CN103586499B - A kind of transmission pin frame of ship loader telescopic boom processing method - Google Patents

A kind of transmission pin frame of ship loader telescopic boom processing method Download PDF

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Publication number
CN103586499B
CN103586499B CN201310528804.4A CN201310528804A CN103586499B CN 103586499 B CN103586499 B CN 103586499B CN 201310528804 A CN201310528804 A CN 201310528804A CN 103586499 B CN103586499 B CN 103586499B
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China
Prior art keywords
needle pin
pin frame
needle
line
processing
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CN201310528804.4A
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Chinese (zh)
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CN103586499A (en
Inventor
管伟伟
柴松
安文新
沈建荣
胡文佳
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Wison Clean Energy Technology Group Co ltd
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Wison Nantong Heavy Industry Co Ltd
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Publication of CN103586499A publication Critical patent/CN103586499A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23BTURNING; BORING
    • B23B35/00Methods for boring or drilling, or for working essentially requiring the use of boring or drilling machines; Use of auxiliary equipment in connection with such methods

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Forklifts And Lifting Vehicles (AREA)
  • Automatic Assembly (AREA)

Abstract

A kind of transmission pin frame of ship loader telescopic boom processing method, comprises the following steps: step one, adjustment needle pin frame and telescopic jib bearing are fitted closely; Step 2, installation needle pin frame; Step 3, recalibration needle pin frame; Step 4, on needle pin retainer, draw horizontal datum; Step 5, carry out pin holes processing; Step 6, needle pin frame panel to be fixedly installed down; Step 7, horizontal datum leveling, lengthwise centers line adjusts; Step 8, location, the starter hole center of circle processing starting point gone out according to needle pin easel painting; After step 9, machined complete, and spot welding position is polished flat; Instant invention overcomes traditional processing technology and carry out bore hole, because structural strength is inadequate, and there is no enough line planes, be difficult to the problem such as the depth of parallelism, perpendicularity after ensureing pin holes processing, improve processing intensity and machining accuracy.

Description

A kind of transmission pin frame of ship loader telescopic boom processing method
Technical field
The present invention relates to ship equipment manufacture field, particularly a kind of transmission pin frame of ship loader telescopic boom processing method.
Background technology
Any workpiece is before ingress engine manufacturing procedure, machined datum line need be marked on component, needle pin frame for inner arm support of ship loader transmission is no exception, this structural type is like " π ", gusset is not strengthened in inside, carries out bore hole by traditional processing technology, because structural strength is inadequate, and there is no enough line planes, be difficult to the depth of parallelism, perpendicularity etc. after ensureing pin holes processing.Traditional technique carries out bore hole one by one according to the positioning datum of structural member line, because structural strength is not enough and line deviation, causes the pin holes after processing cannot meet the installation requirement of equipment.
Summary of the invention
In order to overcome the defect of above-mentioned prior art, the object of the present invention is to provide a kind of transmission pin frame of ship loader telescopic boom processing method, structural strength and precision are all improved a lot.
In order to achieve the above object, technical scheme of the present invention is achieved in that
A kind of transmission pin frame of ship loader telescopic boom processing method, comprises the following steps:
Step one, according to lower railway center line location needle pin frame, ensure needle pin frame center line and orbit centre line parallel, and adjust needle pin frame and telescopic jib bearing is fitted closely, then itself and structure are carried out temporary fixed;
Step 2, installation needle pin frame, and with service bolt, needle pin seat is connected with telescopic jib, the necessary mounting process bolt of each bolt hole, and tighten;
Step 3, recalibration needle pin frame, then install and keep support;
Step 4, according to coordinate value, draw first hole of every section of needle pin frame and the central cross line in last hole, and guarantee pin holes center line line and the telescopic jib central axis of both sides same position, needle pin retainer draws horizontal datum;
After the correction of step 5, needle pin frame, line, take off a numerical control machining center and carry out pin holes processing;
Step 6, needle pin frame panel to be fixedly installed down;
Step 7, according to the horizontal datum leveling that needle pin frame retainer draws, adjust according to lengthwise centers line that it is vertical with machine tool chief axis;
Step 8, location, the starter hole center of circle processing starting point gone out according to needle pin easel painting;
After step 9, machined complete, retainer can be removed, and spot welding position is polished flat.
Instant invention overcomes traditional processing technology and carry out bore hole, because structural strength is inadequate, and there is no enough line planes, be difficult to the problem such as the depth of parallelism, perpendicularity after ensureing pin holes processing, improve processing intensity and machining accuracy.
Accompanying drawing explanation
Fig. 1 is the processing effect figure of step one of the present invention to step 5.
Fig. 2 is the processing effect figure of step 6 of the present invention to step 9.
Detailed description of the invention
Below in conjunction with accompanying drawing, the present invention is described in detail.
A kind of transmission pin frame of ship loader telescopic boom processing method, comprises the following steps:
With reference to Fig. 1, step one, according to lower railway center line location needle pin frame, ensure needle pin frame center line and orbit centre line parallel, and adjust needle pin frame and telescopic jib bearing is fitted closely, then itself and structure are carried out temporary fixed;
Step 2, installation needle pin frame, and with service bolt, needle pin seat is connected with telescopic jib, the necessary mounting process bolt of each bolt hole, and tighten;
Step 3, recalibration needle pin frame, then install and keep support;
Step 4, according to coordinate value, draw first hole of every section of needle pin frame and the central cross line in last hole, and guarantee pin holes center line line and the telescopic jib central axis of both sides same position, needle pin retainer draws horizontal datum;
After the correction of step 5, needle pin frame, line, take off a numerical control machining center and carry out pin holes processing;
With reference to Fig. 2, step 6, needle pin frame panel to be fixedly installed down;
Step 7, according to the horizontal datum leveling that needle pin frame retainer draws, adjust according to lengthwise centers line that it is vertical with machine tool chief axis;
Step 8, location, the starter hole center of circle processing starting point gone out according to needle pin easel painting;
After step 9, machined complete, retainer can be removed, and spot welding position is polished flat.

