CN116100255A - A high-precision wind power planetary frame processing technology - Google Patents

A high-precision wind power planetary frame processing technology Download PDF

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Publication number
CN116100255A
CN116100255A CN202310049577.0A CN202310049577A CN116100255A CN 116100255 A CN116100255 A CN 116100255A CN 202310049577 A CN202310049577 A CN 202310049577A CN 116100255 A CN116100255 A CN 116100255A
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side plate
positioning mechanism
column
planet carrier
wind power
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CN116100255B (en
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陈江波
丁茂盛
徐新荣
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Anhui Yongcheng Machinery Co ltd
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Anhui Yongcheng Machinery Co ltd
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23QDETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
    • B23Q3/00Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23QDETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
    • B23Q2703/00Work clamping
    • B23Q2703/02Work clamping means
    • B23Q2703/10Devices for clamping workpieces of a particular form or made from a particular material
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Wind Motors (AREA)
  • Machine Tool Units (AREA)

Abstract

The invention discloses a high-precision wind power planet carrier processing technology, which relates to the technical field of wind power planet carrier processing, and comprises the steps of firstly placing a planet carrier into a first positioning mechanism in an upward posture of a first side plate where an outer sleeve end is positioned, and carrying out rough machining by utilizing the surfaces of a pair of outer sleeve ends of a machine tool and the top surfaces of stand columns; placing the planet carrier into a second positioning mechanism in a downward posture of the first side plate, and rough machining the bottom surface of the upright post by using a second machine tool; placing the planet carrier in a vertical posture of the first side plate into a positioning mechanism III, and performing rough machining on the inner walls of the side shaft holes and the central shaft opening by utilizing a machine tool III; according to the invention, through changing the clamping gaps and the positions of the clamps, the position and the posture of the planet carrier are adjusted more accurately at multiple angles, and when the product is subjected to repeated clamping and positioning operation, the parameters such as flatness, position degree, verticality and the like are detected in real time, and are adjusted in real time, so that the accuracy of the clamping and limiting operation is effectively improved.

Description

一种高精度风电行星架加工工艺A high-precision wind power planetary frame processing technology

技术领域technical field

本发明涉及风电行星架加工技术领域,具体是一种高精度风电行星架加工工艺。The invention relates to the technical field of wind power planetary frame processing, in particular to a high-precision wind power planetary frame processing technology.

背景技术Background technique

行星架作为风力发电机组用重要组成部分,其质量直接影响整个发电机组的使用寿命。现有的行星架多为采用铸件整体铸造的框架结构,其竖直方向收缩阻力大,收缩量不易控制;收缩时因受阻收缩产生收缩应力,易导致裂纹;在在生产成型后关键区域不允许焊补。因此在加工过程中提高行星架的尺寸精度对于提高行星架成品的质量具有重大意义。The planet carrier is an important part of the wind turbine, and its quality directly affects the service life of the entire generator. Most of the existing planetary frames are frame structures that are integrally cast by castings. The shrinkage resistance in the vertical direction is large, and the amount of shrinkage is difficult to control; shrinkage stress is generated due to hindered shrinkage during shrinkage, which easily leads to cracks; it is not allowed in key areas after production molding welding repair. Therefore, it is of great significance to improve the dimensional accuracy of the planet carrier in the process of processing to improve the quality of the finished product of the planet carrier.

发明内容Contents of the invention

本发明的目的在于提供一种高精度风电行星架加工工艺,以解决上述背景技术中提出的问题。The purpose of the present invention is to provide a high-precision wind power planetary carrier processing technology to solve the problems raised in the above-mentioned background technology.

为实现上述目的,本发明提供如下技术方案:To achieve the above object, the present invention provides the following technical solutions:

一种高精度风电行星架加工工艺,包括下列步骤,A high-precision wind power planetary frame processing technology, comprising the following steps,

步骤一:将行星架以外套端所在的第一侧板向上的姿态置入定位机构一,利用机床一对外套端的表面和立柱的顶面进行粗加工;Step 1: Put the planetary carrier into the positioning mechanism 1 with the first side plate where the jacket end is located upwards, and use the machine tool to perform rough machining on the surface of the pair of jacket ends and the top surface of the column;

步骤二:将行星架以第一侧板向下的姿态置入定位机构二,利用机床二对立柱的底面进行粗加工;Step 2: Put the planet carrier into the positioning mechanism 2 with the first side plate facing down, and use the bottom surface of the second pair of columns of the machine tool for rough machining;

