CN109921567A - A kind of large synchronous compensator rotor rotation formula air-makeup system - Google Patents
A kind of large synchronous compensator rotor rotation formula air-makeup system Download PDFInfo
- Publication number
- CN109921567A CN109921567A CN201910371688.7A CN201910371688A CN109921567A CN 109921567 A CN109921567 A CN 109921567A CN 201910371688 A CN201910371688 A CN 201910371688A CN 109921567 A CN109921567 A CN 109921567A
- Authority
- CN
- China
- Prior art keywords
- air
- wind
- slot
- fan
- rotor
- 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.)
- Granted
Links
Landscapes
- Motor Or Generator Cooling System (AREA)
Abstract
A kind of large synchronous compensator rotor rotation formula air-makeup system, belongs to technical field of motors.The rotor heating when present invention is in order to solve the problems, such as that phase modifier is encouraged by force in extra-high voltage DC transmission system, it is proposed supplementary air type cooling structure, it is adequately cooled rotor, rotor tip installation is centrifugal to suppress fan and axial-flow type induced draught fan, secondary slot and outlet air pair slot are entered the wind in rotor setting, the radial passage for entering the wind secondary slot and outlet air pair slot wind path docking is realized by the ox horn formula air duct in suspension type cooler, the gas for entering the wind secondary slot radial passage output is exported by ox horn formula air duct to outlet air pair slot radial passage, it plays rotation formula and supplements cold wind action in ox horn formula air duct, it realizes directly cooling to outlet air pair slot hot wind, improve rotor-side cooling effect, suspension type cooler is directly connected to external cooler, phase modifier rotor rotation formula air-makeup system proposed by the present invention enhances the cooling effect of phase modulation machine rotor and excitation winding, Structure is simple, is easy to implement.
Description
Technical field
The present invention relates to a kind of synchronous capacitor rotor air-makeup systems, and in particular to a kind of large synchronous compensator rotor wheel
Formula air-makeup system is changed, technical field of motors is belonged to.
Background technique
System for ultra-high voltage transmission large synchronous compensator has fast dynamic response ability and encourages ability, excitation voltage by force
Up to 3.5 times of rated values, encouraging electric current by force is 2.5 times of rated exciting currents；In addition, the phase modifier of ultra-high voltage converter station requires motor mistake
Loading capability is higher than non-salient pole alternator technical requirements and provides motor overload ability, far more than international standard；Therefore, it is necessary to optimize
Rotor cooling structure promotes its overload capacity, guarantees that phase modifier winding will not generate harmful deformation, control end construction temperature rise exists
Zone of reasonableness is most important.
The progress of large synchronous compensator rotor ventilation system cooling technology, to the specific important meaning of extra-high voltage direct-current transmission
Justice.But in the prior art, due to large synchronous compensator Design of ventilation it is unreasonable caused by motor encourage by force and quickly dynamic
The excessively high problem of rotor-side temperature still remains in adjustment process.
Summary of the invention
It has been given below about brief overview of the invention, in order to provide about the basic of certain aspects of the invention
Understand.It should be appreciated that this summary is not an exhaustive overview of the invention.It is not intended to determine pass of the invention
Key or pith, nor is it intended to limit the scope of the present invention.Its purpose only provides certain concepts in simplified form,
Taking this as a prelude to a more detailed description discussed later.
In consideration of it, the invention proposes it is a kind of efficiently, reduce rapidly large-scale phase modifier rotor-side temperature rise rotation formula and mend wind system
System, to solve since motor is encouraged by force and quickly in Dynamic Regulating Process caused by large synchronous compensator Design of ventilation is unreasonable
The excessively high problem of rotor-side temperature, is adequately cooled rotor, and rotor tip installation is centrifugal to suppress fan and axis
Secondary slot and outlet air pair slot are entered the wind in streaming induced draught fan, rotor setting, and the radial passage for entering the wind secondary slot and outlet air pair slot passes through suspension
Wind path docking is realized in ox horn formula air duct in formula cooler, and the gas for entering the wind secondary slot radial passage output is passed through ox horn formula air duct
To outlet air pair slot radial passage, ox horn formula air duct plays rotation formula and supplements cold wind action for output, realizes to outlet air pair slot heat
Wind is directly cooling, improves rotor-side cooling effect.
