CN102145402B - One-time clamping four-shaft linkage rotary milling molding method for numerical control blade roots - Google Patents

One-time clamping four-shaft linkage rotary milling molding method for numerical control blade roots Download PDF

Info

Publication number
CN102145402B
CN102145402B CN 201010551545 CN201010551545A CN102145402B CN 102145402 B CN102145402 B CN 102145402B CN 201010551545 CN201010551545 CN 201010551545 CN 201010551545 A CN201010551545 A CN 201010551545A CN 102145402 B CN102145402 B CN 102145402B
Authority
CN
China
Prior art keywords
processing
cutter
blade root
blade
horizontal
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
CN 201010551545
Other languages
Chinese (zh)
Other versions
CN102145402A (en
Inventor
杨敏
陆爱群
占伟辉
侯光耀
杨兆军
滕树新
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.)
Wuxi Turbine Blade Co Ltd
Original Assignee
Wuxi Turbine Blade 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 Wuxi Turbine Blade Co Ltd filed Critical Wuxi Turbine Blade Co Ltd
Priority to CN 201010551545 priority Critical patent/CN102145402B/en
Publication of CN102145402A publication Critical patent/CN102145402A/en
Application granted granted Critical
Publication of CN102145402B publication Critical patent/CN102145402B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Abstract

The invention provides a one-time clamping four-shaft linkage rotary milling molding method for numerical control blade roots. The method can effectively reduce the field debugging workload of workers and improve the processing efficiency; and a blade root molding cutter is not needed, so that the cutter loss is reduced and the processing cost is reduced. A four-shaft horizontal processing centeris adopted, and the blade root profile processing cutter is a big spiral angle dense teeth milling cutter. The method comprises the following processing steps of: (1) setting a processing programmingorigin in a blade root UG model of a gas compressor; (2) calculating cutter loci of each plane and each curved surface of blade roots according to the processing programming origin, and generating a cutter location file; (3) measuring the position of the processing programming origin relative to the rotary center of a horizontal lathe on site, and obtaining values of X axis and Z axis between thetwo points; and (4) inputting the X-axis and Z-axis values of the on-site measured processing programming center origin relative to the rotary center of the horizontal lathe to the software of a horizontal rotary milling program conversion system, calculating an NC code file of the rotating cutter locus relative to the lathe, and performing profile processing of the blade roots of the gas compressor.

