WO2023272992A1 - Nacelle assembly and wind turbine set - Google Patents

Nacelle assembly and wind turbine set Download PDF

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Publication number
WO2023272992A1
WO2023272992A1 PCT/CN2021/121862 CN2021121862W WO2023272992A1 WO 2023272992 A1 WO2023272992 A1 WO 2023272992A1 CN 2021121862 W CN2021121862 W CN 2021121862W WO 2023272992 A1 WO2023272992 A1 WO 2023272992A1
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WO
WIPO (PCT)
Prior art keywords
nacelle
nacelle assembly
unit
assembly
cabin
Prior art date
Application number
PCT/CN2021/121862
Other languages
French (fr)
Chinese (zh)
Inventor
马加伟
时洪奎
Original Assignee
新疆金风科技股份有限公司
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Publication date
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Publication of WO2023272992A1 publication Critical patent/WO2023272992A1/en

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D9/00Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
    • F03D9/20Wind motors characterised by the driven apparatus
    • F03D9/25Wind motors characterised by the driven apparatus the apparatus being an electrical generator
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D13/00Assembly, mounting or commissioning of wind motors; Arrangements specially adapted for transporting wind motor components
    • F03D13/20Arrangements for mounting or supporting wind motors; Masts or towers for wind motors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D80/00Details, components or accessories not provided for in groups F03D1/00 - F03D17/00
    • F03D80/80Arrangement of components within nacelles or towers
    • F03D80/82Arrangement of components within nacelles or towers of electrical components
    • 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
    • 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
    • Y02E10/728Onshore wind turbines

Definitions

  • the present application relates to the technical field of wind power, in particular to a nacelle assembly and a wind power generating set.
  • the current solution for the nacelle assembly is to enlarge the size simultaneously.
  • the continued enlargement of components such as the nacelle assembly will lead to excessive size and weight of related components.
  • Due to the limitation of land transportation the land-based unit will not be able to transport the large cabin assembly, or in order to meet the needs of land transportation, roads, toll stations, tunnels and bridges need to be rebuilt, which greatly increases the transportation cost, which in turn leads to wind power.
  • the overall cost is rising rapidly.
  • the difficulty of designing and processing components has also increased rapidly, which eventually led to a rapid increase in the cost of wind turbines.
  • the embodiment of the present application provides a nacelle assembly and a wind power generating set.
  • the nacelle assembly can meet the high power requirement of the wind power generating set, and has low cost and is convenient for processing and transportation.
  • a nacelle assembly is proposed for a wind power generating set, the wind power generating set includes a tower and a generator, and the nacelle assembly includes: a connecting seat, which is used to connect the tower and the generator ;
  • the nacelle unit, the number of the nacelle units is multiple and respectively arranged on the connection seat, each nacelle unit includes a nacelle cover and a functional device, the nacelle cover has a receiving cavity, the functional device is at least partly located in the receiving cavity and is used for electrical connection with the generator.
  • a wind power generating set including: a tower; the above-mentioned nacelle assembly, the nacelle assembly is arranged on the tower; a yaw system, connected to the tower and a connecting seat; a generator, It includes a rotationally matched rotor, a stator, and an interface electrically connected to the rotor and the stator.
  • the stator is connected to the connecting seat, and the functional devices of each nacelle unit are electrically connected to the interface; the impeller is connected to the rotor.
  • the nacelle assembly includes a connecting seat and a nacelle unit, the connecting seat is used to connect the tower and the generator, and the number of the nacelle units is multiple and connected to the connecting seat respectively, Since each nacelle cover has an accommodating cavity, and a functional device connected to the generator is installed in the accommodating cavity, the electrical energy converted by the generator can be post-processed by using the functional device, and the number and specifications of the nacelle units can be adjusted to meet the The high power demand of the generator, meanwhile, the nacelle unit can be processed, manufactured and transported separately, the cost is low, and it is beneficial to the overall design, processing and transportation of the nacelle assembly.
  • Fig. 1 is an axonometric view of a wind power generating set according to an embodiment of the present application
  • Fig. 2 is a schematic cross-sectional structure diagram of a wind power generating set according to an embodiment of the present application
  • Fig. 3 is an axonometric view of a nacelle assembly of an embodiment of the present application
  • Fig. 4 is a structural schematic view of the nacelle assembly with the protective cover removed according to one embodiment of the present application;
  • Fig. 5 is a schematic diagram of a partial structure of a nacelle assembly according to an embodiment of the present application.
  • Fig. 6 is a schematic structural view of a nacelle assembly according to another embodiment of the present application.
  • Support frame 23.
  • Horizontal profile 232.
  • Vertical profile 232.
  • orientation words appearing in the following description are all directions shown in the figure, and are not intended to limit the specific structure of the nacelle assembly and the wind power generating set of the present application.
  • the terms “installation” and “connection” should be understood in a broad sense, for example, it can be a fixed connection or a detachable connection, or Connected integrally; either directly or indirectly.
  • the specific meanings of the above terms in this application can be understood according to specific situations.
  • the embodiment of the present application provides a wind power generating set, including a tower 200, a nacelle assembly 100, a yaw system (not shown), a generator 400 and an impeller 300, and the nacelle assembly 100 Set on the tower 200.
  • the yaw system is connected between the tower 200 and the nacelle assembly 100, so that the nacelle assembly 100 is indirectly connected to the tower 200 through the yaw system.
  • the generator 400 includes a rotationally fitted rotor 410, a stator 420, and an interface electrically connected to the rotor 410 and the stator 420.
  • the stator 420 is connected to the nacelle assembly 100, and the impeller 300 is connected to the rotor 410.
  • the impeller 300 includes a hub 310 and The blade 320 and the impeller 300 are connected with the rotor 410 of the generator 400 through the hub 310 .
  • the current solution for the nacelle assembly of wind turbines is to enlarge the size simultaneously.
  • the continued enlargement of components such as the nacelle assembly will lead to excessive size and weight of related components.
  • Due to the limitation of land transportation the land crew will not be able to transport the large cabin assembly.
  • the difficulty of designing and processing components has also increased rapidly, which eventually led to a rapid increase in the cost of wind turbines.
  • the embodiment of the present application also provides a new nacelle assembly 100, which can meet the high power requirements of wind turbines, and is convenient for design, processing and transportation.
  • the nacelle assembly 100 can be produced and sold as an independent component, and of course it can also be used in a wind power generating set as a component of the wind generating set.
  • the nacelle assembly 100 provided by the embodiment of the present application includes a connecting seat 10 and a nacelle unit 20 , and the connecting seat 10 is used for connecting the tower 200 and the generator 400 .
  • the number of cabin units 20 is multiple and are respectively arranged on the connecting seat 10.
  • Each cabin unit 20 includes a cabin cover 21 and a functional device 22.
  • the cabin cover 21 has a receiving cavity 211.
  • the functional device 22 is at least partially located in the receiving cavity 211 and is used to communicate with the
  • the generator 400 is electrically connected, and the functional device 22 can post-process the electric energy converted by the generator.
  • each nacelle unit 20 can be electrically connected to the interface of the generator 400 . Since each nacelle cover 21 has an accommodating cavity 211, and a functional device 22 connected to the generator 400 is arranged in the accommodating cavity 211, the electrical energy converted by the generator 400 can be post-processed by using the functional device 22, and the generator can meet the 400 high power requirements, and at the same time the nacelle unit 20 can be processed and manufactured separately, the cost is low and it is convenient for processing and transportation.
  • the functional device 22 thereof includes at least one of a transformer 222 and a converter 221 . It may include a transformer 222, and may also include a converter 221. Certainly, in some embodiments, the transformer 222 and the converter 221 may also be included at the same time.
  • the transformer 222 and the converter 221 of each functional device 22 are electrically connected to the generator 400 .
  • the transformer 222 can be used to change the AC voltage (current) of a certain value of the generator 400 into another voltage (current) with the same frequency or several different values (current).
  • the converter 221 may be added to the excitation device on the side of the rotor 410 of the generator 400 .
  • the functional device 22 includes a transformer 222 and a converter 221
  • the electric energy converted by the generator 400 can first enter the converter 221, then from the converter 221 to the transformer 222, and then enter the step-up station and the subsequent power grid .
  • the connecting seat 10 includes a seat body 11 and a hollow cavity formed by the seat body 11, the seat body 11 has a first free end 12, a second Two free ends 13 and a plurality of nacelle interfaces 14 at least partially located between the first free end 12 and the second free end 13 .
  • the first free end 12 is used for connecting with the tower 200
  • the second free end 13 is used for connecting with the generator 400
  • each nacelle unit 20 is connected to one of the nacelle interfaces 14 .
  • connection seat 10 adopts the above-mentioned structural form, and can meet the connection requirements with each cabin unit 20 by using the cabin interface 14 .
  • the correspondingly provided first free end 12 can be connected to the tower 200
  • the second free end 13 can be connected to the generator 400 to meet the connection requirements of each nacelle unit 20 with the tower 200 and the generator 400 .
  • the first free end 12 of the nacelle assembly 100 provided in the embodiment of the present application can adopt an annular flange structure.
  • the first free end 12 in the form of an annular flange structure it can facilitate the Detachable connection between assembly 100 and tower 200 .
  • the second free end 13 may adopt an annular flange structure. Since the second free end 13 needs to be connected with the stator 420 of the generator 400, by adopting the annular method
  • the flange structure facilitates the detachable connection between the second free end 13 and the stator 420 of the generator 400, ensures the connection strength between the two, and is convenient for assembly, disassembly and maintenance.
  • the axis of the first free end 12 and the axis of the second free end 13 are arranged to intersect.
  • the connection between the tower 200 and the generator 400 can be realized according to the distribution of the two.
  • the number of nacelle interfaces 14 can be set according to the number of nacelle units 20 , as long as the connection requirements with each nacelle unit 20 can be met.
  • the nacelle cover 21 of each nacelle unit 20 can adopt different shapes, which have accommodating cavities 211 and can satisfy the installation of functional devices 22 and direct contact with the connecting seat 10. Or indirect connection requirements are available.
  • the nacelle cover 21 may adopt a hollow box structure. In some optional embodiments, it may adopt a hollow square structure.