步骤三:将行星架以第一侧板竖放的姿态置入定位机构三,利用机床三对侧边轴孔的内壁以及中心轴口进行粗加工;Step 3: Put the planetary carrier into the positioning mechanism 3 with the vertical position of the first side plate, and use the inner wall of the three pairs of side shaft holes and the center shaft port of the machine tool to perform rough machining;

步骤四:将行星架以第一侧板向上的姿态置入定位机构四,利用机床四对立柱侧面进行粗加工;Step 4: Put the planet carrier into the positioning mechanism 4 with the first side plate facing upwards, and use the machine tool to perform rough machining on the sides of the four pairs of columns;

步骤五:将行星架以第一侧板竖放的姿态置入定位机构五,利用机床五对侧边轴孔的内壁以及中心轴口进行精加工;Step 5: Put the planet carrier into the positioning mechanism 5 with the vertical position of the first side plate, and use the machine tool to finish the inner walls of the 5 pairs of side shaft holes and the center shaft opening;

步骤六:将行星架以第一侧板向上的姿态置入定位机构六,利用机床六对外套端的表面和立柱的顶面进行精加工;Step 6: Put the planet carrier into the positioning mechanism 6 with the attitude of the first side plate upward, and use the machine tool 6 to finish the surface of the jacket end and the top surface of the column;

步骤七:将行星架以第一侧板向下的姿态置入定位机构七,利用机床七对立柱的底面进行精加工。Step 7: Put the planet carrier into the positioning mechanism 7 with the first side plate facing down, and use the machine tool 7 to finish the bottom surface of the column.

作为本发明进一步的方案:在步骤一中,定位机构一通过若干个底定位夹对第二侧板进行夹持实现对行星架的定位,打表校平使立柱顶面跳动控制在2MM以内,第一侧板边沿外圆跳动在1MM以内。As a further solution of the present invention: in step 1, the positioning mechanism clamps the second side plate through several bottom positioning clips to realize the positioning of the planetary carrier, and the meter is leveled so that the beating of the top surface of the column is controlled within 2MM. The runout of the outer circle of the edge of the first side plate is within 1MM.

作为本发明进一步的方案:在步骤二中,定位机构二通过中心限位杆伸入外套端内对其进行限位,通过若干个承托夹具对若干个立柱进行接触实现对第一侧板的支撑,实现对行星架的限位,若干个承托夹具与第一侧板的间隙控制在0.02MM以内。As a further solution of the present invention: in step 2, the positioning mechanism 2 extends into the outer jacket end through the center limit rod to limit its position, and contacts several upright columns through several supporting fixtures to realize the positioning of the first side plate The support realizes the limit of the planet carrier, and the gap between several supporting fixtures and the first side plate is controlled within 0.02MM.

作为本发明进一步的方案:在步骤三中,定位机构三通过设置于支撑架上的若干个侧板夹具对于第一侧板和第二侧板进行分别的夹持限位,通过立柱夹具对立柱进行夹持限位,侧板夹具与行星架接触部位的间隙控制在0.02MM以内,打表侧边轴孔的中心直线度跳动在1MM以内,中心轴孔的位置度在0.3MM以内。As a further solution of the present invention: in step 3, the positioning mechanism 3 clamps and limits the first side plate and the second side plate respectively through several side plate clamps arranged on the support frame, and uses the column clamps to clamp and limit the position of the column. Clamp and limit, the gap between the side plate clamp and the contact part of the planet carrier is controlled within 0.02MM, the center straightness of the side shaft hole of the meter is run out within 1MM, and the position of the central shaft hole is within 0.3MM.

作为本发明进一步的方案:在步骤四中,定位机构三通过若干个承托板对若干个立柱支撑接触,通过若干个轴孔定位夹具对若干个侧边轴孔进行限位支撑;立柱的顶面平面度在0.05MM以内,打表侧边轴孔的中心直线度跳动在1MM以内。As a further solution of the present invention: in step 4, the positioning mechanism 3 supports and contacts several upright columns through several support plates, and performs limit support on several side shaft holes through several shaft hole positioning fixtures; the top of the upright column The flatness of the surface is within 0.05MM, and the straightness of the central straightness of the shaft hole on the side of the table is within 1MM.