Description

The four-axle linked revolution milling of the disposable clamping of a kind of numerical control blade blade root forming method
Technical field
The present invention relates to blade digital control processing method technical field, be specially the four-axle linked revolution milling of the disposable clamping of a kind of numerical control blade blade root forming method.
Background technology
Machining center is efficient, high-precision numerical control machine, four horizontal Machining centers have tool magazine, and it can exchange process tool automatically, and workbench is numerical control turntable, in clamping of workpiece, can realize the processing of a plurality of machined surfaces by automatic tool changer, workbench rotation.General four horizontal Machining centers are mainly processed blade root and the length overall of blade, frock clamp is placed on the inconsistent (see figure 1) in position on the workbench at every turn in reality processing, and the numerical control program center 1 of establishment does not overlap with the centre of gyration 2 of workbench 3, generally can only combine with the setting of B axle commentaries on classics 0,90,180,270 angles and work coordinate system and adjust the processing of finishing product, 4 is the workbench end face among Fig. 1, and 5 is the root center line.The blade root of compressor blade is the dovetail header structure, it is interior, back of the body working face is not parallel, be an angle, can reduce workman's field adjustable workload though adopt blade root moulding cutter (see figure 2) directly to process the blade root profile, accomplish disposable clamping processing, but the work in-process tool wear is big, the processing cost height, the surface roughness of blade root is relatively poor.For improving the working face precision, adopt the close tooth milling cutter of large helix angle φ 32(end face mill R, Fig. 3) finish-milling working face, workpiece needs anglec of rotation processing when finish-milling, though lathe can arbitrarily angledly rotate, but because the blade programming initial point that is contained in the anchor clamps does not overlap with the centre of gyration of lathe, there is a deviate, and the position of each clamping tool is also different, the a collection of blade of every processing, deviate just changes once, and because the existence of deviate, actual Working position just with numerical control program in cutter rail coordinate points inconsistent, make that the workman need do a large amount of field adjustables before processing, working (machining) efficiency is low, and the blade root profile quality of processing also can not get guaranteeing that 6 is the square chest end face, 7 are the programming initial point, 8 is the root center line.
Summary of the invention
At the problems referred to above, the invention provides the four-axle linked revolution milling of the disposable clamping of a kind of numerical control blade blade root forming method, it can effectively reduce workman's field adjustable workload, improves working (machining) efficiency; Do not need to adopt blade root moulding cutter, thereby reduce the cutter loss, cut down finished cost.
Its technical scheme is such, and it adopts four horizontal Machining centers, and blade root profile process tool adopts the close tooth milling cutter of large helix angle, and it is characterized in that: it comprises following procedure of processing:
1, in compressor blade blade root UG model, the machining prgraming initial point is set;
2, calculate the cutter path of each plane of blade root and curved surface according to described machining prgraming initial point, and generate cutter location file (* .cls);
3, workman's in-site measurement machining prgraming center origin draws the X-axis between 2, the value of Z axle with respect to the position of the horizontal machine tool centre of gyration;
4, the machining prgraming center origin of described in-site measurement is imported horizontal revolving with respect to X-axis, the Z axle value of the horizontal machine tool centre of gyration and mill program conversion system software, calculated with respect to the cutter path NC code file in the machine tool rotary by software, carry out the profile processing of compressor blade blade root.
It is further characterized in that: when there is B axle zero drift phenomenon in lathe, in compressor blade blade root UG model the B deviate is set.
The four-axle linked revolution milling of the disposable clamping of a kind of numerical control blade blade root of the present invention forming method, it adopts the close tooth milling cutter of large helix angle to carry out the profile processing of blade root, it can effectively reduce the debugging work load that the scene adds man-hour, improves working (machining) efficiency greatly, and guarantees the blade processing quality.
Description of drawings
Fig. 1 is positioned over position view on the workbench for frock clamp in the actual processing;
Fig. 2 is for processing the blade root schematic diagram with blade root moulding cutter;
Fig. 3 is for adopting the close tooth milling cutter processing of large helix angle blade root schematic diagram;
Fig. 4 is for using the inventive method processing blade root profile process chart.
The specific embodiment
See Fig. 3, Fig. 4, processing method of the present invention, four horizontal Machining centers are adopted in its blade root processing, and it is blade root circular arc finish-milling cutter that cutter adopts the close tooth milling cutter 9,10 of large helix angle, and it comprises the following procedure of processing of the heart:
1, in compressor blade blade root UG model, the machining prgraming initial point is set;
2, calculate the cutter path of each plane of blade root and curved surface according to described machining prgraming initial point, and generate cutter location file (* .cls);
3, workman's in-site measurement machining prgraming center origin draws the X-axis between 2, the value of Z axle with respect to the position of the horizontal machine tool centre of gyration;
4, the machining prgraming center origin of described in-site measurement is imported horizontal revolving with respect to X-axis, the Z axle value of the horizontal machine tool centre of gyration and mill program conversion system software, calculated with respect to the cutter path NC code file in the machine tool rotary by software, be transported in the corresponding horizontal machine tool, carry out the profile processing of compressor blade blade root.

Claims (1)

1. the four-axle linked revolution milling of the disposable clamping of numerical control blade blade root forming method, it adopts four horizontal Machining centers, and blade root profile process tool adopts the close tooth milling cutter of large helix angle, and it is characterized in that: it comprises following procedure of processing:
⑴ arrange the machining prgraming initial point in compressor blade blade root UG model;
⑵ calculate the cutter path of each plane of blade root and curved surface according to described machining prgraming initial point, and generate cutter location file (* .cls);
⑶ workman's in-site measurement machining prgraming initial point draws the X-axis between 2, the value of Z axle with respect to the position of the horizontal machine tool centre of gyration;
⑷ import horizontal revolving with the machining prgraming initial point of described in-site measurement with respect to X-axis, the Z axle value of the horizontal machine tool centre of gyration and mill program conversion system software, calculated with respect to the cutter path NC code file in the machine tool rotary by software, carry out the profile processing of compressor blade blade root; When there is B axle zero drift phenomenon in lathe, in compressor blade blade root UG model, the B deviate is set.
CN 201010551545 2010-11-20 2010-11-20 One-time clamping four-shaft linkage rotary milling molding method for numerical control blade roots Active CN102145402B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201010551545 CN102145402B (en) 2010-11-20 2010-11-20 One-time clamping four-shaft linkage rotary milling molding method for numerical control blade roots