  • each nacelle unit 20 further includes an environmental control system 223, and the environmental control system 223 is configured to adjust the temperature, humidity and air in the accommodating chamber 211.
  • the environment control system 223 can be used to adjust at least one of the temperature, humidity and salinity of the internal environment of the accommodation chamber 211 corresponding to the cabin unit 20, so that the environment in the accommodation chamber 211 The environment is always within the preset range to avoid damage to the functional device 22 due to the value of at least one of temperature, humidity and salinity exceeding the preset range, improve the safety and service life of the cabin assembly 100, and reduce Maintenance costs.
  • the environmental control system 223 includes a heat dissipation device, which is arranged on the nacelle cover 21 and configured to adjust the temperature in the accommodating chamber 211 so that each The temperature in the accommodating cavity 211 of each cabin unit 20 is moderate, so as to avoid damage to the functional devices 22 caused by excessive temperature.
  • the environmental control system 223 may also include a dehumidifier, which is arranged on the nacelle cover 21 and configured to adjust the humidity in the accommodation chamber 211.
  • the humidity in the chamber 211 can always be kept at the lowest level, so as to prevent the functional devices 22 from being corroded or even short-circuited at the connection interface between the functional devices 22 or between the functional devices 22 and the generator 400 due to excessive humidity.
  • the environmental control system 223 may also include a desalter, which is arranged on the nacelle cover 21 and is configured to adjust the salt content in the air in the accommodating cavity 211 to prevent the accommodating of each nacelle unit 20 Excessive salt content in the cavity 211 leads to corrosion of the functional device 22 and protects the functional device 22 .
  • a desalter which is arranged on the nacelle cover 21 and is configured to adjust the salt content in the air in the accommodating cavity 211 to prevent the accommodating of each nacelle unit 20 Excessive salt content in the cavity 211 leads to corrosion of the functional device 22 and protects the functional device 22 .
  • each nacelle unit 20 can install and support the functional device 22 through the nacelle cover 21 itself, and at the same time be directly connected to the connecting seat 10 through the nacelle cover 21, of course this is An optional embodiment.
  • each nacelle unit 20 may also include a support frame 23, the support frame 23 is arranged in the accommodating cavity 211 and connected with the nacelle cover 21, the support frame 23 is at least partially protruded from the nacelle cover 21 and set and Connect with the cabin interface 14.
  • the nacelle assembly 100 provided in the embodiment of the present application can increase the overall strength of the nacelle unit 20 by providing a support frame 23 inside each nacelle unit 20 and connecting it to the nacelle cover 21 . To ensure its anti-load capacity and improve the safety performance of the nacelle assembly 100 .
  • the connection requirements between the nacelle unit 20 and the nacelle interface 14 can be ensured, and the entire wall of the nacelle cover 21 can be Making it thicker and thinner can reduce the overall weight and cost of the nacelle cover 21 , and at the same time, can reduce the risk of damage to the nacelle cover 21 caused by the direct connection of the nacelle cover 21 to the nacelle interface 14 .
  • the supporting frame 23 may adopt a hollow frame structure, which has high strength, light weight and low cost.
  • the supporting frame 23 may be composed of criss-cross profiles connected, and part of the profiles may protrude from the nacelle cover 21 and be connected to the nacelle interface 14 .
  • the support frame 23 may include a plurality of longitudinal profiles 232 and a plurality of transverse profiles 231, the plurality of longitudinal profiles 232 are distributed at intervals along the extending direction of the transverse profiles 231, and the plurality of transverse profiles 231 are The extending direction is distributed at intervals, and each transverse profile 231 intersects with each longitudinal profile 232 and is connected to each other.
  • one of the nacelle interface 14 and the support frame 23 includes a plug-in protrusion, and the other includes a plug-in slot, and the plug-in protrusion and the plug-in slot
  • the shape of the slots matches and plugs into the connection.
  • the cabin interface 14 can be made to include a plurality of connection blocks, and each connection block is provided with an insertion slot, so that the support frame 23 is provided with an insertion protrusion, by inserting the insertion protrusion into the insertion slot Realize the connection between the connection seat 10 and the contact interface.
  • the supporting frame 23 includes longitudinal profiles 232
  • at least a part of the longitudinal profiles 232 may protrude from the nacelle cover 21 and form insertion protrusions.
  • the insertion protrusion is formed on the nacelle interface 14 , as long as it can meet the connection requirements between the support frame 23 and the nacelle interface 14 .
  • the functional devices 22 of each nacelle unit 20 such as the transformer 222, the converter 221 and the environment control system 223 can be combined with the nacelle cover 21 connect.
  • components such as the functional device 22 and the environmental control system 223 can also be arranged on the support frame 23. Since the support frame 23 is located at the nacelle cover 21, the support frame 23 can be placed horizontally, and can be placed toward the functional device 22 and The environmental control system 223 and the like provide a horizontal support surface, which facilitates the assembly and disassembly of the functional device 22 and the environmental control system 223 .
  • disposing the functional device 22 and the environmental control system 223 on the supporting frame 23 is also beneficial to heat dissipation of the functional device 22 and other components, and improves the safety performance of the nacelle unit 20 .
  • the nacelle assembly 100 since the nacelle assembly 100 works outdoors when it is used in a wind power generating set, in order to protect the connecting seat 10 and avoid damage to the connecting seat 10 caused by natural factors such as rainwater outside, the nacelle assembly
  • the unit 100 also includes a protective cover 30 , the protective cover 30 is arranged to cover the connection seat 10 , and the protective cover 30 is provided with an escape opening corresponding to each cabin unit 20 .
  • the connection seat 10 can be protected, which can prevent the wind, frost, snow and rain in the natural environment from corroding the connection seat 10, and at the same time prevent rainwater from entering the generator 400, the tower 200 and other equipment through the connection seat 10. interior, improving the safety performance of the nacelle assembly 100 and the wind power generating set.
  • the protective cover 30 can adopt various structural forms, which can be a hollow shell structure, and the protective cover 30 is arranged to cover the connecting seat 10,
  • the protective cover 30 can be connected with the connection base 10 , and can prevent the connection between the connection base 10 and the nacelle unit 20 , the tower 200 and the generator 400 from interfering.
  • the implementation of the present application further includes a control cabinet 40, the functional device 22 of at least one cabin unit 20 is electrically connected to the control cabinet 40, and the corresponding functional device 22 is controlled through the control cabinet 40.
  • the control cabinet 40 can be arranged inside the protective cover 30 .
  • connection between the nacelle unit 20 and the nacelle interface 14 is to adopt one including a plug-in protrusion, and the other includes a plug-in slot, and the plug-in slot
  • the connecting protrusion matches the shape of the socket slot and is plugged and connected. This is an optional implementation mode, but is not limited to the above-mentioned mode.
  • the cabin interface 14 may also include a first flange
  • the support frame 23 may include a second flange
  • the first flange and The shapes of the second flanges are matched and connected to each other, which can also meet the connection requirements between each nacelle unit 20 and the connecting seat 10 .
  • the number of nacelle units 20 included therein can be set according to the power demand of the applied wind power generating set.
  • the nacelle assembly 100 may include two nacelle units 20, and the functional device 22 of each nacelle unit 20 can convert the generator 400
  • the post-processing upper limit of electric energy is 3MW, and the two 3MW nacelle units 20 can meet the post-processing requirements of the generator 400 of the 6MW generating set to convert electric energy, thereby satisfying the power demand of the 6MW generating set.
  • the nacelle assembly 100 can also include two nacelle units 20, and the functional device 22 of one nacelle unit 20 can control the generator 400.
  • the post-processing upper limit of the converted electric energy is 3MW, and the functional device 22 of the other nacelle unit 20 can post-process the converted electric energy of the generator 400 up to 4.5MW, thereby meeting the power demand of the 7.5MW unit.
  • the nacelle assembly 100 can include three nacelle units 20, and the functional device 22 of one nacelle unit 20 can convert the electrical energy of the generator 400
  • the post-processing upper limit of the engine room unit 20 is 8MW, and the functional device 22 of the other nacelle unit 20 can convert the electrical energy of the generator 400.
  • the upper limit of post-processing is 1.5MW, which can meet the power demand of 14MW units.
  • the nacelle assembly 100 Since the upper limit of post-processing of the functional device 22 is lower, its cost, processing difficulty, and transportation difficulty are relatively low, and the higher the post-processing upper limit, its cost, processing difficulty, and transportation difficulty will be doubled. If the existing nacelle assembly 100 is used to form a 14MW unit, then the post-processing upper limit of the functional device 22 of the nacelle assembly 100 for post-processing the electric energy converted by the generator 400 will be 14MW, which will result in a The volume of the functional devices 22 such as the cover 21 , the converter 221 , and the transformer 222 is very large, and the requirements for transportation, production and processing are very high. However, the nacelle assembly 100 provided by the embodiment of the present application is in the form of a plurality of nacelle units 20 with post-processing functions, which can meet the high power demand of the wind power generating set.
  • the connecting seat 10 has an axisymmetric structure and has a center line aa, and the number of cabin units 20 is n; where n is greater than or equal to 2
  • n cabin units 20 are divided into two unit groups, each unit group includes at least one cabin unit 20, and the two unit groups are symmetrically distributed on both sides of the central line aa.
  • each unit group may include one cabin unit 20 , and two cabin units 20 are symmetrically distributed on both sides of the central line aa.
  • each group of unit groups can be made to include 2 cabin units 20, wherein the cabin unit 20 of one group of unit groups is connected with another group of unit groups.
  • the cabin units 20 of the unit group are symmetrically distributed on both sides of the central line aa.
  • n is an even number.
  • n may also be an odd number.
  • n is an odd number greater than 2
  • n-1 cabin units 20 are divided into two groups of units, each group of units includes at least one cabin unit 20, and the two groups of units are symmetrically distributed on both sides of the central line aa, leaving one cabin unit 20 It is connected to the area where the connection base 10 is located between the two groups of units.
  • each group of unit groups includes two cabin units 20, wherein one group of units The two cabin units 20 of one group and the two cabin units 20 of another unit group are symmetrically distributed on both sides of the center line aa, and the remaining one cabin unit 20 is connected to the connecting seat 10 in the area between the two groups of units, optional Accordingly, the center of the remaining one cabin unit 20 can be located on the center line aa, further preventing the connecting seat 10 from bearing unbalanced load.