The technological means that the present invention takes is:
A kind of large synchronous compensator rotor rotation formula air-makeup system, including stator core, shaft, centrifugal suppress wind
Fan, external cooler, End winding, out frame and rotor end bell, the stator core are mounted in out frame, shaft peace
In stator core, and air gap is constituted between the two, rotor bushing retaining ring in shaft, End winding is installed on stator core
On, external cooler is installed on the outside of out frame；
The rotation formula air-makeup system further includes that suspension type cooler, axial-flow type induced draught fan, linker and fan keep out the wind
Ring is equipped in shaft and centrifugal suppresses fan, axial-flow type induced draught fan and fan air baffle ring, axial-flow type induced draught fan quilt cover
Inside fan air baffle ring, the centrifugal outside suppressed fan and be placed in fan air baffle ring, suspension type cooler is placed in stator core
In air gap between shaft, suspension type cooler is directly connected to the external cooler of stator core by linker；
The secondary slot of air inlet and outlet air pair slot are offered in shaft, are entered the wind secondary slot and are not connected in shaft with outlet air pair slot, enter the wind
Secondary slot includes entering the wind secondary slot axial ducts and entering the wind secondary slot radial passage, and outlet air pair slot includes outlet air pair slot axial ducts and outlet air
Secondary slot radial passage enters the wind secondary slot axial ducts and is connected with secondary slot radial passage is entered the wind, outlet air pair slot axial ducts and outlet air
Secondary slot radial passage is connected, and stator radial ducts is offered in stator core, ox horn formula wind is arranged in suspension type cooler
Secondary slot radial passage is entered the wind in road, the cooling medium in outlet air pair slot radial passage passes through ox horn formula air duct in suspension type cooler
Forming circuit, centrifugal to suppress fan cooling wind is partially pressed into motor different piece, cooling gas flows to End winding all the way, cold
But gas enters external cooler after flowing into the stator radial ducts of stator core on the outside of the suspension type cooler；Another way is cold
But secondary slot axial ducts are entered the wind in gas flow, and cooling gas is sucked out axial-flow type induced draught fan by outlet air pair slot axial ducts, from
The cooling wind that core type suppresses fan extrusion is isolated with the cooling wind that axial-flow type induced draught fan is sucked out by fan air baffle ring.
Further: the suspension type cooler is thin core structure, and the inlet air open area in ox horn formula air duct is greater than
Vent area is entered the wind secondary slot radial passage and is aligned with the air intake vent in ox horn formula air duct, outlet air pair slot radial passage and ox horn formula wind
The air outlet in road is aligned.Cooling gas by enter the wind secondary slot axial ducts through air inlet secondary slot radial passage directly by hot wind get rid of into
The air intake vent in the ox horn formula air duct of suspension type cooler, hot wind is after suspension type cooler is cooling, from suspension type cooler
The air outlet in ox horn formula air duct flows out, and the cold wind of outflow enters back into outlet air pair slot radial passage, cools down to rotor, most pass through afterwards
The outflow of outlet air pair slot axial ducts, axially, hot wind is directly cooling by suspension type cooler in ox horn formula air duct,
Cold wind after cooling is constantly thrown out of, and the cold wind thrown away is directly added into shaft side, and cooling gas is continuous in shaft side
Rotation circulation, without stator core, directly the cooling gas between stator core and shaft is isolated for suspension type cooler, fixed
Sub- iron core and shaft do not have the direct exchange of cooling gas.
Further: entering the wind secondary slot axial ducts and become narrow gradually along axial direction, outlet air pair slot axial ducts gradually become along axial direction
It is wide.
Further: ox horn formula air duct is 30-40 along axial quantity.
Further: convex lug is arranged in ox horn formula air duct inner wall in the suspension type cooler.
Further: the rotation formula air-makeup system further includes air gap air baffle ring, and air gap air baffle ring is mounted on rotor end bell
On.Air gap air baffle ring is hindered from the centrifugal stator radial direction for suppressing fan and pressing toward suspension type cooler outside and flowing into stator core
Ventilating duct cooling gas is diverted to the outer surface of shaft.
