CN106640555B - Wind power generating set, heat dissipation system and heat dissipation control method thereof - Google Patents

Wind power generating set, heat dissipation system and heat dissipation control method thereof Download PDF

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CN106640555B
CN106640555B CN201611225516.1A CN201611225516A CN106640555B CN 106640555 B CN106640555 B CN 106640555B CN 201611225516 A CN201611225516 A CN 201611225516A CN 106640555 B CN106640555 B CN 106640555B
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cabin
heat dissipation
impeller
heat
temperature
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CN106640555A (en
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方涛
吴凯
武占海
邓刚
方志祥
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Beijing Goldwind Science and Creation Windpower Equipment Co Ltd
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Beijing Goldwind Science and Creation Windpower Equipment Co Ltd
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/20Heat transfer, e.g. cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/20Heat transfer, e.g. cooling
    • F05B2260/232Heat transfer, e.g. cooling characterised by the cooling medium
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction

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  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

公开了一种风力发电机组及其散热系统和散热控制方法,散热系统包括:叶轮散热装置,安装在风力发电机组的机舱内,风力发电机组的轮毂内的热空气通过导风管而被引入到所述叶轮散热装置中并与所述叶轮散热装置中的流体介质换热;机舱散热装置,安装在所述机舱内,所述机舱内的热空气被吸入到所述机舱散热装置并与所述机舱散热装置中的流体介质换热。上述散热系统实现了同时对叶轮系统和机舱进行散热,同时根据温度变化对散热过程自动地进行智能控制。

Disclosed is a wind turbine, its heat dissipation system and heat dissipation control method. The heat dissipation system includes: an impeller heat dissipation device, which is installed in the nacelle of the wind turbine. The hot air in the hub of the wind turbine is introduced into the wind turbine through an air duct. The impeller heat dissipation device exchanges heat with the fluid medium in the impeller heat dissipation device; the engine room heat dissipation device is installed in the engine room, and the hot air in the engine room is sucked into the engine room heat dissipation device and interacts with the engine room heat dissipation device. Heat exchange from fluid media in cabin radiators. The above-mentioned heat dissipation system realizes simultaneous heat dissipation of the impeller system and the engine room, and at the same time automatically and intelligently controls the heat dissipation process according to temperature changes.

Description

风力发电机组及其散热系统和散热控制方法Wind power generating set, heat dissipation system and heat dissipation control method thereof

技术领域technical field

本发明涉及风力发电领域,具体地说,本发明涉及一种风力发电机组及其散热系统和散热控制方法。The present invention relates to the field of wind power generation, and in particular, the present invention relates to a wind generator set, a heat dissipation system and a heat dissipation control method thereof.

背景技术Background technique

在一些风力发电机组中,用于冷却机舱的散热系统安装在机舱外部,机舱内的热量经管路传递到机舱外的换热器进行散热。这样节省了机舱内部空间,可减小机舱尺寸。但是,由于换热器在机舱外部倾斜地安装,实际上发生热交换的有效面积比较小,需要的换热器数量较多,并会对风力发电机组的外观造成不好的影响。In some wind turbines, the heat dissipation system for cooling the nacelle is installed outside the nacelle, and the heat in the nacelle is transferred to the heat exchanger outside the nacelle through pipes for heat dissipation. This saves space inside the cabin and can reduce the size of the cabin. However, since the heat exchanger is installed obliquely outside the nacelle, the effective area for heat exchange is relatively small, and a large number of heat exchangers are required, which will adversely affect the appearance of the wind turbine.

另外,如此设置的散热系统只能对机舱空间进行冷却,却不能同时对叶轮系统内部空间进行冷却而将其内部保持在合适的温度范围内。同时,这种散热系统也不能实现智能控制,而适应周围环境温度的温度来调整散热方式。In addition, the heat dissipation system thus arranged can only cool the nacelle space, but cannot simultaneously cool the interior space of the impeller system to keep the interior within a suitable temperature range. At the same time, this cooling system cannot realize intelligent control, but adjust the cooling method according to the temperature of the surrounding environment.

发明内容SUMMARY OF THE INVENTION

本发明的目的在于提供一种用于风力发电机组的散热系统和散热控制方法,以同时对叶轮系统和机舱进行散热,同时根据温度变化对散热过程自动地进行智能控制。The purpose of the present invention is to provide a heat dissipation system and a heat dissipation control method for a wind turbine, so as to simultaneously dissipate the impeller system and the nacelle, and at the same time automatically and intelligently control the heat dissipation process according to temperature changes.

本发明的另一目的在于提供一种风力发电机组。Another object of the present invention is to provide a wind turbine.

