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CN111878571A - Planet carrier connecting structure - Google Patents

Planet carrier connecting structure Download PDF

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Publication number
CN111878571A
CN111878571A CN202010848985.9A CN202010848985A CN111878571A CN 111878571 A CN111878571 A CN 111878571A CN 202010848985 A CN202010848985 A CN 202010848985A CN 111878571 A CN111878571 A CN 111878571A
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Prior art keywords
main shaft
planet carrier
hole
connection structure
disk
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CN111878571B (en
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熊永强
范世荣
张迅
周兴军
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Nanjing High Speed Gear Manufacturing Co Ltd
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Nanjing High Speed Gear Manufacturing Co Ltd
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H57/00General details of gearing
    • F16H57/08General details of gearing of gearings with members having orbital motion
    • F16H57/082Planet carriers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H57/00General details of gearing
    • F16H57/02Gearboxes; Mounting gearing therein
    • F16H57/023Mounting or installation of gears or shafts in the gearboxes, e.g. methods or means for assembly

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
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Abstract

本发明涉及行星齿轮技术领域,公开了一种行星架连接结构,用于将行星架和主轴进行连接,包括:连接部,连接部设置于行星架上,主轴上开设有连接孔,主轴通过连接孔套设于连接部上,主轴的弹性模量设置为小于连接部的弹性模量;抵持件,连接部上开设有抵持孔,抵持件置于抵持孔内且抵持于抵持孔的内壁上,使得连接部被夹于主轴和抵持件之间;锁紧盘,锁紧盘套设于主轴上,并将主轴向连接部挤压。通过上述结构,该行星架连接结构能够提高主轴与行星架之间的接触压力,从而提高主轴与行星架之间的传扭能力。

Figure 202010848985

The invention relates to the technical field of planetary gears, and discloses a planetary carrier connection structure for connecting the planetary carrier and the main shaft. The hole is sleeved on the connecting part, and the elastic modulus of the main shaft is set to be smaller than the elastic modulus of the connecting part; the abutting piece, the connecting part is provided with a resisting hole, and the resisting piece is placed in the resisting hole and abuts against the resisting part. On the inner wall of the holding hole, the connecting part is clamped between the main shaft and the abutting part; the locking disc is sleeved on the main shaft and presses the main shaft toward the connecting part. Through the above structure, the planet carrier connection structure can increase the contact pressure between the main shaft and the planet carrier, thereby improving the torque transmission capacity between the main shaft and the planet carrier.

Figure 202010848985

Description

一种行星架连接结构A planet carrier connection structure

技术领域technical field

本发明涉及行星齿轮技术领域,尤其涉及一种行星架连接结构。The invention relates to the technical field of planetary gears, in particular to a planet carrier connection structure.

背景技术Background technique

在行星齿轮箱中,为了将主轴传递过来的扭矩传递到行星架上,风电齿轮箱的行星架与主轴一般通过锁紧盘来进行连接。In the planetary gearbox, in order to transmit the torque transmitted from the main shaft to the planet carrier, the planet carrier of the wind turbine gearbox and the main shaft are generally connected by a lock plate.

通常,如图1所示,锁紧盘1’的位置位于行星架的连接部2’的外侧,主轴3’位于行星架的连接部2’的内侧,即锁紧盘1’将行星架的连接部2’收紧按压于主轴3’上。锁紧盘1’产生的压力会通过行星架的连接部2’传递到主轴3’与行星架的连接部2’的接触面上,实现主轴3’与行星架的连接部2’的连接,从而实现将主轴3’扭矩传递到行星架的目的。Usually, as shown in FIG. 1 , the position of the locking disk 1 ′ is located outside the connecting portion 2 ′ of the planet carrier, and the main shaft 3 ′ is located inside the connecting portion 2 ′ of the planet carrier, that is, the locking disk 1 ′ connects the planet carrier’s connecting portion 2 ′. The connecting portion 2' is tightened and pressed on the main shaft 3'. The pressure generated by the locking disc 1' will be transmitted to the contact surface of the main shaft 3' and the connection part 2' of the planet carrier through the connection part 2' of the planet carrier, so as to realize the connection between the main shaft 3' and the connection part 2' of the planet carrier, Thereby, the purpose of transmitting the torque of the main shaft 3' to the planet carrier is achieved.

