CN106002112A - Turbine blade ceramic core soft core support machining method - Google Patents

Turbine blade ceramic core soft core support machining method Download PDF

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Publication number
CN106002112A
CN106002112A CN201610374616.4A CN201610374616A CN106002112A CN 106002112 A CN106002112 A CN 106002112A CN 201610374616 A CN201610374616 A CN 201610374616A CN 106002112 A CN106002112 A CN 106002112A
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soft
tao xin
soft stud
stud
blade
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CN201610374616.4A
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CN106002112B (en
Inventor
蒋睿嵩
汪文虎
崔康
熊峰
熊一峰
林坤阳
赵德中
靳淇超
宋国栋
曹旭康
王楠
邵明伟
刘钟
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Northwestern Polytechnical University
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Northwestern Polytechnical University
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/02Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from one piece

Abstract

The invention discloses a turbine blade ceramic core soft core support machining method, and aims at solving the technical problem that the conventional methods are bad in fitting point consistency between soft core supports and ceramic cores. The technical scheme is that the method comprises the following steps: determining a soft core support point at a blade profile center position at 1/3 of the distance between a blade body and a blade tip of a ceramic core; uniformly arranging two soft core support points on a blade profile curve at 2/3 of the distance between the blade body and the blade tip of the ceramic core; making a cylinder with a diameter of 4mm by taking a soft core support position point as the center and taking a Y-axis direction as an axis; clipping the column by utilizing the curved surface of the ceramic core and the curved surface of a wax mould as boundaries, wherein a geometric body between the two curved surfaces is a soft core support geometric model; and carrying out machining by adopting a VMC-850 machine tool and a hard alloy ball-end mill according to a machining program programmed by a soft core support geometric structure, so that the machining preparation of a wax soft core support is realized. According to the method disclosed in the invention, the fitting point consistency between the soft core supports and the ceramic cores is improved.

