CN105382312A - Finish machining weight control method for two-sided thin-wall numerical control milling machine workpiece - Google Patents

Finish machining weight control method for two-sided thin-wall numerical control milling machine workpiece Download PDF

Info

Publication number
CN105382312A
CN105382312A CN201510845526.4A CN201510845526A CN105382312A CN 105382312 A CN105382312 A CN 105382312A CN 201510845526 A CN201510845526 A CN 201510845526A CN 105382312 A CN105382312 A CN 105382312A
Authority
CN
China
Prior art keywords
sided thin
walled
milling part
number milling
control method
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201510845526.4A
Other languages
Chinese (zh)
Inventor
王家军
陈鹏飞
李海泉
王宏彬
戴浩
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shenyang Aircraft Design and Research Institute Aviation Industry of China AVIC
Original Assignee
Shenyang Aircraft Design and Research Institute Aviation Industry of China AVIC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shenyang Aircraft Design and Research Institute Aviation Industry of China AVIC filed Critical Shenyang Aircraft Design and Research Institute Aviation Industry of China AVIC
Priority to CN201510845526.4A priority Critical patent/CN105382312A/en
Publication of CN105382312A publication Critical patent/CN105382312A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23CMILLING
    • B23C3/00Milling particular work; Special milling operations; Machines therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23CMILLING
    • B23C2215/00Details of workpieces
    • B23C2215/04Aircraft components

Abstract

The invention provides a finish machining weight control method for a two-sided thin-wall numerical control milling machine workpiece, and relates to the field of weight engineering of overall design of planes. The finish machining weight control method is used for design of the two-sided thin-wall numerical control milling machine workpiece and weight control in the machining process and includes the steps that S1, the thickness of the two-sided thin-wall numerical control milling machine workpiece is designed as a thickness having symmetry tolerance with a design value; S2, a design model of the two-sided thin-wall numerical control milling machine workpiece is accurately controlled; S3, optimization design is carried out on the structural stability of the two-sided thin-wall numerical control milling machine workpiece; S4, in the machining process of the two-sided thin-wall numerical control milling machine workpiece, a base material is fixed to a tool; and S5, the base material is machined, and the machining size is measured and corrected in the machining process. According to the finish machining weight control method for the two-sided thin-wall numerical control milling machine workpiece, the two-sided thin-wall numerical control milling machine workpiece is designed and machined, the machining accuracy of a large two-sided thin-wall-structure part can be largely improved, and the weight reducing effect of the two-sided thin-wall numerical control milling machine workpiece in the machining process is improved.

