CN105401195B - A kind of clamp method and clamping device of complex parts anodization - Google Patents

A kind of clamp method and clamping device of complex parts anodization Download PDF

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Publication number
CN105401195B
CN105401195B CN201510866153.9A CN201510866153A CN105401195B CN 105401195 B CN105401195 B CN 105401195B CN 201510866153 A CN201510866153 A CN 201510866153A CN 105401195 B CN105401195 B CN 105401195B
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China
Prior art keywords
anodization
support frame
clamping device
rotary shaft
motor
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CN201510866153.9A
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CN105401195A (en
Inventor
陈舸
巴晓甫
王守川
庞新强
郑超
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AVIC Xian Aircraft Industry Group Co Ltd
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AVIC Aircraft Corp Xian Aircraft Branch
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Abstract

A kind of clamp method and clamping device of complex parts anodization, the support frame of the clamping device is the metal framework of a del, the metal hanger that can be connected with electrode is provided with the top of support frame, there is a rotary rotary shaft in the lower end horizontal connection of support frame, one termination of rotary shaft passes through belt pulley and motor connection, will the part of anodization be fixed on above-mentioned part alignment pin, then immerse in anodization tank liquor;Startup motor is made part and rotated in tank liquor with 12 degree to 15 degree of angular speed each second around rotary shaft.

Description

A kind of clamp method and clamping device of complex parts anodization
Technical field
The application is related to aircraft manufacturing technical field, especially for the anodization production process of aircraft complex type surface parts In, specifically a kind of clamp method and clamping fixture to complex parts anodization.
Background technology
Metal anodised technique plays an important role in industry manufactures.Anodization film layer have it is corrosion-resistant, wear-resisting, The characteristics of surface aesthetic, and different anodization film layers all has specific function.Metal anodised mechanism is in electric current In the presence of, metallic surface is generated specific oxidation film layer.
During oxidation reaction, electric current flows between liquid and metal, makes solution and metal exchange ion, generates oxygen Change film.This reaction generation hydrogen and other salt compounds, hydrogen leave conversion zone, salt chemical combination after rising to liquid level Thing is dissolved into solution.If metal surface can contact fresh solution, anodization can just continue to carry out, and anodization film layer is held It is continuous to thicken.After anodization film layer reaches specific thicknesses, part departs from tank liquor, terminates anodizing operations.And to complex profile zero Part, because the stacking of design of part covers, prevent parts locally surface from gas is smoothly discharged, because between solution and part Form hydrogen to wrap on part, form anodization barrier layer.After part extracts from solution tank, nigrescence, bar are shown as Line shape impression.
The content of the invention
It is an object of the invention to provide a kind of clamp method and clamping fixture of complex parts anodization.
A kind of clamp method of complex parts anodization, it is characterised in that:1) there is a clamping device, the clamping device Support frame is the metal framework of a del, and the metal hanger that can be connected with electrode is provided with the top of support frame, is being propped up The lower end horizontal connection of support has a rotary rotary shaft, and a termination of rotary shaft is connected by belt pulley and motor Connect, motor is fixed on the top of support frame, on the rotating shaft provided with part alignment pin;2) will the part of anodization be fixed on State on part alignment pin, then immerse in anodization tank liquor;3) start motor and make part in tank liquor with 12 degree to 15 degree of each second Angular speed rotated around rotary shaft.
The beneficial effects of the invention are as follows:Drive part to be rotated in tank liquor by belt pulley, make each surface phase of part After inside solution upward.In this process, bubble caused by anodization just can emersion liquid level, metal parts surface contact Fresh solution, the drawbacks of wrapping bubble on part complex profile is eliminated, anodization thicknesses of layers uniformity, meets production need Ask.
The application is described in further detail with reference to embodiments.
Brief description of the drawings
Fig. 1 is that a kind of aircraft end rib design of part for needing anodization is illustrated
Fig. 2 is a kind of anodization clamping fixture structural representation
Fig. 3 is a kind of aircraft end rib part anode clamp method signal
Explanation is numbered in figure:1 part, 2 motors, 3 hooks, 4 support frames, 5 belt pulleys, 6 rotary shafts, 7 alignment pins
Embodiment
Referring to accompanying drawing, embodiment provides carries out anodized clamping to typical end rib part on aircraft, should The two sides of part 1 is slotted, parallel to each other.During anodization, due to not accomplishing that fully horizontally general status is in a face groove Air can escape, and the bubble row in the groove of an other face does not come out.As a result fail to exclude accumulated gas in the groove of bubble, produce The defects of nigrescence, impression.
Fig. 2 is the anodization clamping device schematic diagram that the application proposes, the support frame 4 of the clamping device is an inverted triangle The metal framework of shape, the metal hanger 3 that can be connected with electrode is provided with the top of support frame 4, in order to stable, the metal hanger has Four, the position at four angles of support frame is respectively provided at, in the lower end of support frame 4, horizontal connection has one rotary turn Moving axis 6, a termination of rotary shaft 6 are connected by belt pulley 5 with motor 2, and motor 2 is fixed on the top of support frame 4, is rotating Axle 6 is provided with part alignment pin 7.
During anodization, will the part 1 of anodization the alignment pin 7 of clamping device rotary shaft 6 is fixed on by its positioning hole On, as shown in figure 3, then hanging over four dresses of metal hanger 3 on electrode bar, then part and clamping device are immersed into anodization groove In liquid, notice that liquid level should submerge the part of rotation, kept for the part moment be under liquid level, while liquid level can not contact motor peace Panel is filled, avoids tank liquor corrosion panel and motor.Start motor 2, rotary shaft 6 is driven by belt pulley 5 and is fixed thereon Part 1 rotates, and makes part 1 and is rotated in tank liquor with 12 degree to 15 degree of angular speed each second around rotary shaft 6.Rotary shaft 6 Driving part to be rotated with CAV, make all surface gas of part can discharge quickly, part can continue anodization, So as to avoid the nigrescence of metal surface, impression defect.

