CN102266973A - Machining method for milling two curved surfaces of tapered honeycomb variable-thickness structural part - Google Patents

Machining method for milling two curved surfaces of tapered honeycomb variable-thickness structural part Download PDF

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Publication number
CN102266973A
CN102266973A CN 201110203430 CN201110203430A CN102266973A CN 102266973 A CN102266973 A CN 102266973A CN 201110203430 CN201110203430 CN 201110203430 CN 201110203430 A CN201110203430 A CN 201110203430A CN 102266973 A CN102266973 A CN 102266973A
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China
Prior art keywords
honeycomb
milling
cutter
milling cutter
taper
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CN 201110203430
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Chinese (zh)
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CN102266973B (en
Inventor
郑鑫
孙永飞
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Shenyang Aircraft Industry Group Co Ltd
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Shenyang Aircraft Industry Group Co Ltd
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Priority to CN 201110203430 priority Critical patent/CN102266973B/en
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Publication of CN102266973B publication Critical patent/CN102266973B/en
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Abstract

The invention designs a machining method for milling two curved surfaces of a tapered honeycomb variable-thickness structural part. The machining method is characterized by comprising the following steps of: 1) clamping an equal-thickness honeycomb solidified body so as to position a reference surface and a reference hole of a die; 2) arranging a special honeycomb scale milling cutter for machining a honeycomb on a five-shaft linkage milling machine; 3) setting a cutter rotating center distance of the honeycomb scale milling cutter on the five-shaft linkage milling machine; 4) making the reference surface of the part die a machining reference surface; 5) setting a cutting parameter of the honeycomb scale milling cutter according to a curvature of the machined double-curved-surface tapered honeycomb variable-thickness structural part; and 6) setting a milling path and a milling screw pitch of the honeycomb scale milling cutter according to the variable curvature of the tapered honeycomb variable-thickness structural part, so that the honeycomb scale milling cutter performs milling machining along a spiral trace. By the method, high curvature transition can be realized; therefore, double-curved-surface continuous machining on the surface of the machined part can be realized, damage to the part is avoided and the requirement of the curvature of the machined surface can be met.