  • the arrangement of the above-mentioned plurality of cabin units 20 on the connecting seat 10 is only an optional way, and is not limited to the above-mentioned way.
  • the racks are arranged at intervals in the axial direction, and the projections of each other in the axial direction may at least partially overlap, of course, they may also be arranged in a staggered manner, whichever meets the performance requirements of the nacelle assembly 100 .
  • the generator 400 of the wind power generating set provided in the embodiment of the present application may include multiple windings, and each winding is electrically connected to the functional device 22 of one of the nacelle units 20 through an interface.
  • the electrical connection between the nacelle unit 20 and the generator 400 can be more facilitated, and the post-processing requirements for the electric energy converted by the generator 400 can be met.
  • the connecting seat 10 is used to connect the tower 200 and the generator 400, and the number of the nacelle units 20 is multiple and connected to the connecting seat 10 respectively. It has an accommodating chamber 211, and a functional device 22 connected to the generator 400 is arranged in the accommodating chamber 211, and the electric energy converted by the generator 400 can be post-processed by using the functional device 22, and the quantity and specifications of the nacelle units 20 can be adjusted to meet the The high power demand of the generator 400 and the nacelle unit 20 can be manufactured and transported separately, which is beneficial to the processing and transportation of the nacelle assembly 100 as a whole.
  • the wind power generating set provided by the embodiments of the present application includes the nacelle assembly 100 provided by the above embodiments, and on the basis of meeting its own high power requirements, it is low in production and transportation costs, easy to maintain, and high in power generation efficiency.

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  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Wind Motors (AREA)

Abstract

A nacelle assembly (100) for use in a wind turbine set. The wind turbine set comprises a tower (200) and a generator (400). The nacelle assembly (100) comprises: a connecting seat (10), the connecting seat being used to connect the tower (200) and the generator (400); nacelle units (20), there being multiple nacelle units (20) which are each disposed on the connecting seat (10), each nacelle unit (20) comprising a nacelle cover (21) and a functional device (22), the nacelle cover (21) being provided with an accommodation cavity (211), and the functional device (22) being at least partially located in the accommodation cavity (211) and being used for electrical connection with the generator (400). A wind turbine set comprises the described nacelle assembly (100). The nacelle assembly (100) can meet the high power requirements of a wind turbine set, and is beneficial for design, processing, and transmission.

Description

机舱总成以及风力发电机组Nacelle assembly and wind turbine
相关申请的交叉引用Cross References to Related Applications
本申请要求享有于2021年06月28日提交的中国专利申请第202110723412.8号的优先权,该申请的全部内容通过引用并入本文中。This application claims the priority of Chinese Patent Application No. 202110723412.8 filed on June 28, 2021, the entire content of which is incorporated herein by reference.
技术领域technical field
本申请涉及风电技术领域,特别是涉及一种机舱总成以及风力发电机组。The present application relates to the technical field of wind power, in particular to a nacelle assembly and a wind power generating set.
背景技术Background technique
随着风力发电机组的容量和功率越来越大,目前机舱总成的解决方案是尺寸同步放大。但是机舱总成等部件的持续放大会导致相关零部件的尺寸和重量过大。陆地机组更是会由于陆地运输的限制,导致大的机舱总成无法运输,或者为满足陆地运输需求,需要对道路、收费站或者隧道和桥梁进行改造,大幅度增加了运输成本,进而导致风电的综合成本快速上升。除了运输之外,由于零部件尺寸的持续放大,也导致零部件的设计难度和加工难度快速上升,这最终导致风力发电机组的成本快速上升。With the increasing capacity and power of wind turbines, the current solution for the nacelle assembly is to enlarge the size simultaneously. However, the continued enlargement of components such as the nacelle assembly will lead to excessive size and weight of related components. Due to the limitation of land transportation, the land-based unit will not be able to transport the large cabin assembly, or in order to meet the needs of land transportation, roads, toll stations, tunnels and bridges need to be rebuilt, which greatly increases the transportation cost, which in turn leads to wind power. The overall cost is rising rapidly. In addition to transportation, due to the continuous enlargement of the size of components, the difficulty of designing and processing components has also increased rapidly, which eventually led to a rapid increase in the cost of wind turbines.
因此,亟需一种新的机舱总成以及风力发电机组。Therefore, a new nacelle assembly and a wind power generating set are urgently needed.
发明内容Contents of the invention
本申请实施例提供一种机舱总成以及风力发电机组,机舱总成能够满足风力发电机组的大功率要求,成本低且利于加工及运输。The embodiment of the present application provides a nacelle assembly and a wind power generating set. The nacelle assembly can meet the high power requirement of the wind power generating set, and has low cost and is convenient for processing and transportation.
一方面,根据本申请实施例提出了一种机舱总成,用于风力发电机组,风力发电机组包括塔架以及发电机,机舱总成包括:连接座,连接座用于连接塔架以及发电机;机舱单元,机舱单元的数量为多个且分别设置于连接座,每个机舱单元包括机舱罩以及功能器件,机舱罩具有容纳腔, 功能器件至少部分位于容纳腔并用于与发电机电连接。On the one hand, according to the embodiment of the present application, a nacelle assembly is proposed for a wind power generating set, the wind power generating set includes a tower and a generator, and the nacelle assembly includes: a connecting seat, which is used to connect the tower and the generator ; The nacelle unit, the number of the nacelle units is multiple and respectively arranged on the connection seat, each nacelle unit includes a nacelle cover and a functional device, the nacelle cover has a receiving cavity, the functional device is at least partly located in the receiving cavity and is used for electrical connection with the generator.
另一个方面,根据本申请实施例提供一种风力发电机组,包括:塔架;上述的机舱总成,机舱总成设置于塔架;偏航系统,连接于塔架与连接座;发电机,包括转动配合的转子、定子以及与转子以及定子电连接的接口,定子连接于连接座,各机舱单元的功能器件与接口电连接;叶轮,连接于转子。In another aspect, according to an embodiment of the present application, a wind power generating set is provided, including: a tower; the above-mentioned nacelle assembly, the nacelle assembly is arranged on the tower; a yaw system, connected to the tower and a connecting seat; a generator, It includes a rotationally matched rotor, a stator, and an interface electrically connected to the rotor and the stator. The stator is connected to the connecting seat, and the functional devices of each nacelle unit are electrically connected to the interface; the impeller is connected to the rotor.
根据本申请实施例提供的机舱总成以及风力发电机组,机舱总成包括连接座以及机舱单元,连接座用于连接塔架以及发电机,机舱单元的数量为多个且分别连接于连接座,由于每个机舱罩内均具有容纳腔,并且在容纳腔内设置与发电机连接的功能器件,利用功能器件能够对发电机转换的电能进行后处理,通过对机舱单元数量和规格的调整能够满足发电机的大功率需求,同时机舱单元可以单独加工制造及运输,成本低,且利于机舱总成整体的设计、加工以及运输。According to the nacelle assembly and the wind power generating set provided by the embodiment of the present application, the nacelle assembly includes a connecting seat and a nacelle unit, the connecting seat is used to connect the tower and the generator, and the number of the nacelle units is multiple and connected to the connecting seat respectively, Since each nacelle cover has an accommodating cavity, and a functional device connected to the generator is installed in the accommodating cavity, the electrical energy converted by the generator can be post-processed by using the functional device, and the number and specifications of the nacelle units can be adjusted to meet the The high power demand of the generator, meanwhile, the nacelle unit can be processed, manufactured and transported separately, the cost is low, and it is beneficial to the overall design, processing and transportation of the nacelle assembly.
附图说明Description of drawings
下面将参考附图来描述本申请示例性实施例的特征、优点和技术效果。The features, advantages, and technical effects of the exemplary embodiments of the present application will be described below with reference to the accompanying drawings.
图1是本申请一个实施例的风力发电机组的轴测图;Fig. 1 is an axonometric view of a wind power generating set according to an embodiment of the present application;
图2是本申请一个实施例的风力发电机组的剖视结构示意图;Fig. 2 is a schematic cross-sectional structure diagram of a wind power generating set according to an embodiment of the present application;
图3是本申请一个实施例的机舱总成的轴测图;Fig. 3 is an axonometric view of a nacelle assembly of an embodiment of the present application;
图4是本申请一个实施例的机舱总成去除防护罩的结构示意图;Fig. 4 is a structural schematic view of the nacelle assembly with the protective cover removed according to one embodiment of the present application;
图5是本申请一个实施例的机舱总成的局部结构示意图;Fig. 5 is a schematic diagram of a partial structure of a nacelle assembly according to an embodiment of the present application;
图6是本申请另一个实施例的机舱总成的结构示意图。Fig. 6 is a schematic structural view of a nacelle assembly according to another embodiment of the present application.
其中:in:
100、机舱总成;100. Engine room assembly;
10、连接座;11、座本体;12、第一自由端;13、第二自由端;14、机舱接口;10. Connecting seat; 11. Seat body; 12. First free end; 13. Second free end; 14. Engine room interface;
20、机舱单元;20. Engine room unit;
21、机舱罩;211、容纳腔;21. Nacelle cover; 211. Accommodating cavity;
22、功能器件;221、变流器;222、变压器;223、环控系统;22. Functional device; 221. Converter; 222. Transformer; 223. Environmental control system;
23、支撑架;231、横向型材;232、纵向型材;23. Support frame; 231. Horizontal profile; 232. Vertical profile;
30、防护罩;40、控制柜;30. Protective cover; 40. Control cabinet;
200、塔架;200, tower;
300、叶轮;310、轮毂;320、叶片;300, impeller; 310, hub; 320, blade;
400、发电机;410、转子;420、定子;400, generator; 410, rotor; 420, stator;
aa、中心线。aa, center line.
在附图中,相同的部件使用相同的附图标记。附图并未按照实际的比例绘制。In the figures, the same parts are given the same reference numerals. The figures are not drawn to scale.
