind of flying wheel battery that can carry out fast charging and discharging.
Background technology
At present, mostly normal battery that uses is chemical cell in people's the productive life, and chemical cell is converted into chemical energy with electric energy and stores, and again chemical energy is reduced into electric energy output during use.Though what at present the chemical cell energy storage technology had developed is very ripe, that the chemical cell energy storage technology exists is little such as energy storage density, discharge and recharge number of times limited cause useful life short, require high drawback to the seriously polluted of environment and to working temperature.And the flywheel energy storage that utilizes physical method realization energy storage receives the extensive concern of various countries in recent years as emerging power storage method.
Flying wheel battery just has utilization as far back as ancient times in several thousand, like the base machinery of the potting in ancient times, also all use flywheel technology to modern steam engine and automobile engine.And that the notion of flywheel energy storage battery originates from the seventies in 20th century is early stage, just hopes at first it is applied on the electric automobile, but is limited to technical merit at that time, not developed.Up to the nineties in last century because the development of circuit topology thought, the extensive use of carbon fibre material, and the attention of worldwide to polluting, this novel battery high speed development of having got back demonstrates its more wide application prospect.Change the practicability product into but will flywheel be rotated stored kinetic energy, still have a lot of technological difficulties: as
1) rotary speed of flywheel must very highly just have high energy storage density and kinetic energy effect.But in air ambient, the flywheel of high speed rotating can cause high windage loss, the energy that produces when consuming the flywheel rotation greatly, and battery energy storage capacity speed little, that discharge and recharge is slow.
2) it is infeasible adopting mechanical bearing in the flying wheel battery.There is mechanical friction in mechanical bearing, and flywheel can not keep high speed rotating owing to mechanical friction always when high speed rotating, and the generation great amount of heat causes energy loss on the bearing because the mechanical friction meeting makes, and can't realize the permanently effective storage of kinetic energy.
3) dynamic balancing technique.Because the high speed rotating of flywheel and the quality of flywheel itself, the dynamic balancing technique of rotary body plays important effect to the operate as normal of flywheel.
Summary of the invention
The utility model technical problem to be solved provides a kind of capacity that strengthens Energy Storage of Flywheel Battery, improves the speed that flying wheel battery discharges and recharges, and prolongs the useful life of flying wheel battery and makes things convenient for the flying wheel battery of the use and the maintenance of flying wheel battery.
The purpose of the utility model mainly is achieved through following proposal: a kind of flying wheel battery; It comprises flywheel gear and drives the drive unit that flywheel rotates; Said flywheel gear comprises the magnetic suspension bearing at flywheel, flywheel rotating shaft, flywheel rotating shaft two ends, and the outer periphery of flywheel gear is equipped with the vacuum tightness cover, said vacuum tightness cover and magnetic suspension bearing interference fit; Said flywheel is that inner magnet is processed or on flywheel, set firmly to magnetic material; Said drive unit comprises power transmission shaft and rotor, and said power transmission shaft one end is fixedly connected with rotor, and the other end links to each other with motor or engine; Said rotor process by magnetic material or rotor on outer magnet is set; Leave the gap between the rotor of said drive unit and the flywheel gear, and the parallel axes of the axis of rotor and flywheel rotating shaft or overlap, said flywheel and rotor drive through magnetic field force each other.
Adopting the flying wheel battery of this programme, is to carry out fast charging and discharging, and its operation principle is:
Charging process: the power transmission shaft of drive unit is connected with motor.Drive motor, the then power transmission shaft of drive unit rotation is carried out high speed rotating thereby drive rotor.Since rotor process by magnetic material or rotor on outer magnet is set, flywheel is that inner magnet is processed or on flywheel, set firmly to magnetic material; Because drive unit and flywheel gear matched in clearance, the inner magnet on the outer magnet of rotor or rotor and flywheel or the flywheel is rotated through the coupling drive flywheel in magnetic field like this.When the rotary speed of the rotary speed of flywheel and the power transmission shaft of drive unit is identical, with drive unit away from flywheel gear, the flywheel of vacuum tightness cover then under the support of magnetic suspension bearing in vacuum chamber high speed rotating.Vacuum state is down because no windage loss and flywheel rotating shaft and bracing or strutting arrangement are contactless, and then to keep its kinetic energy for a long time constant for flywheel, thereby reaches the effect of energy storage, and so far flywheel energy storage is that charging process finishes.