目前,行星架常用的材料为QT700,主轴3’常用的材料为钢或者QT400。由于QT700的弹性模量高于QT400,因此在锁紧盘1’压力的作用下,行星架的连接部2’不易发生径向变形(因为行星架的刚度较大),而主轴3’容易发生径向变形(因为主轴3’的刚度较小),这样会使得最终传递到主轴3’和行星架的连接部2’的接触面上的压力较小,使得主轴3’与行星架的连接部2’之间的传扭能力较差。At present, the commonly used material of the planet carrier is QT700, and the commonly used material of the main shaft 3' is steel or QT400. Since the elastic modulus of QT700 is higher than that of QT400, under the action of the pressure of the locking disc 1', the connecting part 2' of the planet carrier is not prone to radial deformation (because the stiffness of the planet carrier is large), while the main shaft 3' is prone to Radial deformation (because the rigidity of the main shaft 3' is small), so that the final pressure transmitted to the contact surface of the main shaft 3' and the connecting part 2' of the planet carrier is small, so that the connecting part of the main shaft 3' and the planet carrier is smaller The torque transfer ability between 2' is poor.

发明内容SUMMARY OF THE INVENTION

本发明的目的在于提供一种行星架连接结构,该行星架连接结构能够提高主轴与行星架之间的接触压力,从而提高主轴与行星架之间的传扭能力。The purpose of the present invention is to provide a planet carrier connection structure, which can increase the contact pressure between the main shaft and the planet carrier, thereby improving the torque transmission capacity between the main shaft and the planet carrier.

为达此目的,本发明采用以下技术方案:For this purpose, the present invention adopts the following technical solutions:

一种行星架连接结构,其用于将行星架和主轴进行连接,包括:连接部,所述连接部设置于所述行星架上,所述主轴上开设有连接孔,所述主轴通过所述连接孔套设于所述连接部上,所述主轴的弹性模量小于所述连接部的弹性模量;抵持件,所述连接部上开设有抵持孔,所述抵持件置于所述抵持孔内且抵持于所述抵持孔的内壁上,使得所述连接部被夹于所述主轴和所述抵持件之间;锁紧盘,所述锁紧盘套设于所述主轴上,并将所述主轴向所述连接部挤压。A planet carrier connection structure, which is used for connecting a planet carrier and a main shaft, comprising: a connecting part, the connecting part is arranged on the planet carrier, a connecting hole is opened on the main shaft, and the main shaft passes through the The connecting hole is sleeved on the connecting part, and the elastic modulus of the main shaft is smaller than the elastic modulus of the connecting part; the abutting piece is provided with a resisting hole on the connecting part, and the resisting piece is placed on the connecting part. the abutting hole is in and abutted on the inner wall of the abutting hole, so that the connecting part is clamped between the main shaft and the abutting piece; a locking plate, the locking plate is sleeved on the main shaft, and press the main shaft to the connecting part.

作为一种行星架连接结构的优选方案,所述主轴与所述连接部套接的部分开设有多个轴向槽,多个所述轴向槽沿所述主轴的周向等间隔均匀分布。As a preferred solution of the planet carrier connection structure, the part where the main shaft is sleeved with the connecting part is provided with a plurality of axial grooves, and the plurality of axial grooves are evenly distributed at equal intervals along the circumference of the main shaft.

作为一种行星架连接结构的优选方案,所述连接部的外周壁面上开设有台阶,所述连接孔套设于所述台阶的小径段上。As a preferred solution of the planet carrier connecting structure, a step is formed on the outer peripheral wall of the connecting portion, and the connecting hole is sleeved on the small diameter section of the step.

作为一种行星架连接结构的优选方案,所述抵持件位于所述台阶的小径段处,并与所述主轴和所述连接部的套接部分正对。As a preferred solution of the planet carrier connection structure, the abutting member is located at the small diameter section of the step, and is directly opposite to the main shaft and the socket portion of the connection portion.

作为一种行星架连接结构的优选方案,所述抵持件的轴向长度与所述主轴和所述连接部的套接部分的长度相等。As a preferred solution of the planet carrier connection structure, the axial length of the abutting member is equal to the length of the main shaft and the socket portion of the connection portion.

作为一种行星架连接结构的优选方案,所述抵持件设置为圆柱形,所述抵持件的外周壁面抵持于所述抵持孔的内壁上。As a preferred solution of the planet carrier connection structure, the resisting member is provided in a cylindrical shape, and the outer peripheral wall surface of the resisting member abuts on the inner wall of the resisting hole.

作为一种行星架连接结构的优选方案,所述抵持件上设有减重孔,所述减重孔的中心轴线设置为与所述连接部的中心轴线重合。As a preferred solution of the planet carrier connection structure, the abutting member is provided with a weight reduction hole, and the central axis of the weight reduction hole is set to coincide with the central axis of the connecting portion.