具体实施方式detailed description
下面将详细描述本申请的各个方面的特征和示例性实施例。在下面的详细描述中,提出了许多具体细节,以便提供对本申请的全面理解。但是,对于本领域技术人员来说很明显的是,本申请可以在不需要这些具体细节中的一些细节的情况下实施。下面对实施例的描述仅仅是为了通过示出本申请的示例来提供对本申请的更好的理解。在附图和下面的描述中,至少部分的公知结构和技术没有被示出,以便避免对本申请造成不必要的模糊;并且,为了清晰,可能夸大了部分结构的尺寸。此外,下文中所描述的特征、结构或特性可以以任何合适的方式结合在一个或更多实施例中。Features and exemplary embodiments of various aspects of the present application will be described in detail below. In the following detailed description, numerous specific details are set forth in order to provide a thorough understanding of the application. It will be apparent, however, to one skilled in the art that the present application may be practiced without some of these specific details. The following description of the embodiments is only to provide a better understanding of the present application by showing examples of the present application. In the drawings and the following description, at least some well-known structures and techniques have not been shown in order to avoid unnecessarily obscuring the application; and, for clarity, the dimensions of some structures may have been exaggerated. Furthermore, the features, structures, or characteristics described hereinafter may be combined in any suitable manner in one or more embodiments.
下述描述中出现的方位词均为图中示出的方向,并不是对本申请的机舱总成以及风力发电机组的具体结构进行限定。在本申请的描述中,还需要说明的是,除非另有明确的规定和限定,术语“安装”、“连接”应做广义理解,例如,可以是固定连接,也可以是可拆卸连接,或一体地连接;可以是直接相连,也可以间接相连。对于本领域的普通技术人员而言,可视具体情况理解上述术语在本申请中的具体含义。The orientation words appearing in the following description are all directions shown in the figure, and are not intended to limit the specific structure of the nacelle assembly and the wind power generating set of the present application. In the description of this application, it should also be noted that unless otherwise specified and limited, the terms "installation" and "connection" should be understood in a broad sense, for example, it can be a fixed connection or a detachable connection, or Connected integrally; either directly or indirectly. For those of ordinary skill in the art, the specific meanings of the above terms in this application can be understood according to specific situations.
如图1以及图2所示,本申请实施例提供一种风力发电机组,包括塔架200、机舱总成100、偏航系统(图未示)、发电机400以及叶轮300,机舱总成100设置于塔架200。为了满足机舱总成100的偏航需求,将偏 航系统连接于塔架200与机舱总成100之间,使得机舱总成100通过偏航系统与塔架200间接连接。发电机400包括转动配合的转子410、定子420以及与转子410和定子420电连接的接口,定子420连接于机舱总成100,叶轮300连接于转子410,可选地,叶轮300包括轮毂310以及叶片320,叶轮300通过轮毂310与发电机400的转子410连接。As shown in Figure 1 and Figure 2, the embodiment of the present application provides a wind power generating set, including a tower 200, a nacelle assembly 100, a yaw system (not shown), a generator 400 and an impeller 300, and the nacelle assembly 100 Set on the tower 200. In order to meet the yaw requirement of the nacelle assembly 100, the yaw system is connected between the tower 200 and the nacelle assembly 100, so that the nacelle assembly 100 is indirectly connected to the tower 200 through the yaw system. The generator 400 includes a rotationally fitted rotor 410, a stator 420, and an interface electrically connected to the rotor 410 and the stator 420. The stator 420 is connected to the nacelle assembly 100, and the impeller 300 is connected to the rotor 410. Optionally, the impeller 300 includes a hub 310 and The blade 320 and the impeller 300 are connected with the rotor 410 of the generator 400 through the hub 310 .
随着风力发电机组的容量和功率越来越大,目前风电机组的机舱总成的解决方案是尺寸同步放大。但是机舱总成等部件的持续放大会导致相关零部件的尺寸和重量过大。陆地机组更是会由于陆地运输的限制,导致大的机舱总成无法运输。除了运输之外,由于零部件尺寸的持续放大,也导致零部件的设计难度和加工难度快速上升,这最终导致风力发电机组的成本快速上升。With the increasing capacity and power of wind turbines, the current solution for the nacelle assembly of wind turbines is to enlarge the size simultaneously. However, the continued enlargement of components such as the nacelle assembly will lead to excessive size and weight of related components. Due to the limitation of land transportation, the land crew will not be able to transport the large cabin assembly. In addition to transportation, due to the continuous enlargement of the size of components, the difficulty of designing and processing components has also increased rapidly, which eventually led to a rapid increase in the cost of wind turbines.
基于上述技术问题,本申请实施例还提供一种新的机舱总成100,机舱总成100能够满足风力发电机组的大功率要求,利于设计、加工及运输。该机舱总成100可以作为独立的构件生产、销售,当然也可以用于风力发电机组并作为风力发电机组的组成部分。Based on the above technical problems, the embodiment of the present application also provides a new nacelle assembly 100, which can meet the high power requirements of wind turbines, and is convenient for design, processing and transportation. The nacelle assembly 100 can be produced and sold as an independent component, and of course it can also be used in a wind power generating set as a component of the wind generating set.
如图3至图5所示,本申请实施例提供的机舱总成100包括连接座10以及机舱单元20,连接座10用于连接塔架200以及发电机400。机舱单元20的数量为多个且分别设置于连接座10,每个机舱单元20包括机舱罩21以及功能器件22,机舱罩21具有容纳腔211,功能器件22至少部分位于容纳腔211并用于与发电机400电连接,功能器件22能够对发电机转换的电能进行后处理。As shown in FIGS. 3 to 5 , the nacelle assembly 100 provided by the embodiment of the present application includes a connecting seat 10 and a nacelle unit 20 , and the connecting seat 10 is used for connecting the tower 200 and the generator 400 . The number of cabin units 20 is multiple and are respectively arranged on the connecting seat 10. Each cabin unit 20 includes a cabin cover 21 and a functional device 22. The cabin cover 21 has a receiving cavity 211. The functional device 22 is at least partially located in the receiving cavity 211 and is used to communicate with the The generator 400 is electrically connected, and the functional device 22 can post-process the electric energy converted by the generator.
本申请实施例提供的机舱总成100,在用于风力发电机组时,各机舱单元20的功能器件22可以与发电机400的接口电连接。由于每个机舱罩21内均具有容纳腔211,并且在容纳腔211内设置与发电机400连接的功能器件22,利用功能器件22能够对发电机400转换的电能进行后处理,能够满足发电机400的大功率需求,同时机舱单元20可以单独加工制造,成本低且利于加工以及运输。When the nacelle assembly 100 provided by the embodiment of the present application is used in a wind power generating set, the functional devices 22 of each nacelle unit 20 can be electrically connected to the interface of the generator 400 . Since each nacelle cover 21 has an accommodating cavity 211, and a functional device 22 connected to the generator 400 is arranged in the accommodating cavity 211, the electrical energy converted by the generator 400 can be post-processed by using the functional device 22, and the generator can meet the 400 high power requirements, and at the same time the nacelle unit 20 can be processed and manufactured separately, the cost is low and it is convenient for processing and transportation.
作为一种可选地实施方式,本申请实施例提供的机舱总成100,其功能器件22包括变压器222以及变流器221中的至少一者。其可以包括变压 器222,也可以包括变流器221。当然,在有些实施例中也可以同时包括变压器222以及变流器221。每个功能器件22的变压器222以及变流器221与所述发电机400电连接。通过变压器222可以用来将发电机400某一数值的交流电压(电流)变成频率相同的另一种或几种数值不同的电压(电流)的设备。对于变流器221,可以将变流器221加在发电机400的转子410侧的励磁装置。其主要功能是在转子410转速n变化时,通过变流器221控制励磁的幅值、相位、频率等,使定子420侧能向电网输入恒频电。当功能器件22包括变压器222以及变流器221时,可以使得发电机400转换的电能先进入变流器221,然后由变流器221再到变压器222,然后进入升压站及后续的电网中。As an optional implementation manner, in the nacelle assembly 100 provided in the embodiment of the present application, the functional device 22 thereof includes at least one of a transformer 222 and a converter 221 . It may include a transformer 222, and may also include a converter 221. Certainly, in some embodiments, the transformer 222 and the converter 221 may also be included at the same time. The transformer 222 and the converter 221 of each functional device 22 are electrically connected to the generator 400 . The transformer 222 can be used to change the AC voltage (current) of a certain value of the generator 400 into another voltage (current) with the same frequency or several different values (current). As for the converter 221 , the converter 221 may be added to the excitation device on the side of the rotor 410 of the generator 400 . Its main function is to control the amplitude, phase and frequency of the excitation through the converter 221 when the speed n of the rotor 410 changes, so that the stator 420 side can input constant frequency power to the grid. When the functional device 22 includes a transformer 222 and a converter 221, the electric energy converted by the generator 400 can first enter the converter 221, then from the converter 221 to the transformer 222, and then enter the step-up station and the subsequent power grid .
在一些可选地实施例中,本申请实施例提供的机舱总成100,连接座10包括座本体11以及由座本体11围合形成的中空腔,座本体11具有第一自由端12、第二自由端13以及至少部分位于第一自由端12以及第二自由端13之间的多个机舱接口14。第一自由端12用于与塔架200连接,第二自由端13用于与发电机400连接,每个机舱单元20连接于其中一个机舱接口14。In some optional embodiments, the nacelle assembly 100 provided by the embodiment of the present application, the connecting seat 10 includes a seat body 11 and a hollow cavity formed by the seat body 11, the seat body 11 has a first free end 12, a second Two free ends 13 and a plurality of nacelle interfaces 14 at least partially located between the first free end 12 and the second free end 13 . The first free end 12 is used for connecting with the tower 200 , the second free end 13 is used for connecting with the generator 400 , and each nacelle unit 20 is connected to one of the nacelle interfaces 14 .
连接座10采用上述结构形式,利用机舱接口14能够满足与各机舱单元20之间的连接需求。而相应设置的第一自由端12可以与塔架200连接,第二自由端13可以与发电机400连接,满足各机舱单元20与塔架200以及发电机400的连接需求。The connection seat 10 adopts the above-mentioned structural form, and can meet the connection requirements with each cabin unit 20 by using the cabin interface 14 . The correspondingly provided first free end 12 can be connected to the tower 200 , and the second free end 13 can be connected to the generator 400 to meet the connection requirements of each nacelle unit 20 with the tower 200 and the generator 400 .