Description

A kind of two-sided thin-walled number milling part fine finishining weight control method
Technical field
The present invention relates to weight engineering field in preliminary design of aircraft, in particular to one two-sided thin-walled number milling part fine finishining weight control method.
Background technology
The mechanical processing technique of airplane parts is the important component part of aircraft manufacturing technology, along with the extensive use with Computerized Numerical Control processing technology that improves constantly of aircraft technology performance, the quantity of machined part is being on the increase, especially integral structure component increases more remarkable, wherein, integral panel, owing to decreasing the quantity of part and connector, simplifies rapport, decrease assembly work amount, number of applications aboard gets more and more.
Integral panel comprises web, rib, connecting hole and periphery and strengthens boss, there is the integral panel of large contour dimension, thin web plate, double-side type cavity configuration, because metal removal rate is large, Numerical Control Processing Working Procedure is concentrated, because it is two-sided thin-wall part structure, add and easily cause unstability and distortion man-hour, difficulty of processing is comparatively large, realizes the processing of such part high-precision and there is larger difficulty.
Therefore, when processing such part, the psychological condition that people always exist " the large insurance of size; the little danger of size ", the size of the part of processing often major part is positioned at the overgauge part of the margin of tolerance, part, close to the upper poor limit, directly causes two-sided thin-walled number milling part weight seriously overweight.
The technical problem needing now solution badly how to design a kind of two-sided thin-walled number milling part fine finishining weight control method.
Summary of the invention
The object of the invention is to solve above-mentioned deficiency of the prior art, a kind of two-sided thin-walled number milling part fine finishining weight control method is provided.
Object of the present invention is achieved through the following technical solutions: a kind of two-sided thin-walled number milling part fine finishining weight control method, for the Weight control in the design of two-sided thin-walled number milling part, process, it is characterized in that, comprises the steps,
In the described two-sided thin-walled number milling part process of design:
S1, is designed to the thickness with design load with symmetric tolerance to the thickness of two-sided thin-walled number milling part;
S2, accurately controls designing a model of described two-sided thin-walled number milling part;
S3, is optimized design to described two-sided thin-walled number milling part structural stability;
In the described two-sided thin-walled number milling part process of processing:
S4, is fixed on mother metal in frock;
S5, processes mother metal, measures and revise in process to processing dimension.
In such scheme preferably, accurately control to comprise to carry out Accurate Model to the angle residual fraction that closes of described two-sided thin-walled number milling part to designing a model of described two-sided thin-walled number milling part in S2.
In above-mentioned either a program preferably, in S3, the mode of optimal design comprises the version of rib on the quantity of rib on adjustment web, the position adjusting rib on web and adjustment web.
In above-mentioned either a program preferably, in S4, mother metal is fixed on the two-sided thin-walled number milling part model after optimizing in mode in frock and S3 and matches.
In above-mentioned either a program preferably, the mother metal mode be fixed in frock comprises vacuum suction, the auxiliary pressing plate of edge increase, on rib, increases supplemental support.
In above-mentioned either a program preferably, the mother metal mode be fixed in frock comprises vacuum suction, edge increases auxiliary pressing plate, on rib, increase the combination of at least two kinds of modes in supplemental support.
The beneficial effect of two-sided thin-walled number milling part fine finishining weight control method provided by the present invention is, two-sided thin-walled number milling part fine finishining weight control method provided by the present invention is adopted to process two-sided thin-walled number milling part, significantly improve the machining accuracy of the two-sided thin-wall construction part of large scale, two-sided thin-walled number milling part weight loss effect is remarkable, both saved raw-material cost, the precision of two-sided thin-walled number milling part can have been ensured again.
Accompanying drawing explanation
Fig. 1 is the schematic flow sheet of the preferred embodiment according to two-sided thin-walled number milling part fine finishining weight control method of the present invention;
Detailed description of the invention
In order to understand the two-sided thin-walled number milling part fine finishining weight control method according to the present invention program better, be further elaborated explanation below in conjunction with the preferred embodiment of accompanying drawing to two-sided thin-walled number milling part fine finishining weight control method of the present invention.
As shown in Figure 1, two-sided thin-walled number milling part fine finishining weight control method provided by the invention is used for the Weight control in the design of two-sided thin-walled number milling part, process, comprises the steps,
In the described two-sided thin-walled number milling part process of design:
S1, is designed to the thickness with design load with symmetric tolerance to the thickness of two-sided thin-walled number milling part; S2, accurately controls designing a model of described two-sided thin-walled number milling part; S3, is optimized design to described two-sided thin-walled number milling part structural stability;
In the described two-sided thin-walled number milling part process of processing:
S4, is fixed on mother metal in frock; S5, processes mother metal, measures and revise in process to processing dimension.
In the S1-S5 of the two-sided thin-walled number milling part fine finishining weight control method provided in the invention described above, accurately control to comprise to carry out Accurate Model to the angle residual fraction that closes of described two-sided thin-walled number milling part to designing a model of described two-sided thin-walled number milling part in S2; In S3, the mode of optimal design comprises the version of rib on the quantity of rib on adjustment web, the position adjusting rib on web and adjustment web; The mode that in S4, mother metal is fixed in frock is determined according to the two-sided thin-walled number milling part model after optimization in S3; The mother metal mode be fixed in frock comprises vacuum suction, edge increases auxiliary pressing plate, on rib, increases supplemental support.
Two-sided thin-walled number milling part fine finishining weight control method involved in the present invention is applied in two-sided thin-walled number milling part fine finishining Weight control, in two-sided thin-walled number milling part fine finishining Weight control process, mainly comprise the following aspects:
1. dimensional tolerance controls
The dimensional tolerance distribution of two-sided thin-walled number milling part has a significant impact pts wt, and when Element Design, trying one's best dimensional tolerance design is symmetric tolerance, and selects narrower tolerance zone as far as possible.If asymmetric tolerance range must be selected, plus tolerance part should be compressed as far as possible.Firmly stop the phenomenon that dimensional tolerance only has plus tolerance.
2. the quality that designs a model accurately controls
In numerical control part design process, must the strict designing quality controlling threedimensional model, actual processing technology should be taken into full account, partly Accurate Model is carried out to residual grade the in angle of closing that can not process, make Theoretical Design state and reality can machining state consistent.
3. structural stability design monitoring is optimized
In the design process, calculate, analyze the structural stability of part, by modified node method form, optimize the structural stability improving two-sided thin-walled number milling part, to improve the machining accuracy of part in process.
4. strengthen process structural stability
Select suitable part fixed form or various ways combining form, be fixed on by blank in frock, main purpose is the structural stability strengthening part in process.The mode strengthening process structural stability mainly comprises following several mode: the stability of part when (1) selects suitable fixture to improve machining, and integral wall plate parts is employing vacuum adsorption type fixed form as far as possible; (2) auxiliary pressing plate is increased at the blank edge of part; (3) for the poor part of segmental stability, suitably supplemental support is increased according to design of part feature.
5. Dimension Measurement controls
Measure accessory size in real time in part process, adjust the depth of cut in time, particular content is as follows: (1) keeps part to be processed stationary state in frock, measures accessory size in real time, strengthens monitoring; (2) the comprehensive dimensional measurement to part should be ensured when measuring, be of a size of 50mm × 50mm region and should have a dimensional measurement point at least; (3), when measuring, if Dimension Measurement does not meet the demands, should the depth of cut be adjusted, carry out supplementary processing, until can pull down from frock after meeting the demands.
For the process of the outer panel of aircraft, further explanation is set forth to two-sided thin-walled number milling part fine finishining weight control method of the present invention.The outer panel appearance and size of aircraft is: 4300mm × 1200mm × 100mm, and web thickness design load is 2mm, and dimensional tolerance is ± 0.25mm and (0 ~ 0.5mm) two kinds.Part theoretical weight 54.19kg, the part actual weight that weight control method is in the prior art produced is 58.55kg, overweight more, does not meet the demands.The outer panel of the aircraft produced after adopting two-sided thin-walled number milling part fine finishining weight control method provided by the invention to carry out Weight control to the outer panel of aircraft in design, process has loss of weight by a relatively large margin, it is produced the weight drawn and conforms to design designing requirement, meets design requirement.
The outer panel parts character of the above-mentioned aircraft adopting weight control method of the prior art to produce and the overweight analysis of causes:
A) large scale, thin web plate, the machine-made spares of thin-wall construction, structural stability is poor, and difficulty of processing is large;
B) because machining accuracy can not be guaranteed, actual adding, processes according to the dimensional tolerance upper limit man-hour.
Two-sided thin-walled number milling part fine finishining weight control method provided by the invention is adopted the outer panel of above-mentioned aircraft to be carried out to the Weight control of process.Design phase at the outer panel of above-mentioned aircraft: (1) adjust size tolerance.Adjustment accessory size tolerance range, cancels the former tolerance range only having plus tolerance, and compresses symmetric tolerance, accessory size tolerance is adjusted to ± 0.2mm.(2) outer panel model quality accurately controls.Strengthen the control to the modeling accuracy of part model, carry out supplementary modeling to closing angle residual fraction, theoretical model and actual processing technology state are consistent.(3) design of part optimizing stability.Analyze design of part stability, design is optimized to the position of part reinforcement and form.(4) structural stability in man-hour is added.Because this inside parts vallecular cavity reinforcement height differs, effective support can not be provided time fixing, therefore, increase supplemental support at reinforcement height compared with on the crosspoint of lower part.(5) accessory size control in man-hour is added.A, carry out dimensional measurement under the stationary state of part in frock; B, thickness measure is carried out to every 50mm × 50mm scope of outer panel part; C, in part process, in real time measure outer panel part size everywhere; D, outer panel accessory size control by size nominal value, carry out supplementary processing, until the rear that meets the demands is pulled down from frock to the size region that do not meet design requirement.
Compare for convenience, employing commonsense method processing parts is numbered part-1, the dash number adopting the processing of fine finishining loss of weight Process is part-2, and part-2 is part-1 loss of weight 3.29kg comparatively, Be very effective.Two pts wt contrast situations refer to table 1.
Table 1 machine adds part weight contrast information slip
Provided by the invention two-sided thin-walled number milling part fine finishining weight control method is adopted to carry out Weight control to aircraft outer panel in design, process segment by above-mentioned, weight control method more of the prior art is compared, and significantly improves the machining accuracy of the outer panel of the two-sided thin-walled of above-mentioned aircraft.Under the above-mentioned aircraft outer panel performance of guarantee meets the requirements of precondition, two-sided thin-walled number milling part fine finishining weight control method provided by the invention is adopted to carry out Weight control in the design of above-mentioned aircraft outer panel, process segment, the part comparatively adopting other processes to process is compared, weight loss effect is remarkable, makes the weight of the outer panel of production phase gained aircraft and the weight of design phase almost without residual quantity.
More than be described in detail in conjunction with two-sided thin-walled number milling part fine finishining weight control method specific embodiment of the present invention, but be not limitation of the present invention, everyly according to technical spirit of the present invention, technical scope of the present invention is all belonged to any simple modification made for any of the above embodiments, also it should be noted that, comprise any combination between each part mentioned above according to the category of two-sided thin-walled number milling part fine finishining weight control method technical scheme of the present invention.