Discharge process: the power transmission shaft of drive unit is connected with generator.This moment drive unit and flywheel gear near and to keep certain clearance, the rotary speed of rotor be zero or be lower than the rotary speed of flywheel.But because the coupling in magnetic field between the outer magnet of rotor or rotor and the inner magnet on flywheel or the flywheel; Rotary speed of rotator improves gradually, and the rotary speed of flywheel progressively reduces, to the power transmission shaft output kinetic energy; Drive generator for electricity generation, thereby realize the flywheel direct generation of electricity.So far discharge process finishes.
Owing to the vacuum tightness cover is set in the periphery of flywheel gear; So just make the parts of flywheel gear all be in the vacuum state; When flywheel carries out high speed rotating, windage loss can not occur like this, can produce higher energy storage density within a short period of time, charging rate improves greatly.When flying wheel battery discharged, because no frictional dissipation, the energy of battery storage can be fully used, and had improved the stored energy capacitance of flying wheel battery, the useful life of prolongation flying wheel battery.And the actuating force that drives flywheel is the magnetic field force between rotor and the flywheel, and it is simple in structure, is convenient to the volume production and the maintaining of flying wheel battery.
As preferably, said rotor shapes is a circular sleeve, and the cross section of said vacuum tightness cover is an annulus, and the diameter of said circular sleeve is greater than the diameter of annulus cylindrical.The diameter of circular sleeve when flywheel energy storage, can make flywheel that the effect of the rotation quickened is arranged greater than the diameter of vacuum tightness cover cross section cylindrical.
As preferably, said flywheel gear is arranged in the rotor, the axis of said flywheel rotating shaft and the dead in line of rotor, and the vacuum tightness cover of said flywheel gear and the gap of rotor are 1～10mm.Leave the gap of 1-10mm between the vacuum tightness cover of flywheel gear and the rotor, then can produce stronger magnetic field force between circular sleeve and the flywheel, realize that flywheel and rotor drive through magnetic field force each other.
As preferably, the circumferential surface of said rotor is inboard to be respectively equipped with axial outer magnet and outer magnet radially with the inboard, lower surface, and axial inner magnet and inner magnet radially are set respectively outside the flywheel circumferential surface outside and the lower surface simultaneously.On the axial inner surface of rotor and inner radial surface, outer magnet is set all, flywheel is provided with axially and inner magnet radially accordingly, and the magnetic field force between rotor and the flywheel is strengthened, and limits the axial motion of flywheel simultaneously, and flywheel is normally rotated around self axis.
As preferably, said flywheel gear is arranged at outside the circular sleeve, the axis of said flywheel rotating shaft and the parallel axes of rotor, and the vacuum tightness cover of said flywheel gear and the gap of rotor are 1～10mm.Leave the gap of 1-10mm between flywheel gear and the rotor, make between circular sleeve and the flywheel and can produce stronger magnetic field force, realize that flywheel and rotor drive through magnetic field force each other.Simultaneously flywheel gear is arranged at outside the rotor, can make drive unit can move easily with near or away from flywheel gear, carry out fast charging and discharging.When the axis of said flywheel rotating shaft simultaneously and the parallel axes of rotor are installed; The diameter of the flywheel in the vacuum sealed cover will be much smaller than the external diameter of circular sleeve, and flying wheel battery is when charging, when circular sleeve rotates with lower speed like this; Flywheel is done accelerated motion; The diameter of circular sleeve is big more, and the rotation of flywheel is fast more, and the time of flywheel charging is short more.
As preferably, be provided with axial outer magnet, the axial inner magnet of flywheel circumferential surface arranged outside outside the circumferential surface of said rotor.The circumferential surface outside of rotor is provided with axial outer magnet, the axial inner magnet of flywheel circumferential surface arranged outside.And inner magnet, outer magnet laterally arrange, and then magnetic force is the strongest between two magnets, accelerate the driving time between rotor and the flywheel, promptly accelerate the speed that discharges and recharges.
