CN102672391A - Concentricity positioning tooling method of large members - Google Patents

Concentricity positioning tooling method of large members Download PDF

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Publication number
CN102672391A
CN102672391A CN2012101379302A CN201210137930A CN102672391A CN 102672391 A CN102672391 A CN 102672391A CN 2012101379302 A CN2012101379302 A CN 2012101379302A CN 201210137930 A CN201210137930 A CN 201210137930A CN 102672391 A CN102672391 A CN 102672391A
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China
Prior art keywords
flange
fine rule
concentricity
face
ring flange
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Granted
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CN2012101379302A
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Chinese (zh)
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CN102672391B (en
Inventor
吕中季
彭凤霞
许鑫
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WUXI QIAOLIAN WIND POWER TECHNOLOGY Co Ltd
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WUXI QIAOLIAN WIND POWER TECHNOLOGY Co Ltd
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Priority to CN201210137930.2A priority Critical patent/CN102672391B/en
Publication of CN102672391A publication Critical patent/CN102672391A/en
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Publication of CN102672391B publication Critical patent/CN102672391B/en
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Abstract

The invention relates to a concentricity positioning tooling method of large members, comprising a second flange, wherein the second flange is in an open type structure; a first flange ring and a third flange plate are respectively installed on two ends of the second flange; cross lines are marked on the end face of each of the flanges; and the concentricity tooling of a fourth flange and a fifth flange plate is completed through following steps. With the adoption of a method for pulling a plurality of thin lines, a concentric position between the members needing installing can be conveniently found out, the installation is accurate and fast, and the product qualification rate is high. The concentricity positioning tooling method of the large members can ensure the concentricity requirement on installing without adopting large measuring devices or even providing any special field and professional operators, thereby being low in cost. The concentricity positioning tooling method of the large members is widely applied to field work such as welding of petroleum pipelines, welding of tap water pipelines and installing of large equipment, and is flexible to use.