作为一种行星架连接结构的优选方案,所述锁紧盘包括外盘和内盘,所述内盘轴向滑动设置于所述外盘的内圈面上,所述内盘的截面形状为楔形,当所述内盘插入所述外盘和所述主轴之间时,所述锁紧盘能够对所述主轴进行挤压锁紧。作为一种行星架连接结构的优选方案,所述外盘的内圈面设置为斜面,并与所述内盘的楔形面平行。As a preferred solution of the planet carrier connection structure, the locking disk includes an outer disk and an inner disk, the inner disk is axially slidably arranged on the inner ring surface of the outer disk, and the cross-sectional shape of the inner disk is wedge-shaped. When the inner disk is inserted between the outer disk and the main shaft, the locking disk can squeeze and lock the main shaft. As a preferred solution of the planet carrier connection structure, the inner ring surface of the outer disk is set as an inclined surface and is parallel to the wedge-shaped surface of the inner disk.

作为一种行星架连接结构的优选方案,所述内盘上设有连接台,所述连接台通过螺栓轴向连接于所述外盘的端面。As a preferred solution of the planet carrier connection structure, the inner disk is provided with a connection table, and the connection table is axially connected to the end face of the outer disk through bolts.

本发明的有益效果:Beneficial effects of the present invention:

本发明提供了一种行星架连接结构,其用于将行星架与主轴进行连接,该行星架连接结构包括连接部、抵持件和锁紧盘,连接部设置于行星架上,主轴上开设有连接孔,主轴通过连接孔套设于连接部上,主轴的弹性模量设置为小于连接部的弹性模量,连接部上开设有抵持孔,抵持件置于抵持孔内且抵持于抵持孔的内壁上,使得连接部夹于主轴和抵持件之间,锁紧盘套设于主轴上并将主轴向连接部方向锁紧并挤压,使得主轴紧压于连接部上,从而实现主轴与行星架之间的传扭。在上述结构中,由于主轴的弹性模量小于行星架的连接部的弹性模量,主轴受到锁紧盘挤压时,会变形而按压行星架的连接部,增加了主轴与行星架的连接部之间的接触压力,从而提高了主轴与行星架之间的传扭能力。The invention provides a planet carrier connection structure, which is used to connect the planet carrier with the main shaft. The planet carrier connection structure includes a connection part, a resisting member and a locking disc. The connection part is arranged on the planet carrier, and the main shaft is opened There is a connecting hole, the main shaft is sleeved on the connecting part through the connecting hole, the elastic modulus of the main shaft is set to be smaller than the elastic modulus of the connecting part, the connecting part is provided with a resisting hole, and the resisting piece is placed in the resisting hole and abutting It is held on the inner wall of the abutting hole, so that the connecting part is clamped between the main shaft and the abutting part, and the locking disc is sleeved on the main shaft and the main shaft is locked and squeezed towards the connecting part, so that the main shaft is tightly pressed against the connection part. on the upper part, so as to realize the torque transmission between the main shaft and the planet carrier. In the above structure, since the elastic modulus of the main shaft is smaller than the elastic modulus of the connecting part of the planet carrier, when the main shaft is squeezed by the lock plate, it will deform and press the connecting part of the planet carrier, and the connecting part between the main shaft and the planet carrier is increased. The contact pressure between the main shaft and the planet carrier improves the torque transmission capacity between the main shaft and the planet carrier.

附图说明Description of drawings

图1是现有技术中的行星架连接结构的示意图;Fig. 1 is the schematic diagram of the planet carrier connection structure in the prior art;

图2是本发明具体实施方式所述的行星架连接结构的示意图;2 is a schematic diagram of a planet carrier connection structure according to a specific embodiment of the present invention;

图3是本发明具体实施方式所述的行星架连接结构中的主轴的示意图。FIG. 3 is a schematic diagram of the main shaft in the planet carrier connection structure according to the specific embodiment of the present invention.

图1中:In Figure 1:

1’、锁紧盘;2’、连接部;3’、主轴。1', the locking disc; 2', the connecting part; 3', the main shaft.

图2-图3中:In Figure 2-Figure 3:

1、连接部;12、抵持孔;14、台阶;2、抵持件;21、减重孔;3、锁紧盘;31、外盘;32、内盘;100、主轴;101、连接孔;102、轴向槽。1. Connecting part; 12. Resisting hole; 14. Step; 2. Resisting piece; 21. Weight reduction hole; 3. Locking disc; 31. Outer disc; 32. Inner disc; 100. Spindle; 101. Connecting hole; 102. Axial groove.

具体实施方式Detailed ways

为使本发明解决的技术问题、采用的技术方案和达到的技术效果更加清楚,下面将结合附图对本发明实施例的技术方案做进一步的详细描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。In order to make the technical problems solved by the present invention, the technical solutions adopted and the technical effects achieved more clearly, the technical solutions of the embodiments of the present invention will be described in further detail below with reference to the accompanying drawings. Obviously, the described embodiments are only the present invention. Some examples, but not all examples. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative efforts shall fall within the protection scope of the present invention.