作为一种可选地实施方式,本申请实施例提供的机舱总成100,其第一自由端12可以采用环形法兰结构,通过将第一自由端12采用环形法兰结构形式,能够利于机舱总成100与塔架200之间的可拆卸连接。As an optional implementation mode, the first free end 12 of the nacelle assembly 100 provided in the embodiment of the present application can adopt an annular flange structure. By adopting the first free end 12 in the form of an annular flange structure, it can facilitate the Detachable connection between assembly 100 and tower 200 .
可选地,本申请实施例提供的机舱总成100,其第二自由端13可以采用环形法兰结构,由于第二自由端13需要与发电机400的定子420连接,通过将其采用环形法兰结构,利于第二自由端13与发电机400的定子420之间的可拆卸连接,保证二者之间的连接强度,便于装拆以及维修。Optionally, in the nacelle assembly 100 provided in the embodiment of the present application, the second free end 13 may adopt an annular flange structure. Since the second free end 13 needs to be connected with the stator 420 of the generator 400, by adopting the annular method The flange structure facilitates the detachable connection between the second free end 13 and the stator 420 of the generator 400, ensures the connection strength between the two, and is convenient for assembly, disassembly and maintenance.
一些可选地实施例中,第一自由端12的轴线以及第二自由端13的轴线相交设置。能够根据塔架200与发电机400的分布情况实现与二者之间 的连接。In some optional embodiments, the axis of the first free end 12 and the axis of the second free end 13 are arranged to intersect. The connection between the tower 200 and the generator 400 can be realized according to the distribution of the two.
可选地,本申请实施例提供的机舱总成100,其机舱接口14的数量可以根据机舱单元20的数量设置,只要能够满足与各机舱单元20之间的连接需求均可。Optionally, in the nacelle assembly 100 provided in the embodiment of the present application, the number of nacelle interfaces 14 can be set according to the number of nacelle units 20 , as long as the connection requirements with each nacelle unit 20 can be met.
可选地,本申请实施例提供的机舱总成100,各机舱单元20的机舱罩21可以采用不同的形状,其具有容纳腔211且能够满足功能器件22的安装以及与连接座10之间直接或者间接连接需求均可。一些可选地实施例中,机舱罩21可以采用中空箱型结构。一些可选地实施例中,其可以采用中空的方形结构体。Optionally, in the nacelle assembly 100 provided in the embodiment of the present application, the nacelle cover 21 of each nacelle unit 20 can adopt different shapes, which have accommodating cavities 211 and can satisfy the installation of functional devices 22 and direct contact with the connecting seat 10. Or indirect connection requirements are available. In some optional embodiments, the nacelle cover 21 may adopt a hollow box structure. In some optional embodiments, it may adopt a hollow square structure.
在一些可选地实施例中,本申请实施例提供的机舱总成100,每个机舱单元20还包括环控系统223,环控系统223被配置为调节容纳腔211内的温度、湿度以及空气中的盐分中的至少一者。通过使得每个机舱单元20包括环控系统223,能够利用环控系统223对该机舱单元20对应的容纳腔211内部环境的温度、湿度以及盐分的至少一者进行调节,使得容纳腔211内的环境始终在预设的范围至内,避免因温度、湿度以及盐分中的至少一者的数值超出预设的范围导致功能器件22的损坏,提高机舱总成100的安全性以及使用寿命,并降低维修成本。In some optional embodiments, in the nacelle assembly 100 provided in the embodiment of the present application, each nacelle unit 20 further includes an environmental control system 223, and the environmental control system 223 is configured to adjust the temperature, humidity and air in the accommodating chamber 211. at least one of the salt in the By making each cabin unit 20 include an environment control system 223, the environment control system 223 can be used to adjust at least one of the temperature, humidity and salinity of the internal environment of the accommodation chamber 211 corresponding to the cabin unit 20, so that the environment in the accommodation chamber 211 The environment is always within the preset range to avoid damage to the functional device 22 due to the value of at least one of temperature, humidity and salinity exceeding the preset range, improve the safety and service life of the cabin assembly 100, and reduce Maintenance costs.
作为一种可选地实施方式,本申请实施例提供的机舱总成100,其环控系统223包括散热装置,散热装置设置于机舱罩21且被配置为调节容纳腔211内的温度,使得每个机舱单元20的容纳腔211内温度适中,避免温度过高导致功能器件22的损毁。As an optional implementation mode, in the nacelle assembly 100 provided in the embodiment of the present application, the environmental control system 223 includes a heat dissipation device, which is arranged on the nacelle cover 21 and configured to adjust the temperature in the accommodating chamber 211 so that each The temperature in the accommodating cavity 211 of each cabin unit 20 is moderate, so as to avoid damage to the functional devices 22 caused by excessive temperature.
在一些可选地示例中,环控系统223还可以包括除湿器,除湿器设置于机舱罩21且被配置为调节容纳腔211内的湿度,通过设置除湿器,使得每个机舱单元20的容纳腔211内湿度能够始终保持在最低,避免湿度过高对功能器件22造成腐蚀甚至造成功能器件22间或者功能器件22与发电机400之间的连接接口短路。In some optional examples, the environmental control system 223 may also include a dehumidifier, which is arranged on the nacelle cover 21 and configured to adjust the humidity in the accommodation chamber 211. The humidity in the chamber 211 can always be kept at the lowest level, so as to prevent the functional devices 22 from being corroded or even short-circuited at the connection interface between the functional devices 22 or between the functional devices 22 and the generator 400 due to excessive humidity.
作为一种可选地实施方式,环控系统223还可以包括除盐器,除盐器设置于机舱罩21且被配置为调节容纳腔211内空气中的盐分,避免每个机舱单元20的容纳腔211内盐分过高导致对功能器件22的腐蚀,对功能 器件22进行防护。As an optional implementation, the environmental control system 223 may also include a desalter, which is arranged on the nacelle cover 21 and is configured to adjust the salt content in the air in the accommodating cavity 211 to prevent the accommodating of each nacelle unit 20 Excessive salt content in the cavity 211 leads to corrosion of the functional device 22 and protects the functional device 22 .
在一些可选地实施例中,本申请提供的实施例,每个机舱单元20可以通过机舱罩21本身来安装并支撑功能器件22,同时通过机舱罩21直接与连接座10连接,当然此为一种可选的实施例。In some optional embodiments, in the embodiment provided by this application, each nacelle unit 20 can install and support the functional device 22 through the nacelle cover 21 itself, and at the same time be directly connected to the connecting seat 10 through the nacelle cover 21, of course this is An optional embodiment.
在一些其他的示例中,也可以使得每个机舱单元20还包括支撑架23,支撑架23设置于容纳腔211内并与机舱罩21连接,支撑架23至少部分凸出于机舱罩21设置并与机舱接口14连接。本申请实施例提供的机舱总成100,通过在每个机舱单元20内部设置支撑架23并使其与机舱罩21连接,能够增加机舱单元20整体的强度。保证其抗载荷能力,提高机舱总成100的安全性能。并且,通过将支撑架23至少部分凸出于机舱罩21设置并使其与机舱接口14连接,既能够保证机舱单元20与机舱接口14之间的连接需求,并且可以将机舱罩21整体的壁厚做的更薄,减轻机舱罩21整体重量及成本,同时,可以降低机舱罩21直接与机舱接口14连接导致机舱罩21损坏的风险。In some other examples, each nacelle unit 20 may also include a support frame 23, the support frame 23 is arranged in the accommodating cavity 211 and connected with the nacelle cover 21, the support frame 23 is at least partially protruded from the nacelle cover 21 and set and Connect with the cabin interface 14. The nacelle assembly 100 provided in the embodiment of the present application can increase the overall strength of the nacelle unit 20 by providing a support frame 23 inside each nacelle unit 20 and connecting it to the nacelle cover 21 . To ensure its anti-load capacity and improve the safety performance of the nacelle assembly 100 . Moreover, by setting the support frame 23 at least partially protruding from the nacelle cover 21 and connecting it to the nacelle interface 14, the connection requirements between the nacelle unit 20 and the nacelle interface 14 can be ensured, and the entire wall of the nacelle cover 21 can be Making it thicker and thinner can reduce the overall weight and cost of the nacelle cover 21 , and at the same time, can reduce the risk of damage to the nacelle cover 21 caused by the direct connection of the nacelle cover 21 to the nacelle interface 14 .
在一些可选地实施例中,本申请实施例提供的机舱总成100,其支撑架23可以采用镂空的框架结构,强度高,重量轻且成本低。可选地,支撑架23可以包括横纵交错的型材连接而成,可以使得部分型材凸出于机舱罩21设置并与机舱接口14连接。In some optional embodiments, in the nacelle assembly 100 provided in the embodiment of the present application, the supporting frame 23 may adopt a hollow frame structure, which has high strength, light weight and low cost. Optionally, the supporting frame 23 may be composed of criss-cross profiles connected, and part of the profiles may protrude from the nacelle cover 21 and be connected to the nacelle interface 14 .
一些可选地实施例中,支撑架23可以包括多个纵向型材232以及多个横向型材231,多个纵向型材232沿横向型材231的延伸方向间隔分布,多个横向型材231沿纵向型材232的延伸方向间隔分布,每个横向型材231与各纵向型材232相交设置并相互连接。In some optional embodiments, the support frame 23 may include a plurality of longitudinal profiles 232 and a plurality of transverse profiles 231, the plurality of longitudinal profiles 232 are distributed at intervals along the extending direction of the transverse profiles 231, and the plurality of transverse profiles 231 are The extending direction is distributed at intervals, and each transverse profile 231 intersects with each longitudinal profile 232 and is connected to each other.
作为一种可选地实施方式,本申请实施例提供的机舱总成100,机舱接口14以及支撑架23的一者包括插接凸起,另一者包括插接槽,插接凸起与插接槽的形状相匹配并插接连接。机舱接口14与支撑架23采用上述连接方式,利于机舱单元20与底座之间的拆装,同时能够保证二者之间的连接强度。As an optional implementation mode, in the nacelle assembly 100 provided in the embodiment of the present application, one of the nacelle interface 14 and the support frame 23 includes a plug-in protrusion, and the other includes a plug-in slot, and the plug-in protrusion and the plug-in slot The shape of the slots matches and plugs into the connection. The above connection method between the nacelle interface 14 and the support frame 23 facilitates the disassembly and assembly of the nacelle unit 20 and the base, and at the same time ensures the connection strength between the two.