As preferably, the magnetic pole of said magnetic suspension bearing is that the paired magnetic pole of NNSS is arranged.The field structure layout is divided into two kinds of NNSS and NSNS, and for electromagnet, along with the increase of power frequency, the eddy current loss under the NNSS topology layout is less than the topology layout of NSNS.The work Control current frequency of magnetic bearing more than 10KHz, is therefore considered the influence of eddy current loss usually, and magnetic suspension bearing adopts the paired pole configuration of NNSS.Simultaneously in order to reduce the coupling effect between magnetic pole, require stator structure about, about must symmetry, number of magnetic poles is generally elected 8 multiple as.
As preferably, said axial inner magnet is permanent magnetism or soft magnetic sheet with inner magnet radially, axially outer magnet and radially outer magnet be permanent magnetism or electromagnetic material sheet.
As preferably, said vacuum tightness cover is the thin walled cavity of the non-magnetic material sealing of processing.The vacuum tightness cover is processed by non-magnetic material, can not influence the effect of magnetic field force between rotor and the flywheel.
In a word, the utility model makes that flywheel gear can produce higher energy storage density within a short period of time, charging rate improves greatly; When flying wheel battery discharged, because no frictional dissipation, the energy of battery storage can be fully used, and had improved the stored energy capacitance of flying wheel battery, the useful life of prolongation flying wheel battery; And have simple in structurely, be convenient to the volume production of flying wheel battery and the advantage of maintaining.
Description of drawings
Fig. 1 is the axial cross section sketch map of embodiment 1;
Fig. 2 is the magnetic pole layout structure of magnetic suspension bearing among the embodiment 1;
Fig. 3 is the axial cross section sketch map of embodiment 2.
Illustrate: the 1-flywheel, the rotating shaft of 2-flywheel, the 3-magnetic suspension bearing, 4-vacuum tightness cover, the axial inner magnet of 5-, 6-is inner magnet radially, the 7-power transmission shaft, the 8-rotor, the axial outer magnet of 9-, 10-is outer magnet radially.
Embodiment
Pass through embodiment below, and combine accompanying drawing, do further bright specifically the technical scheme of the utility model.
Embodiment 1:
A kind of flying wheel battery; As shown in Figure 1; Comprise flywheel gear and drive the drive unit that flywheel rotates; Said flywheel gear comprises that flywheel 1, flywheel rotating shaft 2, flywheel rotating shaft 2 two ends are used for the magnetic suspension bearing 3 of support flying wheel rotating shaft 2, and the magnetic pole of said magnetic suspension bearing 3 is that the paired magnetic pole of NNSS is arranged.As shown in Figure 2, flywheel gear also comprises the peripheral vacuum tightness cover 4 that is provided with, and vacuum tightness cover 4 is circular thin walled cavity for the cross section of the sealing that non-magnetic material is processed.Said vacuum tightness cover 4 and magnetic suspension bearing 3 interference fit, said flywheel 1 are processed for magnetic material or are set firmly inner magnet in the circumferential surface outside of flywheel 1.Because it is higher that flywheel 1 is directly processed cost by magnetic material; Therefore in the present embodiment; The circumferential surface outside that is chosen in flywheel 1 and the outside of lower surface are provided with axial inner magnet 5 and inner magnet 6 radially respectively; Said axial inner magnet 5 be permanent magnetism or soft magnetic sheet with inner magnet 6 radially, and the magnetic pole of said radially inner magnet 6 also is the paired magnetic pole layout of NNSS, and is as shown in Figure 2.Said drive unit comprises power transmission shaft 7 and rotor 8, and said power transmission shaft 7 one ends are fixedly connected with rotor 8, and the other end links to each other with motor or engine.Said rotor 8 is a circular sleeve; To process cost by permanent magnetic material higher because circular cover connects simply; Therefore in the present embodiment; In the circumferential surface inboard of circular sleeve axial outer magnet 9 is set, the inboard, lower surface is provided with radially outer magnet 10, and said axial outer magnet 9 is permanent magnetism or electromagnetic plate with outer magnet 10 radially.Said axial inner magnet and axial outer magnet 9, radially inner magnet 6 laterally arranges with outer magnet 10 radially.Said flywheel gear is arranged in the circular sleeve, the dead in line of the axis of said flywheel rotating shaft 2 and rotor 8, the vacuum tightness cover 4 of said flywheel gear and rotor 8 the gap be 5mm.