在本发明的描述中,除非另有明确的规定和限定,术语“相连”、“连接”、“固定”应做广义理解,例如,可以是固定连接,也可以是可拆卸连接,或成一体;可以是机械连接,也可以是电连接;可以是直接相连,也可以通过中间媒介间接相连,可以是两个元件内部的连通或两个元件的相互作用关系。对于本领域的普通技术人员而言,可以具体情况理解上述术语在本发明中的具体含义。In the description of the present invention, unless otherwise expressly specified and limited, the terms "connected", "connected" and "fixed" should be understood in a broad sense, for example, it may be a fixed connection, a detachable connection, or an integrated ; It can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium, and it can be the internal connection of two elements or the interaction relationship between the two elements. For those of ordinary skill in the art, the specific meanings of the above terms in the present invention can be understood in specific situations.

在本发明中,除非另有明确的规定和限定,第一特征在第二特征之“上”或之“下”可以包括第一和第二特征直接接触,也可以包括第一和第二特征不是直接接触而是通过它们之间的另外的特征接触。而且,第一特征在第二特征“之上”、“上方”和“上面”包括第一特征在第二特征正上方和斜上方,或仅仅表示第一特征水平高度高于第二特征。第一特征在第二特征“之下”、“下方”和“下面”包括第一特征在第二特征正下方和斜下方,或仅仅表示第一特征水平高度小于第二特征。In the present invention, unless otherwise expressly specified and limited, a first feature "on" or "under" a second feature may include the first and second features in direct contact, or may include the first and second features Not directly but through additional features between them. Also, the first feature being "above", "over" and "above" the second feature includes the first feature being directly above and obliquely above the second feature, or simply means that the first feature is level higher than the second feature. The first feature is "below", "below" and "below" the second feature includes the first feature being directly below and diagonally below the second feature, or simply means that the first feature has a lower level than the second feature.

下面结合附图并通过具体实施例来对本发明所提供的行星架连接结构的技术方案进行说明。The technical solution of the planet carrier connection structure provided by the present invention will be described below with reference to the accompanying drawings and through specific embodiments.

本实施例提供一种行星架连接结构,其用于将行星架和主轴100进行连接,如图2所示,该行星架连接结构包括设置于行星架上的连接部1和锁紧盘3,主轴100上开设有连接孔101,主轴100通过连接孔101套设于连接部1上,主轴100的弹性模量小于连接部1的弹性模量,锁紧盘3套设于主轴100上,并将主轴100向连接部1方向锁紧并挤压,使得主轴100紧压于连接部1上,从而实现主轴100与行星架之间的传扭。通过上述结构中,由于主轴100的弹性模量小于行星架的连接部1的弹性模量,主轴100受到锁紧盘3挤压时,会变形而按压行星架的连接部1,有利于增大主轴100与行星架的连接部1之间的接触压力,能够提高主轴100与行星架之间的传扭能力。This embodiment provides a planet carrier connection structure, which is used to connect the planet carrier and the main shaft 100. As shown in FIG. 2, the planet carrier connection structure includes a connection part 1 and a locking disk 3 arranged on the planet carrier, The main shaft 100 is provided with a connection hole 101, the main shaft 100 is sleeved on the connection part 1 through the connection hole 101, the elastic modulus of the main shaft 100 is smaller than the elastic modulus of the connection part 1, and the locking disk 3 is sleeved on the main shaft 100, and The main shaft 100 is locked and squeezed toward the connection part 1, so that the main shaft 100 is pressed against the connection part 1, so as to realize the torque transmission between the main shaft 100 and the planet carrier. With the above structure, since the elastic modulus of the main shaft 100 is smaller than the elastic modulus of the connecting portion 1 of the planet carrier, when the main shaft 100 is pressed by the locking plate 3, it will deform and press the connecting portion 1 of the planet carrier, which is beneficial to increase the The contact pressure between the main shaft 100 and the connecting portion 1 of the planet carrier can improve the torque transmission capability between the main shaft 100 and the planet carrier.

如图3所示,优选地,主轴100与连接部1套接的部分开设有轴向槽102,轴向槽102用于降低主轴100径向的刚度,使得主轴100受到锁紧盘3挤压时容易产生径向变形而挤压连接部1,从而增大主轴100与连接部1之间的接触压力,有利于提高主轴100与行星架之间的传扭能力。更为优选地,轴向槽102设置有多个,多个轴向槽102沿主轴100的周向等间隔均匀分布,使得主轴100与连接部1套接的部分的刚度能够均匀降低,使得主轴100与连接部1之间的接触压力沿主轴100的周向分布均匀。As shown in FIG. 3 , preferably, the part where the main shaft 100 is sleeved with the connecting part 1 is provided with an axial groove 102 . It is easy to produce radial deformation and squeeze the connecting part 1, thereby increasing the contact pressure between the main shaft 100 and the connecting part 1, which is beneficial to improve the torque transmission capacity between the main shaft 100 and the planet carrier. More preferably, a plurality of axial grooves 102 are provided, and the plurality of axial grooves 102 are evenly distributed at equal intervals along the circumferential direction of the main shaft 100, so that the rigidity of the part where the main shaft 100 is sleeved with the connecting portion 1 can be uniformly reduced, so that the main shaft 100 can be uniformly reduced. The contact pressure between 100 and the connecting portion 1 is uniformly distributed along the circumferential direction of the main shaft 100 .

