CN105896820A - Exhaust gas turbine driven electric excitation generator - Google Patents
Exhaust gas turbine driven electric excitation generator Download PDFInfo
- Publication number
- CN105896820A CN105896820A CN201610256123.0A CN201610256123A CN105896820A CN 105896820 A CN105896820 A CN 105896820A CN 201610256123 A CN201610256123 A CN 201610256123A CN 105896820 A CN105896820 A CN 105896820A
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- Prior art keywords
- exhaust gas
- gas turbine
- stator
- rotor
- stator core
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Classifications
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
- H02K7/18—Structural association of electric generators with mechanical driving motors, e.g. with turbines
- H02K7/1807—Rotary generators
- H02K7/1823—Rotary generators structurally associated with turbines or similar engines
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/10—Adaptations for driving, or combinations with, electric generators
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B41/00—Engines characterised by special means for improving conversion of heat or pressure energy into mechanical power
- F02B41/02—Engines with prolonged expansion
- F02B41/10—Engines with prolonged expansion in exhaust turbines
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K1/00—Details of the magnetic circuit
- H02K1/06—Details of the magnetic circuit characterised by the shape, form or construction
- H02K1/12—Stationary parts of the magnetic circuit
- H02K1/14—Stator cores with salient poles
- H02K1/145—Stator cores with salient poles having an annular coil, e.g. of the claw-pole type
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K1/00—Details of the magnetic circuit
- H02K1/06—Details of the magnetic circuit characterised by the shape, form or construction
- H02K1/22—Rotating parts of the magnetic circuit
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K1/00—Details of the magnetic circuit
- H02K1/06—Details of the magnetic circuit characterised by the shape, form or construction
- H02K1/22—Rotating parts of the magnetic circuit
- H02K1/24—Rotor cores with salient poles ; Variable reluctance rotors
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K16/00—Machines with more than one rotor or stator
- H02K16/04—Machines with one rotor and two stators
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K3/00—Details of windings
- H02K3/04—Windings characterised by the conductor shape, form or construction, e.g. with bar conductors
- H02K3/28—Layout of windings or of connections between windings
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
- H02P9/00—Arrangements for controlling electric generators for the purpose of obtaining a desired output
- H02P9/48—Arrangements for obtaining a constant output value at varying speed of the generator, e.g. on vehicle
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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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Synchronous Machinery (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Abstract
The invention relates to an exhaust gas turbine driven electric excitation generator. The exhaust gas turbine driven electric excitation generator comprises a shaft, an exhaust gas turbine, an exhaust gas turbine housing, two sets of excitation windings, two stator cores, two sets of armature windings, a rotor iron core and a motor housing, wherein the exhaust gas turbine and the rotor iron core are fixed on the shaft; two end surfaces of the rotor iron core are each provided with a rotor pole which is convex in the axial direction; the stator cores are fixed on the inner wall of the housing; the end surfaces, facing toward the rotor core, of the stator cores, are each provided with a convex stator pole in the axial direction; the armature windings wind around the stator poles; and the excitation windings winds around the stator cores in the radial direction of the stator cores and are embedded into magnetic isolation grooves of the stator cores. The technical rotor of the exhaust gas turbine driven electric excitation generator is manufactured in an integrated molded way, and has no excitation windings, and can be suitable for the high temperature and high speed work environment for the exhaust gas turbine. The technical rotor of the exhaust gas turbine driven electric excitation generator uses electrified coils for excitation and has no positioning torque, and can quickly accelerate, wherein two end surfaces of the rotor are each provided with the armature winding and the motor specific power is high.
Description
Technical field
The present invention relates to a kind of electric excitation generator driven by exhaust gas turbine, belong to car electrics technical field.
Background technology
Thermal power generation at present is all to use turbine generator machine technology, and the steam turbine generator gross efficiency of efficiency power generation can bring up to more than 60%-70%.