The utility model can carry out fast charging and discharging, and its operation principle is:
Charging process: the power transmission shaft 7 of drive unit is connected with motor.Drive motor, then power transmission shaft 7 rotations of drive unit are carried out high speed rotating thereby drive rotor 8.Axial outer magnet 9 and outer magnet 10 radially are set on the rotor 8; Simultaneously flywheel 1 is provided with axial inner magnet parallel with axial outer magnet 9 and outer magnet radially 10 and inner magnet 6 radially; Drive unit and flywheel gear matched in clearance; Rotor 8 rotates like this, and the coupling through magnetic field drives flywheel 1 and is rotated.When the rotary speed of the rotary speed of flywheel 1 and the power transmission shaft 7 of drive unit is identical, with drive unit away from flywheel gear, 1 on the flywheel of vacuum tightness cover 4 under the support of magnetic suspension bearing 3 in vacuum chamber high speed rotating.Vacuum state is down because no windage loss and flywheel rotating shaft 2 and bracing or strutting arrangement are contactless, and then to keep its kinetic energy for a long time constant for flywheel, thereby reaches the effect of energy storage, and so far flywheel energy storage is that charging process finishes.
Discharge process: the power transmission shaft 7 of drive unit is connected with generator.This moment drive unit and flywheel gear near and to keep certain clearance, the rotary speed of rotor 8 be zero or be lower than the rotary speed of flywheel 1.But because the coupling in magnetic field between rotor 8 and the flywheel 1, rotor 8 rotary speeies improve gradually, and the rotary speed of flywheel 1 progressively reduces, and to power transmission shaft 7 output kinetic energies, drive generator for electricity generation, thereby realize the flywheel direct generation of electricity.So far discharge process finishes.
Owing to vacuum tightness cover 4 is set in the periphery of flywheel gear; So just make the parts of flywheel gear all be in the vacuum state; When flywheel 1 carries out high speed rotating, windage loss can not occur like this, can produce higher energy storage density within a short period of time, charging rate improves greatly.When flying wheel battery discharged, because no frictional dissipation, the energy of battery storage can be fully used, and had improved the stored energy capacitance of flying wheel battery, the useful life of prolongation flying wheel battery.And the actuating force that drives flywheel 1 is the magnetic field force between rotor 8 and the flywheel 1, and it is simple in structure, is convenient to the volume production and the maintaining of flying wheel battery.
Embodiment 2:
The drive unit among embodiment 2 and the embodiment 1 and the structural similarity of flywheel gear; Its difference is; Drive unit is different with the installation site of flywheel gear, and is as shown in Figure 3, and said flywheel gear is arranged at outside the circular sleeve of rotor 8; The parallel axes of the axis of said flywheel rotating shaft 2 and rotor 8, the vacuum tightness cover 4 of said flywheel gear is 5mm with the gap of rotor 8.The fixed structure that said drive unit and flywheel gear are realized laterally arranging is for existing conventional fixed form, because of not within the protection range of the utility model, so repeat no more.
Because drive unit and flywheel gear are set up in parallel, have only rotor 8 axial outer magnets 9 parallel simultaneously, therefore in the present embodiment, do not have radially outer magnet 10 with the axial inner magnet of flywheel 1.
Flywheel gear is arranged at outside the rotor; Not only can make drive unit can move easily with near or away from flywheel gear, carry out fast charging and discharging, and; When the external diameter of the circular sleeve of drive unit diameter, when charging, can shorten the charging interval of flywheel widely much larger than flywheel.