作为本发明进一步的方案:步骤五中,定位机构五的定位机构四的结构一致,定位装夹时调节各立柱底面的平面度0.05MM以内,打表侧边轴孔的中心直线度跳动在0.05MM以内、圆柱度0.012MM、位置度0.08MM、同心度0.025MM、垂直度0.04MM。As a further solution of the present invention: in step 5, the structure of the positioning mechanism 4 of the positioning mechanism 5 is consistent, and the flatness of the bottom surface of each column is adjusted within 0.05MM when positioning and clamping, and the center straightness of the side shaft hole of the table is beating within 0.05mm Within MM, cylindricity 0.012MM, position degree 0.08MM, concentricity 0.025MM, verticality 0.04MM.

作为本发明进一步的方案:在步骤六中,定位机构六与定位机构一结构一致,打表校平立柱顶面跳动控制在0.05MM以内,打表第一侧板边沿的外圆跳动在0.1MM以内;外套端部位的同心度0.04MM、圆柱度0.03MM、中心直线度跳动0.04MM。As a further solution of the present invention: in step 6, the structure of the positioning mechanism 6 is consistent with that of the positioning mechanism 1, the runout of the top surface of the meter leveling column is controlled within 0.05MM, and the outer circle runout of the edge of the first side plate of the watchmaker is within 0.1MM Within; the concentricity of the jacket end is 0.04MM, the cylindricity is 0.03MM, and the center straightness beating is 0.04MM.

作为本发明进一步的方案:在步骤七中,定位机构七其通过支撑夹具对若干个立柱顶面进行支撑,实现对行星架的限位,打表各支撑夹具与立柱的间隙控制在0.02MM以内,打表第一侧板外圆跳动在0.1MM以内:立柱顶面的平面度跳动在0.04MM以内,中心轴口的圆柱度0.03MM、同心度0.04MM。As a further solution of the present invention: in step 7, the positioning mechanism 7 supports the top surfaces of several columns through the supporting fixtures to realize the limit of the planet carrier, and the gap between the supporting fixtures and the columns is controlled within 0.02MM. , The runout of the outer circle of the first side plate of the table is within 0.1MM: the flatness runout of the top surface of the column is within 0.04MM, the cylindricity of the central shaft port is 0.03MM, and the concentricity is 0.04MM.

与现有技术相比,本发明的有益效果是:本发明通过设置若干个定位机构,以不同的定位姿态对行星架件限位固定,以此适应不同机床对于行星架不同位置的加工操作需要,本申请的定位机构在进行,通过若干个不同位置的间距以多个点位,实现对行星架的支撑固定,以此提高对行星架的限位稳定性,同时通过对各个夹具夹持间隙以及位置的改变,实现对行星架的位置姿态进行更多角度更精确的调节,在产品在重复的装夹定位操作时,实时进行平面度、位置度、垂直度等参数的实时检测,并进行实时调整,有效的提高了夹持限位操作的准确性。Compared with the prior art, the beneficial effect of the present invention is that the present invention sets several positioning mechanisms to limit and fix the planetary carrier with different positioning postures, so as to adapt to the processing operation needs of different machine tools for different positions of the planetary frame , the positioning mechanism of the present application is in progress, and the support and fixation of the planet carrier is realized through the spacing of several different positions and multiple points, so as to improve the limit stability of the planet carrier. And position changes, to achieve more angles and more precise adjustments to the position and attitude of the planetary carrier. When the product is in repeated clamping and positioning operations, real-time detection of parameters such as flatness, position, and verticality are performed in real time, and carried out. Real-time adjustment effectively improves the accuracy of the clamping limit operation.

附图说明Description of drawings

图1为本发明的工艺流程图;Fig. 1 is a process flow diagram of the present invention;

图2为本发明步骤一的行星架状态示意图;Fig. 2 is a schematic diagram of the state of the planetary carrier in Step 1 of the present invention;

图3为本发明步骤二的行星架状态示意图;Fig. 3 is a schematic diagram of the state of the planet carrier in step 2 of the present invention;

图4为本发明步骤三的行星架状态示意图;Fig. 4 is a schematic diagram of the state of the planetary carrier in Step 3 of the present invention;

图5为本发明步骤四的行星架状态示意图;Fig. 5 is a schematic diagram of the state of the planetary carrier in Step 4 of the present invention;

图6为本发明步骤七的行星架状态示意图。Fig. 6 is a schematic diagram of the state of the planetary carrier in Step 7 of the present invention.