At present, the thermal efficiency of engine is mostly below 35%, and the waste gas of the HTHP of engine emission has taken away the 40% of fuel thermal energy, and major part engine can not effectively utilize these energy.Exhaust gas turbocharge device achieves the utilization of portion kinetic energy, improves the fuel availability of engine, and current application is more and more extensive.
Automobile current generator is the alternating current generator driven by belt pulley mostly at present, and this electrical power generators efficiency is about 50%.Therefore the gross efficiency of driven by engine electrical power generators is only by about 17.5%.This is far smaller than the generating efficiency of steam turbine generator.
The waste gas direct drive generator generating discharged hence with engine, can effectively utilize the feature that steam turbine generator generating efficiency is high, improve the fuel utilization ratio of automobile.
Exhaust turbine generator is the focus of research both at home and abroad, the mandate patent of invention of such as Patent No. 201410814049.0: exhaust gas turbo generator group, (turbine i.e. turbo, the meaning of turbine) proposes a kind of generating set including turbine, magneto and inverter.Described turbine is in order to receive waste gas to be rotated by described exhaust gas driven.This magneto is driven in order to generate electricity by the rotation of described turbine.
The U.S. patent Nos authorized: Exhaust energy recovery and generator for use with
An engine, the patent No.: 4694694, also disclose that the generator that a kind of engine exhaust reclaims, its motor uses p-m rotor, it is impossible to adapt to the high temperature residing for exhaust gas turbine, run up environment.Similar also has the patent of invention authorized: engine exhaust turbine drives magneto, the patent No.: 201310473600.5.
Applicant 2016 obtains and authorizes patent of invention: a kind of turbocharging power generation device, and Patent No. 2014100754333 proposes and a kind of includes shell, bearing, stator, controller and the turbocharging power generation device of rotor being made up of exhaust driven gas turbine, air inlet turbine, axle, rotor core.After the exhaust gas driven exhaust driven gas turbine that engine is discharged, coaxial air inlet turbine and rotor core is driven to rotate, it is achieved supercharging and the generating to air inlet.This patent is pointed out, if rotor core is without excitation source, is then suitable for the ultrahigh speed operating of exhaust gas turbine；If rotor is without permanent magnet, then rotor structure is simple, heatproof is high so that TRT can be operated near the blast pipe that temperature is higher.
Along with the carrying out of research, applicant innovates the configuration mode of Exciting Windings for Transverse Differential Protection and armature winding, can radially centralized excitation, the total winding length of Exciting Windings for Transverse Differential Protection is less, and excitation efficiency is high.Therefore the present invention proposes a kind of novel topological structure, it is possible to achieve such scheme.
The innovative point of the application also resides in two end faces of rotor all armature winding, and motor specific power is high；Armature winding is the centralized winding around axial coiling, and therefore armature winding winding length is the least.
Applicant not yet retrieves the closely-related report of electric excitation generator driven by exhaust gas turbine of the application at present.
Summary of the invention
In order to invent a kind of electric excitation generator driven by exhaust gas turbine, it is achieved away from the excitation function of high-temp waste gas turbine, reclaiming engine exhaust energy, the present invention adopts the following technical scheme that
A kind of electric excitation generator driven by exhaust gas turbine, it is characterised in that:
It is made up of axle (1), exhaust gas turbine (2), exhaust gas turbine shell (3), the first Exciting Windings for Transverse Differential Protection (4), the first stator core (5), the first armature winding (6), rotor core (7), the second armature winding (8), the second stator core (9), the second Exciting Windings for Transverse Differential Protection (10) and motor housing (11)；
The end of axle (1) is fixed with exhaust gas turbine (2), and the centre of axle (1) is fixed with the rotor core (7) of disc type；
Rotor core (7) is formed in one manufacture, and without excitation source, under the effect of bearing, exhaust gas turbine (2) can drive rotor core (7) to rotate；
Rotor core (7) all has rotor pole protruding vertically on two axial end faces；Described rotor pole is in fan annular；