Should be understood that embodiment only to be used to the utility model is described and be not used in the restriction the utility model scope.Should understand in addition; After the content of having read the utility model instruction; Those skilled in the art can make various changes or modification to the vacuum plant of flywheel gear or the structures such as magnetic means between flywheel rotor and the rotor, and these equivalent form of values fall within the application's appended claims institute restricted portion equally.
Claims (9)
1. flying wheel battery; It comprises flywheel gear and drives the drive unit that flywheel rotates; Said flywheel gear comprises the magnetic suspension bearing (3) at flywheel (1), flywheel rotating shaft (2), flywheel rotating shaft (2) two ends, and it is characterized in that: the outer periphery of flywheel gear is equipped with vacuum tightness cover (4), said vacuum tightness cover (4) and magnetic suspension bearing (3) interference fit; Said flywheel (1) is processed for magnetic material or on flywheel (1), is set firmly inner magnet; Said drive unit comprises power transmission shaft (7) and rotor (8), and said power transmission shaft (7) one ends are fixedly connected with rotor (8), and the other end links to each other with motor or engine; Said rotor (8) process by magnetic material or rotor (8) on outer magnet is set; Leave the gap between the rotor of said drive unit and the flywheel gear, and the parallel axes of the axis of rotor and flywheel rotating shaft or overlap, said flywheel (1) drives through magnetic field force with rotor (8) each other.
2. flying wheel battery according to claim 1 is characterized in that: said rotor (8) is shaped as circular sleeve, and the cross section of said vacuum tightness cover (4) is an annulus, and the diameter of said circular sleeve is greater than the diameter of annulus cylindrical.
3. flying wheel battery according to claim 2; It is characterized in that: said flywheel gear is arranged in the rotor (8); The dead in line of the axis of said flywheel rotating shaft (2) and rotor (8), the vacuum tightness cover (4) of said flywheel gear is 1 ~ 10mm with the gap of rotor (8).
4. flying wheel battery according to claim 3; It is characterized in that: the circumferential surface of said rotor (8) is inboard to be respectively equipped with axial outer magnet (9) and outer magnet (10) radially with the inboard, lower surface, and axial inner magnet (5) and inner magnet (6) radially are set respectively outside flywheel (1) the circumferential surface outside and the lower surface simultaneously.
5. flying wheel battery according to claim 2; It is characterized in that: said flywheel gear is arranged at outside the circular sleeve; The parallel axes of the axis of said flywheel rotating shaft (2) and rotor (8), the vacuum tightness cover (4) of said flywheel gear is 1 ~ 10mm with the gap of rotor (8).
6. flying wheel battery according to claim 5 is characterized in that: the circumferential surface outside of said rotor (8) is provided with axial outer magnet (9), the axial inner magnet of flywheel (1) circumferential surface arranged outside (5).
7. flying wheel battery according to claim 4 is characterized in that: said axial inner magnet (5) be permanent magnetism or soft magnetic sheet with inner magnet (6) radially, axial outer magnet (9) and radially outer magnet (10) be permanent magnetism or electromagnetic material sheet.
8. according to claim 1 or 3 or 5 described flying wheel batteries, it is characterized in that: the thin walled cavity of the sealing that said vacuum tightness cover (4) is processed for non-magnetic material.