在本实施例中,连接部1的外周壁面上开设有台阶14,连接孔101套设于台阶14的小径段上,主轴100在连接部1上进行连接时,主轴100能够通过其端部抵接于台阶面上进行定位,有助于主轴100与连接部1的连接和定位。In this embodiment, a step 14 is formed on the outer peripheral wall of the connecting portion 1 , and the connecting hole 101 is sleeved on the small diameter section of the step 14 . When the main shaft 100 is connected to the connecting portion 1 , the main shaft 100 can touch the Positioning on the stepped surface is helpful for the connection and positioning of the main shaft 100 and the connecting portion 1 .

优选地,连接部1为QT700件,即连接部1采用QT700制成,使得行星架的弹性模量较高,刚度较大,受到外界作用力时不易发生变形。主轴100为QT400件,即主轴100采用QT400制成,使得主轴100的弹性模量较小,刚度较小,受到外界作用力时容易发生变形。主轴100套设于连接部1上时,在锁紧盘3的锁紧作用下,主轴100被锁紧盘3向连接部1方向压紧而发生变形,使得主轴100紧压于连接部1上,有利于提高主轴100与连接部1之间的接触压力,从而提高该行星架连接结构的传扭能力。Preferably, the connecting portion 1 is made of QT700, that is, the connecting portion 1 is made of QT700, so that the planet carrier has a high elastic modulus and high rigidity, and is not easily deformed when subjected to external forces. The main shaft 100 is made of QT400, that is, the main shaft 100 is made of QT400, so that the main shaft 100 has a small elastic modulus and low rigidity, and is easily deformed when subjected to external forces. When the main shaft 100 is sleeved on the connecting part 1 , under the locking action of the locking plate 3 , the main shaft 100 is pressed by the locking plate 3 towards the connecting part 1 and deformed, so that the main shaft 100 is tightly pressed on the connecting part 1 . , which is beneficial to increase the contact pressure between the main shaft 100 and the connecting portion 1 , thereby improving the torque transmission capability of the planet carrier connection structure.

在本实施例中,该行星架连接结构还包括抵持件2,连接部1上开设有抵持孔12,抵持件2置于抵持孔12内且抵持于抵持孔12的内壁上,使得连接部1被夹于主轴100和抵持件2之间,抵持件2用于支撑连接部1的抵持孔12,进一步提高连接部1的刚度使其不易变形,从而保证主轴100与连接部1之间的接触压力。In this embodiment, the planet carrier connecting structure further includes a resisting member 2 , a resisting hole 12 is formed on the connecting portion 1 , and the resisting member 2 is placed in the resisting hole 12 and resists the inner wall of the resisting hole 12 , so that the connecting part 1 is clamped between the main shaft 100 and the abutting member 2, and the abutting member 2 is used to support the abutting hole 12 of the connecting part 1, which further improves the rigidity of the connecting part 1 so that it is not easily deformed, thereby ensuring the main shaft. 100 and the contact pressure between the connecting part 1.

优选地,抵持件2位于台阶14的小径段处,并与主轴100和连接部1的套接部分正对,抵持件2与主轴100和连接部1的套接部分正对,使得主轴100和连接部1的套接部分被锁紧盘3和抵持件2夹紧,进一步保证主轴100与连接部1之间的接触压力。更为优选地,抵持件2的轴向长度与主轴100和连接部1的套接部分的长度相等,使得抵持件2能够对主轴100和连接部1的全部套接部分起到支撑作用,有利于保证主轴100与连接部1之间接触压力的平稳,提高主轴100和行星架之间传扭的稳定性。Preferably, the abutting member 2 is located at the small diameter section of the step 14 and is directly opposite the main shaft 100 and the socket part of the connecting part 1, and the abutting member 2 is directly opposite to the main shaft 100 and the socket part of the connecting part 1, so that the main shaft 100 and the socket part of the connecting part 1 are directly opposite 100 and the socket part of the connecting part 1 are clamped by the locking plate 3 and the abutting member 2 , which further ensures the contact pressure between the main shaft 100 and the connecting part 1 . More preferably, the axial length of the abutting member 2 is equal to the length of the main shaft 100 and the sleeved portion of the connecting portion 1 , so that the abutting member 2 can support all the sleeved portions of the main shaft 100 and the connecting portion 1 . , which is beneficial to ensure the stability of the contact pressure between the main shaft 100 and the connecting portion 1 and improve the stability of the torque transmission between the main shaft 100 and the planet carrier.