Claims (1)

1. a transmission pin frame of ship loader telescopic boom processing method, is characterized in that: comprise the following steps:
Step one, according to lower railway center line location needle pin frame, ensure needle pin frame center line and orbit centre line parallel, and adjust needle pin frame and telescopic jib bearing is fitted closely, then needle pin frame and telescopic jib bearing are carried out temporary fixed;
Step 2, installation needle pin frame, and with service bolt, needle pin seat is connected with telescopic jib, the necessary mounting process bolt of each bolt hole, and tighten;
Step 3, recalibration needle pin frame, then install needle pin frame retainer;
Step 4, according to coordinate value, draw the starter hole of every section of needle pin frame and the central cross line in last hole and guarantee pin holes center line line and the telescopic jib central axis of both sides same position, needle pin frame retainer draws horizontal datum;
After the correction of step 5, needle pin frame, line, take off a numerical control machining center and carry out pin holes processing;
Step 6, needle pin frame panel to be fixedly installed down;
Step 7, according to the horizontal datum leveling that needle pin frame retainer draws, adjust according to lengthwise centers line that it is vertical with machine tool chief axis;
Step 8, location, the starter hole center of circle processing starting point gone out according to needle pin easel painting;
After step 9, machined complete, needle pin frame retainer is removed, and spot welding position is polished flat.
CN201310528804.4A 2013-10-30 2013-10-30 A kind of transmission pin frame of ship loader telescopic boom processing method Active CN103586499B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310528804.4A CN103586499B (en) 2013-10-30 2013-10-30 A kind of transmission pin frame of ship loader telescopic boom processing method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310528804.4A CN103586499B (en) 2013-10-30 2013-10-30 A kind of transmission pin frame of ship loader telescopic boom processing method

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CN103586499A CN103586499A (en) 2014-02-19
CN103586499B true CN103586499B (en) 2016-01-06