Present invention effect achieved are as follows:
Large-scale phase modifier is encouraging by force the ventilation cooling system relatively high, traditional with fast dynamic response process temperature of rotor
Seriously limit the safe and stable operation of large-scale phase modifier, the progress of large synchronous compensator rotor ventilation system cooling technology,
To the specific important meaning of extra-high voltage direct-current transmission.Therefore, the present invention is logical towards UHV Transmission Engineering phase modulation machine rotor
Air cooling system there are the problem of and a kind of large synchronous compensator rotor rotation formula air-makeup system for proposing, obtain rotor
To sufficient cooling, rotor tip installation is centrifugal to suppress fan and axial-flow type induced draught fan, and rotor setting is entered the wind secondary slot and gone out
Wind path pair is realized by the ox horn formula air duct in suspension type cooler in wind pair slot, the radial passage for entering the wind secondary slot and outlet air pair slot
It connects, the gas for entering the wind secondary slot radial passage output is exported by ox horn formula air duct to outlet air pair slot radial passage, ox horn formula wind
Road plays rotation formula and supplements cold wind action, realizes that large-scale phase modulation machine rotor throws away hot wind and is rapidly cooled, and in time as cold
Wind fills into rotor again, effectively enhances the ability that cooling gas takes away phase modifier rotor-side heat, reduces phase modifier quick
Dynamic response and the by force maximum temperature of rotor and excitation winding when encouraging, reduce phase modifier rotor-side thermal deformation, improve rotor-side
Cooling effect.
Detailed description of the invention
Fig. 1 is a kind of axial sectional view of large synchronous compensator rotor rotation formula air-makeup system of the present invention；
Fig. 2 is ox horn formula air channel structure schematic diagram；
In figure: the secondary slot of 1- air inlet, 2- outlet air pair slot, 3- suspension type cooler, 4- stator core, 5- shaft, 6- are centrifugal
Suppress fan, 7- axial-flow type induced draught fan, 8- external cooler, 9- linker, 10- End winding, 11- stator radial ventilation
Road, 12- air gap, 13- fan air baffle ring, 14- air gap air baffle ring, 15- out frame, 16- rotor end bell, 1- enter the wind secondary slot, 1-1
Enter the wind secondary slot axial ducts, 1-2 enters the wind secondary slot radial passage, 2- outlet air pair slot, 2-1 outlet air pair slot axial ducts, 2-2 outlet air pair
Slot radial passage；
Arrow show a kind of flowing side of cooling gas in large synchronous compensator rotor rotation formula air-makeup system in figure
To.
Specific embodiment
For clarity and conciseness, all features of actual implementation mode are not described in the description.However, should
Understand, much decisions specific to embodiment must be made, during developing any this practical embodiments so as to reality
The objectives of existing developer, for example, meeting restrictive condition those of related to system and business, and these restrictive conditions
It may be changed with the difference of embodiment.In addition, it will also be appreciated that although development is likely to be very multiple
It is miscellaneous and time-consuming, but for the those skilled in the art for having benefited from the disclosure of invention, this development is only example
Capable task.
Here, also it should be noted is that, in order to avoid having obscured the present invention because of unnecessary details, applying for text
Illustrate only in part with closely related apparatus structure and/or processing step according to the solution of the present invention, and be omitted and this
The little other details of inventive relationship.
Embodiment: referring to Fig. 1 and Fig. 2, a kind of large synchronous compensator rotor rotation formula air-makeup system of present embodiment
Including entering the wind secondary slot 1, outlet air pair slot 2, suspension type cooler 3, stator core 4, shaft 5, centrifugal suppressing fan 6, axial-flow type
Induced draught fan 7, external cooler 8, linker 9, End winding 10, stator radial ducts 11, air gap 12, fan air baffle ring
13, air gap air baffle ring 14, out frame 15, rotor end bell 16, entering the wind secondary slot 1 includes entering the wind secondary slot axial ducts 1-1, and air inlet is secondary
Slot radial passage 1-2, outlet air pair slot 2 include outlet air pair slot axial ducts 2-1, outlet air pair slot radial passage 2-2, enter the wind secondary fluted shaft
It is connected to air duct 1-1 with air inlet pair slot radial passage 1-2, outlet air pair slot axial ducts 2-1 and outlet air pair slot radial passage 2-2
It is connected, enters the wind secondary slot 1 and be not connected in shaft with outlet air pair slot 2, fan air baffle ring 13 is installed, axial-flow type is inhaled in shaft 5
Wind fan 7 is enclosed in inside fan air baffle ring 13, and air gap air baffle ring 14 is mounted on rotor end bell 16；Stator core 4 is mounted on
In out frame 15, stator radial ducts 11 is connected with external cooler 8.