为了实现上述目的,本发明提供了一种用于风力发电机组的散热系统,所述散热系统包括:叶轮散热装置,安装在风力发电机组的机舱内,风力发电机组的轮毂内的热空气通过导风管而被引入到所述叶轮散热装置中并与所述叶轮散热装置中的流体介质换热;机舱散热装置,安装在所述机舱内,所述机舱内的热空气被吸入到所述机舱散热装置并与所述机舱散热装置中的流体介质换热。In order to achieve the above object, the present invention provides a heat dissipation system for a wind turbine generator set, the heat dissipation system includes: an impeller heat sink, installed in the nacelle of the wind turbine generator set, and the hot air in the hub of the wind turbine generator set passes through the guide The air duct is introduced into the impeller heat sink and exchanges heat with the fluid medium in the impeller heat sink; the engine room heat sink is installed in the engine room, and the hot air in the engine room is sucked into the engine room A heat sink and heat exchange with the fluid medium in the nacelle heat sink.

优选地,所述散热系统还包括外部散热装置,所述外部散热装置安装在所述机舱外,以冷却所述叶轮散热装置和所述机舱散热装置中的被加热的流体介质。Preferably, the heat dissipation system further includes an external heat dissipation device installed outside the nacelle to cool the impeller heat dissipation device and the heated fluid medium in the nacelle heat dissipation device.

优选地,所述叶轮散热装置包括:叶轮换热器,使来自所述轮毂的热空气与流体介质换热并将降温后的空气排到所述机舱内;叶轮换热风扇,通过所述导风管将所述轮毂内的热空气吹送至所述叶轮换热器;管道,在所述叶轮换热器和所述外部散热装置之间输送流体介质。Preferably, the impeller heat dissipation device includes: an impeller heat exchanger, which exchanges heat between the hot air from the hub and the fluid medium and discharges the cooled air into the engine room; an impeller heat exchange fan, which passes through the guide The air duct blows the hot air in the hub to the impeller heat exchanger; the duct transports the fluid medium between the impeller heat exchanger and the external heat sink.

优选地,所述机舱散热装置包括:机舱换热器,使所述机舱内的热空气与流体介质换热并将降温后的空气排到机舱内;机舱换热风扇,将所述机舱内的热空气吹送到所述机舱换热器;管道,在所述机舱换热器和所述外部散热装置之间输送流体介质。Preferably, the cabin heat dissipation device includes: a cabin heat exchanger, which exchanges heat between the hot air in the cabin and the fluid medium and discharges the cooled air into the cabin; a cabin heat exchange fan; Hot air is blown to the cabin heat exchanger; ducts that carry a fluid medium between the cabin heat exchanger and the external heat sink.

优选地,在所述管道上设置有电动泵,以使流体介质在所述管道内流动。Preferably, an electric pump is provided on the pipeline to make the fluid medium flow in the pipeline.

优选地,所述叶轮散热装置和所述机舱散热装置安装在所述机舱内的顶部。Preferably, the impeller heat sink and the nacelle heat sink are mounted on top of the nacelle.

优选地,所述外部散热装置包括外部换热器,使从所述叶轮散热装置和所述机舱散热装置接收的流体介质与外界空气换热。Preferably, the external heat sink includes an external heat exchanger for exchanging heat with the fluid medium received from the impeller heat sink and the nacelle heat sink with outside air.

根据本发明的实施例,提供了一种用于风力发电机组的散热控制方法,所述散热控制方法控制上述散热系统的操作,包括:在所述轮毂内的温度达到T1时,启动所述叶轮散热装置;在风力发电机组的机舱内的温度达到比T1大的T2时,启动所述机舱散热装置;在所述机舱内的温度达到风力发电机组的最高极限温度T3时,使风力发电机组停机;在所述机舱内的温度从T3下降到T2时,停用所述机舱散热装置;在所述机舱内的温度从T2下降到比T1小的T4时,停用所述叶轮散热装置。According to an embodiment of the present invention, a heat dissipation control method for a wind turbine is provided. The heat dissipation control method controls the operation of the above-mentioned heat dissipation system, including : when the temperature in the hub reaches T1, starting the Impeller cooling device; when the temperature in the nacelle of the wind turbine reaches T2, which is greater than T1, the engine room cooling device is activated ; when the temperature in the nacelle reaches the highest limit temperature T3 of the wind turbine, make The wind turbine is stopped; when the temperature in the nacelle drops from T3 to T2, the nacelle cooling device is deactivated ; when the temperature in the nacelle drops from T2 to T4 , which is smaller than T1 , Deactivate the impeller heat sink.

