CN102699630A - Numerically controlled processing method for thin-walled part with open lateral groove end - Google Patents

Numerically controlled processing method for thin-walled part with open lateral groove end Download PDF

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Publication number
CN102699630A
CN102699630A CN2012101825905A CN201210182590A CN102699630A CN 102699630 A CN102699630 A CN 102699630A CN 2012101825905 A CN2012101825905 A CN 2012101825905A CN 201210182590 A CN201210182590 A CN 201210182590A CN 102699630 A CN102699630 A CN 102699630A
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edge strip
processing
groove
woollen
open end
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CN2012101825905A
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CN102699630B (en
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王乐宇
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Shenyang Aircraft Industry Group Co Ltd
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Shenyang Aircraft Industry Group Co Ltd
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Abstract

The invention relates to a numerically controlled processing method for a thin-walled part with an open lateral groove end, and adopts the technical scheme that a woolen bottom plane and a lateral plane are taken as positioning criteria; firstly, roughing is carried out on the outline of the edge strip on the side with a groove; then, woolen placing is changed in such a manner that the original lateral plane serves as a bottom plate while the original bottom plate serves as a lateral plane, and grooves are also formed by taking the two planes as positioning criteria; during the outline processing of the part, the part of the part except the open end of the edge strip is processed first, the open end of the edge strip is kept in connection with circumferential woolen, the thickness processing of the edge strip is fulfilled under the state, and then the connection between the open end of the edge strip and the woolen is cut off, so as to form the outline of the open end of the edge strip; and the method that the outer side and the inner side of the edge strip are processed in an alternated manner (namely the outer side layer of the edge strip is fulfilled and then the inner side layer of the edge strip is fulfilled) is adopted, and the required thickness of the edge strip is obtained finally after the operation is carried out repeatedly. The method has the advantages that the position of the groove on the outer side of the edge strip is more accurate; the open end of the edge strip meets the product requirement; and the favorable surface roughness of the edge strip is guaranteed.