Claims (6)

1. a two-sided thin-walled number milling part fine finishining weight control method, for the Weight control in the design of two-sided thin-walled number milling part, process, is characterized in that, comprise the steps, in the described two-sided thin-walled number milling part process of design:
S1, is designed to the thickness with design load with symmetric tolerance to the thickness of two-sided thin-walled number milling part;
S2, accurately controls designing a model of described two-sided thin-walled number milling part;
S3, is optimized design to described two-sided thin-walled number milling part structural stability;
In the described two-sided thin-walled number milling part process of processing:
S4, is fixed on mother metal in frock;
S5, processes mother metal, measures and revise in process to processing dimension.
2. two-sided thin-walled number milling part fine finishining weight control method as claimed in claim 1, it is characterized in that, accurately control to comprise to carry out Accurate Model to the angle residual fraction that closes of described two-sided thin-walled number milling part to designing a model of described two-sided thin-walled number milling part in S2.
3. two-sided thin-walled number milling part fine finishining weight control method as claimed in claim 1, is characterized in that, in S3, the mode of optimal design comprises the version of rib on the quantity of rib on adjustment web, the position adjusting rib on web and adjustment web.
4. two-sided thin-walled number milling part fine finishining weight control method as claimed in claim 1, is characterized in that, in S4, mother metal is fixed on the two-sided thin-walled number milling part model after optimizing in mode in frock and S3 and matches.
5. two-sided thin-walled number milling part fine finishining weight control method as claimed in claim 4, is characterized in that, the mother metal mode be fixed in frock comprises vacuum suction, edge increases auxiliary pressing plate, on rib, increases supplemental support.
6. two-sided thin-walled number milling part fine finishining weight control method as claimed in claim 4, it is characterized in that, the mother metal mode be fixed in frock comprises vacuum suction, edge increases auxiliary pressing plate, on rib, increase the combination of at least two kinds of modes in supplemental support.
CN201510845526.4A 2015-11-26 2015-11-26 Finish machining weight control method for two-sided thin-wall numerical control milling machine workpiece Pending CN105382312A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510845526.4A CN105382312A (en) 2015-11-26 2015-11-26 Finish machining weight control method for two-sided thin-wall numerical control milling machine workpiece

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510845526.4A CN105382312A (en) 2015-11-26 2015-11-26 Finish machining weight control method for two-sided thin-wall numerical control milling machine workpiece

Publications (1)

Publication Number Publication Date
CN105382312A true CN105382312A (en) 2016-03-09

Family

ID=55415448

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510845526.4A Pending CN105382312A (en) 2015-11-26 2015-11-26 Finish machining weight control method for two-sided thin-wall numerical control milling machine workpiece

Country Status (1)

Country Link
CN (1) CN105382312A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106270681A (en) * 2016-10-17 2017-01-04 珠海杰赛科技有限公司 A kind of processing method on abnormity elongate configuration plate milling limit
CN107442823A (en) * 2017-06-23 2017-12-08 成都飞机工业(集团)有限责任公司 A kind of high-rate wireless LAN method of large span vallecular cavity
CN107577863A (en) * 2017-08-31 2018-01-12 中国航空工业集团公司沈阳飞机设计研究所 A kind of part actual weight computational methods based on CATIA
CN113441765A (en) * 2021-06-25 2021-09-28 成都飞机工业(集团)有限责任公司 Milling method of double-sided frame type part