It is that the first stator core (5) and the second stator core (9), the first stator core (5) and the second stator core (9) are separately fixed on the inwall of (11) two end faces of motor housing respectively outside the both ends of the surface of rotor core (7)；
First stator core (5) has the first axially projecting stator poles towards the side of rotor core (7), and the second stator core (9) has the second axially projecting stator poles towards the side of rotor core (7)；Described first stator poles and the second stator poles are in fan annular；
Have every magnetic groove in the first stator core (5) between every three the first stator poles；Also have every magnetic groove in the second stator core (9) between every three the second stator poles；In each first stator poles and being all wound with a centralized armature coil in the second stator poles, two three armature coils between magnetic groove are around to identical；Adjacent armature coil between magnetic groove is around on the contrary；
A phase armature winding is formed after the series connection of synchronous armature coil, each phase armature winding in first stator core (5) forms the first armature winding (6) by wye connection, and each phase armature winding in the second stator core (9) forms the second armature winding (8) by wye connection；
First Exciting Windings for Transverse Differential Protection (4) around the first stator core (5) radial direction coiling and be embedded into the first stator core (5) in magnetic groove；Second Exciting Windings for Transverse Differential Protection (10) around the second stator core (9) radial direction coiling and be embedded into the second stator core (9) in magnetic groove；
Permanent magnet (8) is parallel to axle (1) placement and magnetizing direction is perpendicular to axle (1)；Adjacent the first Exciting Windings for Transverse Differential Protection (4) or adjacent the second Exciting Windings for Transverse Differential Protection (10) are around on the contrary.
A kind of electric excitation generator driven by exhaust gas turbine as above, it is characterised in that:
First stator core (5), the second stator core (9) and rotor core (7) are made up of No yield point permeability magnetic material, and exhaust gas turbine shell (3) and motor housing (11) are that non-magnet material is made.
A kind of electric excitation generator driven by exhaust gas turbine as above, it is characterised in that:
Rotor core (7) each end face has 2N rotor pole, and N is natural number；First stator poles and the second stator poles are alignd in a circumferential direction；The rotor pole of rotor core (7) both ends of the surface differs 90/N mechanical angle in a circumferential direction.
Beneficial effects of the present invention is as follows:
(1) the technology rotor of the present invention is formed in one manufacture, without Exciting Windings for Transverse Differential Protection, is suitable for the high temperature residing for exhaust gas turbine, working environment at a high speed；
(2) use hot-wire coil excitation, without location torque, can accelerate rapidly；And electric excitation generator can arbitrarily regulate the size of exciting current, thus keep the direct current exporting burning voltage under variable speed varying load operating mode；
(3) two end faces of rotor all have armature winding, and motor specific power is high；Two rotors by certain angle that staggers, thus can reduce the torque pulsation of driving；
(4) Exciting Windings for Transverse Differential Protection coiling direction is the most special, can radially centralized excitation, the total winding length of Exciting Windings for Transverse Differential Protection is less, and excitation efficiency is high.
Accompanying drawing explanation
Fig. 1 is one electric excitation generator driven by exhaust gas turbine sectional side elevation of the present invention.Wherein: 1 axle, 2, exhaust gas turbine, 3, exhaust gas turbine shell, the 4, first Exciting Windings for Transverse Differential Protection, the 5, first stator core, the 6, first armature winding, 7, rotor core, the 8, second armature winding, the 9, second stator core, the 10, second Exciting Windings for Transverse Differential Protection, 11, motor housing.
Fig. 2 is the side view of the present invention a kind of electric excitation generator driven by exhaust gas turbine the first armature winding.Wherein: 1 axle, the 4, first Exciting Windings for Transverse Differential Protection, the 5, first stator core, the 6, first armature winding.
Fig. 3 is one electric excitation generator driven by exhaust gas turbine Exciting Windings for Transverse Differential Protection side view of the present invention.Wherein: 1 axle, the 4, first Exciting Windings for Transverse Differential Protection, the 5, first stator core.
Fig. 4 is one electric excitation generator driven by exhaust gas turbine rotor core side view of the present invention.Wherein: 1 axle, 7, rotor core, 12, rotor pole.