In addition, embodiment is described with reference to Fig. 1 according to a kind of implementation, a kind of large size described in present embodiment
Synchronous capacitor rotor rotation formula air-makeup system, it is centrifugal suppress fan 6 by cooling wind be divided into multichannel indentation motor different piece,
Cooling gas flows to End winding 10 all the way, and cooling gas flow direction enters the wind secondary slot 1 all the way, and cooling gas is cooling in suspension type all the way
On the outside of device 3 flow into stator core 4 stator radial ducts 11, axial-flow type induced draught fan 7 by the cooling gas of outlet air pair slot 2 from
Outlet air pair slot axial ducts 2-1 is sucked out, and the centrifugal cooling wind for suppressing the extrusion of fan 6 is sucked out cold with axial-flow type induced draught fan 7
But wind is isolated by fan air baffle ring 13.
In addition, embodiment is described with reference to Fig. 1 according to a kind of implementation, a kind of large size described in present embodiment
Synchronous capacitor rotor rotation formula air-makeup system enters the wind the physically barrier completely in shaft 4 of secondary slot 1 and outlet air pair slot 2,
It enters the wind secondary slot 1 and outlet air pair slot is non-interconnected structure, internal cooling gas is the ox horn formula air duct by suspension type cooler 3
3-1 realizes the connection of cooling circulation, and air inlet pair slot axial ducts 1-1 becomes narrow gradually along axial direction, outlet air pair slot axial ducts 2-
1 gradually broadens along axial direction.
In addition, illustrating present embodiment, one kind described in present embodiment in conjunction with Fig. 1, Fig. 2 according to a kind of implementation
Large synchronous compensator rotor rotation formula air-makeup system, suspension type cooler 3 be thin core structure, suspension type cooler 3 as
In air gap 12 between stator core 4 and shaft 5, ox horn formula air duct 3-1 is set in suspension type cooler 3, it is radial to enter the wind secondary slot
Cooling medium in air duct 1-2, outlet air pair slot radial passage 2-2 is formed back by ox horn formula air duct 3-1 in suspension type cooler 3
Road, cooling gas are directly got rid of hot wind into suspension type by air inlet pair slot radial passage 1-2 by air inlet pair slot axial ducts 1-1
The air intake vent 3-1-1 of 3 ox horn formula air duct 3-1 of cooler, hot wind is after suspension type cooler 3 is cooling, from suspension type cooler 3
The air outlet 3-1-2 of ox horn formula air duct 3-1 flows out, and the cold wind of outflow enters back into outlet air pair slot radial passage 2-2, carries out to rotor
It is cooling, it is most flowed out afterwards through outlet air pair slot axial ducts 2-1, axially, hot wind passes through suspension in ox horn formula air duct 3-1
Formula cooler 3 is directly cooling, and cold wind after cooling is constantly thrown out of, and the cold wind thrown away is directly added into 5 side of shaft, and cooling
Gas is in the continuous rotation circulation in 5 side of shaft, and without stator core 4, suspension type cooler 3 directly by stator core 4 and turns
Cooling gas isolation between axis 5, the direct exchange of the not no cooling gas of stator core 4 and shaft 5.
In addition, illustrating present embodiment, one kind described in present embodiment in conjunction with Fig. 1, Fig. 2 according to a kind of implementation
Large synchronous compensator rotor rotation formula air-makeup system, ox horn formula air duct 3-1 air intake vent 3-1-1 area are greater than air outlet 3-1-2
Area is 30-40 along axial quantity, and air inlet pair slot radial passage 1-2 is aligned with ox horn formula air duct 3-1 air intake vent 3-1-1, goes out
Wind pair slot radial passage 2-2 is aligned with ox horn formula air duct 3-1 air outlet 3-1-2.
In addition, illustrating present embodiment, one kind described in present embodiment in conjunction with Fig. 1, Fig. 2 according to a kind of implementation
Large synchronous compensator rotor rotation formula air-makeup system, convex lug 3- is arranged in ox horn formula air duct 3-1 inner wall in suspension type cooler 3
2, suspension type cooler 3 is directly connected to the external cooler 8 of stator core by linker 9.