Description

Turbo blade Tao Xin soft stud processing method
Technical field
The present invention relates to a kind of Tao Xin soft stud processing method, particularly to a kind of turbo blade Tao Xin soft stud processing side Method.
Background technology
Aero-engine hollow turbine vane essence casts forming period length, wall thickness accuracy is on the low side, percent defective is high, always system One of bottleneck that about the new machine of China is developed.
Prepare the qualified essence casting wax pattern of wall thickness accuracy and be to ensure that the most important condition of hollow turbine vane wall thickness.Essence casting wax pattern wall Thickness relies primarily on Tao Xin and ensures with accurately mating of wax molds.For controlling Tao Xin position in wax molds, Stud need to be used Tao Xin to be positioned and supports, by wax material pair in the counterforce counteraction wax pattern cavity filling process of stud The active force of Tao Xin, thus reduce Tao Xin deformation and drift, control the wall thickness deviation distribution of essence casting wax pattern.At present, core Support has metal material stud and the soft stud of waxiness.Because metal stud is in mould matched moulds and wax-pattern pressing process, Ke Nengyin Extruding causes Tao Xin to rupture, thus frequently with the soft stud of the waxiness being made up of soft wax to realize Tao Xin at wax in actual production Location in mould.
" " complicated hollow turbine vane precisely casting wax mold Tao Xin soft stud location technology " [J] Cui Kang, Wang Wenhu is special for document Kind of casting and non-ferrous alloy 2013.33 (1) p53-56 " point out space layout and the structure chi of current Tao Xin setting element The very little Experience Design that relies primarily on completes, and owing to being theoretically unsound, frequently results in Tao Xin location imperfect, and discloses The location technology of the soft stud of Tao Xin waxiness, by setting up Tao Xin position error TRANSFER MODEL, Optimal Method of Select Locating algorithm, Accurately give Tao Xin positioning layout point.And in terms of the preparation of the soft stud of waxiness, domestic not yet have particular study to see All reports, and actual production is usually the rectangle wax disk(-sc) of fixed thickness, wax disk(-sc) is bonded on ceramic core by the used time, During compacting essence casting wax pattern, stud is wrapped up by wax material and combines together with essence casting wax pattern.Owing to essence casting wax pattern wall thickness is not It is uniformly distributed, takes the rectangle wax disk(-sc) of fixed thickness, stud will be caused not fit with wax molds completely, thus shadow Ring wax pattern wall thickness accuracy, and soft stud needs workman's manual operation, soft stud and Tao Xin laminating points with Tao Xin laminating process Concordance is poor, and production efficiency is low.
Summary of the invention
In order to overcome the deficiency of the soft stud of existing method and Tao Xin laminating points concordance difference, the present invention provides a kind of turbine leaf Sheet Tao Xin soft stud processing method.The method determines one in Tao Xin blade blade profile center at blade tip position 1/3 Soft stud point, is evenly arranged two soft stud points at Tao Xin blade, with soft core at blade tip position 2/3 in blade profile curve Centered by support location point, Y direction is axis, does the cylinder of diameter of phi 4mm, utilizes Tao Xin curved surface and wax molds Curved surface is border cuts cylinder, and between two curved surfaces, geometrical body is soft stud geometric model;According to soft stud geometry The processor of establishment, uses VMC-850 lathe, and hard alloy bulb milling cutter is processed, it is achieved the soft core of waxiness Prepared by the processing of support.Improve the concordance of soft stud and Tao Xin laminating points.
The technical solution adopted for the present invention to solve the technical problems: a kind of turbo blade Tao Xin soft stud processing method, It is characterized in comprising the following steps:
Step 1, determine leaf basin, blade back soft stud position.
Tao Xin blade segment length is 75mm, and print point cross section I and cross section II height are respectively the 1/3 and 2/3 of blade, Section line is projected to XZ plane, obtains cross section I and cross section II.Cross section I is along the intersection of Y-direction Yu Tao Xin leaf basin Trisection, obtains a Q1、Q2, halve along the intersection of Y-direction with Tao Xin leaf basin, obtain a Q in cross section II3, point Q1、Q2、Q3It is Tao Xin leaf pelvic part position soft stud print point.Cross section I is along the intersection three of Y direction Yu Tao Xin blade back Decile, obtains a Q4、Q5, halve along the intersection of Y direction with Tao Xin blade back, obtain a Q in cross section II6, point Q4、Q5、Q6It is Tao Xin blade back position soft stud print point.
Step 2, determine leaf basin, blade back soft stud geometry.
Centered by some Q1, Q2, Q3, Y-axis is that axis makees Φ 4mm cylinder respectively, utilizes Tao Xin leaf basin profile With wax molds profile, cylinder is carried out cutting, obtain leaf basin soft stud geometry.In with some Q4, Q5, Q6 being The heart, Y-axis is that axis makees Φ 4mm cylinder respectively, utilizes Tao Xin blade back profile to carry out cylinder with wax molds profile Cutting, obtains blade back soft stud geometry.
Step 3, analyze soft stud material, select Digit Control Machine Tool, fixture, cutter, technological parameter.
Soft stud material is essence casting wax material, has less coefficient of thermal expansion and shrinkage factor, higher thermostability;According to Tao Xin size, soft stud is set as the cylinder of Φ 4mm;