Fig. 5 is the magnetic linkage figure during present invention one phase armature winding different exciting electric current.
Detailed description of the invention
Below in conjunction with the accompanying drawings the invention is described in further details.
Fig. 1 is one electric excitation generator driven by exhaust gas turbine sectional side elevation of the present invention.
Described electric excitation generator driven by exhaust gas turbine is made up of axle (1), exhaust gas turbine (2), exhaust gas turbine shell (3), the first Exciting Windings for Transverse Differential Protection (4), the first stator core (5), the first armature winding (6), rotor core (7), the second armature winding (8), the second stator core (9), the second Exciting Windings for Transverse Differential Protection (10) and motor housing (11).
The end of axle (1) is fixed with exhaust gas turbine (2), and the centre of axle (1) is fixed with the rotor core (7) of disc type.
Rotor core (7) is formed in one manufacture, and without excitation source, under the effect of bearing, exhaust gas turbine (2) can drive rotor core (7) to rotate.
Rotor core (7) all has rotor pole protruding vertically on two axial end faces；Described rotor pole is in fan annular；
It is that the first stator core (5) and the second stator core (9), the first stator core (5) and the second stator core (9) are separately fixed on the inwall of (11) two end faces of motor housing respectively outside the both ends of the surface of rotor core (7).
First stator core (5) has the first axially projecting stator poles towards the side of rotor core (7), and the second stator core (9) has the second axially projecting stator poles towards the side of rotor core (7)；Described first stator poles and the second stator poles are in fan annular；
Have every magnetic groove in the first stator core (5) between every three the first stator poles；Also have every magnetic groove in the second stator core (9) between every three the second stator poles；In each first stator poles and being all wound with a centralized armature coil in the second stator poles, two three armature coils between magnetic groove are around to identical；Adjacent armature coil between magnetic groove is around on the contrary.
A phase armature winding is formed after the series connection of synchronous armature coil, each phase armature winding in first stator core (5) forms the first armature winding (6) by wye connection, and each phase armature winding in the second stator core (9) forms the second armature winding (8) by wye connection.
Permanent magnet (8) is parallel to axle (1) placement and magnetizing direction is perpendicular to axle (1)；Adjacent the first Exciting Windings for Transverse Differential Protection (4) or adjacent the second Exciting Windings for Transverse Differential Protection (10) are around on the contrary.
The first rotor (5) unshakable in one's determination, the second stator core (9) and stator core (7) are made up of No yield point permeability magnetic material, and exhaust gas turbine shell (3) and motor housing (11) are that non-magnet material is made.
Fig. 2 is the side view of the present invention a kind of electric excitation generator driven by exhaust gas turbine the first armature winding.
Have every magnetic groove in the first stator core (5) between every three the first stator poles；Also have every magnetic groove in the second stator core (9) between every three the second stator poles；In each first stator poles and being all wound with a centralized armature coil in the second stator poles, two three armature coils between magnetic groove are around to identical；Adjacent armature coil between magnetic groove is around on the contrary；
A phase armature winding is formed after the series connection of synchronous armature coil, each phase armature winding in first stator core (5) forms the first armature winding (6) by wye connection, and each phase armature winding in the second stator core (9) forms the second armature winding (8) by wye connection.
Fig. 3 is one electric excitation generator driven by exhaust gas turbine Exciting Windings for Transverse Differential Protection side view of the present invention.
Have every magnetic groove in the first stator core (5) between every three the first stator poles；Also have every magnetic groove in the second stator core (9) between every three the second stator poles.
First Exciting Windings for Transverse Differential Protection (4) around the first stator core (5) radial direction coiling and be embedded into the first stator core (5) in magnetic groove；Second Exciting Windings for Transverse Differential Protection (10) around the second stator core (9) radial direction coiling and be embedded into the second stator core (9) in magnetic groove.
Fig. 4 is one electric excitation generator driven by exhaust gas turbine rotor core side view of the present invention.