可选地,可以使得机舱接口14包括多个连接块,每个连接块上设置有插接槽,使得支撑架23上设置有插接凸起,通过将插接凸起插接于插 接槽实现连接座10与接触接口之间的连接。Optionally, the cabin interface 14 can be made to include a plurality of connection blocks, and each connection block is provided with an insertion slot, so that the support frame 23 is provided with an insertion protrusion, by inserting the insertion protrusion into the insertion slot Realize the connection between the connection seat 10 and the contact interface.
可选地,当支撑架23包括纵向型材232时,可以使得至少部分数量的纵向型材232凸出于机舱罩21设置并形成插接凸起。Optionally, when the supporting frame 23 includes longitudinal profiles 232, at least a part of the longitudinal profiles 232 may protrude from the nacelle cover 21 and form insertion protrusions.
可以理解的是,不限于在支撑架23上设置插接凸起,在机舱接口14上设置插接凹槽,在一些其他的实施例中,也可以使得插接凹槽形成于支撑架23,插接凸起形成于机舱接口14,只要能够满足支撑架23与机舱接口14之间的连接需求均可。It can be understood that, it is not limited to provide insertion protrusions on the support frame 23, and provide insertion grooves on the cabin interface 14. In some other embodiments, the insertion grooves can also be formed on the support frame 23, The insertion protrusion is formed on the nacelle interface 14 , as long as it can meet the connection requirements between the support frame 23 and the nacelle interface 14 .
作为一种可选地实施方式,本申请实施例提供的机舱总成100,其各机舱单元20的功能器件22如变压器222、变流器221以及环控系统223等部件均可以与机舱罩21连接。当然,在有些实施例中,也可以将功能器件22及环控系统223等部件设置于支撑架23,由于支撑架23位于机舱罩21的,支撑架23可以水平放置,可以向功能器件22以及环控系统223等提供水平支撑面,利于功能器件22以及环控系统223的装拆。并且,当支撑架23采用镂空的框架结构时,将功能器件22以及环控系统223等设置于支撑架23上还利于功能器件22等部件的散热,提高机舱单元20的安全性能。As an optional implementation mode, in the nacelle assembly 100 provided in the embodiment of the present application, the functional devices 22 of each nacelle unit 20 such as the transformer 222, the converter 221 and the environment control system 223 can be combined with the nacelle cover 21 connect. Of course, in some embodiments, components such as the functional device 22 and the environmental control system 223 can also be arranged on the support frame 23. Since the support frame 23 is located at the nacelle cover 21, the support frame 23 can be placed horizontally, and can be placed toward the functional device 22 and The environmental control system 223 and the like provide a horizontal support surface, which facilitates the assembly and disassembly of the functional device 22 and the environmental control system 223 . Moreover, when the supporting frame 23 adopts a hollow frame structure, disposing the functional device 22 and the environmental control system 223 on the supporting frame 23 is also beneficial to heat dissipation of the functional device 22 and other components, and improves the safety performance of the nacelle unit 20 .
作为一种可选地实施方式,由于机舱总成100在用于风力发电机组时是在户外工作,为了对连接座10进行防护,避免外界的雨水等自然因素对连接座10造成损坏,机舱总成100还包括防护罩30,防护罩30包覆连接座10设置,防护罩30对应每个机舱单元20均设置有避让口。通过设置防护罩30,能够对连接座10进行防护,既能够避免自然环境中的风霜雪雨对连接座10进行腐蚀等,同时能够避免雨水通过连接座10进入发电机400、塔架200等设备的内部,提高机舱总成100以及风力发电机组的安全性能。As an optional implementation, since the nacelle assembly 100 works outdoors when it is used in a wind power generating set, in order to protect the connecting seat 10 and avoid damage to the connecting seat 10 caused by natural factors such as rainwater outside, the nacelle assembly The unit 100 also includes a protective cover 30 , the protective cover 30 is arranged to cover the connection seat 10 , and the protective cover 30 is provided with an escape opening corresponding to each cabin unit 20 . By arranging the protective cover 30, the connection seat 10 can be protected, which can prevent the wind, frost, snow and rain in the natural environment from corroding the connection seat 10, and at the same time prevent rainwater from entering the generator 400, the tower 200 and other equipment through the connection seat 10. interior, improving the safety performance of the nacelle assembly 100 and the wind power generating set.
作为一种可选地实施方式,本申请实施例提供的机舱总成100,其防护罩30可以采用多种结构形式,其可以为中空的罩壳结构,防护罩30包覆连接座10设置,防护罩30可以与连接座10连接,并且能够避免连接座10与机舱单元20、塔架200以及发电机400之间的连接产生干涉。As an optional implementation mode, in the nacelle assembly 100 provided in the embodiment of the present application, the protective cover 30 can adopt various structural forms, which can be a hollow shell structure, and the protective cover 30 is arranged to cover the connecting seat 10, The protective cover 30 can be connected with the connection base 10 , and can prevent the connection between the connection base 10 and the nacelle unit 20 , the tower 200 and the generator 400 from interfering.
作为一种可选地实施方式,本申请实施还包括控制柜40,至少一个机 舱单元20的功能器件22与控制柜40电连接,通过控制柜40控制相应的功能器件22。可选地,控制柜40可以设置于防护罩30内。As an optional implementation, the implementation of the present application further includes a control cabinet 40, the functional device 22 of at least one cabin unit 20 is electrically connected to the control cabinet 40, and the corresponding functional device 22 is controlled through the control cabinet 40. Optionally, the control cabinet 40 can be arranged inside the protective cover 30 .
可以理解的是,本申请上述各实施例提供的机舱总成100,其机舱单元20与机舱接口14之间的连接均是采用一者包括插接凸起,另一者包括插接槽,插接凸起与插接槽的形状相匹配并插接连接。此为一种可选地实施方式,但不限于上述方式,在一些其他的实施例中,也可以使得机舱接口14包括第一法兰,支撑架23包括第二法兰,第一法兰以及第二法兰的形状相匹配并相互连接,同样能够满足每个机舱单元20与连接座10之间的连接需求。It can be understood that, in the nacelle assembly 100 provided by the above-mentioned embodiments of the present application, the connection between the nacelle unit 20 and the nacelle interface 14 is to adopt one including a plug-in protrusion, and the other includes a plug-in slot, and the plug-in slot The connecting protrusion matches the shape of the socket slot and is plugged and connected. This is an optional implementation mode, but is not limited to the above-mentioned mode. In some other embodiments, the cabin interface 14 may also include a first flange, the support frame 23 may include a second flange, the first flange and The shapes of the second flanges are matched and connected to each other, which can also meet the connection requirements between each nacelle unit 20 and the connecting seat 10 .
本申请上述各实施例提供的机舱总成100,其所包括的机舱单元20的数量可以根据所应用风力发电机组的功率需求进行设定。In the nacelle assembly 100 provided by the above-mentioned embodiments of the present application, the number of nacelle units 20 included therein can be set according to the power demand of the applied wind power generating set.
示例性地,当机舱总成100所应用的风力发电机组为6MW的机组时,可以使得机舱总成100包括两个机舱单元20,每个机舱单元20的功能器件22能够对发电机400的转换电能的后处理上限为3MW,两个3MW的机舱单元20能够实现6MW的机组的发电机400转换电能的后处理需求,进而满足6MW机组的功率需求。Exemplarily, when the wind power generating set applied to the nacelle assembly 100 is a 6MW unit, the nacelle assembly 100 may include two nacelle units 20, and the functional device 22 of each nacelle unit 20 can convert the generator 400 The post-processing upper limit of electric energy is 3MW, and the two 3MW nacelle units 20 can meet the post-processing requirements of the generator 400 of the 6MW generating set to convert electric energy, thereby satisfying the power demand of the 6MW generating set.
再如,当机舱总成100所应用的风力发电机组为7.5MW的机组时,同样可以使得机舱总成100包括两个机舱单元20,其中一个机舱单元20的功能器件22能够对发电机400的转换电能的后处理上限为3MW,另一个机舱单元20的功能器件22能够对发电机400的转换电能的后处理上限为4.5MW,进而满足7.5MW机组的功率需求。For another example, when the wind power generating set applied to the nacelle assembly 100 is a 7.5MW unit, the nacelle assembly 100 can also include two nacelle units 20, and the functional device 22 of one nacelle unit 20 can control the generator 400. The post-processing upper limit of the converted electric energy is 3MW, and the functional device 22 of the other nacelle unit 20 can post-process the converted electric energy of the generator 400 up to 4.5MW, thereby meeting the power demand of the 7.5MW unit.
又如,当机舱总成100所应用的风力发电机组为14MW的机组时,可以使得机舱总成100包括三个机舱单元20,其中一个机舱单元20的功能器件22能够对发电机400的转换电能的后处理上限为8MW,另一个机舱单元20的功能器件22能够对发电机400的转换电能的后处理上限为4.5MW,第三个机舱单元20的功能器件22能够对发电机400的转换电能的后处理上限为1.5MW,进而满足14MW机组的功率需求。As another example, when the wind power generating set applied to the nacelle assembly 100 is a 14MW unit, the nacelle assembly 100 can include three nacelle units 20, and the functional device 22 of one nacelle unit 20 can convert the electrical energy of the generator 400 The post-processing upper limit of the engine room unit 20 is 8MW, and the functional device 22 of the other nacelle unit 20 can convert the electrical energy of the generator 400. The upper limit of post-processing is 1.5MW, which can meet the power demand of 14MW units.