优选地,在所述轮毂内的温度达到T1时,启动外部散热装置。Preferably, when the temperature in the hub reaches T1 , the external heat dissipation device is activated.

优选地,在所述机舱内的温度达到比T2大且比T3小的T5时,启动电动泵。Preferably, the electric pump is started when the temperature in the nacelle reaches T 5 which is greater than T 2 and less than T 3 .

优选地,在所述机舱内的温度从T3下降到T2时,还停用所述电动泵。Preferably, the electric pump is also deactivated when the temperature in the nacelle drops from T3 to T2.

根据本发明的另一实施例,还提供了一种风力发电机组,所述风力发电机组包括上述散热系统。According to another embodiment of the present invention, there is also provided a wind power generator set including the above heat dissipation system.

优选地,风力发电机组的塔筒内的热空气通过烟囱效应进入机舱内,以通过机舱散热装置进行散热。Preferably, the hot air in the tower of the wind turbine enters into the nacelle through the chimney effect, so as to dissipate heat through the nacelle cooling device.

优选地,在轮毂内的热空气被吸入到叶轮散热装置的叶轮换热器中之后,在轮毂内形成负压,以使外界空气进入轮毂内。Preferably, after the hot air in the wheel hub is sucked into the impeller heat exchanger of the impeller heat sink, negative pressure is formed in the wheel hub, so that outside air enters the wheel hub.

优选地,在机舱散热装置中的机舱换热器将冷却后的空气排到机舱内之后,在机舱内形成正压,从而在轮毂和机舱的空气间形成流动循环。Preferably, after the nacelle heat exchanger in the nacelle heat sink discharges the cooled air into the nacelle, a positive pressure is formed in the nacelle, thereby forming a flow circulation between the hub and the air in the nacelle.

通过本发明所提供的散热系统和散热控制方法,取得了以下有益效果:Through the heat dissipation system and heat dissipation control method provided by the present invention, the following beneficial effects are obtained:

1、将用于冷却轮毂的叶轮散热装置安装在机舱内,增大了轮毂的内部空间,简化了轮毂内安装,同时极大地减少了叶轮散热装置的故障率;1. The impeller cooling device for cooling the hub is installed in the engine room, which increases the internal space of the wheel hub, simplifies the installation in the wheel hub, and greatly reduces the failure rate of the impeller cooling device;

2、轮毂的散热和机舱以及塔筒的散热整合在一起,共同采用一套二次换热系统,简化了整机的散热系统,降低了部件故障率;2. The heat dissipation of the hub is integrated with the heat dissipation of the engine room and the tower, and a set of secondary heat exchange system is used together, which simplifies the heat dissipation system of the whole machine and reduces the failure rate of components;

3、在机舱外部设置外部散热装置,利用外界空气作为冷源进行热交换,达到了无需额外动力,从而能够采用外界空气冷却散热系统内的热水,同时能够提高机组系统的可靠性;3. An external cooling device is installed outside the engine room, and the external air is used as a cold source for heat exchange, so that no additional power is required, so that the hot water in the cooling system can be cooled by the external air, and the reliability of the unit system can be improved at the same time;

4、通过在机舱顶部安装各个换热器和风扇,利用了烟囱效应,既能节省能量,又达到了节省机舱空间,并能降低机舱、轮毂和塔筒内温度的目的,也保持了机舱外形的美观;4. By installing various heat exchangers and fans on the top of the nacelle, the chimney effect is used, which can save energy and save the space of the nacelle, and can reduce the temperature in the nacelle, hub and tower, and maintain the shape of the nacelle. beauty;

5、根据轮毂和机舱内的温度,实现了对散热过程的智能化控制,自适应机组内温度进行自适应的冷却。5. According to the temperature in the hub and the engine room, the intelligent control of the heat dissipation process is realized, and the temperature in the unit is adapted to perform adaptive cooling.

附图说明Description of drawings

图1是根据本发明的实施例的散热系统的示意图;1 is a schematic diagram of a heat dissipation system according to an embodiment of the present invention;

图2是根据本发明的实施例散热控制方法的示意图。FIG. 2 is a schematic diagram of a heat dissipation control method according to an embodiment of the present invention.

具体实施方式Detailed ways

为了使本领域技术人员能够更好的理解本发明,下面结合附图对本发明的具体实施例进行详细描述。In order to enable those skilled in the art to better understand the present invention, specific embodiments of the present invention are described in detail below with reference to the accompanying drawings.

参照图1,图1是根据本发明的实施例的散热系统的示意图。Referring to FIG. 1 , FIG. 1 is a schematic diagram of a heat dissipation system according to an embodiment of the present invention.