Description

The concentricity positioning tool method of large-scale component
Technical field
The present invention relates to field of machining and machinebuilding technology, especially be applicable to the concentricity localization method of large-scale component.
Background technology
In the existing industrial machinery processing and manufacturing; Producing and making in the large-scale component process; If confirmed the position of two flanges, therebetween or both sides add one or more flanges and guarantee its concentricity requirement, for large-scale component; As (the cabin seat is used to carry parts such as the main shaft, step-up gear, spindle bearing holder of wind power generating set to make the cabin seat of wind-driven generator; Its volume and quality are all bigger), can receive different factors such as place to cause producing and make difficulty, make it be difficult to guarantee concentricity requirement.
The method that common employing directly is welded to connect in the prior art; A plurality of flange components of cabin seat are connected into integral body, and this method is difficult to guarantee the concentricity requirement of each flange component in practical operation, and its error is bigger; Poor stability, the finished product qualification rate is low.
For fear of above-mentioned shortcoming, in the prior art, in process, adopt large-scale measurement device to guarantee the concentricity requirement between each flange component, but cost is high.
Summary of the invention
The applicant can't guarantee the concentricity between each parts in the above-mentioned existing production technology; Shortcomings such as poor product quality; A kind of concentricity positioning tool method of large-scale component easy and simple to handle is provided; Thereby need not adopt large-scale measurement device just can guarantee the concentricity requirement of each member, easy to operate, cost is low.
The technical scheme that the present invention adopted is following:
A kind of concentricity positioning tool method of large-scale component; Comprise second flange; Said second flange becomes unenclosed construction, and the two ends of said second flange are separately installed with the first flange circle and the 3rd ring flange, and the end face of each flange part is all drawn the cross line of processing; Accomplish the concentricity frock of the 4th flange and the 5th ring flange through following steps:
The first step: be positioned on the end face of the first flange circle, according to the fixing fine rule a isometric of the line of the cross on the end face of flange circle with the flange loop diameter;
Second step: the mid point of mark fine rule a, the some place pulls out a fine rule b therein;
The 3rd step: adopt with the first step in identical method be positioned on the end face of the 3rd ring flange and fix a fine rule c isometric with the 3rd ring flange diameter; Simultaneously, the mid point of mark fine rule c, this moment, the other end with fine rule b was connected fixing with the midpoint of fine rule c;
The 4th step: when the 4th flange is installed; According to the fixing fine rule d isometric of the line of the cross on the 4th flange one end face with the 4th end face of flange diameter; And the mid point of mark fine rule d, move the 4th flange, the mid point of fine rule d is contacted with fine rule b; Then accomplish the 4th flange location, then through fixing the 4th flange of welding;
The 5th step: adopt identical method in the 3rd, the 4th step; Find out the fine rule e on the 5th ring flange, and the mid point of mark fine rule e, when the 5th ring flange is installed; Move the 5th ring flange; The mid point of fine rule e is contacted with fine rule b, and then accomplish the 5th ring flange location, then through fixing the 5th ring flange of welding.
Its further technical scheme is:
Above-mentioned fine rule can adopt cotton thread or single;
The length of fine rule b is greater than the entire length of required processing work in second step.
Beneficial effect of the present invention is following:
The present invention can find out the concentric position between the required installation component easily through the method for many fine rule backguys, and it is accurate, quick to install, and product percent of pass is high.The present invention need not adopt large-scale measurement device just can guarantee the installation of its concentricity requirement, and any special place and the operating personnel of specialty more need be provided, and cost is low.The present invention uses flexibly in being widely used in the field work installing like petroleum pipeline welding, water supply pipe welding and main equipment.
Description of drawings
Fig. 1 is the structural representation of an embodiment of the present invention.
Fig. 2 is the structural representation of first step method of operating of the present invention.
Fig. 3 is the structural representation of the second step method of operating of the present invention.
Fig. 4 is the structural representation of the 3rd step method of operating of the present invention.
Fig. 5 is the structural representation of FOUR EASY STEPS method of the present invention.
Fig. 6 is the structural representation of the 5th step method of operating of the present invention.
The specific embodiment
Below in conjunction with accompanying drawing, the specific embodiment of the present invention is described.
When the present invention is used for making the cabin seat of wind-driven generator; As shown in Figure 1; The structure of cabin seat is following: comprise open type cone flange 2, an end of cone flange 2 is welded with and cooperates flange circle 1 with it, and the other end of cone flange 2 welds a ring flange 3; Ring flange 3 one face down bondings connect cone flange 4, the end face welding flange 5 of cone flange 4.The cross section of above-mentioned flange arrangement is all greater than semicircle, and the end face of each flange arrangement has all been drawn the cross line before welding.
In the actual processing and making process, the two ends of cone flange 2 are welded with flange circle 1 and ring flange 3 respectively, accomplish the installation of cone flange 4 and ring flange 5 through following steps:
The first step: see Fig. 2, be positioned on the end face of flange circle 1, according to the fixing fine rule a isometric of the line of the cross on the end face of flange circle 1 with flange circle 1 diameter;
Second step: see Fig. 3, the mid point of mark fine rule a, the some place pulls out a fine rule b therein, and the length of fine rule b is greater than the length of whole cabin seat;
The 3rd step: see Fig. 4, adopt with the first step in identical method be positioned on the end face of ring flange 3 and fix a fine rule c isometric with ring flange 3 diameters; Simultaneously, the mid point of mark fine rule c is connected the other end of fine rule b and fixes this moment with the midpoint of fine rule c, and then straight line b passes through the center of circle of flange circle 1, cone flange 2 and ring flange 3, thereby the center of circle that guarantees their threes point-blank;
The 4th step: see Fig. 5; When cone flange 4 is installed, according to the fixing fine rule d isometric of the line of the cross on cone flange 4 one end faces with cone flange 4 end face diameters, and the mid point of mark fine rule d; Move cone flange 4; The mid point of fine rule d is contacted with fine rule b, and then accomplish cone flange 4 location, then through welding fixedly cone flange 4; The center of circle of the center of circle and flange circle 1, cone flange 2 and ring flange 3 that has promptly guaranteed cone flange 4 is on same straight line;
The 5th step: see Fig. 6, adopt as above identical method, find out the fine rule e on the ring flange 5; And the mid point of mark fine rule e, during mounting flange 5, rotary flange dish 5; The mid point of fine rule e is contacted with fine rule b, and then accomplish ring flange 5 location, then through welding fixed flange 5; The center of circle of the center of circle and flange circle 1, cone flange 2, ring flange 3 and cone flange 4 that has promptly guaranteed ring flange 5 is on same straight line.
Promptly can accomplish the completion assembly unit of cabin seat easily through as above step, and guarantee the concentricity between each flange, easy to operate, cost is low, is widely used in installing like petroleum pipeline welding, water supply pipe welding and main equipment in the field work.
Fine rule a of the present invention, fine rule b, fine rule c, fine rule d, fine rule e all can adopt cotton thread, perhaps has the single of solid and tension.
More than describing is to explanation of the present invention, is not that institute of the present invention restricted portion within protection scope of the present invention, can be done any type of modification referring to claim to the qualification of invention.