图中:1、第一侧板;2、第二侧板;3、外套端;4、立柱;401、立柱顶面;402、立柱侧面;403、立柱底面;5、侧边轴孔;6、中心轴口;7、底定位夹;8、中心限位杆;9、承托夹具;10、支撑架;11、侧板夹具;12、立柱夹具;13、承托板;14、轴孔定位夹具;15、支撑夹具。In the figure: 1, the first side plate; 2, the second side plate; 3, the outer jacket end; 4, the column; 401, the top surface of the column; 402, the side of the column; 403, the bottom surface of the column; 5, the side shaft hole; 6 , central shaft port; 7, bottom positioning clamp; 8, center limit rod; 9, support fixture; 10, support frame; 11, side plate fixture; 12, column fixture; 13, support plate; 14, shaft hole Positioning fixture; 15. Supporting fixture.

具体实施方式Detailed ways

下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,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,本领域普通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。The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

请参阅图1-图6,本发明实施例中,一种高精度风电行星架加工工艺,包括下列步骤,首先将行星架以外套端3所在的第一侧板1向上的姿态置入定位机构一,利用机床一对外套端3的表面和立柱的顶面进行粗加工;定位机构一通过若干个底定位夹7对第二侧板2进行夹持实现对行星架的定位,打表校平使立柱顶面401跳动控制在2MM以内,第一侧板1边沿外圆跳动在1MM以内;Please refer to Fig. 1-Fig. 6, in the embodiment of the present invention, a high-precision wind power planetary carrier processing process includes the following steps, firstly, the planetary carrier is placed into the positioning mechanism with the first side plate 1 where the outer casing end 3 is located upwards 1. Use the machine tool to perform rough machining on the surface of the pair of jacket ends 3 and the top surface of the column; the positioning mechanism 1 clamps the second side plate 2 through several bottom positioning clips 7 to realize the positioning of the planetary carrier, and the table is leveled Control the beating of the top surface 401 of the column within 2MM, and the beating of the outer circle of the edge of the first side plate 1 within 1MM;

而后将行星架以第一侧板1向下的姿态置入定位机构二,利用机床二对立柱的底面进行粗加工;定位机构二通过中心限位杆8伸入外套端3内对其进行限位,通过若干个承托夹具9对若干个立柱进行接触实现对第一侧板1的支撑,实现对行星架的限位,若干个承托夹具9与第一侧板1的间隙控制在0.02MM以内;再将行星架以第一侧板1竖放的姿态置入定位机构三,利用机床三对侧边轴孔5的内壁以及中心轴口6进行粗加工;定位机构三通过设置于支撑架10上的若干个侧板夹具11对于第一侧板1和第二侧板2进行分别的夹持限位,通过立柱夹具12对立柱进行夹持限位,侧板夹具11与行星架接触部位的间隙控制在0.02MM以内,打表侧边轴孔5的中心直线度跳动在1MM以内,中心轴孔的位置度在0.3MM以内;而后将行星架以第一侧板1向上的姿态置入定位机构四,利用机床四对立柱侧面402进行粗加工;定位机构三通过若干个承托板13对若干个立柱支撑接触,通过若干个轴孔定位夹具14对若干个侧边轴孔5进行限位支撑;立柱的顶面平面度在0.05MM以内,打表侧边轴孔5的中心直线度跳动在1MM以内;Then the planet carrier is inserted into the positioning mechanism two with the downward attitude of the first side plate 1, and the bottom surface of the two pairs of columns of the machine tool is used to carry out rough machining; Position, through several supporting fixtures 9 to contact several columns to realize the support of the first side plate 1, to realize the limit of the planet carrier, the gap between several supporting fixtures 9 and the first side plate 1 is controlled at 0.02 Within MM; then put the planet carrier into the positioning mechanism 3 with the vertical position of the first side plate 1, and use the machine tool 3 to perform rough machining on the inner wall of the side shaft hole 5 and the central shaft port 6; the positioning mechanism 3 is set on the support Several side plate clamps 11 on the frame 10 respectively clamp and limit the first side plate 1 and the second side plate 2, and clamp and limit the column through the column clamp 12, and the side plate clamps 11 are in contact with the planet carrier The gap between the parts is controlled within 0.02MM, the center straightness of the side shaft hole 5 is within 1MM, and the position of the central shaft hole is within 0.3MM; then the planet carrier is placed with the first side plate 1 upward Enter the positioning mechanism 4, use the four pairs of column sides 402 of the machine tool to carry out rough machining; the positioning mechanism 3 supports and contacts several columns through several support plates 13, and carries out several side shaft holes 5 through several shaft hole positioning fixtures 14. Limit support; the flatness of the top surface of the column is within 0.05MM, and the straightness of the center of the shaft hole 5 on the side of the watch is run out within 1MM;