根据本发明的实施例,提供了一种用于风力发电机组的散热系统,该散热系统用于同时对轮毂和机舱进行冷却,同时能够通过烟囱效应对塔筒进行一定程度的冷却。According to an embodiment of the present invention, a heat dissipation system for a wind turbine is provided, the heat dissipation system is used to cool the hub and the nacelle at the same time, and at the same time, the tower can be cooled to a certain extent through the chimney effect.

该散热系统包括均安装在机舱3内的叶轮散热装置和机舱散热装置以及安装在机舱3外部的外部散热装置,轮毂15内的热空气经过导风管13的引导而被进入到叶轮散热装置内,并与叶轮散热装置中的流体介质进行换热,冷却后的空气排出到机舱3内。这样,在轮毂15内因一部分空气内吸走,所以产生微负压,外界空气可经过轮毂15上的缝隙进入到轮毂15内,从而降低轮毂15内的温度,对轮毂15内各个部件进行了冷却。The heat dissipation system includes an impeller heat dissipation device and a cabin heat dissipation device both installed in the engine room 3 and an external heat dissipation device installed outside the engine room 3. The hot air in the hub 15 is guided by the air duct 13 and enters the impeller heat dissipation device. , and exchange heat with the fluid medium in the impeller cooling device, and the cooled air is discharged into the nacelle 3 . In this way, a part of the air is sucked away in the hub 15, so a slight negative pressure is generated, and the outside air can enter the hub 15 through the gap on the hub 15, thereby reducing the temperature in the hub 15 and cooling the various components in the hub 15. .

机舱3内的热空气可被直接吸入到机舱散热装置中,并与机舱散热装置中的流体介质进行换热,冷却后的空气排出到机舱3内。这样,机舱3内部温度得以降低,并且冷却了机舱3内的各个部件。The hot air in the nacelle 3 can be directly sucked into the nacelle radiator and exchange heat with the fluid medium in the nacelle radiator, and the cooled air is discharged into the nacelle 3 . In this way, the temperature inside the nacelle 3 is lowered, and various components in the nacelle 3 are cooled.

由于叶轮散热装置和机舱散热装置都将冷却后的空气排出到机舱3内,从而可在机舱3内形成微正压,同时由于轮毂15在进行冷却时可形成微负压,从而机舱3内的空气可流向轮毂15,从而未经处理的外界空气不会进入机舱3,避免了污染机舱3,降低了机舱内部各部件的故障率。Since both the impeller heat sink and the engine room heat sink discharge the cooled air into the engine room 3, a slight positive pressure can be formed in the engine room 3, and at the same time, since the hub 15 can form a slight negative pressure during cooling, the air in the engine room 3 The air can flow to the hub 15, so that the untreated outside air will not enter the nacelle 3, thus avoiding the pollution of the nacelle 3 and reducing the failure rate of various components inside the nacelle.

在叶轮散热装置和机舱散热装置内与热空气进行换热后温度升高的流体介质可流向外部散热装置,以进行冷却,从而被外部散热装置冷却后的流体介质可再流回到叶轮散热装置和机舱散热装置,继续与热空气换热。The fluid medium whose temperature increases after heat exchange with the hot air in the impeller heat sink and the cabin heat sink can flow to the external heat sink for cooling, so that the fluid medium cooled by the external heat sink can flow back to the impeller heat sink And the cabin cooling device, continue to exchange heat with the hot air.

上述流体介质可以具体地为水,或其他合适的冷却剂。The above-mentioned fluid medium may in particular be water, or other suitable coolant.

具体地说,叶轮散热装置可包括叶轮换热风扇12和叶轮换热器11,叶轮换热风扇12通过导风管13吸入轮毂15内的热空气,并使热空气流经叶轮换热器11。这时,由于轮毂15内形成的微负压,外界空气便可进入轮毂15内。热空气可在叶轮换热器11中与低温的流体介质进行换热,之后叶轮换热器11将温度降低后的空气排出到机舱3内,从而实现对轮毂15的散热。叶轮换热器11可通过安装支架8安装到机舱3的顶部。Specifically, the impeller heat dissipation device may include an impeller heat exchange fan 12 and an impeller heat exchanger 11 . The impeller heat exchange fan 12 sucks the hot air in the hub 15 through the air duct 13 and makes the hot air flow through the impeller heat exchanger 11 . At this time, due to the slight negative pressure formed in the hub 15 , the outside air can enter the hub 15 . The hot air can exchange heat with the low-temperature fluid medium in the impeller heat exchanger 11 , and then the impeller heat exchanger 11 discharges the air with reduced temperature into the nacelle 3 , thereby realizing heat dissipation to the hub 15 . The impeller heat exchanger 11 can be mounted to the top of the nacelle 3 by means of the mounting bracket 8 .