In addition, embodiment is described with reference to Fig. 1 according to a kind of implementation, a kind of large size described in present embodiment
Synchronous capacitor rotor rotation formula air-makeup system, air gap air baffle ring 14 hinder to be pressed from centrifugal fan 6 of suppressing toward suspension type cooling
The outside of device 3 and 11 cooling gas of stator radial ducts for flowing into stator core 4 is diverted to the outer surface of shaft 5.
Although disclosed embodiment is as above, its content is only to facilitate understand technical side of the invention
Case and the embodiment used, are not intended to limit the present invention.Any those skilled in the art to which this invention pertains, not
Under the premise of being detached from disclosed core technology scheme, any modification and change can be made in form and details in implementation
Change, but protection scope defined by the present invention, the range that the appended claims that must still be subject to limits.
Claims (6)
1. a kind of large synchronous compensator rotor rotation formula air-makeup system, including stator core (4), shaft (5), centrifugal suppress
Fan (6), external cooler (8), End winding (10), out frame (15) and rotor end bell (16), the stator core (4)
It is mounted in out frame (15), shaft (5) is mounted in stator core (4), and constitutes air gap (12) between the two, shaft
(5) rotor bushing retaining ring (16) on, End winding (10) are installed on stator core (4), and external cooler (8) is installed on stator
The outside of base (15)；
It is characterized by: the rotation formula air-makeup system further includes suspension type cooler (3), axial-flow type induced draught fan (7), connection
Device (9) and fan air baffle ring (13), be equipped on shaft (5) it is centrifugal suppress fan (6), axial-flow type induced draught fan (7) and
Fan air baffle ring (13), axial-flow type induced draught fan (7) are enclosed in fan air baffle ring (13) inside, and centrifugal fan (6) of suppressing is set
In the outside of fan air baffle ring (13), suspension type cooler (3) is placed in the air gap (12) between stator core (4) and shaft (5)
In, suspension type cooler (3) is directly connected to the external cooler (8) of stator core (4) by linker (9)；
The secondary slot (1) of air inlet and outlet air pair slot (2) are offered in shaft (5), enter the wind secondary slot (1) and outlet air pair slot (2) in shaft
It is not connected to, enters the wind secondary slot (1) including entering the wind secondary slot axial ducts (1-1) and entering the wind secondary slot radial passage (1-2), outlet air pair slot
(2) include outlet air pair slot axial ducts (2-1) and outlet air pair slot radial passage (2-2), enter the wind secondary slot axial ducts (1-1) and into
Wind pair slot radial passage (1-2) is connected, and outlet air pair slot axial ducts (2-1) are connected with outlet air pair slot radial passage (2-2),
It is offered in stator core (4) stator radial ducts (11), ox horn formula air duct (3-1) is set in suspension type cooler (3), into
Cooling medium in wind pair slot radial passage (1-2), outlet air pair slot radial passage (2-2) passes through suspension type cooler (3) interior ox
Angie type air duct (3-1) forming circuit, centrifugal to suppress fan (6) cooling wind is partially pressed into motor different piece, cooling air all the way
Body flows to End winding (10), and cooling gas flows into the stator radial ventilation of stator core (4) on the outside of suspension type cooler (3)
Road (11) enters external cooler (8) afterwards；Another way cooling gas flow direction enters the wind secondary slot axial ducts (1-1), axial-flow type air draught
Fan (7) by cooling gas by outlet air pair slot axial ducts (2-1) be sucked out, it is centrifugal suppress fan (6) extrusion cooling wind with
The cooling wind that axial-flow type induced draught fan (7) is sucked out is isolated by fan air baffle ring (13).
2. a kind of large synchronous compensator rotor rotation formula air-makeup system according to claim 1, it is characterised in that: described
Suspension type cooler (3) be thin core structure, air intake vent (3-1-1) area in ox horn formula air duct (3-1) is greater than air outlet (3-
1-2) area is entered the wind secondary slot radial passage (1-2) and is aligned with the air intake vent (3-1-1) in ox horn formula air duct (3-1), outlet air pair slot diameter
It is aligned to air duct (2-2) with the air outlet (3-1-2) in ox horn formula air duct (3-1).
