CN106475611B - A kind of automatic compensation processing method of annular web class casting - Google Patents

A kind of automatic compensation processing method of annular web class casting Download PDF

Info

Publication number
CN106475611B
CN106475611B CN201611033813.6A CN201611033813A CN106475611B CN 106475611 B CN106475611 B CN 106475611B CN 201611033813 A CN201611033813 A CN 201611033813A CN 106475611 B CN106475611 B CN 106475611B
Authority
CN
China
Prior art keywords
support plate
center line
center
theoretical
difference
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.)
Active
Application number
CN201611033813.6A
Other languages
Chinese (zh)
Other versions
CN106475611A (en
Inventor
周代忠
郝卓
王传滨
杨轶博
马良
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.)
AECC Shenyang Liming Aero Engine Co Ltd
Original Assignee
Shenyang Liming Aero Engine Group Co Ltd
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 Liming Aero Engine Group Co Ltd filed Critical Shenyang Liming Aero Engine Group Co Ltd
Priority to CN201611033813.6A priority Critical patent/CN106475611B/en
Publication of CN106475611A publication Critical patent/CN106475611A/en
Application granted granted Critical
Publication of CN106475611B publication Critical patent/CN106475611B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23QDETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
    • B23Q23/00Arrangements for compensating for irregularities or wear, e.g. of ways, of setting mechanisms

Abstract

A kind of automatic compensation processing method of annular web class casting, belongs to Computerized Numerical Control processing technology field.Including:Part rotation center is overlapped with table core, if a pair of of support plate center line and workbench fixing axle X or theory Z angle are a;By part rotated counterclockwise by angle a, keep support plate center line parallel with fixing axle X or Z, obtains support plate center line to part rotation center theory vertical range b;Two sections are selected, angle difference a1 between support plate actual center line and theoretical centerline is calculated;According to a1 rotary tables, support plate angle is corrected;Third section is selected, obtains correcting rear carrier plate center line, obtains and corrects rear carrier plate center line to part rotation center vertical range b1;The difference of b1 and b is assigned to the general global variable parameter of lathe by the b1 for determining each pair of support plate;Nc program gets up processing dimension and b1 global variable parameter associations corresponding with the difference of b, when processing, the global variable parameter is called to realize automatic compensation processing.