在本实施例中,抵持件2设置为圆柱形,抵持件2的外周壁面抵持于抵持孔12的内壁上,增大了抵持件2与抵持孔12抵持面积,能够进一步保证主轴100与连接部1之间接触压力的平稳,提高主轴100和行星架之间传扭的稳定性。In this embodiment, the resisting member 2 is set in a cylindrical shape, and the outer peripheral wall surface of the resisting member 2 abuts on the inner wall of the resisting hole 12 , which increases the abutting area between the resisting member 2 and the resisting hole 12 . The stability of the contact pressure between the main shaft 100 and the connecting portion 1 is further ensured, and the stability of the torque transmission between the main shaft 100 and the planet carrier is improved.

优选地,抵持件2上开设有减重孔21,减重孔21设置为通孔,能够去除抵持件2上的部分材料,不仅有利于减轻抵持件2的重量,还能降低抵持件2的制造成本。具体地,减重孔21的中心轴线设置为与连接部1的中心轴线重合,使得抵持件2自身的质量能够以自身的中心轴线(即连接部1的中心轴线)为中心均匀分布,有利于避免产生不均匀的转动惯量而影响扭矩的传递。在其他实施例中,减重孔21还可以设置为多个,多个减重孔21以连接部1的中心轴线为中心在同一圆周面上均匀分布,使得抵持件2自身的质量能够以自身的中心轴线(即连接部1的中心轴线)为中心均匀分布,同样能避免产生不均匀的转动惯量而影响扭矩的传递。Preferably, a weight-reducing hole 21 is formed on the resisting member 2, and the weight-reducing hole 21 is set as a through hole, which can remove part of the material on the resisting member 2, which is not only conducive to reducing the weight of the resisting member 2, but also reducing the resistance Manufacturing cost of holder 2. Specifically, the central axis of the weight-reducing hole 21 is set to coincide with the central axis of the connecting portion 1, so that the mass of the abutting member 2 can be evenly distributed around its own central axis (ie, the central axis of the connecting portion 1). It is beneficial to avoid the uneven moment of inertia that affects the transmission of torque. In other embodiments, the weight reduction holes 21 may also be provided in multiple numbers, and the multiple weight reduction holes 21 are evenly distributed on the same circumferential surface with the central axis of the connecting portion 1 as the center, so that the mass of the abutting member 2 can be equal to The central axis of itself (ie the central axis of the connecting portion 1 ) is evenly distributed at the center, which can also avoid the generation of uneven rotational inertia and affect the transmission of torque.

更为优选地,抵持件2设置为钢制件,即抵持件2采用金属钢制成,使得抵持件2的支撑能力强。可以理解的是,抵持件2所用钢材的具体型号在本实施例中不做限定,本领域技术人员可以根据实际需要进行选择。More preferably, the resisting member 2 is set as a steel member, that is, the resisting member 2 is made of metal steel, so that the resisting member 2 has a strong supporting capacity. It can be understood that the specific model of the steel used for the abutting member 2 is not limited in this embodiment, and those skilled in the art can select according to actual needs.

在本实施例中,锁紧盘3包括外盘31和内盘32,外盘31和内盘32均设置为圆环状,内盘32滑动设置于外盘31的内圈面上,内盘32通过螺栓轴向连接于外盘31上,并能在螺栓的作用下沿外盘31的内圈面轴向滑动。内盘32的截面形状为楔形,内盘32在螺栓的作用下沿轴向插入外盘31的内圈时,锁紧盘3的内径会缩小,使得锁紧盘3锁紧并挤压主轴100,使主轴100发生变形而挤压连接部1,使得主轴100与连接部1之间产生接触压力而连接,最终实现主轴100与行星架之间的扭矩传递。In this embodiment, the locking disc 3 includes an outer disc 31 and an inner disc 32, the outer disc 31 and the inner disc 32 are both arranged in a ring shape, the inner disc 32 is slidably arranged on the inner ring surface of the outer disc 31, and the inner disc 32 is axially connected to the outer disc 31 through bolts. on the outer disk 31, and can slide axially along the inner ring surface of the outer disk 31 under the action of the bolt. The cross-sectional shape of the inner disk 32 is wedge-shaped. When the inner disk 32 is inserted into the inner ring of the outer disk 31 in the axial direction under the action of the bolt, the inner diameter of the locking disk 3 will be reduced, so that the locking disk 3 is locked and squeezes the main shaft 100, so that the main shaft is locked. 100 deforms and squeezes the connecting portion 1 , so that contact pressure is generated between the main shaft 100 and the connecting portion 1 for connection, and finally the torque transmission between the main shaft 100 and the planet carrier is realized.