3. a kind of large synchronous compensator rotor rotation formula air-makeup system according to claim 2, it is characterised in that: air inlet
Secondary slot axial ducts (1-1) become narrow gradually along axial direction, and outlet air pair slot axial ducts (2-1) gradually broaden along axial direction.
4. a kind of large synchronous compensator rotor rotation formula air-makeup system according to claim 3, it is characterised in that: ox horn
Formula air duct (3-1) is 30-40 along axial quantity.
5. a kind of large synchronous compensator rotor rotation formula air-makeup system according to claim 4, it is characterised in that: described
Convex lug (3-2) is arranged in suspension type cooler (3) interior ox horn formula air duct (3-1) inner wall.
6. a kind of -5 any large synchronous compensator rotor rotation formula air-makeup system, feature exist according to claim 1
In: the rotation formula air-makeup system further includes air gap air baffle ring (14), and air gap air baffle ring (14) is mounted on rotor end bell (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910371688.7A CN109921567B (en) | 2019-05-06 | 2019-05-06 | Rotor alternate type air supplement system of large synchronous phase modulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910371688.7A CN109921567B (en) | 2019-05-06 | 2019-05-06 | Rotor alternate type air supplement system of large synchronous phase modulator |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109921567A true CN109921567A (en) | 2019-06-21 |
| CN109921567B CN109921567B (en) | 2019-12-24 |
Family
ID=66979069
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910371688.7A Expired - Fee Related CN109921567B (en) | 2019-05-06 | 2019-05-06 | Rotor alternate type air supplement system of large synchronous phase modulator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109921567B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111046539A (en) * | 2019-11-27 | 2020-04-21 | 上海电气电站设备有限公司 | Water-cooled rotor forced excitation temperature rise calculation method based on instantaneous movement method |
Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS59175353A (en) * | 1983-03-23 | 1984-10-04 | Yaskawa Electric Mfg Co Ltd | Cooler of rotary electric machine |
| CN2560151Y (en) * | 2002-01-10 | 2003-07-09 | 武汉三维汽轮电机股份有限公司 | Large indoor cooled steam turbogenerator cooling structure |
| CN101123380A (en) * | 2007-05-25 | 2008-02-13 | 中国科学院电工研究所 | Steamship generator with rotor free cooling and stator evaporation cooling |
| CN202183689U (en) * | 2011-07-30 | 2012-04-04 | 南阳防爆集团股份有限公司 | Internal wind path structure for 2-pole motor |
| CN102983678A (en) * | 2012-11-14 | 2013-03-20 | 哈尔滨电机厂有限责任公司 | Electric generator cooling wind path structure |
| CN103023217A (en) * | 2012-12-18 | 2013-04-03 | 上海电机学院 | Overall machine wind path structure of high-power and high-peed permanent magnet synchronous motor |
| CN203387357U (en) * | 2013-07-31 | 2014-01-08 | 广东鸿源众力发电设备有限公司 | Centralized open ventilation and cooling system of bulb through-flow type hydraulic turbine generator |
| CN206542299U (en) * | 2016-12-22 | 2017-10-03 | 哈尔滨理工大学 | A kind of compact medium-sized high pressure motor of novel cooling structure |
| CN207559750U (en) * | 2017-10-25 | 2018-06-29 | 石家庄金士顿轴承科技有限公司 | A kind of high-speed permanent magnet motor direct connection centrifugal blower heat sink |
| CN108429403A (en) * | 2018-05-21 | 2018-08-21 | 广东上水能源科技有限公司 | A kind of motor based on coolant liquid is from driving cooling structure |
| CN108448818A (en) * | 2018-05-21 | 2018-08-24 | 广东上水能源科技有限公司 | A kind of brushless dual-feed motor cooling structure based on coolant liquid |
| CN208571857U (en) * | 2018-05-21 | 2019-03-01 | 广东上水能源科技有限公司 | A kind of motor cooling based on coolant liquid |
-
2019
- 2019-05-06 CN CN201910371688.7A patent/CN109921567B/en not_active Expired - Fee Related
Patent Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS59175353A (en) * | 1983-03-23 | 1984-10-04 | Yaskawa Electric Mfg Co Ltd | Cooler of rotary electric machine |