Description

The numerical-control processing method of the thin-walled parts that band side groove termination opens wide
Technical field
The invention mainly is applicable to adopts the plate digital control processing, and the edge strip outside is fluted, and the edge strip termination opens wide, and edge strip thickness≤2mm, highly>and the part of 40mm.
Background technology
At aviation field, fluted to the outside, the termination opens wide; And thickness≤2mm, highly>problem that exists in the edge strip part processing of 40mm is: at first, between edge strip outside groove and woollen baseplane apart from less; If directly on platen, use machine tool chief axis pivot angle machined grooves; Therefore lathe headstock can interfere with workbench, processes part that this type of edge strip outside has groove and all be with woollen baseplane and side plane as positioning reference, processes all sites except that groove; Use square chest or other working position apparatus bed hedgehopping parts then, again with part baseplane and the datum hole that processed as positioning reference processing edge strip outside groove.Employing the method processing, the workman needs the lifting station utensil, has increased production time, and variation has taken place the positioning reference that machined grooves adopted, and influence the accurate of groove location.Secondly; The part that the edge strip termination opens wide all is to adopt first processing parts profile, and promptly first cutting-off part and border woolen cloth are connected to form the part largest contours, the method processing of back processing edge strip thickness; The method can not go wrong when edge strip thickness>2mm or edge strip height≤40mm; But when edge strip thickness≤2mm and height>40mm, the steadiness that edge strip is opened wide end reduces, and work in-process can produce bigger vibration; The edge strip thickness that makes this place easily becomes defective work less than the minimum dimension that product design requires.The 3rd, when the processing height approaches edge strip, all be through the elder generation processing edge strip outside, processing inboard acquisition edge strip thickness, the mode of the processing of layering is from high to low all adopted in both sides.When edge strip thickness thickness≤2mm and height>40mm, edge strip processes the outside and causes the edge strip rigidity to reduce, and edge strip trembleed when processing was inboard, was attended by the cutter vibration simultaneously, caused edge strip surface roughness variation.
Summary of the invention
In order to overcome the above problems, the invention provides a kind of and is applicable to that the edge strip outside is fluted, and the edge strip termination opens wide, and edge strip thickness≤2mm, highly>and the numerical-control processing method of the part of 40mm.
The technical scheme that the invention is adopted is: the numerical-control processing method of the thin-walled parts that band side groove termination opens wide is following:
1) processing of edge strip outside groove: with woollen baseplane and side plane as locating benchmark; The edge strip profile of the fluted side of elder generation's roughing; Change woollen modes of emplacement then; With original side plane as the baseplane; The baseplane is as side plane; Still process groove as the location benchmark, again woolen cloth is returned to former modes of emplacement with these two planes;
2) processing of opening wide end of edge strip: during the processing parts profile; Process the part except that edge strip is opened wide the termination earlier; Keep edge strip to open wide end and woollen being connected in border; Under this state, accomplish the processing of edge strip thickness; Cut off edge strip again and open wide end and woollen being connected, form edge strip and open wide the end profile;
3) processing of edge strip thickness: adopt and alternately to process outer, the inboard method of edge strip, accomplish one deck processing back in the edge strip outside then accomplish the inboard one deck processing of edge strip, so back and forth, final acquisitions need edge strip.
The beneficial effect of the invention is: 1. adopt the processing method of edge strip of the present invention outside groove, processing edge strip outside groove need not to use working position apparatuses such as square chest, has saved the required working time of workman's lifting station utensil, has improved part processing efficient.In addition, this method processing edge strip outside positioning reference that groove adopted is consistent with the positioning reference that adopt at other positions of processing, has eliminated the position error that the positioning reference conversion is brought, and the edge strip that processes outside groove location is more accurate.2. adopt edge strip of the present invention to open wide the processing method of end; When processing parts edge strip thickness, kept edge strip to open wide end and woollen being connected, when cutting proceeded to edge strip and opens wide end, the vibration of edge strip generation conducted to the border woolen cloth through connection; Thereby vibration intensity is weakened; The edge strip steadiness improves, and guarantees that edge strip opens wide end thickness and satisfy the product design requirement, obtains qualified products.3. adopt the processing method of edge strip thickness of the present invention; The rigidity that in process, has kept high thin edge strip to greatest extent; The vibration and the cutter that have reduced the edge strip work in-process tremble the influence that edge strip caused, and guarantee that edge strip obtains the surface of good roughness.
Description of drawings
Fig. 1 is the sketch map of the invention processing edge strip.
The specific embodiment
The numerical-control processing method of the thin-walled parts that embodiment band side groove termination opens wide
Method is following: as shown in Figure 1,1-is woollen among the figure; 2-part edge strip is opened wide end; 3-part edge strip is opened wide the woollen connection of end; The high thin edge strip of 4-; 5-edge strip outside groove.
1) processing of edge strip outside groove: with woollen baseplane and side plane as positioning reference; The edge strip profile of elder generation's roughing fluted side changes woollen modes of emplacement then, with original side plane as the baseplane; The baseplane is as side plane; Still process groove as positioning reference, again woolen cloth is returned to former modes of emplacement, down accomplish the processing at other positions again with these two planes.
2) processing of opening wide end of edge strip: during the processing parts profile; The part of processing except that edge strip is opened wide the termination keeps edge strip to open wide end and woollen being connected in border earlier, under this state, accomplishes the processing of edge strip thickness; Cut off edge strip again and open wide end and woollen being connected, form edge strip and open wide the end profile.
3) processing of edge strip thickness: because the mode of the processing of layering is from high to low all adopted in processing edge strip both sides; Thereby be adjusted into and alternately process outer, the inboard method of edge strip; Accomplish one deck processing back in the edge strip outside and transfer to accomplish the inboard one deck processing of edge strip; The edge strip thickness so reciprocal, that final acquisition needs.