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101609324A (en) * 2008-06-16 2009-12-23 应建仁 Process for controlling distribution of tooling tolerance
CN102854841A (en) * 2012-09-29 2013-01-02 广东工业大学 Shape and position error in-situ compensating and processing method for curved surface parts
JP2013000845A (en) * 2011-06-17 2013-01-07 Mitsubishi Heavy Ind Ltd Plate workpiece machining method and machined body
CN104112029A (en) * 2013-04-22 2014-10-22 上海上飞飞机装备制造有限公司 Optimized design method of airplane process equipment
CN105081677A (en) * 2014-05-07 2015-11-25 哈尔滨飞机工业集团有限责任公司 Machining method of intensive rib-structure integral panel parts

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101609324A (en) * 2008-06-16 2009-12-23 应建仁 Process for controlling distribution of tooling tolerance
JP2013000845A (en) * 2011-06-17 2013-01-07 Mitsubishi Heavy Ind Ltd Plate workpiece machining method and machined body
CN102854841A (en) * 2012-09-29 2013-01-02 广东工业大学 Shape and position error in-situ compensating and processing method for curved surface parts
CN104112029A (en) * 2013-04-22 2014-10-22 上海上飞飞机装备制造有限公司 Optimized design method of airplane process equipment
CN105081677A (en) * 2014-05-07 2015-11-25 哈尔滨飞机工业集团有限责任公司 Machining method of intensive rib-structure integral panel parts

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
陈代鑫等: ""飞机薄壁结构件数控加工重量误差控制研究"", 《数控加工》 *

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106270681A (en) * 2016-10-17 2017-01-04 珠海杰赛科技有限公司 A kind of processing method on abnormity elongate configuration plate milling limit
CN107442823A (en) * 2017-06-23 2017-12-08 成都飞机工业(集团)有限责任公司 A kind of high-rate wireless LAN method of large span vallecular cavity
CN107442823B (en) * 2017-06-23 2019-11-05 成都飞机工业(集团)有限责任公司 A kind of high-rate wireless LAN method of large span vallecular cavity
CN107577863A (en) * 2017-08-31 2018-01-12 中国航空工业集团公司沈阳飞机设计研究所 A kind of part actual weight computational methods based on CATIA
CN113441765A (en) * 2021-06-25 2021-09-28 成都飞机工业(集团)有限责任公司 Milling method of double-sided frame type part
CN113441765B (en) * 2021-06-25 2022-06-14 成都飞机工业(集团)有限责任公司 Milling method of double-sided frame type part

Similar Documents

Publication Publication Date Title
CN105382312A (en) Finish machining weight control method for two-sided thin-wall numerical control milling machine workpiece
CN106425303B (en) A kind of large thin-wall bay section processing method of casing and fixture
CN103921145B (en) A kind of clamping method of controlling accurate lopps thin-walled parts machining distortion
CN106624632B (en) The slim polyhedron rudder skeleton of titanium alloy and its processing method
CN104077442A (en) Method for controlling machining accuracy of large integrated thin-walled parts based on finite element analysis
CN105149662B (en) A kind of glass steel material cone circle shell pieces class method of processing parts
CN107052715A (en) A kind of large-scale Integral Wing Panel numerical-control processing method
CN106216966B (en) Based on adaptive machining covering high-efficiency machining method
CN103084639A (en) Method for strengthening process rigidity of thin-wall blade based on non-uniform allowance
CN104816166B (en) The progressive molding hole flanging instrument and flange hole technology of perforate reaming integration
CN104070513B (en) The accurate scribble method of thin-wall special-shaped casting cabin body
CN105904108B (en) A kind of large-scale sheet laser cutting clamper and its processing method
CN103586737A (en) Compensation method for high-precision numerical-control milling for molded surfaces of blades
CN107617853A (en) A kind of processing method of stainless sheet steel part thickness control
CN107695628B (en) Processing method for deformed bracket part made of aluminum alloy material
CN103406725A (en) Flutter model truss machining method
CN102554304A (en) Method for machining 45-degree intersected shaft holes of milling head
CN108788208B (en) Boring method for machining intersection angle box hole system
CN110238697A (en) A kind of presetting cutter method of three-axis numerical control milling
Boivie et al. Development of a hybrid manufacturing cell; integration of additive manufacturing with CNC machining
CN105215968A (en) Large aerospace thin-wall titanium alloy foundry goods conformal Machining Technology for Cutting
CN106112067A (en) Many auricles hole in piece part processing drill jig and cutter automatic design method
CN106078252A (en) A kind of with fiberglass cambered surface and the clamp for machining of ladder hole type parts and processing method
CN205630030U (en) A adjustable frock for scarf
CN208696994U (en) Cutter tool setting device

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20160309