再将行星架以第一侧板1竖放的姿态置入定位机构五,利用机床五对侧边轴孔5的内壁以及中心轴口6进行精加工;定位机构五的定位机构四的结构一致,定位装夹时调节各立柱底面403的平面度0.05MM以内,打表侧边轴孔5的中心直线度跳动在0.05MM以内、圆柱度0.012MM、位置度0.08MM、同心度0.025MM、垂直度0.04MM;将行星架以第一侧板1向上的姿态置入定位机构六,利用机床六对外套端3的表面和立柱的顶面进行精加工;定位机构六与定位机构一结构一致,打表校平立柱顶面401跳动控制在0.05MM以内,打表第一侧板1边沿的外圆跳动在0.1MM以内;外套端3部位的同心度0.04MM、圆柱度0.03MM、中心直线度跳动0.04MM;将行星架以第一侧板1向下的姿态置入定位机构七,利用机床七对立柱的底面进行精加工;定位机构七其通过支撑夹具15对若干个立柱顶面401进行支撑,实现对行星架的限位,打表各支撑夹具15与立柱的间隙控制在0.02MM以内,打表第一侧板1外圆跳动在0.1MM以内:立柱顶面401的平面度跳动在0.04MM以内,中心轴口6的圆柱度0.03MM、同心度0.04MM。Then put the planet carrier into the positioning mechanism 5 with the vertical position of the first side plate 1, and use the machine tool 5 to finish the inner wall of the side shaft hole 5 and the central shaft port 6; the structure of the positioning mechanism 4 of the positioning mechanism 5 is consistent. When positioning and clamping, adjust the flatness of the bottom surface 403 of each column within 0.05MM, the center straightness of the side shaft hole 5 on the side of the table runs within 0.05MM, the cylindricity 0.012MM, the position degree 0.08MM, the concentricity 0.025MM, the vertical The degree is 0.04MM; the planet carrier is placed into the positioning mechanism 6 with the first side plate 1 facing upwards, and the surface of the jacket end 3 and the top surface of the column are finished using the machine tool 6; the structure of the positioning mechanism 6 is consistent with that of the positioning mechanism 1. The runout of the top surface 401 of the metering and leveling column is controlled within 0.05MM, the outer circle runout of the first side plate 1 edge of the metering is within 0.1MM; the concentricity of the 3 parts of the jacket end is 0.04MM, the cylindricity is 0.03MM, and the center straightness Jump 0.04MM; put the planet carrier into the positioning mechanism 7 with the first side plate 1 facing down, and use the machine tool 7 to finish the bottom surface of the column; Support, to realize the limit of the planet carrier, control the gap between each supporting fixture 15 and the column within 0.02MM, and control the outer circle runout of the first side plate 1 within 0.1MM: the flatness runout of the column top surface 401 is within 0.02MM. Within 0.04MM, the cylindricity of the central shaft port 6 is 0.03MM, and the concentricity is 0.04MM.

以上所述,仅是本发明的较佳实施例而已,并非对本发明作任何形式上的限制,虽然本发明已以较佳实施例揭示如上,然而并非用以限定本发明,任何本领域技术人员,在不脱离本发明技术方案范围内,当可利用上述揭示的技术内容做出些许更动或修饰为等同变化的等效实施例,但凡是未脱离本发明技术方案内容,依据本发明的技术实质对以上实施例所作的任何简单修改、等同变化与修饰,均仍属于本发明技术方案的范围内。The above description is only a preferred embodiment of the present invention, and does not limit the present invention in any form. Although the present invention has been disclosed as above with preferred embodiments, it is not intended to limit the present invention. Anyone skilled in the art , without departing from the scope of the technical solution of the present invention, when the technical content disclosed above can be used to make some changes or be modified into equivalent embodiments with equivalent changes, but as long as it does not depart from the technical solution of the present invention, the technical content of the present invention In essence, any simple modifications, equivalent changes and modifications made to the above embodiments still fall within the scope of the technical solution of the present invention.