Rotor core (7) each end face has 2N rotor pole, and N is natural number, in the present embodiment, N=2；First stator poles and the second stator poles are alignd in a circumferential direction；The rotor pole of rotor core (7) both ends of the surface differs 90/N mechanical angle in a circumferential direction.
Fig. 5 is the magnetic linkage figure during present invention one phase armature winding different exciting electric current.Its each phase magnetic linkage converts along with the difference of rotor-position.
A kind of electric excitation generator driven by exhaust gas turbine proposed the present invention below is operated the explanation of principle.
Its operation principle is: if passing to exciting current to Exciting Windings for Transverse Differential Protection, and the most each stator poles can produce excitation field.When the rotor rotates, can increase or reduce the magnetic flux in each stator poles successively, thus cause the magnetic flux change of each phase armature winding linkage.Therefore, threephase armature winding can induce three-phase alternating current, and its induced electromotive force is just directly proportional to the interconversion rate of magnetic flux.The rectified circuit rectifies of this three-phase alternating voltage just can charge a battery, or powers to automobile electrical equipment.Owing to exciting current is adjustable, therefore by regulating the size of exciting current, it is possible to realize stablizing of the output voltage under generating state.
Claims (3)
1. an electric excitation generator driven by exhaust gas turbine, it is characterised in that:
It is made up of axle (1), exhaust gas turbine (2), exhaust gas turbine shell (3), the first Exciting Windings for Transverse Differential Protection (4), the first stator core (5), the first armature winding (6), rotor core (7), the second armature winding (8), the second stator core (9), the second Exciting Windings for Transverse Differential Protection (10) and motor housing (11)；
The end of axle (1) is fixed with exhaust gas turbine (2), and the centre of axle (1) is fixed with the rotor core (7) of disc type；
Rotor core (7) is formed in one manufacture, and without excitation source, under the effect of bearing, exhaust gas turbine (2) can drive rotor core (7) to rotate；
Rotor core (7) all has rotor pole protruding vertically on two axial end faces；Described rotor pole is in fan annular；
It is that the first stator core (5) and the second stator core (9), the first stator core (5) and the second stator core (9) are separately fixed on the inwall of (11) two end faces of motor housing respectively outside the both ends of the surface of rotor core (7)；
First stator core (5) has the first axially projecting stator poles towards the side of rotor core (7), and the second stator core (9) has the second axially projecting stator poles towards the side of rotor core (7)；Described first stator poles and the second stator poles are in fan annular；
Have every magnetic groove in the first stator core (5) between every three the first stator poles；Also have every magnetic groove in the second stator core (9) between every three the second stator poles；In each first stator poles and being all wound with a centralized armature coil in the second stator poles, two three armature coils between magnetic groove are around to identical；Adjacent armature coil between magnetic groove is around on the contrary；
A phase armature winding is formed after the series connection of synchronous armature coil, each phase armature winding in first stator core (5) forms the first armature winding (6) by wye connection, and each phase armature winding in the second stator core (9) forms the second armature winding (8) by wye connection；
First Exciting Windings for Transverse Differential Protection (4) around the first stator core (5) radial direction coiling and be embedded into the first stator core (5) in magnetic groove；Second Exciting Windings for Transverse Differential Protection (10) around the second stator core (9) radial direction coiling and be embedded into the second stator core (9) in magnetic groove；
Permanent magnet (8) is parallel to axle (1) placement and magnetizing direction is perpendicular to axle (1)；Adjacent the first Exciting Windings for Transverse Differential Protection (4) or adjacent the second Exciting Windings for Transverse Differential Protection (10) are around on the contrary.
2. a kind of electric excitation generator driven by exhaust gas turbine as claimed in claim 1, it is characterised in that:
First stator core (5), the second stator core (9) and rotor core (7) are made up of No yield point permeability magnetic material, and exhaust gas turbine shell (3) and motor housing (11) are that non-magnet material is made.