9. flying wheel battery according to claim 1 is characterized in that: the magnetic pole of said magnetic suspension bearing (3) is that the paired magnetic pole of NNSS is arranged.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201120527533 CN202550787U (en) | 2011-12-16 | 2011-12-16 | Flywheel battery |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201120527533 CN202550787U (en) | 2011-12-16 | 2011-12-16 | Flywheel battery |
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| Publication Number | Publication Date |
|---|---|
| CN202550787U true CN202550787U (en) | 2012-11-21 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201120527533 Expired - Fee Related CN202550787U (en) | 2011-12-16 | 2011-12-16 | Flywheel battery |
Country Status (1)
| Country | Link |
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| CN (1) | CN202550787U (en) |
Cited By (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102420493A (en) * | 2011-12-16 | 2012-04-18 | 杭州英若飞科技有限公司 | Flywheel battery |
| CN103498771A (en) * | 2013-09-18 | 2014-01-08 | 杜文娟 | Gravity energy replenishing device depending on gravity to replenish energy of flywheel battery and application method |
| CN103498769A (en) * | 2013-09-18 | 2014-01-08 | 杜文娟 | Elasticity energy charging device for replenishing energy capacity for fly wheel battery and application method thereof |
| CN104454397A (en) * | 2013-09-18 | 2015-03-25 | 杜文娟 | Gravity-based charge device for flywheel battery |
| CN104454394A (en) * | 2013-09-18 | 2015-03-25 | 杜文娟 | Elasticity energy charging device for replenishing energy of flywheel battery |
| CN104442434A (en) * | 2013-09-18 | 2015-03-25 | 杜文娟 | Device for controlling electricity generation and supplementing flywheel battery energy by utilizing gravity |
| WO2015039543A1 (en) * | 2013-09-18 | 2015-03-26 | 柳超 | Automatic engaging/disengaging elastic force drive apparatus replenishing flywheel battery energy |
| WO2015039515A1 (en) * | 2013-09-18 | 2015-03-26 | 林磊 | Flexible energy supplement apparatus for flywheel battery, capable of being rapidly separated, and use method |
| WO2015039548A1 (en) * | 2013-09-18 | 2015-03-26 | 黄捷 | Apparatus utilizing manpower to replenish flywheel battery energy and method of use |
| WO2015039507A1 (en) * | 2013-09-18 | 2015-03-26 | 林磊 | Flexible energy supplement apparatus for flywheel battery, capable of being automatically separated |
| WO2015039533A1 (en) * | 2013-09-18 | 2015-03-26 | 柳超 | Fast engaging/disengaging manual drive apparatus replenishing flywheel battery energy and method of use |
| WO2015039528A1 (en) * | 2013-09-18 | 2015-03-26 | 黄捷 | Elastic potential energy apparatus with elastic power generation replenishing flywheel battery energy |
| WO2015039532A1 (en) * | 2013-09-18 | 2015-03-26 | 柳超 | Method of using elastic potential energy apparatus with elastic power generation replenishing flywheel battery energy |
| WO2015039535A1 (en) * | 2013-09-18 | 2015-03-26 | 柳超 | Elastic drive apparatus replenishing energy of flywheel battery and able to automatically engage and disengage and method of use |
| WO2015039525A1 (en) * | 2013-09-18 | 2015-03-26 | 柳超 | Automatic engaging/disengaging manual drive apparatus replenishing flywheel battery energy and method of use |
| CN107276366A (en) * | 2015-11-16 | 2017-10-20 | 熵零股份有限公司 | A kind of system of energy adjusting method and the application energy adjusting method |
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2011
- 2011-12-16 CN CN 201120527533 patent/CN202550787U/en not_active Expired - Fee Related
Cited By (31)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102420493A (en) * | 2011-12-16 | 2012-04-18 | 杭州英若飞科技有限公司 | Flywheel battery |
| WO2015039528A1 (en) * | 2013-09-18 | 2015-03-26 | 黄捷 | Elastic potential energy apparatus with elastic power generation replenishing flywheel battery energy |
| CN104454397A (en) * | 2013-09-18 | 2015-03-25 | 杜文娟 | Gravity-based charge device for flywheel battery |
| WO2015039532A1 (en) * | 2013-09-18 | 2015-03-26 | 柳超 | Method of using elastic potential energy apparatus with elastic power generation replenishing flywheel battery energy |
| CN104454394A (en) * | 2013-09-18 | 2015-03-25 | 杜文娟 | Elasticity energy charging device for replenishing energy of flywheel battery |