Description

The hyperboloid milling method of taper honeycomb thickening degree structural member
Technical field
The present invention relates to a kind of hyperboloid milling method of taper honeycomb thickening degree structural member, belong to the field of machining of cellular material structural member.
Background technology
Originally the processing of general honeycomb all is equal thickness, the machining of rule shape part, method generally is according to being become two-dimentional strip boards by the expansion profile blanking of Seiko part with the equal thickness honeycomb board, splice and combine into the profile state of required processing parts then, when in machining, realizing the materials processing of thickening degree like this, under the automated programming control of CNC milling machine, a kind of is vertical milling, tool marks appear walking in piece surface, another kind is the lateral circumferential ring cutting, rib appears chewing or going out in piece surface, is difficult to realize that curved surface continuously and the processing on thickening degree structural member fairing surface.
Summary of the invention
The technical problem to be solved in the present invention provides a kind of hyperboloid milling method of taper honeycomb thickening degree structural member, this method can realize good curvature transition, the treatment of surfaces of components realization hyperboloid is processed continuously, avoided injuring part, finally realize the curvature requirement of finished surface.
For overcoming the above problems, concrete technical scheme of the present invention is as follows: a kind of hyperboloid milling method of taper honeycomb thickening degree structural member is characterized in that may further comprise the steps:
1) the equal thickness honeycomb is solidified on body clamping to the five interlock milling machine table face, with the datum level and the datum hole location of supporting mould;
2) the special-purpose honeycomb goldfish scale milling cutter of processing honeycomb is installed on five interlock milling machines;
3) the actual cutter length according to the honeycomb goldfish scale milling cutter is provided with the cutter pivot distance of honeycomb goldfish scale milling cutter at five interlock milling machines;
4) datum level with component die is a processing datum;
5) cutting parameter of honeycomb goldfish scale milling cutter is set at the curvature of processed hyperboloid taper honeycomb thickening degree structural member;
6) according to the variation curvature of taper honeycomb thickening degree part, the milling path and the milling pitch of honeycomb goldfish scale milling cutter is set, make the honeycomb goldfish scale milling cutter carry out milling processing with spiral trajectory.
Described honeycomb goldfish scale milling cutter carries out milling processing with spiral trajectory, its movement locus is that cutter direction of advance and its downward vertical direction add 15 degree both direction feedings simultaneously, form helical form, pitch forms spiral taper curved surface and carries out milling smaller or equal to 3mm.
The hyperboloid milling method of this taper honeycomb thickening degree structural member has adopted the spiral milling, changed original in cutting and crosscut, make the processing of hyperboloid taper honeycomb thickening degree structural member after, precision improves greatly, has also improved operating efficiency simultaneously.
Description of drawings
Fig. 1 is the hyperboloid milling machining locus schematic diagram of taper honeycomb thickening degree structural member.
Wherein 1, spiral milling machining locus; 2, cutter is processed initial initial point; U, cutter processing direction of advance; V and the vertical direction of cutter processing direction of advance; The pitch of t, spiral milling machining locus.
The specific embodiment
A kind of hyperboloid milling method of taper honeycomb thickening degree structural member is characterized in that may further comprise the steps:
1) the equal thickness honeycomb is solidified on body clamping to the five interlock milling machine table face, with the datum level and the datum hole location of supporting mould;
2) the special-purpose honeycomb goldfish scale milling cutter of processing honeycomb is installed on five interlock milling machines; This milling cutter is commercial promptly available;
3) the actual cutter length according to the honeycomb goldfish scale milling cutter is provided with the cutter pivot distance of honeycomb goldfish scale milling cutter at five interlock milling machines;
4) datum level with component die is a processing datum;
5) cutting parameter of honeycomb goldfish scale milling cutter is set at the curvature of processed hyperboloid taper honeycomb thickening degree structural member;
6) according to the variation curvature of taper honeycomb thickening degree part, the milling path and the milling pitch of honeycomb goldfish scale milling cutter is set, make the honeycomb goldfish scale milling cutter carry out milling processing with spiral trajectory.
When the bi-curved curvature of taper honeycomb thickening degree structural member changed between 152 ~ 633, the cutting parameter that the honeycomb goldfish scale milling cutter is set was 18000 revolutions per seconds of rotating speeds, cutting feed rate 1200 mm/second.Precise and penetrating direction is laterally to be U, vertically be the V+15 degree, other direction feed simultaneously, and pitch is smaller or equal to 3mm, and one-tenth spiral taper track cuts the curved surface of taper honeycomb thickening degree structural member.Wherein, avoid materials processing wildness thorn, and guarantee the quality on milling surface vertically for the V+15 degree is material to be taken away when the high-speed cutting cellular material for the fish scale tooth that guarantees to reduce the honeycomb goldfish scale milling cutter.

Claims (2)

1. the hyperboloid milling method of a taper honeycomb thickening degree structural member is characterized in that may further comprise the steps:
1) the equal thickness honeycomb is solidified on body clamping to the five interlock milling machine table face, with the datum level and the datum hole location of supporting mould;
2) the special-purpose honeycomb goldfish scale milling cutter of processing honeycomb is installed on five interlock milling machines;
3) the actual cutter length according to the honeycomb goldfish scale milling cutter is provided with the cutter pivot distance of honeycomb goldfish scale milling cutter at five interlock milling machines;
4) datum level with component die is a processing datum;
5) cutting parameter of honeycomb goldfish scale milling cutter is set at the curvature of processed hyperboloid taper honeycomb thickening degree structural member;
6) according to the variation curvature of taper honeycomb thickening degree part, the milling path and the milling pitch of honeycomb goldfish scale milling cutter is set, make the honeycomb goldfish scale milling cutter carry out milling processing with spiral trajectory.
2. the hyperboloid milling method of taper honeycomb thickening degree structural member as claimed in claim 1, it is characterized in that: described honeycomb goldfish scale milling cutter carries out milling processing with spiral trajectory, its movement locus is that cutter direction of advance and its downward vertical direction add 15 degree both direction feedings simultaneously, pitch forms spiral taper curved surface and carries out milling smaller or equal to 3mm.
CN 201110203430 2011-07-20 2011-07-20 Machining method for milling two curved surfaces of tapered honeycomb variable-thickness structural part Expired - Fee Related CN102266973B (en)