Description

A kind of automatic compensation processing method of annular web class casting
Technical field
The invention belongs to Computerized Numerical Control processing technology field, the automatic compensation more particularly to a kind of annular web class casting is processed Method is suitable for the different NC systems such as CNC milling machine, Siemens, farad gram.
Background technology
In aero-engine field, there are some annular frame precision castings with dispersion shape spoke, these parts are inside and outside There are multiple support plates between ring, as shown in Figure 1, there is the boss face for needing to process and hole characteristic at two side position of support plate, There are the dimension relationship relationships of degree of precision for these boss processing back edge profile and support plate center line and outer surface.Due to this zero Part is that there are larger manufacturing tolerances for monoblock cast, support plate and inner and outer rings, and part Working position is caused to use digital control processing very Difficulty needs to be manually adjusted according to each part status, and processing efficiency is low, influences to realize automation batch machining.
Invention content
In view of the problems of the existing technology, the present invention provides a kind of annular web class promoting processing efficiency and quality The automatic compensation processing method of casting, the method achieve the automatic compensation of the unstable position of frame precision casting branch Board position to add Work.
To achieve the goals above, the present invention adopts the following technical scheme that:A kind of automatic compensation of annular web class casting Processing method includes the following steps:
Step 1:Part rotation center is kept overlapping with platen center, and is fixed by fixture, if part Theoretical angle between the support plate theoretical centerline of a pair of of support plate and the fixing axle X or Z of platen is a;
Step 2:By part rotated counterclockwise by angle a, make the support plate theoretical centerline of a pair of of support plate described in step 1 It is parallel with the fixing axle X or Z of platen, obtain the support plate theoretical centerline to support plate to part rotation center theory Vertical range b;
Step 3:This to selecting section different at two respectively close to machining area position on support plate, by surveying online The both sides for measuring section, obtain two respective virtual center points in section, while obtaining the respective theoretical center in described two sections Point;The virtual center point in two sections of connection obtains support plate actual center line, and the theoretical center point in two sections of connection is propped up Plate theory center line;By applying trigonometric function relationship, this is calculated to support plate machining area measuring point support plate practical center Angle difference a1 between line and support plate theoretical centerline;
Step 4:According in step 3 it is calculated this to support plate machining area measuring point support plate actual center line with branch Angle difference a1 between plate theory center line rotates platen, corrects the angle to support plate;
Step 5:Third section is selected between two sections described in step 3, passes through the on-line measurement section Both sides, obtain the virtual center point in the section, cross the virtual center point and do a straight line for being parallel to support plate theoretical centerline, The straight line is revised support plate center line, obtain revised support plate center line to part rotation center vertical range b1;
Step 6:The theoretical vertical range b of the support plate theoretical centerline of each pair of support plate to part rotation center be it is identical, The vertical range b1 of each pair of support plate revised support plate center line to part rotation center is different, using step 1 to step Method described in five determines the revised support plate center line of each pair of support plate to the vertical range b1 of part rotation center, and it is each right to obtain The difference of support plate b1 and b, and the difference is assigned to the general global variable parameter of lathe, interim storage successively;
Step 7:Nc program uses global variable programming mode, and processing dimension and b1 is corresponding with the difference of b Global variable parameter association gets up, when processing, call b1 global variable parameters corresponding with the difference of b realize automatic compensation plus Work ensures part actual processing demand.
Beneficial effects of the present invention:
It is unstable that the present invention solves such spray size, it is difficult to the problem of digital control processing.
It is proven:The processing method of the present invention is greatly improved in the outer mold surface processing of complicated casing part The processing efficiency of such part by numerical control lathe, eliminates the human intervention of process, reduces the stand-by period of lathe, convenient The arrangement of Workshop Production task.
Description of the drawings
Fig. 1 is a kind of structural schematic diagram of annular web class casting;
Fig. 2 is by the schematic diagram after part rotated counterclockwise by angle a shown in FIG. 1;
Fig. 3 is to select the schematic diagram of section and determining support plate actual center line and support plate theoretical centerline at two;
Fig. 4 is the angle difference calculated using trigonometric function relationship between support plate actual center line and support plate theoretical centerline The schematic diagram of a1;
Fig. 5 is the schematic diagram for selecting third section and determining revised support plate center line;
In figure:1-outer shroud, 2-inner ring, 3-support plates, 4-boss, 5-platen centers and part rotation center, 6-support plate actual center lines, 7-support plate theoretical centerlines, 8-revised support plate center lines.
Specific implementation mode
The present invention is described in further detail in the following with reference to the drawings and specific embodiments.
A kind of automatic compensation processing method of annular web class casting, includes the following steps:
Step 1:Part rotation center is kept overlapping with platen center, and is fixed by fixture, such as Fig. 1 institutes Show, if the theoretical angle between the support plate theoretical centerline of a pair of of support plate of part and the fixing axle X or Z of platen is a;
Step 2:By part rotated counterclockwise by angle a, make the support plate theoretical centerline of a pair of of support plate described in step 1 It is parallel with the fixing axle X or Z of platen, as shown in Fig. 2, showing that the support plate theoretical centerline to support plate is rotated to part The theoretical vertical range b at center, b values each support plate in actual parts is fixed;
Step 3:Section C-C and D-D different at two are selected respectively to close machining area position on support plate at this, led to The both sides for crossing on-line measurement section obtain the respective virtual center point C1 and D1 in two sections, while obtaining described two sections Respective theoretical center point C2 and D2;The virtual center point C1 and D1 in two sections of connection obtain support plate actual center line 6, connect The theoretical center point C2 and D2 in two sections obtains support plate theoretical centerline 7, as shown in Figure 3;By applying trigonometric function relationship, Calculate the angle difference between support plate machining area measuring point support plate actual center line 6 and support plate theoretical centerline 7 A1, as shown in Figure 4;
Tg a1=d/c
In formula, angles of the a1-between support plate machining area measuring point support plate actual center line and support plate theoretical centerline Difference, two sections d-are in the difference in height of vertical direction, two section differences in height in the horizontal direction of c-;
Step 4:According in step 3 it is calculated this to support plate machining area measuring point support plate actual center line 6 with Angle difference a1 between support plate theoretical centerline 7 rotates platen, corrects the angle to support plate;
Step 5:Third section E-E is selected between two sections C-C and D-D described in step 3, by online The both sides for measuring the section show that the virtual center point in the section, the excessively virtual center point are done one and be parallel in branch plate theory The straight line of heart line 7, the straight line are revised support plate center line 8, in showing that revised support plate center line 8 is rotated to part The vertical range b1 of the heart, as shown in Figure 5;
Step 6:The theoretical vertical range b of the support plate theoretical centerline of each pair of support plate to part rotation center be it is identical, The vertical range b1 of each pair of support plate revised support plate center line to part rotation center is different, using step 1 to step Method described in five determines the revised support plate center line of each pair of support plate to the vertical range b1 of part rotation center, and it is each right to obtain The difference of support plate b1 and b, and the difference is assigned to the general global variable parameter of lathe successively (the R series of such as Siemens becomes Amount), interim storage;
Step 7:These unstable sizes of numerically controlled machining programme ordered pair use global variable programming mode, by processing dimension And b1 global variable parameter associations corresponding with the difference of b get up, and when processing, call b1 global variables corresponding with the difference of b Parameter realizes automatic compensation processing, ensures part actual processing demand.