优选地,内盘32上设有连接台321,连接台321通过螺栓轴向连接于外盘31的端面上,使得内盘32能够在连接台321和螺栓的作用下沿轴向滑动而插入外盘31的内圈使得锁紧盘3锁紧并挤压主轴100,实现锁紧功能。Preferably, the inner disk 32 is provided with a connecting table 321, and the connecting table 321 is axially connected to the end surface of the outer disk 31 through bolts, so that the inner disk 32 can slide axially under the action of the connecting table 321 and the bolts and be inserted into the inner surface of the outer disk 31. The ring locks the locking disc 3 and squeezes the main shaft 100 to realize the locking function.

更为优选地,外盘31的内圈面设置为斜面,并与内盘32的楔形面平行,有利于避免内盘32插入外盘31的内圈时,内盘32与外盘31之间出现空隙,有利于提高该锁紧盘3的锁紧强度。More preferably, the inner ring surface of the outer disk 31 is set as an inclined surface and is parallel to the wedge-shaped surface of the inner disk 32, which is beneficial to avoid a gap between the inner disk 32 and the outer disk 31 when the inner disk 32 is inserted into the inner ring of the outer disk 31, which is conducive to improving the performance of the inner disk 31. The locking strength of the locking disc 3 .

显然,本发明的上述实施例仅仅是为了清楚说明本发明所作的举例,而并非是对本发明的实施方式的限定。对于所属领域的普通技术人员来说,能够进行各种明显的变化、重新调整和替代而不会脱离本发明的保护范围。这里无需也无法对所有的实施方式予以穷举。凡在本发明的精神和原则之内所作的任何修改、等同替换和改进等,均应包含在本发明权利要求的保护范围之内。Obviously, the above-mentioned embodiments of the present invention are only examples for clearly illustrating the present invention, rather than limiting the embodiments of the present invention. For those of ordinary skill in the art, various obvious changes, readjustments and substitutions can be made without departing from the protection scope of the present invention. There is no need and cannot be exhaustive of all implementations here. Any modification, equivalent replacement and improvement made within the spirit and principle of the present invention shall be included within the protection scope of the claims of the present invention.

Claims (10)