Claims (2)

  1. A kind of 1. clamp method of complex parts anodization, it is characterised in that:1) there are a clamping device, the branch of the clamping device Support is the metal framework of a del, and the metal hanger that can be connected with electrode is provided with the top of support frame, is being supported The lower end horizontal connection of frame has a rotary rotary shaft, a termination of rotary shaft by belt pulley and motor connection, Motor is fixed on the top of support frame, on the rotating shaft provided with part alignment pin;2) will anodization part be fixed on it is above-mentioned On part alignment pin, then immerse in anodization tank liquor;3) start motor and make part in tank liquor with 12 degree to 15 degree of each second Angular speed is rotated around rotary shaft.
  2. 2. a kind of clamping device of complex parts anodization, it is characterised in that the support frame of the clamping device is an inverted triangle The metal framework of shape, the metal hanger that can be connected with electrode is provided with the top of support frame, in the lower end horizontal connection of support frame There is a rotary rotary shaft, a termination of rotary shaft is fixed on support frame by belt pulley and motor connection, electrode Top, on the rotating shaft provided with part alignment pin.
CN201510866153.9A 2015-11-30 2015-11-30 A kind of clamp method and clamping device of complex parts anodization Active CN105401195B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510866153.9A CN105401195B (en) 2015-11-30 2015-11-30 A kind of clamp method and clamping device of complex parts anodization

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Application Number Priority Date Filing Date Title
CN201510866153.9A CN105401195B (en) 2015-11-30 2015-11-30 A kind of clamp method and clamping device of complex parts anodization

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CN105401195A CN105401195A (en) 2016-03-16
CN105401195B true CN105401195B (en) 2017-12-19

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Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107604345A (en) * 2016-07-12 2018-01-19 沈阳黎明国际动力工业有限公司 A kind of device for aluminum alloy casing class part chemical oxidation
CN109202426B (en) * 2018-09-12 2023-09-08 广西建工集团第一安装工程有限公司 On-site pipe penetrating tool device and process for large vertical fixed pipe plate type heat exchanger
CN113249761B (en) * 2020-02-12 2022-07-15 上海飞机制造有限公司 Anodization stores pylon
CN111945213B (en) * 2020-07-06 2022-10-28 西安飞机工业(集团)有限责任公司 Pictographic anode clamp for electroplating multiple plating surfaces of slide rail part

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102428214A (en) * 2009-04-28 2012-04-25 托纳斯管理控股有限公司 Plant for the surface processing of parts
CN202849573U (en) * 2012-09-25 2013-04-03 广州中国科学院先进技术研究所 Anode oxidation device
CN104109894A (en) * 2014-07-18 2014-10-22 郑州轻工业学院 Magnesium alloy composite surface protective treatment equipment and magnesium alloy composite surface protective treatment method
CN205275734U (en) * 2015-11-30 2016-06-01 中航飞机股份有限公司西安飞机分公司 Clamping device of complicated shape anodization

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Publication number Priority date Publication date Assignee Title
FR2906265B1 (en) * 2006-09-22 2008-12-19 Frederic Vacheron INSTALLATION FOR PROCESSING THE SURFACE OF PIECES BY IMMERSION IN A TREATMENT FLUID.
JP2009120864A (en) * 2007-11-12 2009-06-04 Yamamoto Mekki Shikenki:Kk Plating jig
IT1397751B1 (en) * 2010-01-26 2013-01-24 Sat Surface Aluminium Technologies S P A STATION FOR ANODIZATION TREATMENT IN A VERTICAL PAINTING SYSTEM OF ALUMINUM PROFILES AND PAINTING SYSTEM THAT INTEGRATES THIS STATION FOR ANODIZATION TREATMENT.
CN104894629B (en) * 2015-06-26 2017-03-29 张家口时代橡胶制品股份有限公司 Phosphatization production line workpiece hanger

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102428214A (en) * 2009-04-28 2012-04-25 托纳斯管理控股有限公司 Plant for the surface processing of parts
CN202849573U (en) * 2012-09-25 2013-04-03 广州中国科学院先进技术研究所 Anode oxidation device
CN104109894A (en) * 2014-07-18 2014-10-22 郑州轻工业学院 Magnesium alloy composite surface protective treatment equipment and magnesium alloy composite surface protective treatment method
CN205275734U (en) * 2015-11-30 2016-06-01 中航飞机股份有限公司西安飞机分公司 Clamping device of complicated shape anodization

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Address after: No. 710089 in Shaanxi province Xi'an city Yanliang District West Avenue

Patentee after: AVIC Xi'an Aircraft Industry Group Co.,Ltd.

Address before: 1 No. 710089 Shaanxi province Xi'an city Yanliang District West Avenue

Patentee before: AVIC AIRCRAFT Corp.

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TR01 Transfer of patent right

Effective date of registration: 20210611

Address after: 1 No. 710089 Shaanxi province Xi'an city Yanliang District West Avenue

Patentee after: AVIC AIRCRAFT Corp.

Address before: 1 No. 710089 Shaanxi province Xi'an city Yanliang District West Avenue

Patentee before: XI'AN AIRCRAFT BRANCH OF XI'AN AIRCRAFT INTERNATIONAL Corp.