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Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5350588A (en) * 1976-10-18 1978-05-09 Hitachi Zosen Corp Method for drilling long materials
US7273333B2 (en) * 2003-06-25 2007-09-25 The Boeing Company Methods and apparatus for counterbalance-assisted manufacturing operations
CN101073839A (en) * 2007-05-28 2007-11-21 中铁宝桥股份有限公司 Method for manufacturing ear-plate pin hinged-connection structure of stayed-cable bridge
CN101623769A (en) * 2009-06-25 2010-01-13 辽河石油勘探局 Processing method of porous tube plate of fuel oil steam injection boiler
CN102179540A (en) * 2011-04-22 2011-09-14 海波重型工程科技股份有限公司 Sample mold drilling method for steel truss girder whole node rod
CN102211215A (en) * 2011-06-03 2011-10-12 韩以伦 Automatic location punching system of underfloor steel keel and use method thereof in container
CN102962485A (en) * 2012-11-14 2013-03-13 中铁九桥工程有限公司 Parallelogram cross-section whole node rod piece lineation drilling technique

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110135411A1 (en) * 2009-12-03 2011-06-09 Inman John E Drill template with integral vacuum attach having plugs

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5350588A (en) * 1976-10-18 1978-05-09 Hitachi Zosen Corp Method for drilling long materials
US7273333B2 (en) * 2003-06-25 2007-09-25 The Boeing Company Methods and apparatus for counterbalance-assisted manufacturing operations
CN101073839A (en) * 2007-05-28 2007-11-21 中铁宝桥股份有限公司 Method for manufacturing ear-plate pin hinged-connection structure of stayed-cable bridge
CN101623769A (en) * 2009-06-25 2010-01-13 辽河石油勘探局 Processing method of porous tube plate of fuel oil steam injection boiler
CN102179540A (en) * 2011-04-22 2011-09-14 海波重型工程科技股份有限公司 Sample mold drilling method for steel truss girder whole node rod
CN102211215A (en) * 2011-06-03 2011-10-12 韩以伦 Automatic location punching system of underfloor steel keel and use method thereof in container
CN102962485A (en) * 2012-11-14 2013-03-13 中铁九桥工程有限公司 Parallelogram cross-section whole node rod piece lineation drilling technique

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SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of invention: A processing method for driving pin frame of telescopic boom of ship loader

Effective date of registration: 20220519

Granted publication date: 20160106

Pledgee: Nantong Jiangsu rural commercial bank Limited by Share Ltd.

Pledgor: WISON(NANTONG) HEAVY INDUSTRY Co.,Ltd.

Registration number: Y2022980005940

PE01 Entry into force of the registration of the contract for pledge of patent right
PC01 Cancellation of the registration of the contract for pledge of patent right

Date of cancellation: 20221122

Granted publication date: 20160106

Pledgee: Nantong Jiangsu rural commercial bank Limited by Share Ltd.

Pledgor: WISON(NANTONG) HEAVY INDUSTRY Co.,Ltd.

Registration number: Y2022980005940

PC01 Cancellation of the registration of the contract for pledge of patent right
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of invention: A Machining Method for Driving Pin Frame of Ship Loader Telescopic Boom

Effective date of registration: 20221123

Granted publication date: 20160106

Pledgee: Nantong Jiangsu rural commercial bank Limited by Share Ltd.

Pledgor: WISON(NANTONG) HEAVY INDUSTRY Co.,Ltd.

Registration number: Y2022980023140

PE01 Entry into force of the registration of the contract for pledge of patent right
PC01 Cancellation of the registration of the contract for pledge of patent right

Granted publication date: 20160106

Pledgee: Nantong Jiangsu rural commercial bank Limited by Share Ltd.

Pledgor: WISON(NANTONG) HEAVY INDUSTRY Co.,Ltd.

Registration number: Y2022980023140

PC01 Cancellation of the registration of the contract for pledge of patent right
CP03 Change of name, title or address

Address after: 226000 port industrial zone 3, Nantong Economic and Technological Development Zone, Jiangsu Province

Patentee after: Wison Clean Energy Technology Group Co.,Ltd.

Country or region after: China

Address before: 226009 Jianghai Road 189, Nantong Economic and Technological Development Zone, Jiangsu Province

Patentee before: WISON(NANTONG) HEAVY INDUSTRY Co.,Ltd.

Country or region before: China

CP03 Change of name, title or address