1.一种行星架连接结构,用于将行星架和主轴(100)进行连接,其特征在于,包括:1. A planet carrier connection structure for connecting the planet carrier and the main shaft (100), characterized in that, comprising: 连接部(1),所述连接部(1)设置于所述行星架上,所述主轴(100)上开设有连接孔(101),所述主轴(100)通过所述连接孔(101)套设于所述连接部(1)上,所述主轴(100)的弹性模量小于所述连接部(1)的弹性模量;A connecting part (1), the connecting part (1) is arranged on the planet carrier, a connecting hole (101) is opened on the main shaft (100), and the main shaft (100) passes through the connecting hole (101) sleeved on the connecting portion (1), the elastic modulus of the main shaft (100) is smaller than the elastic modulus of the connecting portion (1); 抵持件(2),所述连接部(1)上开设有抵持孔(12),所述抵持件(2)置于所述抵持孔(12)内且抵持于所述抵持孔(12)的内壁上,使得所述连接部(1)被夹于所述主轴(100)和所述抵持件(2)之间;A resisting piece (2), a resisting hole (12) is formed on the connecting portion (1), and the resisting piece (2) is placed in the resisting hole (12) and resists against the resisting piece on the inner wall of the holding hole (12), so that the connecting portion (1) is clamped between the main shaft (100) and the abutting member (2); 锁紧盘(3),所述锁紧盘(3)套设于所述主轴(100)上,并将所述主轴(100)向所述连接部(1)挤压。A locking disc (3) is sleeved on the main shaft (100), and the main shaft (100) is pressed towards the connecting part (1). 2.根据权利要求1所述的行星架连接结构,其特征在于,所述主轴(100)与所述连接部(1)套接的部分开设有多个轴向槽(102),多个所述轴向槽(102)沿所述主轴(100)的周向等间隔均匀分布。2 . The planet carrier connection structure according to claim 1 , wherein a plurality of axial grooves ( 102 ) are provided in the part where the main shaft ( 100 ) is sleeved with the connecting portion ( 1 ), and a plurality of The axial grooves (102) are evenly distributed at equal intervals along the circumference of the main shaft (100). 3.根据权利要求1所述的行星架连接结构,其特征在于,所述连接部(1)的外周壁面上开设有台阶(14),所述连接孔(101)套设于所述台阶(14)的小径段上。3 . The planet carrier connection structure according to claim 1 , wherein a step ( 14 ) is formed on the outer peripheral wall of the connection portion ( 1 ), and the connection hole ( 101 ) is sleeved on the step ( 3 . 14) on the small diameter section. 4.根据权利要求3所述的行星架连接结构,其特征在于,所述抵持件(2)位于所述台阶(14)的小径段处,并与所述主轴(100)和所述连接部(1)的套接部分正对。4. The planet carrier connection structure according to claim 3, wherein the abutting member (2) is located at the small diameter section of the step (14), and is connected to the main shaft (100) and the connection The socket part of the part (1) is facing. 5.根据权利要求1所述的行星架连接结构,其特征在于,所述抵持件(2)的轴向长度与所述主轴(100)和所述连接部(1)的套接部分的长度相等。5 . The planet carrier connection structure according to claim 1 , wherein the axial length of the abutting member ( 2 ) is the same as the length of the main shaft ( 100 ) and the socket portion of the connecting portion ( 1 ). 6 . equal length. 6.根据权利要求1所述的行星架连接结构,其特征在于,所述抵持件(2)设置为圆柱形,所述抵持件(2)的外周壁面抵持于所述抵持孔(12)的内壁上。6 . The planet carrier connection structure according to claim 1 , wherein the resisting member ( 2 ) is provided in a cylindrical shape, and the outer peripheral wall surface of the resisting member ( 2 ) resists the resisting hole. 7 . (12) on the inner wall. 7.根据权利要求1所述的行星架连接结构,其特征在于,所述抵持件(2)上设有减重孔(21),所述减重孔(21)的中心轴线设置为与所述连接部(1)的中心轴线重合。7 . The planet carrier connection structure according to claim 1 , wherein a weight-reducing hole ( 21 ) is provided on the abutting member ( 2 ), and the central axis of the weight-reducing hole ( 21 ) is set to align with the The central axes of the connecting parts (1) are coincident. 8.根据权利要求1所述的行星架连接结构,其特征在于,所述锁紧盘(3)包括外盘(31)和内盘(32),所述内盘(32)轴向滑动设置于所述外盘(31)的内圈面上,所述内盘(32)的截面形状为楔形,当所述内盘(32)插入所述外盘(31)和所述主轴(100)之间时,所述锁紧盘(3)能够对所述主轴(100)进行挤压锁紧。8 . The planet carrier connection structure according to claim 1 , wherein the locking disk ( 3 ) comprises an outer disk ( 31 ) and an inner disk ( 32 ), and the inner disk ( 32 ) is axially slidably arranged on the On the inner ring surface of the outer disk (31), the cross-sectional shape of the inner disk (32) is wedge-shaped, and when the inner disk (32) is inserted between the outer disk (31) and the main shaft (100), the lock The shrink disk (3) can squeeze and lock the main shaft (100). 9.根据权利要求8所述的行星架连接结构,其特征在于,所述外盘(31)的内圈面设置为斜面,并与所述内盘(32)的楔形面平行。9 . The planet carrier connection structure according to claim 8 , wherein the inner ring surface of the outer disk ( 31 ) is set as an inclined surface and is parallel to the wedge-shaped surface of the inner disk ( 32 ). 10 . 10.根据权利要求8所述的行星架连接结构,其特征在于,所述内盘(32)上设有连接台(321),所述连接台(321)通过螺栓轴向连接于所述外盘(31)的端面。10 . The planet carrier connection structure according to claim 8 , wherein a connecting platform ( 321 ) is provided on the inner disk ( 32 ), and the connecting platform ( 321 ) is axially connected to the outer disk ( 10 . 10 . 31) of the end face.
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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4249298A (en) * 1978-03-27 1981-02-10 Hitachi, Ltd. Method for connecting two members
CN110185782A (en) * 2019-06-24 2019-08-30 南京高速齿轮制造有限公司 The planet carrier and main shaft connection structure of wind turbine gearbox
CN110821971A (en) * 2019-12-11 2020-02-21 南京高速齿轮制造有限公司 Shrink dish and gear box
CN212839334U (en) * 2020-08-21 2021-03-30 南京高速齿轮制造有限公司 Planet carrier connecting structure

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4249298A (en) * 1978-03-27 1981-02-10 Hitachi, Ltd. Method for connecting two members
CN110185782A (en) * 2019-06-24 2019-08-30 南京高速齿轮制造有限公司 The planet carrier and main shaft connection structure of wind turbine gearbox
CN110821971A (en) * 2019-12-11 2020-02-21 南京高速齿轮制造有限公司 Shrink dish and gear box
CN212839334U (en) * 2020-08-21 2021-03-30 南京高速齿轮制造有限公司 Planet carrier connecting structure

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