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CN 201110203430 CN102266973B (en) 2011-07-20 2011-07-20 Machining method for milling two curved surfaces of tapered honeycomb variable-thickness structural part

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Application Number Priority Date Filing Date Title
CN 201110203430 CN102266973B (en) 2011-07-20 2011-07-20 Machining method for milling two curved surfaces of tapered honeycomb variable-thickness structural part

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CN102266973A true CN102266973A (en) 2011-12-07
CN102266973B CN102266973B (en) 2013-03-20

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104668925A (en) * 2013-12-02 2015-06-03 昌河飞机工业(集团)有限责任公司 Numerical control machining method of paper-based honeycomb part
CN105302064A (en) * 2015-11-30 2016-02-03 沈阳飞机工业(集团)有限公司 Stroke milling method of double-surface twisted web
CN106903357A (en) * 2017-04-18 2017-06-30 成都飞机工业(集团)有限责任公司 The processing method in thin-walled honeycomb core Curve Machining type face
CN107617772A (en) * 2017-10-26 2018-01-23 佛山市保利来建材实业有限公司 A kind of hyperboloid aluminum veneer ends cutting equipment and its cutting technique
CN109570908A (en) * 2017-09-28 2019-04-05 成都飞机工业(集团)有限责任公司 A kind of honeycomb core part featheredge type method for processing surface based on ultrasonic wave lathe

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0064573A1 (en) * 1981-05-11 1982-11-17 PD - Pries Drucklufttechnik GmbH Method and device for surfacing light-construction honeycombs
US4907920A (en) * 1989-01-18 1990-03-13 The Boeing Company Milling cutter for honeycomb core material
CN1346730A (en) * 2001-10-18 2002-05-01 浙江大学 Method for machining cellular flexible structure material
CN101428355A (en) * 2008-12-09 2009-05-13 成都飞机工业(集团)有限责任公司 Milling method for honeycomb parts

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0064573A1 (en) * 1981-05-11 1982-11-17 PD - Pries Drucklufttechnik GmbH Method and device for surfacing light-construction honeycombs
US4907920A (en) * 1989-01-18 1990-03-13 The Boeing Company Milling cutter for honeycomb core material
CN1346730A (en) * 2001-10-18 2002-05-01 浙江大学 Method for machining cellular flexible structure material
CN101428355A (en) * 2008-12-09 2009-05-13 成都飞机工业(集团)有限责任公司 Milling method for honeycomb parts

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
《中国机械工程》 20060630 柯映林 等 NOMEX蜂窝芯高速铣削加工工艺的优化 第17卷, 第12期 *

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104668925A (en) * 2013-12-02 2015-06-03 昌河飞机工业(集团)有限责任公司 Numerical control machining method of paper-based honeycomb part
CN105302064A (en) * 2015-11-30 2016-02-03 沈阳飞机工业(集团)有限公司 Stroke milling method of double-surface twisted web
CN105302064B (en) * 2015-11-30 2018-01-16 沈阳飞机工业(集团)有限公司 A kind of row blanking method of two-sided distortion web
CN106903357A (en) * 2017-04-18 2017-06-30 成都飞机工业(集团)有限责任公司 The processing method in thin-walled honeycomb core Curve Machining type face
CN109570908A (en) * 2017-09-28 2019-04-05 成都飞机工业(集团)有限责任公司 A kind of honeycomb core part featheredge type method for processing surface based on ultrasonic wave lathe
CN107617772A (en) * 2017-10-26 2018-01-23 佛山市保利来建材实业有限公司 A kind of hyperboloid aluminum veneer ends cutting equipment and its cutting technique

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