Claims (1)

1. the numerical-control processing method of the thin-walled parts opened wide of band side groove termination is characterized in that method is following:
1) processing of edge strip outside groove: with woollen baseplane and side plane as locating benchmark; The edge strip profile of the fluted side of elder generation's roughing; Change woollen modes of emplacement then; With original side plane as the baseplane; The baseplane is as side plane; Still process groove as the location benchmark, again woolen cloth is returned to former modes of emplacement with these two planes;
2) processing of opening wide end of edge strip: during the processing parts profile; The part of processing except that edge strip is opened wide the termination keeps edge strip to open wide end and woollen being connected in border earlier, under this state, accomplishes the processing of edge strip thickness; Cut off edge strip again and open wide end and woollen being connected, form edge strip and open wide the end profile;
3) processing of edge strip thickness: adopt and alternately to process outer, the inboard method of edge strip, accomplish one deck processing back in the edge strip outside then accomplish the inboard one deck processing of edge strip, so back and forth, final acquisitions need edge strip.
CN201210182590.5A 2012-06-06 2012-06-06 Numerically controlled processing method for thin-walled part with open lateral groove end Expired - Fee Related CN102699630B (en)

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CN201210182590.5A CN102699630B (en) 2012-06-06 2012-06-06 Numerically controlled processing method for thin-walled part with open lateral groove end

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103753110A (en) * 2014-01-09 2014-04-30 北华航天工业学院 Thin-wall elliptical part numerical control machining method
CN109604691A (en) * 2019-01-16 2019-04-12 沈阳飞机工业(集团)有限公司 A kind of processing method of the fixator class part of Double curve degree variable curvature deformed cross-section strip communication groove
CN113305517A (en) * 2021-06-21 2021-08-27 成都爱乐达航空制造股份有限公司 Method for processing side wall holes of ribs and flanges
CN114310195A (en) * 2022-01-19 2022-04-12 成都飞机工业(集团)有限责任公司 Stable machining method for thin-wall edge strip inclined end face structure

Citations (4)

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CN101104242A (en) * 2007-09-11 2008-01-16 西安飞机工业(集团)有限责任公司 Numerically controlled processing method for plane wing rib beam part
CN101704183A (en) * 2009-12-10 2010-05-12 西安飞机工业(集团)有限责任公司 Horizontal numerical control machining method of plane beam-type parts
CN102319989A (en) * 2011-09-06 2012-01-18 上海交通大学 Manufacturing method of airplane horizontal tail beam edge strip

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3724734A1 (en) * 1987-07-25 1989-02-02 Gmoehling Leichtmetall Magazine pallet for workpieces
CN101104242A (en) * 2007-09-11 2008-01-16 西安飞机工业(集团)有限责任公司 Numerically controlled processing method for plane wing rib beam part
CN101704183A (en) * 2009-12-10 2010-05-12 西安飞机工业(集团)有限责任公司 Horizontal numerical control machining method of plane beam-type parts
CN102319989A (en) * 2011-09-06 2012-01-18 上海交通大学 Manufacturing method of airplane horizontal tail beam edge strip

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
刘川烈: "某型机主起落架舱梁数字化的高效创新加工", 《装备制造技术》 *

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103753110A (en) * 2014-01-09 2014-04-30 北华航天工业学院 Thin-wall elliptical part numerical control machining method
CN109604691A (en) * 2019-01-16 2019-04-12 沈阳飞机工业(集团)有限公司 A kind of processing method of the fixator class part of Double curve degree variable curvature deformed cross-section strip communication groove
CN109604691B (en) * 2019-01-16 2020-06-19 沈阳飞机工业(集团)有限公司 Method for machining fixator part with double-curvature variable-curvature special-shaped cross section provided with communicating groove
CN113305517A (en) * 2021-06-21 2021-08-27 成都爱乐达航空制造股份有限公司 Method for processing side wall holes of ribs and flanges
CN114310195A (en) * 2022-01-19 2022-04-12 成都飞机工业(集团)有限责任公司 Stable machining method for thin-wall edge strip inclined end face structure

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