COOLING OF ELECTRICAL MACHINES
20220021275 · 2022-01-20
Inventors
- Sergio Romero Perez (Barcelona, ES)
- Julio Cesar URRESTY (Barcelona, ES)
- Cesar MUÑIZ CASAIS (Barcelona, ES)
- Stefan Keller (Barcelona, ES)
- Marc Cabré Gimeno (Barcelona, ES)
Cpc classification
F05B2220/706
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
H02K9/197
ELECTRICITY
H02K7/1838
ELECTRICITY
F05B2260/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D80/60
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
H02K9/08
ELECTRICITY
Y02E10/72
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
International classification
H02K9/197
ELECTRICITY
F03D80/60
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
H02K3/24
ELECTRICITY
Abstract
An electrical machine (50) comprising a rotor (70), a stator (60), a stator cooling system (80) including stator cooling channels (66) conducting cooling fluid to active parts of the stator (60), and a rotor cooling system (90) for cooling active parts of the rotor (70) is provided. The rotor cooling system (90) is configured to provide a rotor cooling gas flow, and the rotor cooling gas flow is cooled by the stator cooling channels (66). Methods for cooling electrical machines (50) are also provided, as well as wind turbines comprising generators with cooling systems.
Claims
1-15: (canceled)
16. An electrical machine, comprising: a rotor; a stator; a stator cooling system comprising stator cooling channels configured to conduct a cooling liquid to active parts of the stator; a rotor cooling system configured to provide a rotor cooling gas flow to active parts of the rotor; and wherein the stator cooling channels are configured for cooling the rotor cooling gas flow.
17. The electrical machine according to claim 16, wherein the rotor cooling system comprises gas flow channels in contact with the stator cooling channels.
18. The electrical machine according to claim 16, wherein the stator comprises electrical coils and the stator cooling channels are provided along one or more of the electrical coils.
19. The electrical machine according to claim 18, wherein the stator comprises cooling jackets surrounding the electrical coils, the cooling jackets comprising one or more of the stator cooling channels.
20. The electrical machine according to claim 17, wherein the gas flow channels in contact with the stator cooling channels are provided between adjacent electrical coils of the stator.
21. The electrical machine according to claim 17, wherein the gas flow channels in contact with the stator cooling channels are provided in a stator core.
22. The electrical machine according to claim 16, wherein the rotor cooling gas flow (90) is provided through an air gap (55) between the rotor (70) and the stator (60).
23. The electrical machine according to claim 17, wherein the gas flow channels are in contact with the stator cooling channels upstream from the air gap.
24. The electrical machine according to claim 23, wherein the gas flow channels comprise deflectors.
25. The electrical machine according to claim 16, further comprising a liquid-liquid or liquid-air heat exchanger disposed to cool the cooling liquid after the cooling liquid has been heated up.
26. A wind turbine comprising a generator, wherein the generator comprises the electrical machine according to claim 16.
27. The wind turbine according to claim 26, wherein the generator is a direct driven permanent magnet generator.
28. A method for cooling an electrical machine having a rotor and a stator, the method comprising: cooling parts of the stator by passing liquid through cooling channels in the stator; cooling parts of the rotor with a rotor cooling gas flow, and directing the rotor cooling gas flow when heated up to the cooling channels in the stator to cool down the rotor cooling gas flow.
29. The method of claim 28, wherein the cooling gas flow is a cooling air flow.
30. The method of claim 28, further comprising cooling the liquid after passing through the cooling channels in the stator.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0020] Non-limiting examples of the present disclosure will be described in the following, with reference to the appended drawings, in which:
[0021]
[0022]
[0023]
[0024]
[0025]
[0026]
[0027]
DETAILED DESCRIPTION OF EXAMPLES
[0028] In these figures the same reference signs have been used to designate matching elements.
[0029]
[0030]
[0031] It should be appreciated that the rotor shaft 163, gearbox 164, and generator 162 may generally be supported within the nacelle 161 by a support frame or bedplate 165 positioned atop the wind turbine tower 170.