叶轮散热装置的管道可具体包括出水管7和回水管4,叶轮换热器11的出入口可分别通过出水管7和回水管4连接到外部散热装置,以实现流体介质的循环。The pipes of the impeller heat dissipation device can specifically include a water outlet pipe 7 and a water return pipe 4, and the inlet and outlet of the impeller heat exchanger 11 can be connected to the external heat dissipation device through the water outlet pipe 7 and the water return pipe 4 respectively, so as to realize the circulation of the fluid medium.

机舱散热装置可包括机舱换热风扇10和机舱换热器9,机舱换热风扇10吸入机舱3内的热空气,并使热空气流经机舱换热器9,这样热空气便可在机舱换热器9中与低温的流体介质进行换热,之后机舱换热器9可将温度降低后的空气排出到机舱3内,从而实现对机舱3的散热。同样,机舱换热器9可通过安装支架8安装到机舱3的顶部。The cabin heat dissipation device may include a cabin heat exchange fan 10 and a cabin heat exchanger 9. The cabin heat exchange fan 10 sucks the hot air in the cabin 3 and makes the hot air flow through the cabin heat exchanger 9, so that the hot air can be exchanged in the cabin. The heat exchanger 9 exchanges heat with the low-temperature fluid medium, and then the engine room heat exchanger 9 can discharge the air whose temperature has been lowered into the engine room 3 , so as to realize the heat dissipation of the engine room 3 . Likewise, the nacelle heat exchanger 9 can be mounted to the top of the nacelle 3 by means of the mounting brackets 8 .

机舱散热装置的管道可具体包括出水管7和回水管4,机舱换热器9的出入口可分别通过出水管7和回水管4连接到外部散热装置,以实现流体介质的循环。机舱换热器9的出水管和回水管与叶轮换热器11的出水管和回水管可共享同一出水管和同一回水管。The pipes of the engine room heat dissipation device may specifically include a water outlet pipe 7 and a water return pipe 4, and the inlet and outlet of the engine room heat exchanger 9 can be connected to the external heat dissipation device through the water outlet pipe 7 and the water return pipe 4 respectively, so as to realize the circulation of the fluid medium. The water outlet pipe and the water return pipe of the engine room heat exchanger 9 and the water outlet pipe and the water return pipe of the impeller heat exchanger 11 may share the same water outlet pipe and the same water return pipe.

外部散热装置可包括外部换热器6,以将从叶轮换热器11和机舱换热器9中流出的温度升高的流体介质与外部空气进行换热,从而降低流体介质的温度。The external heat sink may include an external heat exchanger 6 to exchange heat with the external air of the fluid medium with increased temperature flowing from the impeller heat exchanger 11 and the nacelle heat exchanger 9, thereby reducing the temperature of the fluid medium.

具体地说,叶轮换热器11和机舱换热器9中温度升高的流体介质经出水管7流到外部换热器6中,在与外界空气换热而温度降低之后,流体介质经回水管4流回到叶轮换热器11和机舱换热器9中。Specifically, the fluid medium whose temperature is increased in the impeller heat exchanger 11 and the engine room heat exchanger 9 flows into the external heat exchanger 6 through the water outlet pipe 7, and after the heat exchange with the outside air and the temperature decreases, the fluid medium flows back to the external heat exchanger 6. The water pipe 4 flows back into the impeller heat exchanger 11 and the nacelle heat exchanger 9 .

为了促使管道内的流体介质流动,可在出水管7上设置电动泵5,从而能够加速散热系统中的流体介质在机舱内换热器与机舱外换热器之间循环流动,促进散热。In order to promote the flow of the fluid medium in the pipeline, an electric pump 5 can be provided on the water outlet pipe 7, so that the fluid medium in the heat dissipation system can be accelerated to circulate between the heat exchanger in the cabin and the heat exchanger outside the cabin to promote heat dissipation.

另外,在导风管13上可以设置网罩14。In addition, a mesh cover 14 may be provided on the air duct 13 .

同时,上述叶轮散热装置、机舱散热装置和外部散热装置的数量可根据实际安装情况和散热需求适当地设置,例如,可设置两个机舱散热装置。At the same time, the numbers of the above-mentioned impeller heat sinks, cabin heat sinks and external heat sinks may be appropriately set according to the actual installation situation and heat dissipation requirements, for example, two engine room heat sinks may be set.