Soft stud is parallel with Tao Xin Y-axis, in conjunction with Tao Xin overall structure, selects: lathe is three axis numerically controlled machine, according to Soft stud diameter, determines that tool diameter≤1mm, selection cutter are carbide-tipped milling cutter, and its cutter Probe-radius is 0.5mm。
Prepared by step 4, soft stud blank.
Use neutral detergent to add water cleanings, get rid of wicking surface oil film of making pottery;Selected soft stud wax material is passed through water Bath heating, controls wax liquid temperature less than 100 DEG C;Wax-coated liquid near soft stud position, Wax-coated liquid size is big In soft stud size, in case digital control processing surplus.
Step 5, soft stud digital control processing.
Utilize common CAD/CAM software to be programmed, and Path is carried out simulating, verifying.Add what man-hour selected Lathe is: VMC-850, and the cutter of selection is: hard alloy bulb milling cutter, and lathe selection of speed is 1300r/min, Feed speed is 800mm/min.
The invention has the beneficial effects as follows: the method determines one in Tao Xin blade blade profile center at blade tip position 1/3 Individual soft stud point, is evenly arranged two soft stud points at Tao Xin blade, with soft at blade tip position 2/3 in blade profile curve Centered by stud location point, Y direction is axis, does the cylinder of diameter of phi 4mm, utilizes Tao Xin curved surface and wax pattern mould Tool curved surface is border cuts cylinder, and between two curved surfaces, geometrical body is soft stud geometric model;Tie according to soft stud geometry The processor of structure establishment, uses VMC-850 lathe, and hard alloy bulb milling cutter is processed, it is achieved waxiness is soft Prepared by the processing of stud.Improve the concordance of soft stud and Tao Xin laminating points.Test result shows: diameter of phi 4mm The soft stud of waxiness, stud and wax-pattern, the laminating gap of Tao Xin are reduced to below 0.5mm by maximum 2mm;Use Numerical control positioning and process technology, each Tao Xin soft stud preparation time saves about 1.5 hours.
With detailed description of the invention, the present invention is elaborated below in conjunction with the accompanying drawings.
Accompanying drawing explanation
Fig. 1 is the flow chart of turbo blade Tao Xin of the present invention soft stud processing method.
Fig. 2 is Tao Xin localized cross-sectional schematic diagram in turbo blade Tao Xin of the present invention soft stud processing method.
Fig. 3 is turbo blade Tao Xin of the present invention soft stud processing method middle period basin soft stud point schematic diagram.
Fig. 4 is blade back soft stud point schematic diagram in turbo blade Tao Xin of the present invention soft stud processing method.
Fig. 5 is turbo blade Tao Xin of the present invention soft stud processing method middle period basin soft stud geometry schematic diagram.
Fig. 6 is blade back soft stud geometry schematic diagram in turbo blade Tao Xin of the present invention soft stud processing method.
Detailed description of the invention
With reference to Fig. 1-6.Turbo blade Tao Xin of the present invention soft stud processing method specifically comprises the following steps that
Step 1, determine leaf basin, blade back soft stud position.
In the present embodiment, Tao Xin blade segment length is 75mm, and print point cross section I and cross section II height are respectively blade 1/3 and 2/3, section line is projected to XZ plane, obtains cross section I and cross section II, cross section I is along Y-direction and Tao Xin The intersection trisection of leaf basin, obtains a Q1、Q2, halve along the intersection of Y-direction with Tao Xin leaf basin, obtain in cross section II To a Q3, put Q1、Q2、Q3It is Tao Xin leaf pelvic part position soft stud print point.Cross section I is along Y direction and Tao Xin The intersection trisection of blade back, obtains a Q4、Q5, halve along the intersection of Y direction with Tao Xin blade back, obtain in cross section II To a Q6, put Q4、Q5、Q6It is Tao Xin blade back position soft stud print point.
Step 2, determine leaf basin, blade back soft stud geometry.
Centered by some Q1, Q2, Q3, Y-axis is that axis makees Φ 4mm cylinder respectively, utilizes Tao Xin leaf basin profile With wax molds profile, cylinder is carried out cutting, i.e. can get leaf basin soft stud geometry.With some Q4, Q5, Q6 Centered by, Y-axis is that axis makees Φ 4mm cylinder respectively, utilizes Tao Xin blade back profile and wax molds profile to cylinder Carry out cutting, i.e. can get blade back soft stud geometry.
Step 3, analyze soft stud material, select Digit Control Machine Tool, fixture, cutter, technological parameter.
According to practical situation, soft stud material is essence casting wax material, has less coefficient of thermal expansion and shrinkage factor, higher Thermostability;According to Tao Xin size, soft stud is set as the cylinder of Φ 4mm;
In the present embodiment, soft stud is parallel with Tao Xin Y-axis, in conjunction with Tao Xin overall structure, selects: lathe is three-axis numerical control Lathe, according to soft stud diameter, determines that tool diameter≤1mm, selection cutter are carbide-tipped milling cutter, its cutter ball Head radius is 0.5mm.
Prepared by step 4, soft stud blank.
Specifically comprise the following steps that
(1) use neutral detergent to add water cleanings, get rid of wicking surface oil film of making pottery;
(2) dewaxing: selected soft stud wax material is passed through in beaker heating in water bath, controls wax liquid temperature and be less than 100℃;
(3) waxing: Wax-coated liquid near soft stud position, its size should be greater than soft stud size, in case numerical control adds Spare time measures.
Step 5, soft stud digital control processing.
Utilize common CAD/CAM software to be programmed, and Path is carried out simulating, verifying.Add what man-hour selected Lathe is: VMC-850, and the cutter of selection is: hard alloy bulb milling cutter, and lathe selection of speed is 1300r/min, Feed speed is 800mm/min.