Claims (1)

1. a kind of automatic compensation processing method of annular web class casting, which is characterized in that include the following steps:
Step 1:Part rotation center is kept overlapping with platen center, and is fixed by fixture, if a pair of part Theoretical angle between the support plate theoretical centerline of support plate and the fixing axle X or Z of platen is a;
Step 2:By part rotated counterclockwise by angle a, make the support plate theoretical centerline and machine of a pair of of support plate described in step 1 The fixing axle X or Z of bed workbench are parallel, obtain the support plate theoretical centerline to support plate to part rotation center it is theoretical vertically Distance b;
Step 3:Section different at two is selected respectively to close machining area position on support plate at this, passes through on-line measurement and cuts The both sides in face obtain two respective virtual center points in section, while obtaining the respective theoretical center point in described two sections;Even The virtual center point for connecing two sections obtains support plate actual center line, and the theoretical center point in two sections of connection obtains branch plate theory Center line;By applying trigonometric function relationship, this is calculated to support plate machining area measuring point support plate actual center line and branch Angle difference a1 between plate theory center line;
Step 4:According in step 3 it is calculated this to support plate machining area measuring point support plate actual center line and branch foliation By the angle difference a1 between center line, platen is rotated, the angle to support plate is corrected;
Step 5:Third section is selected between two sections described in step 3, passes through the two of the on-line measurement section Side obtains the virtual center point in the section, crosses the virtual center point and does a straight line for being parallel to support plate theoretical centerline, this is straight Line is revised support plate center line, obtain revised support plate center line to part rotation center vertical range b1;
Step 6:The theoretical vertical range b of the support plate theoretical centerline of each pair of support plate to part rotation center be it is identical, it is each right The vertical range b1 of support plate revised support plate center line to part rotation center is different, using step 1 to step 5 institute The method stated determines that the revised support plate center line of each pair of support plate to the vertical range b1 of part rotation center, obtains each pair of support plate The difference of b1 and b, and the difference is assigned to the general global variable parameter of lathe, interim storage successively;
Step 7:Nc program uses global variable programming mode, by processing dimension and the b1 overall situations corresponding with the difference of b Variable parameter associates, and when processing, calls b1 global variable parameters corresponding with the difference of b to realize automatic compensation processing, protects Demonstrate,prove part actual processing demand.
CN201611033813.6A 2016-11-22 2016-11-22 A kind of automatic compensation processing method of annular web class casting Active CN106475611B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611033813.6A CN106475611B (en) 2016-11-22 2016-11-22 A kind of automatic compensation processing method of annular web class casting

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611033813.6A CN106475611B (en) 2016-11-22 2016-11-22 A kind of automatic compensation processing method of annular web class casting

Publications (2)

Publication Number Publication Date
CN106475611A CN106475611A (en) 2017-03-08
CN106475611B true CN106475611B (en) 2018-09-18

Family

ID=58274491

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611033813.6A Active CN106475611B (en) 2016-11-22 2016-11-22 A kind of automatic compensation processing method of annular web class casting

Country Status (1)

Country Link
CN (1) CN106475611B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111552232A (en) * 2020-04-03 2020-08-18 中国航发哈尔滨东安发动机有限公司 Single machine calculation-free automatic alignment processing method
CN111390252B (en) * 2020-04-24 2022-05-10 成都飞机工业(集团)有限责任公司 Machining method for high-precision lug set of aviation structural part
CN114061635A (en) * 2021-11-23 2022-02-18 黑龙江建龙钢铁有限公司 Position measuring method for substituting absolute value encoder