当需要进行散热时,叶轮换热风扇12将轮毂15内的热空气经由导风管吸入到叶轮换热器11中,使得热空气在叶轮换热器11中与温度相对低的流体介质进行热交换,之后冷却后的空气可被排出到机舱3内,而轮毂15内由于一部分空气被吸走而形成一定负压,在负压作用下,外界空气可流入到轮毂15内,从而降低了轮毂15内的空气温度和内部件的温度。在机舱3内的空气温度达到需要进行散热的温度时,机舱换热风扇10吸入机舱3内的热空气,使得热空气在机舱换热器9中与温度相对较低的流体介质进行热交换,而冷却后的空气可被排出到机舱3内,从而降低了机舱3内的空气温度和内部件的温度。When heat dissipation is required, the impeller heat exchange fan 12 sucks the hot air in the hub 15 into the impeller heat exchanger 11 through the air duct, so that the hot air is heated with the relatively low temperature fluid medium in the impeller heat exchanger 11 After exchange, the cooled air can be discharged into the cabin 3, and a certain negative pressure is formed in the hub 15 due to a part of the air being sucked away. Under the action of the negative pressure, the outside air can flow into the hub 15, thereby reducing the hub 15 Air temperature inside and temperature of internal components. When the air temperature in the nacelle 3 reaches the temperature that needs to be dissipated, the nacelle heat exchange fan 10 inhales the hot air in the nacelle 3, so that the hot air exchanges heat with the relatively low temperature fluid medium in the nacelle heat exchanger 9, The cooled air can be discharged into the nacelle 3, thereby reducing the air temperature in the nacelle 3 and the temperature of the internal components.

从叶轮换热器11和机舱换热器9内流出的温度较高的流体介质在电动泵5的作用下经由出水管7流到外部换热器6中,从而在外部换热器6中与外部空气换热,这样,流体介质的温度得以降低,之后经由回水管4再次流回到叶轮换热器11和机舱换热器9中,继续进行换热。The fluid medium with higher temperature flowing out from the impeller heat exchanger 11 and the engine room heat exchanger 9 flows into the external heat exchanger 6 through the water outlet pipe 7 under the action of the electric pump 5 , so as to be combined with the external heat exchanger 6 in the external heat exchanger 6 . The external air exchanges heat, so that the temperature of the fluid medium is lowered, and then flows back to the impeller heat exchanger 11 and the cabin heat exchanger 9 through the return pipe 4 to continue heat exchange.

同时,由于轮毂15内的负压和机舱3内正压作用,从而可以在轮毂15内部和机舱3内形成空气循环。At the same time, due to the action of the negative pressure in the hub 15 and the positive pressure in the nacelle 3 , air circulation can be formed inside the hub 15 and the nacelle 3 .

另外,在风力发电机组的塔筒1内,也存在发热部件,例如电控柜和电缆等部件,塔筒1内的热空气可通过烟囱效应向上进入到机舱3内,这些热空气便可由机舱换热器9散热,温度得以降低,机舱散热装置在对机舱3进行散热的同时也降低了塔筒1内的温度。In addition, there are also heat-generating components in the tower 1 of the wind turbine, such as electrical control cabinets and cables. The hot air in the tower 1 can enter the nacelle 3 upward through the chimney effect, and these hot air can be released from the nacelle. The heat exchanger 9 dissipates heat, and the temperature is lowered. The nacelle heat sink radiates heat to the nacelle 3 and also reduces the temperature in the tower 1 .

根据本发明的另一实施例,提供了一种控制上述散热系统的散热控制方法,下面参照图2对该方法进行描述。According to another embodiment of the present invention, a heat dissipation control method for controlling the above heat dissipation system is provided, and the method will be described below with reference to FIG. 2 .

当轮毂15内的温度小于T1时,可不启动上述散热系统进行散热,叶轮换热风扇12、叶轮换热器11以及机舱换热风扇10和机舱换热器9可不开启,电动泵5也不启动。When the temperature in the hub 15 is lower than T1, the above-mentioned heat dissipation system may not be activated for heat dissipation, the impeller heat exchange fan 12, the impeller heat exchanger 11, the cabin heat exchange fan 10 and the cabin heat exchanger 9 may not be turned on, and the electric pump 5 may not be turned on either. .

当轮毂15内的温度达到T1时,启动叶轮散热装置和外部散热装置,对轮毂15的内部空间进行散热。具体地,启动叶轮换热风扇12、叶轮换热器11和外部换热器6,轮毂15内的热空气在叶轮换热器11中与流体介质换热,温度降低后的空气被排放到机舱3内,而外界空气由于轮毂15内的负压进入轮毂15内,从而降低轮毂15内的温度。When the temperature in the hub 15 reaches T 1 , the impeller heat dissipation device and the external heat dissipation device are activated to dissipate heat in the inner space of the hub 15 . Specifically, the impeller heat exchange fan 12, the impeller heat exchanger 11 and the external heat exchanger 6 are activated, the hot air in the hub 15 exchanges heat with the fluid medium in the impeller heat exchanger 11, and the air whose temperature is lowered is discharged to the nacelle 3, and the outside air enters into the hub 15 due to the negative pressure in the hub 15, thereby reducing the temperature in the hub 15.