Claims (3)

1. the concentricity positioning tool method of a large-scale component; It is characterized in that: comprise second flange; Said second flange becomes unenclosed construction, and the two ends of said second flange are separately installed with the first flange circle and the 3rd ring flange, and the end face of each flange part is all drawn the cross line of processing; Accomplish the concentricity frock of the 4th flange and the 5th ring flange through following steps:
The first step: be positioned on the end face of the first flange circle, according to the fixing fine rule a isometric of the line of the cross on the end face of flange circle with the flange loop diameter;
Second step: the mid point of mark fine rule a, the some place pulls out a fine rule b therein;
The 3rd step: adopt with the first step in identical method be positioned on the end face of the 3rd ring flange and fix a fine rule c isometric with the 3rd ring flange diameter; Simultaneously, the mid point of mark fine rule c, this moment, the other end with fine rule b was connected fixing with the midpoint of fine rule c;
The 4th step: when the 4th flange is installed; According to the fixing fine rule d isometric of the line of the cross on the 4th flange one end face with the 4th end face of flange diameter; And the mid point of mark fine rule d, move the 4th flange, the mid point of fine rule d is contacted with fine rule b; Then accomplish the 4th flange location, then through fixing the 4th flange of welding;
The 5th step: adopt identical method in the 3rd, the 4th step; Find out the fine rule e on the 5th ring flange, and the mid point of mark fine rule e, when the 5th ring flange is installed; Move the 5th ring flange; The mid point of fine rule e is contacted with fine rule b, and then accomplish the 5th ring flange location, then through fixing the 5th ring flange of welding.
2. the concentricity positioning tool method of large-scale component as claimed in claim 1, it is characterized in that: above-mentioned fine rule can adopt cotton thread or single.
3. the concentricity positioning tool method of large-scale component as claimed in claim 1 is characterized in that: the length of fine rule b is greater than the entire length of required processing work in second step.
CN201210137930.2A 2012-05-07 2012-05-07 Concentricity positioning tooling method of large members Expired - Fee Related CN102672391B (en)

Priority Applications (1)

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CN201210137930.2A CN102672391B (en) 2012-05-07 2012-05-07 Concentricity positioning tooling method of large members

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Application Number Priority Date Filing Date Title
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CN102672391B CN102672391B (en) 2014-11-19

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105252178A (en) * 2015-11-17 2016-01-20 宜昌船舶柴油机有限公司 Concentricity control method for axial welding of multilayer annular plates
CN106197229A (en) * 2016-07-15 2016-12-07 兰州兰石重型装备股份有限公司 The measuring method of minor diameter tankage abutted flange concentricity

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4496093A (en) * 1983-06-06 1985-01-29 Taylor Jr Julius E Apparatus for aligning abutting pipes
CN1733417A (en) * 2000-12-08 2006-02-15 中国建筑第八工程局工业设备安装公司一公司 Flange positioner
CN101907201A (en) * 2010-08-09 2010-12-08 中建五局第三建设有限公司 Construction method for positioning sleeve by automatic leveling plumb method
CN102121315A (en) * 2011-01-07 2011-07-13 中建五局第三建设有限公司 Hole reserving construction method for tightly-fixed steel sleeve

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4496093A (en) * 1983-06-06 1985-01-29 Taylor Jr Julius E Apparatus for aligning abutting pipes
CN1733417A (en) * 2000-12-08 2006-02-15 中国建筑第八工程局工业设备安装公司一公司 Flange positioner
CN101907201A (en) * 2010-08-09 2010-12-08 中建五局第三建设有限公司 Construction method for positioning sleeve by automatic leveling plumb method
CN102121315A (en) * 2011-01-07 2011-07-13 中建五局第三建设有限公司 Hole reserving construction method for tightly-fixed steel sleeve

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105252178A (en) * 2015-11-17 2016-01-20 宜昌船舶柴油机有限公司 Concentricity control method for axial welding of multilayer annular plates
CN106197229A (en) * 2016-07-15 2016-12-07 兰州兰石重型装备股份有限公司 The measuring method of minor diameter tankage abutted flange concentricity
CN106197229B (en) * 2016-07-15 2018-08-31 兰州兰石重型装备股份有限公司 The measurement method of minor diameter tankage abutted flange concentricity

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