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008045444A3 (en) * 2006-10-10 2008-06-05 Novartis Ag Method of surface manufacture with an apex decentered from a spindle axis
JP4266791B2 (en) * 2003-11-28 2009-05-20 株式会社牧野フライス製作所 Machining method
CN102430765A (en) * 2011-10-28 2012-05-02 湖北三江航天险峰电子信息有限公司 Self-adaptive compensation method for detecting turning error of large part of rotary body
CN102794610A (en) * 2012-08-24 2012-11-28 沈阳黎明航空发动机(集团)有限责任公司 Method for processing thin wall welder cases of revolving body structures
CN102814512A (en) * 2012-08-24 2012-12-12 沈阳黎明航空发动机(集团)有限责任公司 On-line measuring method for radials profile of compressor disc-like part of engine
CN103586737A (en) * 2013-09-30 2014-02-19 沈阳黎明航空发动机(集团)有限责任公司 Compensation method for high-precision numerical-control milling for molded surfaces of blades
CN103729541A (en) * 2013-10-24 2014-04-16 沈阳黎明航空发动机(集团)有限责任公司 Method for determining machining position of rotation angle of precise rotary disc
CN105798705A (en) * 2014-12-30 2016-07-27 武汉重型机床集团有限公司 Machining compensation method for high-precision hole system of austenitic stainless steel plate part

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4266791B2 (en) * 2003-11-28 2009-05-20 株式会社牧野フライス製作所 Machining method
WO2008045444A3 (en) * 2006-10-10 2008-06-05 Novartis Ag Method of surface manufacture with an apex decentered from a spindle axis
CN102430765A (en) * 2011-10-28 2012-05-02 湖北三江航天险峰电子信息有限公司 Self-adaptive compensation method for detecting turning error of large part of rotary body
CN102794610A (en) * 2012-08-24 2012-11-28 沈阳黎明航空发动机(集团)有限责任公司 Method for processing thin wall welder cases of revolving body structures
CN102814512A (en) * 2012-08-24 2012-12-12 沈阳黎明航空发动机(集团)有限责任公司 On-line measuring method for radials profile of compressor disc-like part of engine
CN103586737A (en) * 2013-09-30 2014-02-19 沈阳黎明航空发动机(集团)有限责任公司 Compensation method for high-precision numerical-control milling for molded surfaces of blades
CN103729541A (en) * 2013-10-24 2014-04-16 沈阳黎明航空发动机(集团)有限责任公司 Method for determining machining position of rotation angle of precise rotary disc
CN105798705A (en) * 2014-12-30 2016-07-27 武汉重型机床集团有限公司 Machining compensation method for high-precision hole system of austenitic stainless steel plate part

Also Published As

Publication number Publication date
CN106475611A (en) 2017-03-08

Similar Documents

Publication Publication Date Title
CN106475611B (en) A kind of automatic compensation processing method of annular web class casting
JP5651345B2 (en) Method and apparatus for generating control data for controlling a tool on a machine tool comprising at least five axes
CN110899860B (en) Numerical control machining method for linear contact spiral bevel gear pair
CN104384586A (en) Method for processing integral impeller by using four-axis numerical-control milling machine
CN105033671A (en) Two-shaft numerical control device used for machining shoe molds
CN103659460B (en) The method that point of a knife follows processing is realized at four axle horizontal Machining centers
CN111266803B (en) Processing method of thin-wall special-shaped metal casting
CN103084854A (en) Numerical control machining tool and rotary work platform thereof
CN109648368B (en) Workpiece coordinate system setting method for eliminating rotation error of numerical control machining workbench
CN109079260B (en) Cylindrical gear eccentric positioning device and numerical control chamfering algorithm
CN203171257U (en) Numerical control machining tool and revolving table thereof
CN205324817U (en) A quick full -automatic numerical control groove cutting machine for processing of vertical multislot
CN101773983B (en) Method for manufacturing complex graphite core for titanium alloy castings
CN108788208B (en) Boring method for machining intersection angle box hole system
CN105423970B (en) A kind of localization method of casing support plate manufacture
CN104646764A (en) Machining method of inclination driving gear box body hole system
CN110238697A (en) A kind of presetting cutter method of three-axis numerical control milling
CN103111529A (en) Machining method of U-shaped sheet metal part resilience mould tire
CN103394974B (en) A kind of multistation processing method
CN103128517B (en) Processing technology of heat-resisting alloy steel ware double-open-mold glass mold
CN208051431U (en) Four axis finishing impression processing tool of mould for glass bottle inner cavity
CN105583474B (en) A kind of numerical control gear hobbing process control method for gear reparation
CN103949712A (en) Processing method for ensuring form and position tolerance during slotting of key grooves in holes
CN205394027U (en) Numerical control mechanism is moved to five quintuplets on L type
Suri et al. Development of Gear Hobbing Fixture Design for Reduction in Machine Setting Time

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
CP01 Change in the name or title of a patent holder
CP01 Change in the name or title of a patent holder

Address after: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6

Patentee after: Chinese Hangfa Shenyang Liming Aero engine limited liability company

Address before: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6

Patentee before: Liming Aeroplane Engine (Group) Co., Ltd., Shenyang City