Claims (8)

1.一种高精度风电行星架加工工艺,其特征在于,包括下列步骤:1. A high-precision wind power planetary carrier processing technology is characterized in that, comprising the following steps: 步骤一:将行星架以外套端(3)所在的第一侧板(1)向上的姿态置入定位机构一,利用机床一对外套端(3)的表面和立柱的顶面进行粗加工;Step 1: Put the planetary carrier into the positioning mechanism 1 with the first side plate (1) where the outer casing end (3) is located upwards, and use the machine tool to perform rough machining on the surface of the pair of outer casing ends (3) and the top surface of the column; 步骤二:将行星架以第一侧板(1)向下的姿态置入定位机构二,利用机床二对立柱的底面进行粗加工;Step 2: Put the planet carrier into the positioning mechanism 2 with the first side plate (1) facing down, and use the bottom surface of the second pair of columns of the machine tool to perform rough machining; 步骤三:将行星架以第一侧板(1)竖放的姿态置入定位机构三,利用机床三对侧边轴孔(5)的内壁以及中心轴口(6)进行粗加工;Step 3: Put the planetary carrier into the positioning mechanism 3 with the vertical position of the first side plate (1), and use the inner walls of the three pairs of side shaft holes (5) and the center shaft port (6) of the machine tool to perform rough machining; 步骤四:将行星架以第一侧板(1)向上的姿态置入定位机构四,利用机床四对立柱侧面(402)进行粗加工;Step 4: Put the planet carrier into the positioning mechanism 4 with the first side plate (1) facing upwards, and use the four pairs of column sides (402) of the machine tool for rough machining; 步骤五:将行星架以第一侧板(1)竖放的姿态置入定位机构五,利用机床五对侧边轴孔(5)的内壁以及中心轴口(6)进行精加工;Step 5: Put the planet carrier into the positioning mechanism 5 with the first side plate (1) vertically placed, and use the inner walls of the five pairs of side shaft holes (5) and the center shaft port (6) of the machine tool to finish machining; 步骤六:将行星架以第一侧板(1)向上的姿态置入定位机构六,利用机床六对外套端(3)的表面和立柱的顶面进行精加工;Step 6: Put the planet carrier into the positioning mechanism 6 with the first side plate (1) facing upwards, and use the machine tool 6 to finish the surface of the jacket end (3) and the top surface of the column; 步骤七:将行星架以第一侧板(1)向下的姿态置入定位机构七,利用机床七对立柱的底面进行精加工。Step 7: Put the planet carrier into the positioning mechanism 7 with the first side plate (1) facing down, and use the machine tool 7 to finish the bottom surface of the column. 2.根据权利要求1所述的一种高精度风电行星架加工工艺,其特征在于,在步骤一中,定位机构一通过若干个底定位夹(7)对第二侧板(2)进行夹持实现对行星架的定位,打表校平使立柱顶面(401)跳动控制在2MM以内,第一侧板(1)边沿外圆跳动在1MM以内。2. A kind of high-precision wind power planetary carrier processing technology according to claim 1, characterized in that, in step 1, the positioning mechanism 1 clamps the second side plate (2) through several bottom positioning clamps (7) Keep realizing the positioning of the planetary carrier, make a meter leveling so that the runout of the top surface of the column (401) is controlled within 2MM, and the runout of the outer circle of the edge of the first side plate (1) is within 1MM. 3.根据权利要求1所述的一种高精度风电行星架加工工艺,其特征在于,在步骤二中,定位机构二通过中心限位杆(8)伸入外套端(3)内对其进行限位,通过若干个承托夹具(9)对若干个立柱进行接触实现对第一侧板(1)的支撑,实现对行星架的限位,若干个承托夹具(9)与第一侧板(1)的间隙控制在0.02MM以内。3. A kind of high-precision wind power planetary carrier processing technology according to claim 1, characterized in that, in step 2, the positioning mechanism 2 extends into the outer sleeve end (3) through the center limit rod (8) to carry out the process. Limiting, contacting several uprights through several supporting fixtures (9) to support the first side plate (1), and realizing limiting the planet carrier, several supporting fixtures (9) and the first side The gap between the plates (1) is controlled within 0.02MM. 4.