Claims (1)

1. a turbo blade Tao Xin soft stud processing method, it is characterised in that comprise the following steps:
Step 1, determine leaf basin, blade back soft stud position;
Tao Xin blade segment length is 75mm, and print point cross section I and cross section II height are respectively the 1/3 and 2/3 of blade, Section line is projected to XZ plane, obtains cross section I and cross section II;Cross section I is along the intersection of Y-direction Yu Tao Xin leaf basin Trisection, obtains a Q1、Q2, halve along the intersection of Y-direction with Tao Xin leaf basin, obtain a Q in cross section II3, point Q1、Q2、Q3It is Tao Xin leaf pelvic part position soft stud print point;Cross section I is along the intersection three of Y direction Yu Tao Xin blade back Decile, obtains a Q4、Q5, halve along the intersection of Y direction with Tao Xin blade back, obtain a Q in cross section II6, point Q4、Q5、Q6It is Tao Xin blade back position soft stud print point;
Step 2, determine leaf basin, blade back soft stud geometry;
Centered by some Q1, Q2, Q3, Y-axis is that axis makees Φ 4mm cylinder respectively, utilizes Tao Xin leaf basin profile With wax molds profile, cylinder is carried out cutting, obtain leaf basin soft stud geometry;In with some Q4, Q5, Q6 being The heart, Y-axis is that axis makees Φ 4mm cylinder respectively, utilizes Tao Xin blade back profile to carry out cylinder with wax molds profile Cutting, obtains blade back soft stud geometry;
Step 3, analyze soft stud material, select Digit Control Machine Tool, fixture, cutter, technological parameter;
Soft stud material is essence casting wax material, has less coefficient of thermal expansion and shrinkage factor, higher thermostability;According to Tao Xin size, soft stud is set as the cylinder of Φ 4mm;
Soft stud is parallel with Tao Xin Y-axis, in conjunction with Tao Xin overall structure, selects: lathe is three axis numerically controlled machine, according to Soft stud diameter, determines that tool diameter≤1mm, selection cutter are carbide-tipped milling cutter, and its cutter Probe-radius is 0.5mm;
Prepared by step 4, soft stud blank;
Use neutral detergent to add water cleanings, get rid of wicking surface oil film of making pottery;Selected soft stud wax material is passed through water Bath heating, controls wax liquid temperature less than 100 DEG C;Wax-coated liquid near soft stud position, Wax-coated liquid size is big In soft stud size, in case digital control processing surplus;
Step 5, soft stud digital control processing;
Utilize common CAD/CAM software to be programmed, and Path is carried out simulating, verifying;Add what man-hour selected Lathe is: VMC-850, and the cutter of selection is: hard alloy bulb milling cutter, and lathe selection of speed is 1300r/min, Feed speed is 800mm/min.
CN201610374616.4A 2016-05-31 2016-05-31 The soft stud processing methods of turbo blade Tao Xin Expired - Fee Related CN106002112B (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106777561A (en) * 2016-11-29 2017-05-31 朱金焰 A kind of layout method of turbo blade essence casting wax pattern Tao Xin clamping elements
CN107748827A (en) * 2017-11-09 2018-03-02 广东工业大学 Hollow cylindrical components processing method, system, equipment and storage medium
CN110405139A (en) * 2019-08-28 2019-11-05 贵州航天风华精密设备有限公司 A kind of investment casting method controlling aero-engine hollow blade wall thickness
CN111318641A (en) * 2020-04-09 2020-06-23 上海交通大学 Method for controlling offset size of water-soluble core wax mold of complex thin-wall hollow casting

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GB2111881A (en) * 1981-12-16 1983-07-13 Vickers Plc Investment casting process and mould
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CN102873275A (en) * 2012-09-28 2013-01-16 西安航空动力股份有限公司 Fixing method of isometric crystal and columnar crystal ceramic mold core in mold shell
CN103056313A (en) * 2013-01-05 2013-04-24 沈阳黎明航空发动机(集团)有限责任公司 Method for enhancing strength of single crystal blade core by metal core support
CN104399888A (en) * 2014-11-07 2015-03-11 沈阳黎明航空发动机(集团)有限责任公司 Investment casting method capable of controlling wall thickness of aero-engine hollow blade
CN104526856A (en) * 2014-12-31 2015-04-22 西安交通大学 Method for improving position accuracy of mold core of integrated type ceramic mold
CN104923722A (en) * 2015-06-24 2015-09-23 西安航空动力股份有限公司 Method for controlling hollow guide blade upper edge plate cavity wall thickness

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2111881A (en) * 1981-12-16 1983-07-13 Vickers Plc Investment casting process and mould
CN101695741A (en) * 2009-10-30 2010-04-21 沈阳黎明航空发动机(集团)有限责任公司 Method for positioning mold core and mold shell of hollow blade
CN102873275A (en) * 2012-09-28 2013-01-16 西安航空动力股份有限公司 Fixing method of isometric crystal and columnar crystal ceramic mold core in mold shell
CN103056313A (en) * 2013-01-05 2013-04-24 沈阳黎明航空发动机(集团)有限责任公司 Method for enhancing strength of single crystal blade core by metal core support
CN104399888A (en) * 2014-11-07 2015-03-11 沈阳黎明航空发动机(集团)有限责任公司 Investment casting method capable of controlling wall thickness of aero-engine hollow blade
CN104526856A (en) * 2014-12-31 2015-04-22 西安交通大学 Method for improving position accuracy of mold core of integrated type ceramic mold
CN104923722A (en) * 2015-06-24 2015-09-23 西安航空动力股份有限公司 Method for controlling hollow guide blade upper edge plate cavity wall thickness

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106777561A (en) * 2016-11-29 2017-05-31 朱金焰 A kind of layout method of turbo blade essence casting wax pattern Tao Xin clamping elements
CN107748827A (en) * 2017-11-09 2018-03-02 广东工业大学 Hollow cylindrical components processing method, system, equipment and storage medium
CN110405139A (en) * 2019-08-28 2019-11-05 贵州航天风华精密设备有限公司 A kind of investment casting method controlling aero-engine hollow blade wall thickness
CN111318641A (en) * 2020-04-09 2020-06-23 上海交通大学 Method for controlling offset size of water-soluble core wax mold of complex thin-wall hollow casting

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