当机舱3内的温度达到T2时,其中,T2大于T1,进一步启动机舱散热装置,对机舱3进行散热。具体地,启动机舱换热风扇10和机舱换热器9,机舱3内的热空气在机舱换热器9中与流体介质换热,温度降低后的空气被排放机舱3内,从而降低机舱3内的温度。When the temperature in the cabin 3 reaches T 2 , where T 2 is greater than T 1 , the cabin heat dissipation device is further activated to dissipate heat in the cabin 3 . Specifically, the engine room heat exchange fan 10 and the engine room heat exchanger 9 are activated, the hot air in the engine room 3 exchanges heat with the fluid medium in the engine room heat exchanger 9, and the air whose temperature is lowered is discharged into the engine room 3, thereby reducing the temperature of the engine room 3. temperature inside.

当机舱3内的温度达到T5时,其中,T5大于T2,进一步启动电动泵5,从而加速管道内流体介质的流动,促进叶轮换热器11、机舱换热器9和外部换热器6中的换热,使轮毂15和机舱3内的温度更快地降低。When the temperature in the nacelle 3 reaches T 5 , where T 5 is greater than T 2 , the electric pump 5 is further started, thereby accelerating the flow of the fluid medium in the pipeline, promoting the impeller heat exchanger 11 , the nacelle heat exchanger 9 and the external heat exchange The heat exchange in the generator 6 reduces the temperature in the hub 15 and the nacelle 3 more quickly.

当机舱3内的温度达到风力发电机组的最高极限温度T3时,风力发电机组停止运行,避免机组因高温发生故障。When the temperature in the nacelle 3 reaches the highest limit temperature T3 of the wind power generator set, the wind power generator set stops running to avoid the fault of the wind power generator set due to high temperature.

在机组停机期间,利用散热系统继续对机舱和轮毂进行散热,当机舱3内的温度从T3回落到T2时,这时机舱3内的温度不再过高,停用机舱换热装置,此外,还可以进一步停用电动泵5。During the shutdown of the unit, the heat dissipation system is used to continue to dissipate the heat of the engine room and the hub. When the temperature in the engine room 3 drops from T3 to T2, the temperature in the engine room 3 is no longer too high, and the engine room heat exchange device is deactivated. In addition, the electric pump 5 can be further deactivated.

当机舱3内的温度进一步从T2回落到T4时,其中,T4小于T1,此时机舱和轮毂内的温度都相对较低,可不再进行散热,因而可停用叶轮散热装置,至此散热系统停止运行。When the temperature in the nacelle 3 further drops from T 2 to T 4 , where T 4 is smaller than T 1 , the temperatures in the nacelle and the hub are relatively low, and heat dissipation can no longer be performed, so the impeller cooling device can be disabled, At this point the cooling system stops working.

需要说明的是,在上述控制过程期间,需要实时测量轮毂和机舱内的温度,因此,在散热系统中设置有测量温度的多个温度传感器,这些温度传感器可将温度数据传送到风力风电机组的电控柜,电控柜根据这些数据控制各个换热风扇和换热器以及电动泵等部件的操作,从而控制散热过程。It should be noted that during the above control process, the temperature in the hub and the nacelle needs to be measured in real time. Therefore, a plurality of temperature sensors for measuring temperature are provided in the cooling system, and these temperature sensors can transmit the temperature data to the wind turbine. The electric control cabinet, according to these data, controls the operation of each heat exchange fan, heat exchanger, electric pump and other components, thereby controlling the heat dissipation process.

根据本发明的另一实施例,还提供了一种风力发电机组,该风力发电机组具有上述散热系统并采用上述散热控制方法,对轮毂、机舱和塔筒进行散热,维持机组处于适于发电的温度范围内。According to another embodiment of the present invention, a wind turbine generator set is also provided. The wind turbine generator set has the above-mentioned heat dissipation system and adopts the above-mentioned heat dissipation control method to dissipate heat from the hub, the nacelle and the tower, so as to maintain the generator set in a condition suitable for power generation. within the temperature range.