根据权利要求1所述的一种高精度风电行星架加工工艺,其特征在于,在步骤三中,定位机构三通过设置于支撑架(10)上的若干个侧板夹具(11)对于第一侧板(1)和第二侧板(2)进行分别的夹持限位,通过立柱夹具(12)对立柱进行夹持限位,侧板夹具(11)与行星架接触部位的间隙控制在0.02MM以内,打表侧边轴孔(5)的中心直线度跳动在1MM以内,中心轴孔的位置度在0.3MM以内。4. A kind of high-precision wind power planetary carrier processing technology according to claim 1, characterized in that, in step three, the positioning mechanism three uses several side plate clamps (11) arranged on the support frame (10) for The first side plate (1) and the second side plate (2) are respectively clamped and limited, and the column is clamped and limited by the column clamp (12). The gap between the side plate clamp (11) and the contact part of the planet carrier Control within 0.02MM, the central straightness of the table-making side shaft hole (5) jumps within 1MM, and the position of the central shaft hole is within 0.3MM. 5.根据权利要求1所述的一种高精度风电行星架加工工艺,其特征在于,在步骤四中,定位机构三通过若干个承托板(13)对若干个立柱支撑接触,通过若干个轴孔定位夹具(14)对若干个侧边轴孔(5)进行限位支撑;立柱的顶面平面度在0.05MM以内,打表侧边轴孔(5)的中心直线度跳动在1MM以内。5. A kind of high-precision wind power planetary frame processing technology according to claim 1, characterized in that, in step 4, the positioning mechanism 3 supports and contacts several columns through several support plates (13), and through several The shaft hole positioning fixture (14) provides limit support for several side shaft holes (5); the flatness of the top surface of the column is within 0.05MM, and the center straightness runout of the side shaft hole (5) is within 1MM . 6.根据权利要求1所述的一种高精度风电行星架加工工艺,其特征在于,在步骤五中,定位装夹时调节各立柱底面(403)的平面度0.05MM以内,打表侧边轴孔(5)的中心直线度跳动在0.05MM以内、圆柱度0.012MM、位置度0.08MM、同心度0.025MM、垂直度0.04MM。6. A kind of high-precision wind power planetary carrier processing technology according to claim 1, characterized in that, in step 5, when positioning and clamping, adjust the flatness of the bottom surface (403) of each column within 0.05MM, and press the side of the table The central straightness of the shaft hole (5) runs out within 0.05MM, the cylindricity is 0.012MM, the positional degree is 0.08MM, the concentricity is 0.025MM, and the verticality is 0.04MM. 7.根据权利要求1所述的一种高精度风电行星架加工工艺,其特征在于,在步骤六中,打表校平立柱顶面(401)跳动控制在0.05MM以内,打表第一侧板(1)边沿的外圆跳动在0.1MM以内;外套端(3)的同心度0.04MM、圆柱度0.03MM、中心直线度跳动0.04MM。7. A high-precision wind power planetary carrier processing technology according to claim 1, characterized in that, in step 6, the runout of the top surface (401) of the metering and leveling column is controlled within 0.05MM, and the first side of the metering is The runout of the outer circle of the edge of the plate (1) is within 0.1MM; the concentricity of the outer jacket end (3) is 0.04MM, the cylindricity is 0.03MM, and the runout of the center straightness is 0.04MM. 8.根据权利要求1所述的一种高精度风电行星架加工工艺,其特征在于,在步骤七中,定位机构七其通过支撑夹具(15)对若干个立柱顶面(401)进行支撑,实现对行星架的限位,打表各支撑夹具(15)与立柱的间隙控制在0.02MM以内,打表第一侧板(1)外圆跳动在0.1MM以内:立柱顶面(401)的平面度跳动在0.04MM以内,中心轴口(6)的圆柱度0.03MM、同心度0.04MM。8. A kind of high-precision wind power planetary carrier processing technology according to claim 1, characterized in that, in step seven, the positioning mechanism seven supports several column top surfaces (401) through the supporting fixture (15), Realize the limit of the planet carrier, control the gap between each supporting fixture (15) and the column within 0.02MM, and control the outer circle runout of the first side plate (1) within 0.1MM: the top surface of the column (401) The runout of the flatness is within 0.04MM, the cylindricity of the central shaft port (6) is 0.03MM, and the concentricity is 0.04MM.
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