[0032] The nacelle 161 is rotatably coupled to the tower 170 through the yaw system 20 in such a way that the nacelle 161 is able to rotate about a yaw axis YA. The yaw system 20 comprises a yaw bearing having two bearing components configured to rotate with respect to the other. The tower 170 is coupled to one of the bearing components and the bedplate or support frame 165 of the nacelle 161 is coupled to the other bearing component. The yaw system 20 comprises an annular gear 21 and a plurality of yaw drives 22 with a motor 23, a gearbox 24 and a pinion 25 for meshing with the annular gear 21 for rotating one of the bearing components with respect to the other.
[0033] Blades 120 are coupled to the hub 110 with a pitch bearing 100 in between the blade 120 and the hub 110. The pitch bearing 100 comprises an inner ring and an outer ring. A wind turbine blade may be attached either at the inner bearing ring or at the outer bearing ring, whereas the hub is connected at the other. A blade 120 may perform a relative rotational movement with respect to the hub 110 when a pitch system 107 is actuated. The inner bearing ring may therefore perform a rotational movement with respect to the outer bearing ring. The pitch system 107 of
[0034] The energy produced by the generator may be delivered to a converter which adapts the output electrical power of the generator to the requirements of the power grid. The electrical machine may comprise electrical phases, e.g. three electrical phases. The converter may be arranged inside the nacelle or inside the tower or externally.
[0035]
[0036] In an aspect of the present disclosure, a method for cooling an electrical machine 50 is provided. The method comprises cooling parts of a stator by passing liquid 80 through cooling channels 66 in the stator 60, and cooling parts of a rotor 70 with a cooling gas flow 90. The cooling gas flow 90 is cooled by the liquid in the cooling channels 66 in the stator.
[0037] It may be seen in
[0038] The cooling gas may be cooling air, although other gases could be envisaged. Throughout the present disclosure, reference will generally be made to an air flow, but it should be clear that other gases might be used.
[0039] As the cold air passes along the rotor, the air heats up, i.e. heat flow occurs from warm parts of the rotor towards the cold air. The heated up air may be recirculated back towards the rotor, but towards this end, it needs to be cooled down again. As it may be seen in
[0040] The cooling air flow may be driven by one or more fans or ventilators. In order to provide a sufficient mass air flow towards the rotor, one or more fans may be provided.
[0041] In some examples, the method may further comprise cooling the liquid (in cooling channels 66) after passing through the cooling channels in the stator. E.g. a liquid-liquid or liquid-air heat exchanger may be used for cooling the heated up liquid.
[0042] The liquid for cooling parts of the stator may be water, but may also be any other heat transfer liquid suitable for cooling.
[0043]
[0044] In the example, the electrical generator comprising a rotor 70 which is configured to rotate about a rotational axis, and a stator 60 radially surrounding the rotor. A radial air gap 55 is arranged between rotor 70, and stator 60.
[0045] Various aspects of the disclosure will thus be explained with reference to the example of
[0046] With reference to
[0047] In some examples, one or more fans or ventilators may be used to provide the rotor cooling gas flow.
[0048] In some examples, the stator 60 may comprise electrical coils 64 and the stator cooling channels are provided along one or more of the electrical coils 64, as is shown in the examples of
[0049] In this particular example, the stator cooling channels 66 surround one or more of the electrical coils 64. The stator comprises cooling jackets surrounding the electrical coils 64, and the cooling jackets may comprise one or more stator cooling channels.
[0050] The coils 64 may be arranged around teeth 62 on the stator, the teeth forming the stator core. In between two neighbouring coils, a plurality of gas cooling channels 72 may be provided. The gas cooling channels 72 may thus be in direct heat exchange configuration with the liquid used for cooling the stator.
[0051] The liquid for cooling the stator may be water. The cooling gas flow may be cooling air, but other gases might be used.
[0052] The rotor cooling air flow 90 may be provided through an air gap between the rotor 70 and the stator 60. The cooling air flow 90 may thus flow and come in contact with the active parts of the rotor, e.g. electrical coils or permanent magnets. In this particular example, the active parts may be permanent magnets.