| CN2560151Y (en) * | 2002-01-10 | 2003-07-09 | 武汉三维汽轮电机股份有限公司 | Large indoor cooled steam turbogenerator cooling structure |
| CN101123380A (en) * | 2007-05-25 | 2008-02-13 | 中国科学院电工研究所 | Steamship generator with rotor free cooling and stator evaporation cooling |
| CN202183689U (en) * | 2011-07-30 | 2012-04-04 | 南阳防爆集团股份有限公司 | Internal wind path structure for 2-pole motor |
| CN102983678A (en) * | 2012-11-14 | 2013-03-20 | 哈尔滨电机厂有限责任公司 | Electric generator cooling wind path structure |
| CN103023217A (en) * | 2012-12-18 | 2013-04-03 | 上海电机学院 | Overall machine wind path structure of high-power and high-peed permanent magnet synchronous motor |
| CN203387357U (en) * | 2013-07-31 | 2014-01-08 | 广东鸿源众力发电设备有限公司 | Centralized open ventilation and cooling system of bulb through-flow type hydraulic turbine generator |
| CN206542299U (en) * | 2016-12-22 | 2017-10-03 | 哈尔滨理工大学 | A kind of compact medium-sized high pressure motor of novel cooling structure |
| CN207559750U (en) * | 2017-10-25 | 2018-06-29 | 石家庄金士顿轴承科技有限公司 | A kind of high-speed permanent magnet motor direct connection centrifugal blower heat sink |
| CN108429403A (en) * | 2018-05-21 | 2018-08-21 | 广东上水能源科技有限公司 | A kind of motor based on coolant liquid is from driving cooling structure |
| CN108448818A (en) * | 2018-05-21 | 2018-08-24 | 广东上水能源科技有限公司 | A kind of brushless dual-feed motor cooling structure based on coolant liquid |
| CN208571857U (en) * | 2018-05-21 | 2019-03-01 | 广东上水能源科技有限公司 | A kind of motor cooling based on coolant liquid |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111046539A (en) * | 2019-11-27 | 2020-04-21 | 上海电气电站设备有限公司 | Water-cooled rotor forced excitation temperature rise calculation method based on instantaneous movement method |
| CN111046539B (en) * | 2019-11-27 | 2023-09-26 | 上海电气电站设备有限公司 | Water-cooled rotor forced excitation temperature rise calculation method based on instantaneous movement method |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109921567B (en) | 2019-12-24 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102290922B (en) | Double-fed wind generator | |
| JP5358667B2 (en) | Permanent magnet generator | |
| US4574210A (en) | External rotor motor having a cooling system | |
| CN101897106B (en) | Electric machine having a twin axial fan | |
| US8648505B2 (en) | Electrical machine with multiple cooling flows and cooling method | |
| CN105981269B (en) | Totally-enclosed-type traction motor | |
| JP2003204643A (en) | Tapered air gap between rotor and stator for superconducting synchronous machine | |
| CN206595818U (en) | A kind of motor with temperature with high efficiency function | |
| CN105071598A (en) | Inner wind path structure of double-cooling motor | |
| CN109921567A (en) | A kind of large synchronous compensator rotor rotation formula air-makeup system | |
| CN202183693U (en) | Double-fed wind driven generator | |
| JP6592027B2 (en) | Rotating electric machine and its rotor | |
| CA2355427A1 (en) | High-speed electric machine | |
| JP2013034332A (en) | Rotary electric machine | |
| JPH05236690A (en) | Squirrel-cage induction motor for railway vehicle | |
| CN205356061U (en) | Rotor and be equipped with motor of this rotor | |
| US20020127096A1 (en) | Gas-cooled machine, in particular a turbo-generator | |
| US10797565B2 (en) | Motor with inner fan | |
| CN107834774A (en) | A kind of motor of stator with ventilation slot mouth | |
| CN108880106A (en) | A kind of motor with air-cooling apparatus | |
| CN212063670U (en) | Generator with fan | |
| JP5385210B2 (en) | Rotating electric machine | |
| CN113323908A (en) | Air compressor machine, air conditioner and car | |
| CN209344928U (en) | Wheel hub subassembly and vehicle of vehicle | |
| US10826352B2 (en) | Electric machine with variable cooling system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20191224 Termination date: 20200506 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |