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CN206753830U - The engine room cover and wind power generating set of wind power generating set - Google Patents

The engine room cover and wind power generating set of wind power generating set Download PDF

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Publication number
CN206753830U
CN206753830U CN201720383835.9U CN201720383835U CN206753830U CN 206753830 U CN206753830 U CN 206753830U CN 201720383835 U CN201720383835 U CN 201720383835U CN 206753830 U CN206753830 U CN 206753830U
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flange
wind power
generating set
casing
power generating
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CN201720383835.9U
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姚志岗
武青虎
朱长录
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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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    • 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
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/50Manufacturing or production processes characterised by the final manufactured product

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Abstract

本实用新型提供一种风力发电机组的机舱罩和风力发电机组,风力发电机组的机舱罩包括:第一罩壳,第一罩壳具有第一法兰和位于第一法兰上的多个第一通孔;第二罩壳,第二罩壳具有第二法兰和位于第二法兰上的多个第二通孔;第一法兰上设置有凸出部,第二法兰上设置有限位部,凸出部与限位部在第一法兰与第二法兰接合时彼此形状配合,以使第一法兰的多个第一通孔和第二法兰的相对应的多个第二通孔彼此对准。能够实现提高该机舱罩的各罩壳之间的组装效率、节省人力物力、降低生产成本中的一个或多个目的。

The utility model provides a nacelle cover of a wind power generator set and a wind power generator set. The nacelle cover of the wind power generator set includes: a first cover shell, the first cover shell has a first flange and a plurality of third flanges located on the first flange. a through hole; a second cover shell, the second cover shell has a second flange and a plurality of second through holes located on the second flange; a protrusion is provided on the first flange, and a protrusion is provided on the second flange. The limiting portion, the protruding portion and the limiting portion form-fit with each other when the first flange and the second flange are joined, so that the plurality of first through holes of the first flange and the corresponding plurality of first through holes of the second flange are formed. The second through holes are aligned with each other. One or more purposes of improving the assembly efficiency between the various covers of the nacelle cover, saving manpower and material resources, and reducing production costs can be achieved.

Description

风力发电机组的机舱罩和风力发电机组Nacelles and wind turbines for wind turbines

技术领域technical field

本实用新型涉及风力发电技术领域,尤其涉及一种风力发电机组的机舱罩和风力发电机组。The utility model relates to the technical field of wind power generation, in particular to a nacelle cover of a wind power generator set and a wind power generator set.

背景技术Background technique

机舱罩作为风力发电机组不可或缺的一部分,起着保护主机、防风、防雨、防沙、防雷、通风散热等作用。为了便于安装和运输,目前机舱罩通常采用分片设计,然后进行整体运输或分片运输。一台机舱罩通常会分为三片或四片罩壳,且随着风力发电机单机容量的不断升高,机舱的外形尺寸越来越大,为了运输的需要,可能会将机舱罩分成更多片。而各罩壳的装配形式为将每两个相邻的罩壳上的法兰对接,然后采用螺栓将对接后的法兰紧固连接。As an integral part of the wind turbine, the nacelle cover plays the role of protecting the main engine, wind, rain, sand, lightning, ventilation and heat dissipation. In order to facilitate installation and transportation, the current nacelle cover is usually designed in pieces, and then transported as a whole or in pieces. A nacelle cover is usually divided into three or four pieces of shells, and with the continuous increase of the capacity of a single wind turbine, the size of the nacelle is getting larger and larger. For the needs of transportation, the nacelle cover may be divided into more parts. Multiple slices. The assembly form of each casing is to butt the flanges on every two adjacent casings, and then use bolts to fasten the butt-joined flanges.

在各罩壳之间的法兰边对接时,需要在吊具的辅助下对两个相邻的罩壳的法兰进行对齐操作,以使两个法兰上的连接孔对正。但是在对法兰进行对齐操作时,通常需要4个或5个装配工同时配合操作才能完成。因此,现有的机舱罩的装配过程中存在浪费人力、物力等资源的问题。When the flanges between the casings are butted, it is necessary to align the flanges of the two adjacent casings with the assistance of the spreader, so that the connection holes on the two flanges are aligned. However, when aligning flanges, it usually takes 4 or 5 assemblers to cooperate at the same time to complete the operation. Therefore, there is a problem of wasting resources such as manpower and material resources in the assembly process of the existing nacelle cover.

因此,亟需一种新的风力发电机组的机舱罩和风力发电机组。Therefore, need badly a kind of nacelle cover and wind power generating set of new wind generating set.

实用新型内容Utility model content

根据本实用新型的实施例,提供了一种风力发电机组的机舱罩和风力发电机组,能够实现提高该机舱罩的各罩壳之间的组装效率、节省人力物力、降低生产成本中的一个或多个目的。According to an embodiment of the present invention, a nacelle cover of a wind power generating set and a wind power generating set are provided, which can achieve one or more of improving the assembly efficiency between the casings of the nacelle cover, saving manpower and material resources, and reducing production costs. multiple purposes.

根据本实用新型实施例的一个方面,提供了一种风力发电机组的机舱罩,包括:第一罩壳,第一罩壳具有第一法兰和位于第一法兰上的多个第一通孔;第二罩壳,第二罩壳具有第二法兰和位于第二法兰上的多个第二通孔;第一法兰上设置有凸出部,第二法兰上设置有限位部,凸出部与限位部在第一法兰与第二法兰接合时彼此形状配合,以使第一法兰的多个第一通孔和第二法兰的相对应的多个第二通孔彼此对准。According to an aspect of an embodiment of the present invention, there is provided a nacelle cover for a wind power generating set, comprising: a first cover, the first cover has a first flange and a plurality of first passages on the first flange hole; the second casing, the second casing has a second flange and a plurality of second through holes on the second flange; the first flange is provided with a protrusion, and the second flange is provided with a limit When the first flange and the second flange are joined together, the protruding part and the limiting part are in shape fit with each other, so that the plurality of first through holes of the first flange and the corresponding plurality of first through holes of the second flange The two through holes are aligned with each other.

根据本实用新型实施例的一个方面,凸出部连续地设置在第一法兰上。According to an aspect of the embodiment of the present utility model, the protruding part is continuously arranged on the first flange.

根据本实用新型实施例的一个方面,凸出部为两个或两个以上,并且两个或两个以上的凸出部彼此间隔地设置在第一法兰上。According to an aspect of the embodiment of the present invention, there are two or more protrusions, and the two or more protrusions are arranged on the first flange at intervals from each other.

根据本实用新型实施例的一个方面,凸出部设置在第一法兰的端面上,限位部为设置在第二法兰的端面上的凹槽,并且凸出部能够容纳在凹槽中。According to an aspect of the embodiment of the present invention, the protruding part is arranged on the end surface of the first flange, the limiting part is a groove provided on the end surface of the second flange, and the protruding part can be accommodated in the groove .

根据本实用新型实施例的一个方面,凸出部靠近第一法兰与第一罩壳的接合部位,并且凸出部的外表面与第一罩壳的外表面平齐。According to an aspect of the embodiment of the present invention, the protruding part is close to the junction between the first flange and the first housing, and the outer surface of the protruding part is flush with the outer surface of the first housing.

根据本实用新型实施例的一个方面,凸出部设置在第一法兰的边缘部位,限位部为第二法兰的侧面,并且侧面能够抵靠在凸出部的相对应的部位上。According to an aspect of the embodiment of the present invention, the protruding part is arranged on the edge of the first flange, the limiting part is the side of the second flange, and the side can abut against the corresponding part of the protruding part.

根据本实用新型实施例的一个方面,风力发电机组的机舱罩还包括定位销,定位销可拆卸地连接在第一法兰和第二法兰上,以使第一法兰的多个第一通孔和第二法兰的相对应的多个第二通孔彼此对准。According to an aspect of the embodiment of the present utility model, the nacelle cover of the wind power generating set further includes positioning pins, which are detachably connected to the first flange and the second flange, so that the plurality of first flanges of the first flange The through holes and the corresponding plurality of second through holes of the second flange are aligned with each other.

根据本实用新型实施例的一个方面,定位销为两个或两个以上,并且两个或两个以上的定位销中的相邻的两个定位销之间隔开预定距离。According to an aspect of the embodiment of the present invention, there are two or more positioning pins, and there is a predetermined distance between two adjacent positioning pins among the two or more positioning pins.

根据本实用新型实施例的一个方面,定位销包括销体、与销体固定连接的基板、具有第三销孔的压板以及连接件,销体穿入第一法兰设置的第一销孔、第二法兰的相对应的第二销孔以及压板的第三销孔,并且通过连接件将基板与压板连接在一起,以使基板和压板压紧第一法兰和第二法兰。According to an aspect of the embodiment of the present invention, the positioning pin includes a pin body, a substrate fixedly connected to the pin body, a pressure plate with a third pin hole and a connecting piece, and the pin body penetrates into the first pin hole provided by the first flange, The corresponding second pin hole of the second flange and the third pin hole of the pressure plate connect the base plate and the pressure plate through the connecting piece, so that the base plate and the pressure plate press the first flange and the second flange.

根据本实用新型实施例的另一个方面,还提供了一种风力发电机组,包括上述的风力发电机组的机舱罩。According to another aspect of the embodiment of the present utility model, a wind power generating set is also provided, including the above-mentioned nacelle cover of the wind generating set.

综上,本实用新型实施例的风力发电机组的机舱罩和风力发电机组,通过在相邻的两个罩壳的彼此相对的边缘上设置的法兰处对应地设置凸出部和限位部,通过凸出部和限位部彼此形状配合形成定位结构,以在组装两个罩壳时能够在不借助任何外部结构的情况下将两个法兰彼此对齐。因此,在对机舱罩进行装配时,不需要投入过多的人力物力,即可实现风力发电机组机舱的快速装配。能够免去需要多个吊装设备同时操作的复杂操作过程,缩短了装配工时,从而提高了风力发电机组整体的组装效率,也在一定程度上节省了风力发电机组的组装成本。To sum up, the nacelle cover of the wind turbine generator set and the wind turbine generator set according to the embodiment of the utility model are provided with protrusions and stoppers correspondingly at the flanges provided on the opposite edges of the two adjacent shells. , the positioning structure is formed through the shape fit between the protruding part and the limiting part, so that the two flanges can be aligned with each other without any external structure when the two casings are assembled. Therefore, when assembling the nacelle cover, rapid assembly of the nacelle of the wind power generating set can be realized without investing too much manpower and material resources. It can avoid the complicated operation process that requires simultaneous operation of multiple hoisting devices, shorten the assembly man-hours, thereby improving the overall assembly efficiency of the wind power generating set, and also saving the assembly cost of the wind generating set to a certain extent.

附图说明Description of drawings

从下面结合附图对本实用新型的具体实施方式的描述中可以更好地理解本实用新型,其中:Can understand the utility model better from the following in conjunction with accompanying drawing to the description of the specific embodiment of the utility model, wherein:

通过阅读以下参照附图对非限制性实施例所作的详细描述,本实用新型的其它特征、目的和优点将会变得更明显,其中,相同或相似的附图标记表示相同或相似的特征。Other features, objects and advantages of the present invention will become more apparent by reading the following detailed description of non-limiting embodiments with reference to the accompanying drawings, wherein the same or similar reference numerals represent the same or similar features.

图1是根据本实用新型一个实施例的风力发电机组的机舱罩的剖面结构示意图;Fig. 1 is a schematic cross-sectional structure diagram of a nacelle cover of a wind generating set according to an embodiment of the present invention;

图2是由图1的机舱罩形成的机舱的左视结构示意图;Fig. 2 is the left view structural diagram of the nacelle formed by the nacelle cover of Fig. 1;

图3是图1和图2中的机舱罩的第一罩壳和第二罩壳的接合部位的剖面结构示意图;Fig. 3 is a schematic cross-sectional structural view of the junction of the first casing and the second casing of the nacelle cover in Fig. 1 and Fig. 2;

图4是图3中的第一罩壳和第二罩壳的接合部位的结构爆炸示意图;Fig. 4 is a structural exploded schematic view of the junction of the first casing and the second casing in Fig. 3;

图5是根据本实用新型另一个实施例的第一罩壳和第二罩壳的接合部位的结构爆炸示意图;Fig. 5 is a structural exploded schematic view of the junction of the first casing and the second casing according to another embodiment of the present invention;

图6是根据本实用新型再一个实施例的第一罩壳和第二罩壳的接合部位的剖面结构示意图;Fig. 6 is a schematic cross-sectional structural view of the junction of the first casing and the second casing according to another embodiment of the present invention;

图7是根据本实用新型一个实施例的第一罩壳和第二罩壳的接合部位的立体结构示意图;Fig. 7 is a three-dimensional structural schematic view of the junction of the first casing and the second casing according to an embodiment of the present invention;

图8是图7中的A部分放大后的结构示意图。FIG. 8 is an enlarged structural schematic diagram of part A in FIG. 7 .

其中:in:

1-机舱;1 - engine room;

10-第一罩壳;11-第一法兰;110-第一通孔;111-凸边;112-凸棱;113-凸边;10-the first casing; 11-the first flange; 110-the first through hole; 111-the raised edge; 112-the raised edge; 113-the raised edge;

20-第二罩壳;21-第二法兰;210-第二通孔;211-凹槽;212-凹槽;213-侧面;20-second casing; 21-second flange; 210-second through hole; 211-groove; 212-groove; 213-side;

30-第三罩壳;31-第三法兰;30-the third casing; 31-the third flange;

40-螺栓组件;40 - bolt assembly;

50-定位销;51-基板;52-销体;53-压板;54-连接件。50-location pin; 51-base plate; 52-pin body; 53-press plate; 54-connector.

具体实施方式detailed description

下面将详细描述本实用新型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,以便提供对本实用新型的全面理解。但是,对于本领域技术人员来说很明显的是,本实用新型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实用新型的示例来提供对本实用新型的更好的理解。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,以便避免对本实用新型造成不必要的模糊;并且,为了清晰,可能夸大了部分结构的尺寸。在图中相同的附图标记表示相同或类似的结构,因而将省略它们的详细描述。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 invention 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 present invention. It will be apparent, however, to one skilled in the art that the present invention 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 invention by showing examples of the present invention. In the drawings and the following description, at least some of the well-known structures and techniques are not shown in order to avoid unnecessary obscurity of the present invention; and, for clarity, the size of some structures may be exaggerated. The same reference numerals in the drawings denote the same or similar structures, and thus their detailed descriptions will be omitted. 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,并不是对本实用新型的风力发电机组的机舱罩的具体结构进行限定。在本实用新型的描述中,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实用新型中的具体含义。The orientation words appearing in the following description are all the directions shown in the figure, and are not intended to limit the specific structure of the nacelle cover of the wind generating set of the present invention. In the description of the present utility model, 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 integrally connected; can be directly connected or indirectly connected. Those of ordinary skill in the art can understand the specific meanings of the above terms in the present utility model according to specific situations.

本实用新型实施例提供的风力发电机组的机舱罩包括彼此连接的罩壳,根据不同型号的风力发电机组可以将机舱罩分成多个罩壳,每两个相邻的第一罩壳和第二罩壳通过法兰和螺栓组件彼此连接形成机舱,用于放置主机等重要设备。由于本实用新型实施例提供的风力发电机组的机舱罩的相邻两个罩壳连接时的对齐操作简单、便捷,因此能够节省装配工时,从而提高风力发电机组的装配效率。The nacelle cover of the wind power generating set provided by the embodiment of the utility model includes shells connected to each other. According to different types of wind generating sets, the nacelle cover can be divided into multiple shells, and every two adjacent first shells and second The casings are connected to each other through flanges and bolt assemblies to form a nacelle, which is used to place important equipment such as the main engine. Since the alignment operation when connecting two adjacent casings of the nacelle cover of the wind power generating set provided by the embodiment of the utility model is simple and convenient, assembly man-hours can be saved, thereby improving the assembly efficiency of the wind generating set.

为了更好地理解本实用新型,下面结合图1至8根据本实用新型实施例的风力发电机组的机舱罩进行详细描述。In order to better understand the utility model, the nacelle cover of the wind power generating set according to the embodiment of the utility model will be described in detail below with reference to FIGS. 1 to 8 .

图1是根据本实用新型一个实施例的风力发电机组的机舱罩的剖面结构示意图,图2是由图1的机舱罩形成的机舱1的左视结构示意图,图3是图1和图2中的机舱罩的第一罩壳10和第二罩壳20的接合部位的剖面结构示意图。Fig. 1 is a schematic cross-sectional structural view of a nacelle cover of a wind power generating set according to an embodiment of the present invention, Fig. 2 is a left view structural view of the nacelle 1 formed by the nacelle cover of Fig. A schematic cross-sectional structural view of the junction of the first cover 10 and the second cover 20 of the nacelle cover.

根据本实用新型的一个实施例,风力发电机组的机舱罩,包括第一罩壳10和第二罩壳20。第一罩壳10具有第一法兰11和位于第一法兰11上的多个第一通孔110。第二罩壳20具有第二法兰21和位于第二法兰21上的多个第二通孔210。第一法兰11上设置有凸出部,第二法兰21上设置有限位部,凸出部与限位部在第一法兰11与第二法兰21接合时彼此形状配合,以使第一法兰11的多个第一通孔110和第二法兰21的对应的多个第二通孔210彼此对准。According to an embodiment of the present invention, the nacelle cover of the wind power generating set includes a first cover 10 and a second cover 20 . The first casing 10 has a first flange 11 and a plurality of first through holes 110 on the first flange 11 . The second housing 20 has a second flange 21 and a plurality of second through holes 210 on the second flange 21 . The first flange 11 is provided with a protruding portion, and the second flange 21 is provided with a limiting portion, and the protruding portion and the limiting portion are in shape fit with each other when the first flange 11 and the second flange 21 are engaged, so that The plurality of first through holes 110 of the first flange 11 and the corresponding plurality of second through holes 210 of the second flange 21 are aligned with each other.

由此,本实用新型实施例的风力发电机组的机舱罩在相邻的两个罩壳的彼此相对的边缘上设置的法兰处对应地设置凸出部和限位部,通过凸出部和限位部彼此形状配合形成定位结构,从而组装两个罩壳时能够在不借助任何外部结构的情况下将两个法兰彼此对齐。因此,不需要投入过多的人力物力,即可实现风力发电机组机舱1的快速装配。能够免去需要多个吊装设备同时操作的复杂操作过程,缩短了装配工时,从而提高了风力发电机组整体的组装效率,也在一定程度上节省了风力发电机组的组装成本,从而提高了风力发电机组整体的组装效率。并且通过采用在两个罩壳自身上设置定位结构的方式,能够使两个法兰上相对应的多个通孔精确对准,因此能够有效地提高机舱1整体的装配精度,避免通孔彼此错位产生较大误差,而给后续的螺栓组件的装配造成困难。Therefore, the nacelle cover of the wind power generating set according to the embodiment of the utility model is provided with corresponding protrusions and stoppers at the flanges provided on the opposite edges of two adjacent housings, through the protrusions and The position-limiting parts form a positioning structure in shape fit with each other, so that the two flanges can be aligned with each other without any external structure when assembling the two casings. Therefore, rapid assembly of the nacelle 1 of the wind generating set can be realized without investing too much manpower and material resources. It can avoid the complex operation process that requires multiple hoisting equipment to operate at the same time, shorten the assembly man-hours, thereby improving the overall assembly efficiency of the wind turbine, and also saving the assembly cost of the wind turbine to a certain extent, thereby improving wind power generation. Overall assembly efficiency of the unit. And by adopting the method of setting the positioning structure on the two casings themselves, the corresponding multiple through holes on the two flanges can be accurately aligned, so the overall assembly accuracy of the nacelle 1 can be effectively improved, and the through holes can be avoided from being connected to each other. The misalignment produces a large error, which makes it difficult to assemble the subsequent bolt assembly.

本实用新型实施例中的风力发电机组的机舱罩(以下简称机舱罩)所描述的包括第一罩壳和第二罩壳并不仅仅指机舱罩包括两个罩壳,而是指机舱罩包括至少两个罩壳,也是指包括两类罩壳,两类罩壳分别被定义成第一罩壳和第二罩壳,并且在其结合部位处彼此对应地设置定位结构。可以理解的是,在其他的实施例中,机舱罩还可以包括更多个罩壳。The description of the nacelle cover (hereinafter referred to as the nacelle cover) of the wind power generating set in the embodiment of the present invention including the first cover and the second cover does not only mean that the nacelle cover includes two covers, but refers to that the nacelle cover includes At least two casings also refers to including two types of casings, the two types of casings are respectively defined as a first casing and a second casing, and positioning structures are provided corresponding to each other at their joint locations. It can be understood that, in other embodiments, the nacelle cover may also include more shells.

机舱1由风力发电机组的机舱罩构成,具有空腔,并且机舱1通常为六面体结构。示例性地,如果机舱罩只包括两个罩壳时,则此时机舱1可以采取将整体结构分割成两部分结构再进行接合的方式,例如可以沿水平方向(按照附图的观察视角)将机舱1整体分割成两个罩壳,也可以沿机舱1的纵长方向将机舱1分割成两个罩壳。而如果机舱罩包括更多个罩壳时,机舱1可以采取将其所有侧壁皆单独设置为分体结构再进行接合的方式,即机舱1的每个侧壁都形成一个单独的罩壳。或者采取将每两个或者三个相邻的侧壁设置成一个罩壳,然后再将所有的罩壳进行拼接。以下将会根据具体的示例对罩壳不同的组合进行说明。The nacelle 1 is constituted by the nacelle cover of the wind power generating set, has a cavity, and the nacelle 1 is generally a hexahedral structure. Exemplarily, if the nacelle cover only includes two casings, then the nacelle 1 can adopt the method of dividing the overall structure into two parts and then joining them together, for example, the nacelle can be divided along the horizontal direction (according to the viewing angle of the drawing). The nacelle 1 is integrally divided into two casings, and the nacelle 1 can also be divided into two casings along the longitudinal direction of the nacelle 1 . And if the nacelle cover includes more casings, all side walls of the nacelle 1 can be separately arranged as split structures and then joined together, that is, each side wall of the nacelle 1 forms a separate casing. Alternatively, every two or three adjacent side walls are arranged as a casing, and then all the casings are spliced together. The following will describe different combinations of casings according to specific examples.

图2示出的机舱1整体包括底壁、连接在底壁两侧的两个相对的侧壁、顶壁、后端壁以及前端壁(图中示出的前端壁具有圆形的开口)。在本实施例中,机舱1的所有侧壁被形成为三部分结构,即,图2中机舱1包括上方第一罩壳10、位于左下方的第二罩壳20和位于右下方的第三罩壳30(所有方向皆按照附图的观察视角)。通过第二罩壳20和第三罩壳30彼此连接组成机舱1的下半部舱体,当将机舱1内的设备安装完毕后即可将第一罩壳10盖合在下半部舱体上,即将第一罩壳10分别与第二罩壳20和第三罩壳30连接。The nacelle 1 shown in FIG. 2 as a whole includes a bottom wall, two opposite side walls connected on both sides of the bottom wall, a top wall, a rear end wall and a front end wall (the front end wall shown in the figure has a circular opening). In this embodiment, all side walls of the nacelle 1 are formed into a three-part structure, that is, the nacelle 1 in FIG. Housing 30 (all directions are according to the viewing angle of the drawings). The second casing 20 and the third casing 30 are connected to each other to form the lower half of the cabin body of the nacelle 1. After the equipment in the nacelle 1 is installed, the first casing 10 can be covered on the lower half of the cabin body. , that is, the first casing 10 is connected to the second casing 20 and the third casing 30 respectively.

第一罩壳10的边缘处形成有朝向机舱1内部垂直延伸的第一法兰11,第二罩壳20与第一罩壳10以及第三罩壳30接合的边缘处形成有朝向机舱1内部垂直延伸的第二法兰21,第三罩壳30与第一罩壳10和第二罩壳20接合的边缘处形成有朝向机舱1内部垂直延伸的第三法兰31。第一法兰11上设置有多个第一通孔110,第二法兰21上设置有与所述多个第一通孔110对应的多个第二通孔210,第三法兰31上设置有分别与多个第一通孔110和多个第二通孔210对应的第三通孔(图中未示出)。由此,采用多组螺栓组件40分别穿过对应的第一通孔110、第二通孔210以及第三通孔即可将第一罩壳10、第二罩壳20以及第三罩壳30彼此接合。A first flange 11 extending vertically toward the interior of the nacelle 1 is formed at the edge of the first casing 10 , and a flange 11 is formed at the edge of the second casing 20 joining the first casing 10 and the third casing 30 toward the interior of the nacelle 1 . The second flange 21 extending vertically, the third flange 31 vertically extending toward the inside of the nacelle 1 is formed at the edge where the third casing 30 joins the first casing 10 and the second casing 20 . The first flange 11 is provided with a plurality of first through holes 110, the second flange 21 is provided with a plurality of second through holes 210 corresponding to the plurality of first through holes 110, and the third flange 31 Third through holes (not shown in the figure) respectively corresponding to the plurality of first through holes 110 and the plurality of second through holes 210 are provided. Thus, the first casing 10 , the second casing 20 and the third casing 30 can be connected by passing through the corresponding first through holes 110 , second through holes 210 and third through holes respectively by adopting multiple sets of bolt assemblies 40 . join each other.

在本实施中为了进行区分,将同时与第一罩壳10和第二罩壳20连接的罩壳称为第三罩壳,但是可以理解的是,这里只是名称上的区分。在将第三罩壳30与第一罩壳10连接时,第三罩壳30即作为第二罩壳,即在第三罩壳30与第一罩壳10的第一法兰11接合的第三法兰31上设置有限位部。而将第三罩壳30与第二罩壳20连接时,第三罩壳30即作为第一罩壳,即在第三罩壳30与第二罩壳20的第二法兰21接合的第三法兰31上设置有凸出部。当然本实用新型实施例对各个罩壳的位置并不进行限制,在其他的实施例中,三个罩壳还可以彼此互换位置。以下主要以第一罩壳10和第二罩壳20的连接形式对机舱罩中的两个相邻的罩壳之间的接合方式进行详细说明。In this embodiment, in order to distinguish, the shell connected to the first shell 10 and the second shell 20 is called the third shell, but it can be understood that the distinction is only in name. When the third casing 30 is connected to the first casing 10, the third casing 30 acts as the second casing, that is, the third casing 30 is connected with the first flange 11 of the first casing 10. Limiting parts are arranged on the three flanges 31 . When the third casing 30 is connected to the second casing 20, the third casing 30 is used as the first casing, that is, the third casing 30 is connected to the second flange 21 of the second casing 20. Protruding parts are arranged on the three flanges 31 . Of course, the embodiments of the present utility model do not limit the positions of the casings, and in other embodiments, the three casings can also exchange positions with each other. In the following, the connection between two adjacent casings in the nacelle casing will be described in detail mainly in terms of the connection form of the first casing 10 and the second casing 20 .

为了提高第一罩壳10和第二罩壳20的组装效率,在第一罩壳10和第二罩壳20的接合部位对应地设置有定位结构,即,在第一罩壳10的第一法兰11上设置有凸出部,而对应地在第二罩壳20的第二法兰21上设置有限位部,凸出部和限位部的形状彼此相适应,以在第一法兰11和第二法兰21接合时,通过凸出部和限位部彼此形状配合使多个第一通孔110和多个第二通孔210彼此对准。当然,凸出部可以采用一体成型的方式设置在第一法兰11上,也可以采用分体的形式固定连接在第一法兰11上。In order to improve the assembly efficiency of the first casing 10 and the second casing 20, a positioning structure is correspondingly provided at the junction of the first casing 10 and the second casing 20, that is, at the first A protruding portion is provided on the flange 11, and a limiting portion is correspondingly provided on the second flange 21 of the second casing 20. When the flange 11 and the second flange 21 are engaged, the plurality of first through holes 110 and the plurality of second through holes 210 are aligned with each other through the shape fit between the protruding portion and the limiting portion. Of course, the protruding part can be integrally formed on the first flange 11 , or can be fixedly connected to the first flange 11 in a separate form.

图4是图3中的第一罩壳10和第二罩壳20的接合部位的结构爆炸示意图,在一个实施例中,由图3和图4可以看出,凸出部设置在第一法兰11的面向第二法兰21的端面上,限位部为设置在第二法兰21的面向第一法兰11的端面上并能够接收凸出部的凹槽。在一个可选的实施例中,凸出部和限位部之间采用间隙配合的方式,以避免凸出部和限位部出现尺寸误差或者端部侧面存在毛刺等情况时影响第一罩壳10和第二罩壳20以及第三罩壳30彼此之间的装配精度,当然此间隙需要控制在一定范围内,避免影响第一法兰11和第二法兰21彼此对齐。Fig. 4 is a structural exploded view of the junction of the first casing 10 and the second casing 20 in Fig. 3. In one embodiment, it can be seen from Fig. 3 and Fig. On the end surface of the flange 11 facing the second flange 21 , the limiting portion is a groove provided on the end surface of the second flange 21 facing the first flange 11 and capable of receiving the protrusion. In an optional embodiment, a clearance fit is adopted between the protrusion and the limiting part, so as to prevent the first casing from being affected by dimensional errors between the protrusion and the limiting part or burrs on the side of the end. 10 , the assembly accuracy between the second shell 20 and the third shell 30 , of course, the gap needs to be controlled within a certain range, so as to avoid affecting the alignment of the first flange 11 and the second flange 21 .

在本实施例中,具体地,凸出部为设置在第一法兰11上的凸边111,而限位部为设置在第二法兰21上的能够与凸边111配合的凹槽211。示例性地,凸边111设置在靠近第一法兰11与第一罩壳10的接合位置处,并且凸边111的外表面和第一罩壳10的外表面平齐。凹槽211形成在第二法兰21和第二罩壳20的接合位置处并与凸边111的位置相对应,凹槽211包括呈直角布置的两个壁面,以通过两个壁面分别和凸边111的两个相邻并垂直的壁面抵靠配合。当然在其他的实施例中,凸边111与凹槽211贴合的壁面也可以不垂直。通过将凸边111和凹槽211分别设置在靠近第一罩壳10和第二罩壳20一侧,便于装配人员在机舱1外部直接观察第一罩壳10和第二罩壳20的对接情况,并且降低了制造难度。In this embodiment, specifically, the protruding portion is a flange 111 provided on the first flange 11 , and the limiting portion is a groove 211 provided on the second flange 21 capable of cooperating with the flange 111 . Exemplarily, the protruding edge 111 is disposed close to the joint position between the first flange 11 and the first housing 10 , and the outer surface of the protruding edge 111 is flush with the outer surface of the first housing 10 . The groove 211 is formed at the joint position of the second flange 21 and the second casing 20 and corresponds to the position of the flange 111. The groove 211 includes two walls arranged at right angles, so as to pass through the two walls respectively and the flange. Two adjacent and vertical wall surfaces of the edge 111 are abutted and fitted. Of course, in other embodiments, the wall where the protruding edge 111 and the groove 211 fit together may not be vertical. By arranging the flange 111 and the groove 211 on the side close to the first cover 10 and the second cover 20 respectively, it is convenient for the assembler to directly observe the docking condition of the first cover 10 and the second cover 20 outside the nacelle 1 , and reduce the manufacturing difficulty.

在一个可选的实施例中,凸出部连续地设置在第一法兰11上。具体地,由图2可以看出沿第一罩壳10边缘设置的第一法兰11大致呈U形,上述的凸边111沿第一法兰11的整个延伸长度连续地设置,所以凸边111沿第一罩壳10与第二罩壳20以及第三罩壳30的接合部位大致呈U形地延伸。当然,对应地凹槽211沿第二法兰21和第三法兰31的整个延伸长度连续地设置,即,凹槽211对应凸边111大致呈U形地延伸。此时,彼此配合的凸边111和凹槽211可以沿第一罩壳10和第二罩壳20以及第三罩壳30的接合部位形成大致环形的定位结构(此处忽略形成在机舱1的前端壁上的圆形开口)。In an optional embodiment, the protrusions are continuously provided on the first flange 11 . Specifically, it can be seen from FIG. 2 that the first flange 11 arranged along the edge of the first casing 10 is roughly U-shaped, and the above-mentioned raised edge 111 is continuously arranged along the entire extension length of the first flange 11, so the raised edge 111 extends substantially in a U-shape along joints of the first casing 10 , the second casing 20 and the third casing 30 . Certainly, correspondingly, the groove 211 is provided continuously along the entire extension length of the second flange 21 and the third flange 31 , that is, the groove 211 extends substantially in a U-shape corresponding to the flange 111 . At this time, the protruding edge 111 and the groove 211 that cooperate with each other can form a substantially annular positioning structure along the junction of the first casing 10, the second casing 20, and the third casing 30 (here, the position formed in the nacelle 1 is ignored. circular opening in the front wall).

另外,在一些实施例中,凸出部为两个或两个以上,也就是说可以将整个连续延伸设置的凸出部设置成多段的间隔结构,并且两个或两个以上的凸出部彼此间隔地设置在第一法兰11上。具体地,还以图2中的机舱1中设置的法兰结构为例,即两个或两个以上的凸边111沿大U形的第一法兰11的延伸长度间隔地设置,对应地,凹槽211可以沿第二罩壳20的第二法兰21和第三罩壳30的第三法兰31的整个延伸长度间隔地设置。此时,间隔设置并彼此配合的两个或两个以上的凸边111和凹槽211依然可以沿第一罩壳10和第二罩壳20以及第三罩壳30的接合部位形成大致环形的定位结构(此处忽略形成的机舱1的前端壁上的圆形开口)。In addition, in some embodiments, there are two or more protruding parts, that is to say, the entire continuously extending protruding part can be arranged as a multi-stage interval structure, and the two or more protruding parts They are arranged at a distance from each other on the first flange 11 . Specifically, take the flange structure provided in the nacelle 1 in FIG. 2 as an example, that is, two or more flanges 111 are arranged at intervals along the extended length of the large U-shaped first flange 11, correspondingly The grooves 211 may be provided at intervals along the entire extension lengths of the second flange 21 of the second case 20 and the third flange 31 of the third case 30 . At this time, the two or more flanges 111 and grooves 211 that are arranged at intervals and cooperate with each other can still form a substantially annular shape along the joints of the first casing 10 , the second casing 20 and the third casing 30 . Positioning structure (the circular opening formed on the front end wall of the nacelle 1 is ignored here).

当然,在本实施例中,当第二罩壳20和第三罩壳30彼此接合时,可以按照上述方式在第三罩壳30与第二罩壳20接合的第三法兰31处连续地设置凸边111或者间隔地设置两个或两个以上的凸边111,对应地在第二罩壳20与第三罩壳30接合的第二法兰21上设置能够接收第三法兰31上的凸边111的凹槽211,以使彼此配合的凸边111和凹槽211沿第二罩壳20和第三罩壳30的接合部位处大致呈L形地延伸。Of course, in this embodiment, when the second casing 20 and the third casing 30 are joined to each other, the third flange 31 where the third casing 30 and the second casing 20 are joined can be continuously connected in the above-mentioned manner. Provide flanges 111 or provide two or more flanges 111 at intervals, and correspondingly provide a flange capable of receiving the third flange 31 on the second flange 21 where the second casing 20 and the third casing 30 are joined. The groove 211 of the protruding edge 111 , so that the protruding edge 111 and the groove 211 that cooperate with each other extend approximately in an L shape along the junction of the second casing 20 and the third casing 30 .

由此在第一罩壳10、第二罩壳20以及第三罩壳30彼此之间的接合部位连续或者间隔地设置凸出部和限位部,通过凸出部和限位部彼此形状配合,使得第一罩壳10、第二罩壳20以及第三罩壳30彼此之间的对接操作(也叫作合片)可以一次完成,而不需要为了将第一法兰11、第二法兰21以及第三法兰31彼此对齐而在对接过程中对各罩壳进行多次位置调整。能够有效地节省机舱罩的装配时间,从而提高整个风力发电机组的装配效率,同时还能够节省人力成本,进而降低成产成本。并且通过设置凸出部和限位部能够辅助第一法兰11、第二法兰21以及第三法兰31彼此之间进行准确地定位,进而能够提高第一法兰11上的第一通孔110、第二法兰21上的第二通孔210以及第三法兰31上的第三通孔彼此之间的对准度,以便使后续的螺栓装配流程更便利、迅速。同时,各相邻的法兰之间通过凸出部和限位部形成迷宫形结构,能够使得相邻法兰之间具有良好的密封性,进一步提升了机舱1的密封性能。In this way, protrusions and stoppers are provided continuously or at intervals at the junctions between the first case 10, the second case 20 and the third case 30, and the protrusions and the stoppers are in shape fit with each other. , so that the butt joint operation (also called joint piece) between the first casing 10, the second casing 20 and the third casing 30 can be completed at one time, without the need for the first flange 11, the second method The flange 21 and the third flange 31 are aligned with each other so that the positions of the casings are adjusted multiple times during the docking process. It can effectively save the assembly time of the nacelle cover, thereby improving the assembly efficiency of the entire wind power generating set, and can also save labor costs, thereby reducing production costs. And by setting the protruding part and the limit part, it can assist the first flange 11, the second flange 21 and the third flange 31 to be accurately positioned with each other, and then the first communication on the first flange 11 can be improved. The alignment between the hole 110, the second through hole 210 on the second flange 21 and the third through hole on the third flange 31 is to make the subsequent bolt assembly process more convenient and fast. At the same time, a labyrinth structure is formed between the adjacent flanges through the protrusions and the limiting portions, which can make the adjacent flanges have good sealing performance and further improve the sealing performance of the nacelle 1 .

在对第一罩壳10、第二罩壳20以及第三罩壳30进行连接时,示例性地,首先需要将第二罩壳20吊装至指定位置(即图2所示的左下方位置),然后将第三罩壳30吊装至与第二罩壳20对正的位置(即图2所示的右下方位置)。然后可由一名操作人员负责观察第二法兰21和第三法兰31的配合情况,使第二法兰21的凹槽211和第三法兰31的凸边111缓慢贴合。最终使第二法兰21和与第二法兰21相对应的第三法兰31彼此对正,即,能够使第二法兰21上的多个第二通孔210和第三法兰31上的多个第三通孔分别对准。When connecting the first casing 10, the second casing 20, and the third casing 30, for example, first, the second casing 20 needs to be hoisted to a designated position (ie, the lower left position shown in FIG. 2 ). , and then hoist the third casing 30 to a position aligned with the second casing 20 (that is, the lower right position shown in FIG. 2 ). Then an operator can be responsible for observing the cooperation between the second flange 21 and the third flange 31 , so that the groove 211 of the second flange 21 and the convex edge 111 of the third flange 31 can be fitted slowly. Finally, the second flange 21 and the third flange 31 corresponding to the second flange 21 are aligned with each other, that is, the plurality of second through holes 210 on the second flange 21 and the third flange 31 can be aligned with each other. A plurality of third through holes on the top are respectively aligned.

当将第二罩壳20和第三罩壳30组装完成后,即可使用吊装设备将第一罩壳10放置在第二罩壳20和第三罩壳30上,然后可由一名操作人员负责观察第一法兰11和第二法兰21或第一法兰11和第三法兰31之间的配合情况,使第一法兰11的凸边111和第二法兰21的凹槽211以及第一法兰11的凸边111和第三法兰31的凹槽211缓慢贴合,从而将第一法兰11和第二法兰21以及第一法兰11和第三法兰31彼此对正。最终使得第一法兰11上的多个第一通孔110和第二法兰21上的多个第二通孔210以及第一法兰11上的多个第一通孔110和第三法兰31上的多个第三通孔分别对准。After the second casing 20 and the third casing 30 are assembled, the first casing 10 can be placed on the second casing 20 and the third casing 30 using lifting equipment, and then an operator can be responsible for Observe the cooperation between the first flange 11 and the second flange 21 or the first flange 11 and the third flange 31, make the flange 111 of the first flange 11 and the groove 211 of the second flange 21 And the flange 111 of the first flange 11 and the groove 211 of the third flange 31 are slowly fitted together, thereby connecting the first flange 11 and the second flange 21 and the first flange 11 and the third flange 31 to each other Positive. Finally, the plurality of first through holes 110 on the first flange 11 and the plurality of second through holes 210 on the second flange 21 and the plurality of first through holes 110 on the first flange 11 and the third method A plurality of third through holes on the flange 31 are respectively aligned.

在上述实施例中凸出部为设置在第一罩壳10上的凸边111,而限位部为设置在第二罩壳20上的凹槽,但是本实用新型实施例并不限于此。图5是根据本实用新型另一个实施例的第一罩壳10和第二罩壳20的接合部位的剖面结构示意图。如图5所示,在一些实施例中,凸出部为设置在第一法兰11上的凸棱112,限位部为设置在第二法兰21上的能够与凸棱112配合的凹槽212。示例性地,凸棱112设置在远离第一法兰11与第一罩壳10的接合位置处,并且凸棱112需要尽可能远离第一通孔110和第二通孔210,以避免影响螺栓组件40的连接强度。在本实施例中,凸棱112被设置为横截面为三角形的凸棱结构,而凹槽212被设置成与凸棱112对应的横截面为三角形的凹槽结构。当然,本实施例中的由凸棱112和凹槽212组成的定位结构与上述实施例中凸边111和凹槽211组成的定位结构具有相同的优点,故不再加以赘述。In the above embodiment, the protruding part is the flange 111 provided on the first cover 10 , and the limiting part is a groove provided on the second cover 20 , but the embodiment of the present invention is not limited thereto. FIG. 5 is a schematic cross-sectional structural view of the junction of the first casing 10 and the second casing 20 according to another embodiment of the present invention. As shown in FIG. 5 , in some embodiments, the protruding portion is a rib 112 provided on the first flange 11 , and the limiting portion is a concave recess capable of cooperating with the rib 112 provided on the second flange 21 . Slot 212. Exemplarily, the rib 112 is disposed away from the joint position between the first flange 11 and the first casing 10, and the rib 112 needs to be as far away from the first through hole 110 and the second through hole 210 as possible to avoid affecting the bolts. The connection strength of the assembly 40. In this embodiment, the rib 112 is configured as a rib structure with a triangular cross section, and the groove 212 is configured as a groove structure corresponding to the rib 112 with a triangular cross section. Of course, the positioning structure composed of the convex rib 112 and the groove 212 in this embodiment has the same advantages as the positioning structure composed of the convex edge 111 and the groove 211 in the above-mentioned embodiment, so it is not repeated here.

图6是根据本实用新型再一个实施例的第一罩壳10和第二罩壳20的接合部位的剖面结构示意图。如图6所示,在一些实施例中,具体地,凸出部为设置在第一法兰11上的凸边113,限位部为设置在第二法兰21上的能够与凸边113配合的侧面213。示例性地,凸边113设置在第一法兰11的朝向机舱1内部延伸的边缘部位,以使凸边113在第一法兰11的端部形成弯折状结构。侧面213为第二法兰21朝向机舱1内部延伸的端部的侧面,并且侧面213能够与凸边113的朝向第一罩壳10一侧的侧面抵靠配合。通过在第一法兰11上设置凸边113的方式,可以免去对凸出部和限位部两个部位同时进行误差控制复杂操作过程,只需要控制凸边113的设置位置即可。因此,通过彼此形状配合的凸边113和侧面213能够辅助第一法兰11和第二法兰21进行精准定位的同时,还能够简化定位结构,即只需要在第一法兰11上设置与第二法兰21的侧面213相适应的凸出部即可。因此能够进一步降低制造成本。FIG. 6 is a schematic cross-sectional structural view of the junction of the first casing 10 and the second casing 20 according to another embodiment of the present invention. As shown in FIG. 6 , in some embodiments, specifically, the protruding part is a flange 113 provided on the first flange 11 , and the limiting part is a flange 113 provided on the second flange 21 capable of contacting with the flange 113 Mating sides 213 . Exemplarily, the protruding edge 113 is disposed on an edge portion of the first flange 11 extending toward the interior of the nacelle 1 , so that the protruding edge 113 forms a bent structure at the end of the first flange 11 . The side 213 is the side of the end of the second flange 21 extending toward the interior of the nacelle 1 , and the side 213 can abut and fit with the side of the flange 113 facing the side of the first casing 10 . By arranging the convex edge 113 on the first flange 11 , the complex operation process of simultaneously performing error control on the two parts of the convex portion and the limiting portion can be avoided, and only the position of the convex edge 113 needs to be controlled. Therefore, while the first flange 11 and the second flange 21 can be assisted in precise positioning through the mutually form-fitting flange 113 and side surface 213, the positioning structure can also be simplified, that is, only the first flange 11 needs to be provided with a The protruding portion corresponding to the side surface 213 of the second flange 21 is enough. Therefore, the manufacturing cost can be further reduced.

当然,本实用新型的以上实施例中对于凸出部和限位部的设置位置并不进行具体限限定,凸出部和限位部只要设置在相邻两个法兰的接合部位处并能够彼此形状配合以辅助两个相邻的法兰进行定位接合即可。Of course, in the above embodiments of the present utility model, there is no specific limitation on the setting positions of the protruding part and the limiting part. As long as the protruding part and the limiting part are arranged at the junction of two adjacent flanges and can It is only necessary to form fit with each other to assist two adjacent flanges to perform positioning engagement.

图7是根据本实用新型一个实施例的第一罩壳10和第二罩壳20的接合部位的立体结构示意图,图8是图7中的A部分的放大后的结构示意图。请一并参见图7和图8,在一个实施例中,为了在安装螺栓组件40时减小累积误差,机舱罩还包括定位销50。定位销50可拆卸地连接在第一法兰11和第二法兰21上,以使第一法兰11的多个第一通孔110(图中未指示出)和第二法兰21的相对应的多个第二通孔210(图中未指示出)彼此对准。FIG. 7 is a schematic perspective view of the junction of the first housing 10 and the second housing 20 according to an embodiment of the present invention, and FIG. 8 is an enlarged structural diagram of part A in FIG. 7 . Please refer to FIG. 7 and FIG. 8 together. In one embodiment, in order to reduce the cumulative error when installing the bolt assembly 40 , the nacelle cover further includes a positioning pin 50 . The positioning pin 50 is detachably connected on the first flange 11 and the second flange 21, so that the plurality of first through holes 110 (not shown in the figure) of the first flange 11 and the second flange 21 The corresponding plurality of second through holes 210 (not shown in the figure) are aligned with each other.

示例性地,在一个实施例中,定位销50包括基板51、销体52、压板53和连接件54。第一法兰11上对应销体52设置有第一销孔,第二法兰21上对应销体52设置有第二销孔。基板51为长方形的板体,圆柱形销体52固定在基板51上,并从基板51的一侧面竖立地伸出,压板53上对应销体52的尺寸设置有第三销孔。优选地,销体52的远离基板51一端设置为锥体状结构,以便使销体52能够快速准确地穿入各销孔中。由此,通过销体52穿过第三销孔,可将压板53穿设在其上,以使得压板53能够与基板51相对并在基板51和压板53之间形成夹持空间。连接件54能够将基板51和压板53连接在一起。在本实施例中,示例性地,连接件54包括两组彼此配合的螺栓和螺母。Exemplarily, in one embodiment, the positioning pin 50 includes a base plate 51 , a pin body 52 , a pressing plate 53 and a connecting piece 54 . The first flange 11 is provided with a first pin hole corresponding to the pin body 52 , and the second flange 21 is provided with a second pin hole corresponding to the pin body 52 . The base plate 51 is a rectangular plate body. The cylindrical pin body 52 is fixed on the base plate 51 and protrudes vertically from one side of the base plate 51 . The pressing plate 53 is provided with a third pin hole corresponding to the size of the pin body 52 . Preferably, the end of the pin body 52 away from the base plate 51 is configured as a cone-shaped structure, so that the pin body 52 can be inserted into each pin hole quickly and accurately. Thus, the pin body 52 passes through the third pin hole, and the pressure plate 53 can be passed thereon, so that the pressure plate 53 can be opposed to the base plate 51 and a clamping space is formed between the base plate 51 and the pressure plate 53 . The connecting piece 54 can connect the base plate 51 and the pressing plate 53 together. In this embodiment, exemplarily, the connecting member 54 includes two groups of bolts and nuts that cooperate with each other.

具体地,通过定位销50连接第一法兰11和第二法兰21时,需要将销体52依次穿过第一法兰11的第一销孔、第二法兰21的第二销孔以及压板53上的第三销孔,然后通过两个螺栓贯穿基板51、第一法兰11、第二法兰21以及压板53上对应设置的两组连接孔并与两个螺母连接配合。以将基板51和压板53紧固连接。并且销体52与法兰上的销孔之间宜采用过渡配合,以便销体52和法兰的销孔孔壁之间既不会因为缝隙过大导致销体52在销孔中晃动,也不会因为销体52的外径尺寸过大,而难以将销体52插入销孔中。由此,即可通过基板51和压板53将位于其之间的第一法兰11和第二法兰21压紧。Specifically, when connecting the first flange 11 and the second flange 21 through the positioning pin 50, the pin body 52 needs to pass through the first pin hole of the first flange 11 and the second pin hole of the second flange 21 in sequence. And the third pin hole on the pressure plate 53, and then pass through the base plate 51, the first flange 11, the second flange 21 and the two sets of connection holes correspondingly provided on the pressure plate 53 through two bolts and connect with two nuts. In order to securely connect the substrate 51 and the pressing plate 53 . And transition fit should be adopted between the pin body 52 and the pin hole on the flange, so that neither the pin body 52 will shake in the pin hole because the gap is too large between the pin body 52 and the pin hole wall of the flange, nor It is not difficult to insert the pin body 52 into the pin hole because the outer diameter of the pin body 52 is too large. Thus, the first flange 11 and the second flange 21 located therebetween can be pressed tightly by the base plate 51 and the pressing plate 53 .

在一个可选的实施例中,机舱罩可以包括两个或两个以上的定位销50,两个或两个以上的定位销50间隔地布置在第一法兰11和第二法兰21的接合部位处。优选每两个相邻的定位销50之间隔开预定距离,该预定距离由第一法兰11和第二法兰21的长度决定,以使得每一组彼此接合的第一法兰11和第二法兰21上对准的多个第一通孔110和多个第二通孔210能够被两个或两个以上的定位销50分隔成多段数量相等的通孔组,也就是说,每两个相邻的定位销50之间安装的螺栓组件40的数量相等。In an optional embodiment, the nacelle cover may include two or more positioning pins 50, and the two or more positioning pins 50 are arranged at intervals between the first flange 11 and the second flange 21. at the junction. Preferably, there is a predetermined distance between every two adjacent positioning pins 50, and the predetermined distance is determined by the lengths of the first flange 11 and the second flange 21, so that each group of the first flange 11 and the second flange 21 engaged with each other A plurality of first through holes 110 and a plurality of second through holes 210 aligned on the two flanges 21 can be divided into a plurality of equal through hole groups by two or more positioning pins 50, that is to say, each The number of bolt assemblies 40 installed between two adjacent positioning pins 50 is equal.

由此,通过设置定位销50,可以在装配螺栓组件40之前,对已经对齐的第一法兰11和第二法兰21进行定位,能够保持第一法兰11上的第一通孔110和第二法兰21上的第二通孔210的对准精度,以便提高后续的螺栓组件40的安装效率。并且通常法兰的材质为玻璃钢,所以容易在彼此的接合部位处出现变形、翘曲等问题。而由于定位销50的基板51与法兰的接触面积要比螺栓大得多,因此定位销50能够在螺栓组件40的拧紧过程中有效矫正法兰的变形,避免法兰变形后造成第一通孔110和第二通孔210之间无法对准或者第一法兰11和第二法兰21不能完全贴合,而给后续的螺栓组件40的安装操作造成影响。且在机舱罩整体运输时通过只装配两个或两个以上的定位销50,既能预防运输过程中的机舱罩的法兰变形,也能减少临时螺栓的使用,因此简化了操作步骤并避免了资源的浪费。Thus, by setting the positioning pin 50, the aligned first flange 11 and second flange 21 can be positioned before the bolt assembly 40 is assembled, and the first through hole 110 and the first through hole 110 on the first flange 11 can be maintained. The alignment accuracy of the second through hole 210 on the second flange 21 is so as to improve the installation efficiency of the subsequent bolt assembly 40 . And usually the material of the flange is fiberglass, so problems such as deformation and warpage are prone to occur at the joints of each other. And because the contact area between the base plate 51 of the locating pin 50 and the flange is much larger than that of the bolt, the locating pin 50 can effectively correct the deformation of the flange during the tightening process of the bolt assembly 40, avoiding the deformation of the flange and causing the first pass. The misalignment between the hole 110 and the second through hole 210 or the incomplete fit between the first flange 11 and the second flange 21 will affect the subsequent installation operation of the bolt assembly 40 . And when the nacelle cover is transported as a whole, only two or more positioning pins 50 are assembled, which can prevent the deformation of the flange of the nacelle cover during transportation and reduce the use of temporary bolts, thus simplifying the operation steps and avoiding A waste of resources.

而且通过将两个或两个以上的定位销50间隔地布置在第一法兰11和第二法兰21的接合部位处,使得每两个相邻的定位销50之间安装的螺栓组件40数量相等,能够将以往对整个法兰上连接的多组螺栓组件40整体安装步骤改为:将多个螺栓组件40进行分段安装的步骤(即每两个相邻的定位销50之间视为一段螺栓组件40)。因此,在安装螺栓组件40的过程中,能够避免在将多个螺栓组件40安装至第一通孔110和第二通孔210中时出现累积误差(即当螺栓组件40安装到最末端的法兰接合部位时,第一法兰11上的第一通孔110和第二法兰21上的第二通孔210彼此之间可能会出现错位情况),使末端的法兰接合部位处存在较大的内应力,进而存在较大安全隐患的问题。And by arranging two or more positioning pins 50 at intervals at the junction of the first flange 11 and the second flange 21, the bolt assembly 40 installed between every two adjacent positioning pins 50 The number is equal, and the overall installation steps of the multiple sets of bolt assemblies 40 connected on the entire flange can be changed to: the step of installing multiple bolt assemblies 40 in sections (that is, between every two adjacent positioning pins 50, as seen It is a bolt assembly 40). Therefore, in the process of installing the bolt assembly 40, it is possible to avoid accumulative errors when installing a plurality of bolt assemblies 40 into the first through hole 110 and the second through hole 210 (that is, when the bolt assembly 40 is installed to the endmost When the flange joint position is used, the first through hole 110 on the first flange 11 and the second through hole 210 on the second flange 21 may be misaligned with each other), so that there is a relatively large gap at the flange joint position at the end. Large internal stress, and then there is a problem of greater safety hazards.

示例性地,如图2所示,在本实施例中,沿第一法兰11和第二法兰21的接合部位设置有三个定位销50,通过三个定位销50将多个第一通孔110和第二通孔210划分成四组,也就是说安装在第一法兰11和第二法兰21上的所有螺栓组件40需要分为四段进行顺序安装。其他的法兰接合部位处的定位销50的数量设置可以根据法兰接合部位的长度确定,只要能够减小螺栓组件40安装的累积误差即可。Exemplarily, as shown in FIG. 2 , in this embodiment, three positioning pins 50 are provided along the junction of the first flange 11 and the second flange 21 , through which a plurality of first communication pins 50 are arranged. The holes 110 and the second through holes 210 are divided into four groups, that is to say, all the bolt assemblies 40 installed on the first flange 11 and the second flange 21 need to be divided into four sections for sequential installation. The number of positioning pins 50 at other flange joints can be determined according to the length of the flange joints, as long as the cumulative error in the installation of the bolt assembly 40 can be reduced.

在上述实施例中,定位销50包括一个销体52,但是本实用新型实施例并不限于此,在其他的实施例中,还可以在基板51上设置更多个销体52。当然,此时的多个销体52之间的距离需要按照法兰上的销孔之间的距离设置,对应地,需要在压板53上开设多个与销体52对应的第三销孔。此外,销孔和销体52还可以对应地设置成其他形状,例如还可以将销体52设置成方形销、菱形销等,对应的销孔可以为方形孔或者菱形孔等。其他法兰接合部位的定位销50的安装方式与第一法兰11和第二法兰21处的定位销50的安装方式相同,故不再加以赘述。In the above embodiments, the positioning pin 50 includes one pin body 52 , but the embodiment of the present utility model is not limited thereto, and in other embodiments, more pin bodies 52 may be provided on the base plate 51 . Certainly, the distance between the multiple pin bodies 52 at this time needs to be set according to the distance between the pin holes on the flange. Correspondingly, a plurality of third pin holes corresponding to the pin bodies 52 need to be opened on the pressure plate 53 . In addition, the pin hole and the pin body 52 can also be set in other shapes correspondingly, for example, the pin body 52 can also be set as a square pin, a rhombus pin, etc., and the corresponding pin hole can be a square hole or a rhombus hole, etc. The installation methods of the positioning pins 50 at other flange joints are the same as the installation methods of the positioning pins 50 at the first flange 11 and the second flange 21 , so details are not repeated here.

根据本实用新型的一个实施例,还提供了一种风力发电机组(图中未示出),风力发电机组包括上述任一实施例的风力发电机组的机舱罩。因此风力发电机组具有与机舱罩相同的优点,故不再加以赘述。According to an embodiment of the present invention, a wind power generating set (not shown in the figure) is also provided, and the wind generating set includes the nacelle cover of the wind generating set in any one of the above embodiments. Therefore, the wind power generating set has the same advantages as the nacelle cover, so it will not be repeated here.

本实用新型可以以其他的具体形式实现,而不脱离其精神和本质特征。因此,当前的实施例在所有方面都被看作是示例性的而非限定性的,本实用新型的范围由所附权利要求而非上述描述定义,并且,落入权利要求的含义和等同物的范围内的全部改变从而都被包括在本实用新型的范围之中。并且,在不同实施例中出现的不同技术特征可以进行组合,以取得有益效果。本领域技术人员在研究附图、说明书及权利要求书的基础上,应能理解并实现所揭示的实施例的其他变化的实施例。The utility model can be realized in other specific forms without departing from its spirit and essential features. Therefore, the current embodiments are to be considered in all respects as illustrative rather than restrictive, and the scope of the present invention is defined by the appended claims rather than the above description, and falls within the meanings and equivalents of the claims All changes within the range are included in the scope of the present utility model. Moreover, different technical features in different embodiments can be combined to achieve beneficial effects. Those skilled in the art should be able to understand and implement other modified embodiments of the disclosed embodiments on the basis of studying the drawings, specification and claims.

Claims (10)

1. a kind of engine room cover of wind power generating set, including:
First case (10), first case (10) have first flange (11) and more in the first flange (11) Individual first through hole (110);
Second case (20), second case (20) have second flange (21) and more in the second flange (21) Individual second through hole (210);
It is characterized in that:
Protuberance is provided with the first flange (11), limiting section, the protuberance are provided with the second flange (21) When the first flange (11) engages with the second flange (21), form from one another coordinates with the limiting section, so that described the The multiple first through hole (110) of one flange (11) and corresponding the multiple second through hole of the second flange (21) (210) it is aligned with each other.
2. the engine room cover of wind power generating set according to claim 1, it is characterised in that the protuberance is continuously provided In the first flange (11).
3. the engine room cover of wind power generating set according to claim 1, it is characterised in that the protuberance is two or two More than individual, and two or more protuberances are arranged in the first flange (11) at each interval.
4. the engine room cover of wind power generating set according to any one of claim 1 to 3, it is characterised in that the protrusion Portion is arranged on the end face of the first flange (11), and the limiting section is to be arranged on the end face of the second flange (21) Groove (211,212), and the protuberance can be contained in the groove (211,212).
5. the engine room cover of wind power generating set according to claim 4, it is characterised in that the protuberance is close to described One flange (11) and the junction of first case (10), and the outer surface of the protuberance and first case (10) flush with outer surface.
6. the engine room cover of wind power generating set according to any one of claim 1 to 3, it is characterised in that the protrusion Portion is arranged on the edge of the first flange (11), and the limiting section is the side (213) of the second flange (21), and And the side (213) can be resisted against on the corresponding position of the protuberance.
7. the engine room cover of wind power generating set according to claim 1, it is characterised in that also including alignment pin (50), institute State alignment pin (50) to be detachably connected in the first flange (11) and the second flange (21), so that first method The blue the multiple first through hole (110) of (11) and corresponding the multiple second through hole of the second flange (21) (210) it is aligned with each other.
8. the engine room cover of wind power generating set according to claim 7, it is characterised in that the alignment pin (50) is two Or two or more, and between adjacent two alignment pin (50) in two or more alignment pins (50) It is spaced a predetermined distance from.
9. the engine room cover of wind power generating set according to claim 8, it is characterised in that the alignment pin (50) includes pin Body (52), the substrate (51) being fixedly connected with the shank (52), the pressing plate (53) and connector (54) with the 3rd pin-and-hole, The shank (52) penetrates the first pin-and-hole of the first flange (11) setting, corresponding second of the second flange (21) The 3rd pin-and-hole of pin-and-hole and the pressing plate (53), and by the connector (54) by the substrate (51) with it is described Pressing plate (53) links together, so that the substrate (51) and the pressing plate (53) compress the first flange (11) and described the Two flanges (21).
10. a kind of wind power generating set, it is characterised in that including wind-driven generator as claimed in any one of claims 1-9 wherein The engine room cover of group.
CN201720383835.9U 2017-04-12 2017-04-12 The engine room cover and wind power generating set of wind power generating set Active CN206753830U (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108979978A (en) * 2018-07-24 2018-12-11 江苏华纳环保科技有限公司 A kind of wind turbine cabin cover
CN109681395A (en) * 2018-12-28 2019-04-26 重庆海装风电工程技术有限公司 A kind of engine room cover of wind-power electricity generation
CN111456917A (en) * 2020-04-08 2020-07-28 江苏常友环保科技股份有限公司 Novel wind driven generator anti-seepage engine room cover and assembly process thereof
CN111699315A (en) * 2018-02-02 2020-09-22 乌本产权有限公司 Nacelle of a wind power plant, wind power plant having a nacelle and method for servicing such a wind power plant

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111699315A (en) * 2018-02-02 2020-09-22 乌本产权有限公司 Nacelle of a wind power plant, wind power plant having a nacelle and method for servicing such a wind power plant
CN111699315B (en) * 2018-02-02 2023-10-03 乌本产权有限公司 Nacelle for a wind energy installation, wind energy installation comprising a nacelle and method for maintaining such a wind energy installation
US11795921B2 (en) 2018-02-02 2023-10-24 Wobben Properties Gmbh Nacelle of a wind turbine, as well as a wind turbine having a nacelle and method for the maintenance of a wind turbine of this type
CN108979978A (en) * 2018-07-24 2018-12-11 江苏华纳环保科技有限公司 A kind of wind turbine cabin cover
CN109681395A (en) * 2018-12-28 2019-04-26 重庆海装风电工程技术有限公司 A kind of engine room cover of wind-power electricity generation
CN111456917A (en) * 2020-04-08 2020-07-28 江苏常友环保科技股份有限公司 Novel wind driven generator anti-seepage engine room cover and assembly process thereof
CN111456917B (en) * 2020-04-08 2021-03-30 江苏常友环保科技股份有限公司 Novel wind driven generator anti-seepage engine room cover and assembly process thereof

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