通过本发明所提供的散热系统和方法,在将各个散热装置均安装在机舱内的情况下,实现了同时对轮毂和机舱进行散热,简化了轮毂的装配,并降低了散热装置的故障率。另外,能够根据轮毂和机舱内的温度变化,选择合适的散热方式,自动智能化地对散热过程进行控制。With the heat dissipation system and method provided by the present invention, under the condition that each heat dissipation device is installed in the nacelle, the hub and the nacelle can be dissipated at the same time, the assembly of the wheel hub is simplified, and the failure rate of the heat dissipation device is reduced. In addition, according to the temperature changes in the wheel hub and the cabin, the appropriate heat dissipation method can be selected, and the heat dissipation process can be controlled automatically and intelligently.

上面对本发明的具体实施方式进行了详细描述,虽然已表示和描述了一些实施例,但本领域技术人员应该理解,在不脱离由权利要求及其等同物限定其范围的本发明的原理和精神的情况下,可以对这些实施例进行修改和完善,这些修改和完善也应在本发明的保护范围内。The specific embodiments of the present invention have been described in detail above. Although some embodiments have been shown and described, those skilled in the art should understand that the principles and spirit of the present invention, which are defined in the scope of the claims and their equivalents, are not departed from. Under the circumstances, these embodiments can be modified and perfected, and these modifications and improvements should also fall within the protection scope of the present invention.

Claims (12)

1. a kind of cooling system for wind power generating set characterized by comprising
Impeller radiator is mounted in the cabin (3) of wind power generating set, and the heat in the wheel hub (15) of wind power generating set is empty Gas be introduced in the impeller radiator by guide duct (13) and with the fluid media (medium) in the impeller radiator Heat exchange;
Cabin heat dissipation device is mounted in the cabin (3), and the hot-air in the cabin (3) is inhaled into the cabin and dissipates Thermal simultaneously exchanges heat with the fluid media (medium) in the cabin heat dissipation device,
Wherein, the impeller radiator includes:
Impeller heat exchanger (11) makes hot-air and the fluid media (medium) heat exchange from the wheel hub (15) and arranges the air after cooling In to the cabin (3);
Impeller hot-swappable fans (12), by the guide duct (13) by the blowing hot air in the wheel hub (15) to the impeller Heat exchanger (11).
2. cooling system according to claim 1, which is characterized in that the cooling system further includes external radiating device, The external radiating device is mounted on the cabin (3) outside, with the cooling impeller radiator and the cabin heat dissipation device In the fluid media (medium) being heated.
3. cooling system according to claim 2, which is characterized in that the impeller radiator further include:
Pipeline, the trandfer fluid medium between the impeller heat exchanger (11) and the external radiating device.
4. cooling system according to claim 2, which is characterized in that the cabin heat dissipation device includes:
Cabin heat exchanger (9) makes hot-air and fluid media (medium) in the cabin (3) exchange heat and the air after cooling is discharged to machine In cabin (3);
Cabin hot-swappable fans (10), by the blowing hot air in the cabin (3) to the cabin heat exchanger (9);
Pipeline, the trandfer fluid medium between the cabin heat exchanger (9) and the external radiating device.
5. cooling system according to claim 3 or 4, which is characterized in that electrodynamic pump (5) are provided on the pipeline, So that fluid media (medium) flows in the pipeline.
6. cooling system according to claim 1, which is characterized in that the impeller radiator and cabin heat radiation dress Set the top being mounted in the cabin (3).
7. cooling system according to claim 2, which is characterized in that the external radiating device includes external heat exchanger (6), make to exchange heat from the impeller radiator and the received fluid media (medium) of the cabin heat dissipation device and outside air.
8. a kind of cooling control method for wind power generating set, which is characterized in that the cooling control method control is as weighed Benefit require any one of 1 to 7 described in cooling system operation, comprising:
Temperature in the wheel hub (15) reaches T1When, start the impeller radiator;
Temperature in the cabin (3) of wind power generating set, which reaches, compares T1Big T2When, start the cabin heat dissipation device;
Temperature in the cabin (3) reaches the highest threshold temperature T of wind power generating set3When, stop wind power generating set Machine;
Temperature in the cabin (3) is from T3Drop to T2When, deactivate the cabin heat dissipation device;
Temperature in the cabin (3) is from T2Drop to and compares T1Small T4When, deactivate the impeller radiator.
9. cooling control method according to claim 8, which is characterized in that the temperature in the wheel hub (15) reaches T1 When, start external radiating device.
10. cooling control method according to claim 9, which is characterized in that the temperature in the cabin (3) reaches ratio T2Greatly and compare T3Small T5When, start electrodynamic pump (5).
11. cooling control method according to claim 10, which is characterized in that temperature in the cabin (3) is from T3Under Drop to T2When, also deactivate the electrodynamic pump (5).
12. a kind of wind power generating set, which is characterized in that including the cooling system as described in any one of claims 1 to 7.
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