由于功能器件22的后处理上限值越低,其成本、加工难度、运输难度都相对较低,而后处理上限值越高,其成本、加工难度、运输难度等将 倍增。如果采用已有的机舱总成100的方式形成14MW机组,那么该机舱总成100用于对发电机400转换的电能进行后处理的功能器件22的后处理上限就要为14MW,这将导致机舱罩21、变流器221、变压器222等功能器件22的体积非常的庞大,对于运输以及生产加工要求非常。而利用本申请实施例提供的机舱总成100,采用多个具有后处理功能的机舱单元20的形式,既能够满足风力发电机组的大功率需求。Since the upper limit of post-processing of the functional device 22 is lower, its cost, processing difficulty, and transportation difficulty are relatively low, and the higher the post-processing upper limit, its cost, processing difficulty, and transportation difficulty will be doubled. If the existing nacelle assembly 100 is used to form a 14MW unit, then the post-processing upper limit of the functional device 22 of the nacelle assembly 100 for post-processing the electric energy converted by the generator 400 will be 14MW, which will result in a The volume of the functional devices 22 such as the cover 21 , the converter 221 , and the transformer 222 is very large, and the requirements for transportation, production and processing are very high. However, the nacelle assembly 100 provided by the embodiment of the present application is in the form of a plurality of nacelle units 20 with post-processing functions, which can meet the high power demand of the wind power generating set.
可以理解的是,上述对应举例的6MW的机组、7.5MW的机组、14MW的机组对应所包括的机舱单元20的数量以及其后处理上限值的限定只是一种可选地实施方式,但不限于上述方式,具体可以根据需要调节。It can be understood that the number of cabin units 20 included in the 6MW unit, 7.5MW unit, and 14MW unit corresponding to the examples above and the limitation on the upper limit of post-processing are just an optional implementation, but not The method is limited to the above, and can be adjusted as needed.
作为一种可选地实施方式,本申请实施例提供的机舱总成100,连接座10为轴对称结构且具有中心线aa,机舱单元20的数量为n个;其中,n为大于等于2的偶数,n个机舱单元20分成两组单元组,每组单元组包括至少一个机舱单元20,两组单元组对称分布于中心线aa的两侧。通过上述设置,能够平衡连接座10所承受的载荷,避免底座承受偏载。As an optional implementation mode, in the cabin assembly 100 provided in the embodiment of the present application, the connecting seat 10 has an axisymmetric structure and has a center line aa, and the number of cabin units 20 is n; where n is greater than or equal to 2 In an even number, n cabin units 20 are divided into two unit groups, each unit group includes at least one cabin unit 20, and the two unit groups are symmetrically distributed on both sides of the central line aa. Through the above arrangement, the load borne by the connection base 10 can be balanced, and the base can be prevented from bearing unbalanced load.
示例性地,以机舱单元20的数量为2个为例,可以使得每组单元组包括一个机舱单元20,两个机舱单元20对称分布于中心线aa的两侧。Exemplarily, taking two cabin units 20 as an example, each unit group may include one cabin unit 20 , and two cabin units 20 are symmetrically distributed on both sides of the central line aa.
再如,如图3至图5所示,以机舱单元20的数量为4个为例,可以使得每组单元组包括2个机舱单元20,其中一组单元组的机舱单元20与另一组单元组的机舱单元20对称分布于中心线aa的两侧。For another example, as shown in Figures 3 to 5, taking the number of cabin units 20 as 4 as an example, each group of unit groups can be made to include 2 cabin units 20, wherein the cabin unit 20 of one group of unit groups is connected with another group of unit groups. The cabin units 20 of the unit group are symmetrically distributed on both sides of the central line aa.
可以理解的是,当机舱单元20的数量为n时,n为偶数只是一种可选地实施方式。It can be understood that when the number of cabin units 20 is n, it is only an optional implementation manner that n is an even number.
如图6所示,在一些其他的示例中,也可以使得n为奇数。n为大于2的奇数,n-1个机舱单元20分成两组单元组,每组单元组包括至少一个机舱单元20,两组单元组对称分布于中心线aa的两侧,剩余一个机舱单元20连接于连接座10位于两组单元组之间的区域。通过上述设置,能够使得当n为奇数时,能够更好的平衡底座所承受的载荷,避免底座承受偏载。As shown in FIG. 6, in some other examples, n may also be an odd number. n is an odd number greater than 2, n-1 cabin units 20 are divided into two groups of units, each group of units includes at least one cabin unit 20, and the two groups of units are symmetrically distributed on both sides of the central line aa, leaving one cabin unit 20 It is connected to the area where the connection base 10 is located between the two groups of units. Through the above setting, when n is an odd number, the load borne by the base can be better balanced, and the base can be prevented from bearing unbalanced loads.
示例性地,如图6所示,以机舱单元20的数量为5个为例,可以使得 4个机舱单元20分成两组单元组,每组单元组包括两个机舱单元20,其中一组单元组的两个机舱单元20与另一个单元组的两个机舱单元20对称分布于中心线aa的两侧,剩余一个机舱单元20接于连接座10位于两组单元组之间的区域,可选地,剩余一个机舱单元20的中心可以位于中心线aa上,进一步避免连接座10承受偏载。Exemplarily, as shown in FIG. 6, taking the number of cabin units 20 as an example of five, four cabin units 20 can be divided into two groups of units, each group of unit groups includes two cabin units 20, wherein one group of units The two cabin units 20 of one group and the two cabin units 20 of another unit group are symmetrically distributed on both sides of the center line aa, and the remaining one cabin unit 20 is connected to the connecting seat 10 in the area between the two groups of units, optional Accordingly, the center of the remaining one cabin unit 20 can be located on the center line aa, further preventing the connecting seat 10 from bearing unbalanced load.
可以理解的是,上述多个机舱单元20在连接座10上的排布方式只是一种可选地方式,不限于上述方式,例如,可以根据需要,可以使得至少部分数量的机舱单元20在塔架的轴向上间隔分布,彼此在轴向上的投影可以有至少部分重叠,当然也可以错开设置,能够满足机舱总成100的性能要求均可。It can be understood that the arrangement of the above-mentioned plurality of cabin units 20 on the connecting seat 10 is only an optional way, and is not limited to the above-mentioned way. The racks are arranged at intervals in the axial direction, and the projections of each other in the axial direction may at least partially overlap, of course, they may also be arranged in a staggered manner, whichever meets the performance requirements of the nacelle assembly 100 .
作为一种可选地实施方式,本申请实施例提供的风力发电机组,其发电机400可以包括多个绕组,每个绕组通过接口与其中一个机舱单元20的功能器件22电连接。通过上述设置,能够更利于机舱单元20与发电机400之间的电连接,满足对发电机400所转换电能的后处理需求。As an optional implementation manner, the generator 400 of the wind power generating set provided in the embodiment of the present application may include multiple windings, and each winding is electrically connected to the functional device 22 of one of the nacelle units 20 through an interface. Through the above arrangement, the electrical connection between the nacelle unit 20 and the generator 400 can be more facilitated, and the post-processing requirements for the electric energy converted by the generator 400 can be met.
本申请实施例提供的机舱总成100,其连接座10用于连接塔架200以及发电机400,机舱单元20的数量为多个且分别连接于连接座10,由于每个机舱罩21内均具有容纳腔211,并且在容纳腔211内设置与发电机400连接的功能器件22,利用功能器件22能够对发电机400转换的电能进行后处理,通过对机舱单元20数量和规格的调整能够满足发电机400的大功率需求,同时机舱单元20可以单独加工制造及运输,利于机舱总成100整体的加工以及运输。In the nacelle assembly 100 provided in the embodiment of the present application, the connecting seat 10 is used to connect the tower 200 and the generator 400, and the number of the nacelle units 20 is multiple and connected to the connecting seat 10 respectively. It has an accommodating chamber 211, and a functional device 22 connected to the generator 400 is arranged in the accommodating chamber 211, and the electric energy converted by the generator 400 can be post-processed by using the functional device 22, and the quantity and specifications of the nacelle units 20 can be adjusted to meet the The high power demand of the generator 400 and the nacelle unit 20 can be manufactured and transported separately, which is beneficial to the processing and transportation of the nacelle assembly 100 as a whole.
而本申请实施例提供的风力发电机组,因其包括上述各实施例提供的机舱总成100,在满足自身大功率需求基础上,生产以及运输成本低,且易于维修,发电效益高。However, the wind power generating set provided by the embodiments of the present application includes the nacelle assembly 100 provided by the above embodiments, and on the basis of meeting its own high power requirements, it is low in production and transportation costs, easy to maintain, and high in power generation efficiency.
虽然已经参考优选实施例对本申请进行了描述,但在不脱离本申请的范围的情况下,可以对其进行各种改进并且可以用等效物替换其中的部件。尤其是,只要不存在结构冲突,各个实施例中所提到的各项技术特征均可以任意方式组合起来。本申请并不局限于文中公开的特定实施例,而是包括落入权利要求的范围内的所有技术方案。While the application has been described with reference to a preferred embodiment, various modifications may be made and equivalents may be substituted for elements thereof without departing from the scope of the application. In particular, as long as there is no structural conflict, the technical features mentioned in the various embodiments can be combined in any manner. The present application is not limited to the specific embodiments disclosed herein, but includes all technical solutions falling within the scope of the claims.

Claims (18)

  1. 一种机舱总成(100),用于风力发电机组,所述风力发电机组包括塔架(200)以及发电机(400),其中,所述机舱总成(100)包括:A nacelle assembly (100), used for a wind power generating set, the wind power generating set including a tower (200) and a generator (400), wherein the nacelle assembly (100) includes:
    连接座(10),所述连接座(10)用于连接所述塔架(200)以及所述发电机(400);A connecting seat (10), the connecting seat (10) is used to connect the tower (200) and the generator (400);
    机舱单元(20),所述机舱单元(20)的数量为多个且分别设置于所述连接座(10),每个所述机舱单元(20)包括机舱罩(21)以及功能器件(22),所述机舱罩(21)具有容纳腔(211),所述功能器件(22)至少部分位于所述容纳腔(211)并用于与所述发电机(400)电连接。A cabin unit (20), the number of the cabin units (20) is multiple and respectively arranged on the connecting seat (10), each of the cabin units (20) includes a cabin cover (21) and a functional device (22 ), the nacelle cover (21) has an accommodating cavity (211), the functional device (22) is at least partially located in the accommodating cavity (211) and is used for electrical connection with the generator (400).
  2. 根据权利要求1所述的机舱总成(100),其中,每个所述机舱单元(20)的所述功能器件(22)包括变流器(221)以及变压器(222)中的至少一者。The nacelle assembly (100) according to claim 1, wherein the functional device (22) of each nacelle unit (20) includes at least one of a converter (221) and a transformer (222) .