[0053] The rotor cooling system may comprise one or more air flow channels 72 in contact with the stator cooling channels upstream from the air gap 55.
[0054] In the example of
[0055]
[0056]
[0057]
[0058] The cooling jackets may be formed by two thin metal sheet walls having a substantially constant distance between the sheet metal walls.
[0059] Cold liquid enters cooling jacket 66 at inlet 67. The liquid heats up as it flows along the coil, and leaves the cooling jacket as a heated up liquid at outlet 69. From liquid outlet 69, the cooling liquid may be supplied to a cooling system for reducing the temperature of the cooling liquid, such that it can be recirculated again. In an example, a liquid-liquid heat exchanger may be used to cool down the cooling liquid. Any suitable system may be used for providing cooling liquid or cooling down the cooling liquid again. In examples according to the present disclosure, there is no need for an air-liquid or air-air heat exchanger for cooling down the rotor cooling gas flow, since the rotor cooling gas flow is only (actively) cooled by the stator cooling channels. The stator cooling channels may be configured (sized and shaped and arranged) such that their cooling capacity is sufficient for cooling down the stator directly and cooling down the rotor indirectly.
[0060] Electrical connections to the coils are indicated with reference signs 75, 77 and 79 in this figure. The cooling air may flow freely in spaces between the electrical connections and water connections.
[0061] The air cools down as it flows along the cooling jacket, and the cold (or cooler) air may be directed towards the air gap.
[0062] Even though in these examples, cooling jackets have been shown, it should be clear that any sort of liquid cooling body may be provided, e.g. one or more pipes, tubes or other conduits may be used as well.
[0063]
[0064] A cooling gas (e.g. air) flow may flow through the air gap along the permanent magnets 74. In some examples, the air gap may be radially arranged between rotor and stator, and the cooling air flow traverses the air gap axially.
[0065] Before the cooling gas flow reaches the air gap it may have been cooled down by liquid cooling channels in the stator. In this particular example, a single heat exchanger body may be provided which is arranged between electrical coils 64. The single heat exchanger body 100 combined liquid cooling channels in heat exchange with the electrical coils and at the same time in heat exchange relationship with air passages.
[0066]
[0067] In the example of
[0068] In the example of
[0069] In an aspect of the present disclosure, a wind turbine is provided, which comprises a rotor with a plurality of blades, and a generator operatively connected with the rotor. The generator may be according to any of the examples disclosed herein.
[0070] In accordance with an aspect, the generator comprises a generator rotor and a generator stator, and an air gap between the generator rotor and the generator stator. The generator further comprises a stator cooling system comprising stator cooling channels with cooling liquid, and a rotor cooling system comprising a fan to provide a cooling air flow through the air gap. The cooling air flow is positioned in heat exchange arrangement with the stator cooling channels prior to flowing through the air gap.
[0071] In some examples, the stator comprises a plurality of electrical coils, and further comprises cooling jackets surrounding the electrical coils. Cooling jackets are however merely an example of integrating the liquid cooling channels.
[0072] In some examples, the cooling air flow channels may be arranged between the cooling jackets.
[0073] In some examples, the cooling air flow channels and stator cooling channels may be integrated in single heat exchanger device. In other examples, the cooling air flow channels may form a cooling air device, that is separate but placed in contact a stator cooling device.
[0074] In some examples, the rotor cooling system may comprise a closed cycle for the cooling air. A closed cycle for the cooling air may be most efficient since only small amounts of intake air would need to be filtered in a continuous manner. The heat exchange with the stator cooling channels can provide efficient cooling for the cooling air.
[0075] This written description uses examples to disclose the invention, including the preferred embodiments, and also to enable any person skilled in the art to practice the invention, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the invention is defined by the claims, and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims if they have structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal languages of the claims. Aspects from the various embodiments described, as well as other known equivalents for each such aspects, can be mixed and matched by one of ordinary skill in the art to construct additional embodiments and techniques in accordance with principles of this application. If reference signs related to drawings are placed in parentheses in a claim, they are solely for attempting to increase the intelligibility of the claim, and shall not be construed as limiting the scope of the claim.