| CN104442434A (en) * | 2013-09-18 | 2015-03-25 | 杜文娟 | Device for controlling electricity generation and supplementing flywheel battery energy by utilizing gravity |
| WO2015039542A1 (en) * | 2013-09-18 | 2015-03-26 | 柳超 | Gravitational energy charging apparatus for replenishing energy in flywheel battery using gravity |
| WO2015039541A1 (en) * | 2013-09-18 | 2015-03-26 | 柳超 | Gravitational charging apparatus relying on gravitational force to replenish flywheel battery energy and method of use |
| WO2015039543A1 (en) * | 2013-09-18 | 2015-03-26 | 柳超 | Automatic engaging/disengaging elastic force drive apparatus replenishing flywheel battery energy |
| WO2015039515A1 (en) * | 2013-09-18 | 2015-03-26 | 林磊 | Flexible energy supplement apparatus for flywheel battery, capable of being rapidly separated, and use method |
| WO2015039548A1 (en) * | 2013-09-18 | 2015-03-26 | 黄捷 | Apparatus utilizing manpower to replenish flywheel battery energy and method of use |
| WO2015039507A1 (en) * | 2013-09-18 | 2015-03-26 | 林磊 | Flexible energy supplement apparatus for flywheel battery, capable of being automatically separated |
| WO2015039552A1 (en) * | 2013-09-18 | 2015-03-26 | 黄捷 | Elastic charging apparatus for replenishing flywheel battery energy |
| WO2015039533A1 (en) * | 2013-09-18 | 2015-03-26 | 柳超 | Fast engaging/disengaging manual drive apparatus replenishing flywheel battery energy and method of use |
| CN103498771A (en) * | 2013-09-18 | 2014-01-08 | 杜文娟 | Gravity energy replenishing device depending on gravity to replenish energy of flywheel battery and application method |
| CN105378274B (en) * | 2013-09-18 | 2021-05-14 | 赣州市中翔智能科技有限公司 | Gravity energy charging device for supplementing energy of flywheel battery by gravity and using method |
| CN103498769A (en) * | 2013-09-18 | 2014-01-08 | 杜文娟 | Elasticity energy charging device for replenishing energy capacity for fly wheel battery and application method thereof |
| WO2015039535A1 (en) * | 2013-09-18 | 2015-03-26 | 柳超 | Elastic drive apparatus replenishing energy of flywheel battery and able to automatically engage and disengage and method of use |
| WO2015039525A1 (en) * | 2013-09-18 | 2015-03-26 | 柳超 | Automatic engaging/disengaging manual drive apparatus replenishing flywheel battery energy and method of use |
| CN105359390A (en) * | 2013-09-18 | 2016-02-24 | 林磊 | Flexible energy supplement apparatus for flywheel battery, capable of being automatically separated |
| CN105358828A (en) * | 2013-09-18 | 2016-02-24 | 柳超 | Gravitational energy charging apparatus for replenishing energy in flywheel battery using gravity |
| CN105358823A (en) * | 2013-09-18 | 2016-02-24 | 柳超 | Elastic drive apparatus replenishing energy of flywheel battery and able to automatically engage and disengage and method of use |
| CN105359392A (en) * | 2013-09-18 | 2016-02-24 | 林磊 | Flexible energy supplement apparatus for flywheel battery, capable of being rapidly separated, and use method |
| CN105378274A (en) * | 2013-09-18 | 2016-03-02 | 柳超 | Gravitational charging apparatus relying on gravitational force to replenish flywheel battery energy and method of use |
| CN105378276A (en) * | 2013-09-18 | 2016-03-02 | 黄捷 | Apparatus utilizing manpower to replenish flywheel battery energy and method of use |
| CN105378272A (en) * | 2013-09-18 | 2016-03-02 | 黄捷 | Elastic charging apparatus for replenishing flywheel battery energy |
| CN105452654A (en) * | 2013-09-18 | 2016-03-30 | 柳超 | Automatic engaging/disengaging elastic force drive apparatus replenishing flywheel battery energy |
| WO2015039514A1 (en) * | 2013-09-18 | 2015-03-26 | 张淑萍 | Method of using elastic energy charging device for replenishing flywheel battery energy |
| CN103498771B (en) * | 2013-09-18 | 2017-12-26 | 杜文娟 | By the gravity energy charging device and application method of gravity supplement flying wheel battery energy |
| CN105378272B (en) * | 2013-09-18 | 2021-05-14 | 赣州市中翔智能科技有限公司 | Elastic energy charging device for replenishing energy of flywheel battery |
| CN107276366A (en) * | 2015-11-16 | 2017-10-20 | 熵零股份有限公司 | A kind of system of energy adjusting method and the application energy adjusting method |
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