  3. 根据权利要求1所述的机舱总成(100),其中,每个所述机舱单元(20)还包括环控系统(223),所述环控系统(223)被配置为调节所述容纳腔(211)内的温度、湿度以及空气中的盐分中的至少一者。The nacelle assembly (100) according to claim 1, wherein each nacelle unit (20) further comprises an environmental control system (223), and the environmental control system (223) is configured to adjust the accommodating cavity (211) at least one of temperature, humidity and salinity in the air.
  4. 根据权利要求3所述的机舱总成(100),其中,所述环控系统(223)包括散热装置、除湿器以及除盐器中的至少一者,其中,The nacelle assembly (100) according to claim 3, wherein the environmental control system (223) includes at least one of a radiator, a dehumidifier and a desalter, wherein,
    所述散热装置被配置为调节所述容纳腔(211)内的温度;The heat dissipation device is configured to adjust the temperature in the accommodation cavity (211);
    所述除湿器被配置为调节所述容纳腔(211)内的湿度;The dehumidifier is configured to adjust the humidity in the containing cavity (211);
    所述除盐器被配置为调节所述容纳腔(211)内空气中的盐分。The desalter is configured to adjust the salt in the air in the containing chamber (211).
  5. 根据权利要求1至4任意一项所述的机舱总成(100),其中,所述连接座(10)包括座本体(11)以及由所述座本体(11)围合形成的中空腔,所述座本体(11)具有第一自由端(12)、第二自由端(13)以及至少部分位于所述第一自由端(12)以及所述第二自由端(13)之间的多个机舱接口(14),所述第一自由端(12)用于与所述塔架(200)连接,所述第二自由端(13)用于与所述发电机(400)连接,每个所述机舱单元(20)连接于其中一个所述机舱接口(14)。The nacelle assembly (100) according to any one of claims 1 to 4, wherein the connecting seat (10) comprises a seat body (11) and a hollow cavity enclosed by the seat body (11), The seat body (11) has a first free end (12), a second free end (13) and multiple holes at least partially located between the first free end (12) and the second free end (13). a nacelle interface (14), the first free end (12) is used for connecting with the tower (200), and the second free end (13) is used for connecting with the generator (400), each Each of the cabin units (20) is connected to one of the cabin interfaces (14).
  6. 根据权利要求5所述的机舱总成(100),其中,每个所述机舱单元(20)还包括支撑架(23),所述支撑架(23)设置于所述容纳腔(211)内并与所述机舱罩(21)连接,所述支撑架(23)至少部分凸出于所述机舱罩(21)设置并与所述机舱接口(14)连接。The nacelle assembly (100) according to claim 5, wherein each nacelle unit (20) further comprises a support frame (23), and the support frame (23) is arranged in the accommodating cavity (211) And connected with the nacelle cover (21), the support frame (23) at least partially protrudes from the nacelle cover (21) and is connected with the nacelle interface (14).
  7. 根据权利要求6所述的机舱总成(100),其中,所述机舱接口(14)以及所述支撑架(23)的一者包括插接凸起,另一者包括插接槽,所述插接凸起与所述插接槽的形状相匹配并插接连接。The nacelle assembly (100) according to claim 6, wherein one of the nacelle interface (14) and the support frame (23) includes a plug-in protrusion, and the other includes a plug-in slot, and the The insertion protrusion matches the shape of the insertion groove and is connected by insertion.
  8. 根据权利要求6所述的机舱总成(100),其中,所述机舱接口(14)包括第一法兰,所述支撑架(23)包括第二法兰,所述第一法兰以及所述第二法兰的形状相匹配并相互连接。The nacelle assembly (100) according to claim 6, wherein the nacelle interface (14) includes a first flange, the support frame (23) includes a second flange, the first flange and the The shape of the second flange matches and connects with each other.
  9. 根据权利要求6所述的机舱总成(100),其中,所述支撑架(23)为镂空的框架结构。The nacelle assembly (100) according to claim 6, wherein the support frame (23) is a hollow frame structure.
  10. 根据权利要求9所述的机舱总成(100),其中,所述支撑架(23)包括多个纵向型材(232)以及多个横向型材(231),多个所述纵向型材(232)沿所述横向型材(231)的延伸方向间隔分布,多个所述横向型材(231)沿所述纵向型材(232)的延伸方向间隔分布,每个所述横向型材(231)与各所述纵向型材(232)相交设置并相互连接。The nacelle assembly (100) according to claim 9, wherein the support frame (23) comprises a plurality of longitudinal profiles (232) and a plurality of transverse profiles (231), and the plurality of longitudinal profiles (232) are The extending direction of the transverse profiles (231) is distributed at intervals, a plurality of the transverse profiles (231) are distributed at intervals along the extending direction of the longitudinal profiles (232), and each of the transverse profiles (231) is connected to each of the longitudinal profiles (231). Profiles (232) are arranged intersecting and interconnected.
  11. 根据权利要求5所述的机舱总成(100),其中,所述第一自由端(12)包括第一环形法兰,所述第一环形法兰用于与所述塔架(200)可拆卸连接,所述第二自由端(13)包括第二环形法兰,所述第二环形法兰用于与所述发电机(400)可拆卸连接。The nacelle assembly (100) according to claim 5, wherein the first free end (12) comprises a first annular flange, and the first annular flange is adapted to be compatible with the tower (200) For detachable connection, the second free end (13) includes a second annular flange, and the second annular flange is used for detachable connection with the generator (400).
  12. 根据权利要求6所述的机舱总成(100),其中,所述功能器件(22)连接于所述支撑架(23)或机舱罩。The nacelle assembly (100) according to Claim 6, wherein the functional device (22) is connected to the support frame (23) or the nacelle cover.
  13. 根据权利要求1至4任意一项所述的机舱总成(100),其中,所述机舱总成(100)还包括防护罩(30),所述防护罩(30)包覆所述连接座(10)设置,所述防护罩(30)对应每个所述机舱单元(20)均设置有避让口。The nacelle assembly (100) according to any one of claims 1 to 4, wherein the nacelle assembly (100) further comprises a protective cover (30), and the protective cover (30) covers the connecting seat (10) setting, the protective cover (30) is provided with an escape opening corresponding to each of the cabin units (20).
  14. 根据权利要求1至4任意一项所述的机舱总成(100),其中,所述连接座(10)为轴对称结构且具有中心线(aa),所述机舱单元(20)的数量为n个;The nacelle assembly (100) according to any one of claims 1 to 4, wherein the connecting seat (10) is an axisymmetric structure and has a centerline (aa), and the number of the nacelle units (20) is n;
    其中,n为大于等于2的偶数,n个所述机舱单元(20)分成两组单元组,每组所述单元组包括至少一个机舱单元(20),两组所述单元组对称分布于所述中心线(aa)的两侧。Wherein, n is an even number greater than or equal to 2, and the n said cabin units (20) are divided into two groups of unit groups, each group of said unit groups includes at least one cabin unit (20), and said two groups of said unit groups are symmetrically distributed in said on both sides of the center line (aa).
  15. 根据权利要求1至4任意一项所述的机舱总成(100),其中,所述连接座(10)为轴对称结构且具有中心线(aa),所述机舱单元(20)的数量为n个;The nacelle assembly (100) according to any one of claims 1 to 4, wherein the connecting seat (10) is an axisymmetric structure and has a centerline (aa), and the number of the nacelle units (20) is n;
    其中,n为大于2的奇数,n-1个所述机舱单元(20)分成两组单元组,每组所述单元组包括至少一个机舱单元(20),两组所述单元组对称分布于所述中心线(aa)的两侧,剩余一个所述机舱单元(20)连接于所述连接座(10)位于两组所述单元组之间的区域。Wherein, n is an odd number greater than 2, n-1 said cabin units (20) are divided into two groups of unit groups, each group of said unit groups includes at least one cabin unit (20), and said unit groups of two groups are symmetrically distributed in On both sides of the central line (aa), the remaining one cabin unit (20) is connected to the area where the connecting seat (10) is located between two sets of the unit groups.
  16. 根据权利要求1至4任意一项所述的机舱总成(100),其中,所述机舱总成(100)还包括控制柜(40),至少一个机舱单元(20)的所述功能器件(22)与所述控制柜(40)电连接。The nacelle assembly (100) according to any one of claims 1 to 4, wherein the nacelle assembly (100) further comprises a control cabinet (40), the functional device ( 22) It is electrically connected with the control cabinet (40).
  17. 一种风力发电机组,其中,包括:A wind turbine, comprising:
    塔架(200);tower (200);
    如权利要求1至16任意一项所述的机舱总成(100),所述机舱总成(100)设置于所述塔架(200);The nacelle assembly (100) according to any one of claims 1 to 16, wherein the nacelle assembly (100) is arranged on the tower (200);
    偏航系统,连接于所述塔架(200)与所述连接座(10);a yaw system, connected to the tower (200) and the connecting seat (10);
    发电机(400),包括转动配合的转子(410)、定子(420)以及与所述转子(410)及定子(420)电连接的接口,所述定子(420)连接于所述连接座(10),各所述机舱单元(20)的所述功能器件(22)与所述接口电连接;The generator (400) includes a rotor (410), a stator (420) that rotates, and an interface that is electrically connected to the rotor (410) and the stator (420), and the stator (420) is connected to the connecting seat ( 10), the functional devices (22) of each of the cabin units (20) are electrically connected to the interface;
    叶轮(300),连接于所述转子(410)。The impeller (300) is connected to the rotor (410).
  18. 根据权利要求17所述的风力发电机组,其中,所述发电机(400)包括多个绕组,每个所述绕组通过所述接口与其中一个所述机舱单元(20)的所述功能器件(22)电连接。The wind power generating set according to claim 17, wherein the generator (400) comprises a plurality of windings, each of the windings communicates with the functional device ( 22) Electrical connection.
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CN104234947A (en) * 2014-10-10 2014-12-24 中船重工(重庆)海装风电设备有限公司 Cabin environment control device of offshore wind generating set
US20200059178A1 (en) * 2017-05-05 2020-02-20 Wobben Properties Gmbh Wind turbine with overload-capable converter system
CN113357090A (en) * 2021-06-28 2021-09-07 新疆金风科技股份有限公司 Cabin assembly and wind generating set

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