3. a kind of electric excitation generator driven by exhaust gas turbine as claimed in claim 1, it is characterised in that:
Rotor core (7) each end face has 2N rotor pole, and N is natural number；First stator poles and the second stator poles are alignd in a circumferential direction；The rotor pole of rotor core (7) both ends of the surface differs 90/N mechanical angle in a circumferential direction.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610256123.0A CN105896820B (en) | 2016-04-25 | 2016-04-25 | A kind of electric excitation generator driven by exhaust gas turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610256123.0A CN105896820B (en) | 2016-04-25 | 2016-04-25 | A kind of electric excitation generator driven by exhaust gas turbine |
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| Publication Number | Publication Date |
|---|---|
| CN105896820A true CN105896820A (en) | 2016-08-24 |
| CN105896820B CN105896820B (en) | 2018-04-06 |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107612214A (en) * | 2017-10-23 | 2018-01-19 | 史立伟 | A kind of extended-range electric vehicle gas turbine generator |
| CN107681793A (en) * | 2017-10-23 | 2018-02-09 | 史立伟 | High temperature and high speed exhaust turbine dynamoelectric generator |
| CN107681794A (en) * | 2017-10-23 | 2018-02-09 | 史立伟 | Aero-engine spout side fault tolerant electricity generator |
| CN107846123A (en) * | 2017-10-23 | 2018-03-27 | 史立伟 | The reluctance motor of exhaust gas turbine driving |
| CN107846125A (en) * | 2017-10-23 | 2018-03-27 | 史立伟 | Reclaim the turbogenerator of engine exhaust energy |
| CN110556990A (en) * | 2019-09-05 | 2019-12-10 | 哈尔滨理工大学 | Axial magnetic flux low vibration disk type switch reluctance motor |
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| CN104578636A (en) * | 2015-01-20 | 2015-04-29 | 东南大学 | Double-stator axial magnetic field flux-switching type mixing permanent magnetic memory motor |
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| CN1913290A (en) * | 2006-08-23 | 2007-02-14 | 南京航空航天大学 | Radial magnet steel double salient-pole mixed excitation electric machine |
| CN201107842Y (en) * | 2006-12-04 | 2008-08-27 | 袁会文 | Disc type switch reluctance motor |
| CN202085046U (en) * | 2011-06-16 | 2011-12-21 | 东南大学 | Axial magnetic field permanent magnetic brushless motor for smooth torque output |
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Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107612214A (en) * | 2017-10-23 | 2018-01-19 | 史立伟 | A kind of extended-range electric vehicle gas turbine generator |
| CN107681793A (en) * | 2017-10-23 | 2018-02-09 | 史立伟 | High temperature and high speed exhaust turbine dynamoelectric generator |
| CN107681794A (en) * | 2017-10-23 | 2018-02-09 | 史立伟 | Aero-engine spout side fault tolerant electricity generator |
| CN107846123A (en) * | 2017-10-23 | 2018-03-27 | 史立伟 | The reluctance motor of exhaust gas turbine driving |
| CN107846125A (en) * | 2017-10-23 | 2018-03-27 | 史立伟 | Reclaim the turbogenerator of engine exhaust energy |
| CN107612214B (en) * | 2017-10-23 | 2019-08-23 | 烟台业达新能源有限公司 | A kind of extended-range electric vehicle gas turbine generator |
| CN107681794B (en) * | 2017-10-23 | 2019-11-05 | 徐州博云航空科技有限公司 | Aero-engine spout side fault tolerant electricity generator |
| CN107846125B (en) * | 2017-10-23 | 2019-11-12 | 山东唐骏欧铃汽车制造有限公司 | Recycle the turbogenerator of engine exhaust energy |
| CN107681793B (en) * | 2017-10-23 | 2019-11-19 | 徐州诚凯知识产权服务有限公司 | High temperature and high speed exhaust turbine dynamoelectric generator |
| CN107846123B (en) * | 2017-10-23 | 2019-12-06 | 南京秦淮紫云创益企业服务有限公司 | Exhaust turbine driven reluctance machine |
| CN110556990A (en) * | 2019-09-05 | 2019-12-10 | 哈尔滨理工大学 | Axial magnetic flux low vibration disk type switch reluctance motor |
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