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201010551545 CN102145402B (en) 2010-11-20 2010-11-20 One-time clamping four-shaft linkage rotary milling molding method for numerical control blade roots

Publications (2)

Publication Number Publication Date
CN102145402A CN102145402A (en) 2011-08-10
CN102145402B true CN102145402B (en) 2013-09-04

Family

ID=44419991

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201010551545 Active CN102145402B (en) 2010-11-20 2010-11-20 One-time clamping four-shaft linkage rotary milling molding method for numerical control blade roots

Country Status (1)

Country Link
CN (1) CN102145402B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104057129A (en) * 2014-07-11 2014-09-24 二重集团(德阳)重型装备股份有限公司 Method for finely processing and milling large helical surface
CN107570807A (en) * 2017-10-12 2018-01-12 无锡透平叶片有限公司 It is a kind of to replace the method for rough milling shaping tooth form knife rough milling blade root tenon tooth
CN109434470A (en) * 2018-11-29 2019-03-08 伯恩高新科技(惠州)有限公司 A kind of process equipment and method of fan blade
CN113319340B (en) * 2021-06-03 2022-08-02 南通中能机械制造有限公司 Machining process for milling mushroom-shaped blade root by using horizontal machining center

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR960704667A (en) * 1993-09-29 1996-10-09 디터 클리스트·게르하르트 퀼 PROCESS FOR MILLING A TURBINE BLADE SECTION EXTENDING ALONG MAIN AXIS
CN101066570B (en) * 2007-05-18 2012-01-04 云南大为化工装备制造有限公司 Numerically controlled process of cutting spatial curved surface for inserting inclined pipe to barrel
CN100548549C (en) * 2008-03-26 2009-10-14 西北工业大学 Multiple curved faces island five-axis helical method for processing

Also Published As

Publication number Publication date
CN102145402A (en) 2011-08-10

Similar Documents

Publication Publication Date Title
CN102773503B (en) Single point diamond lathe and method for machining special-shape workpiece
CN102962654B (en) Processing method for no-crown guide blade of steam turbine
CN102145402B (en) One-time clamping four-shaft linkage rotary milling molding method for numerical control blade roots
CN106625153A (en) Blade grinding robot workstation and blade grinding method
CN106270812B (en) A kind of method of lathe in machining helical surface of enveloping worm
CN101710236B (en) Numerical-control processing method of multi-space hole welding groove on large-scale spherical space curved surface
CN1613590A (en) Method and apparatus for turbine blades milling with once clamping
CN112719379B (en) Milling method for multiple composite inclined planes of square pipe
CN101412129B (en) Computing formula for processing rocker shaft eccentric toothed sector of numerical control gear shaping machine and processing method
CN103592888A (en) Post-processing method for domestic double pendulum head five shaft machine tool
CN102629120B (en) Nonlinear error processing method for using angle head toolholder to carry out numerical control processing
CN109434219A (en) A kind of four axis side edge mill teeth methods
CN108919749B (en) Method for realizing coordinate origin tracking in five-axis machine tool without tool position origin tracking
CN102147601A (en) Machining method for online measurement and compensation of high-precision blade
CN111761406B (en) Rapid clamping method for workpiece respective degree step-by-step alignment based on-machine measurement
CN108237374B (en) Three-axis linkage machining method for curved surface of multi-blade rotating wheel
CN205111454U (en) Novel digit control machine tool trajectory control system
CN106862628A (en) Main shaft of numerical control machine tool orientation self-control slotting tool is to right angle processing method in die cavity
CN102147221A (en) Three-coordinate measuring method of blade with T-shaped root
CN101633126B (en) Configuration method of clamping tool suitable to machine tool for processing complicated workpiece
CN202963469U (en) SPDT (simple point diamond turning)
CN112439951B (en) Gear chamfering and milling method based on geometric adaptive compensation
Lingli et al. Research and Development of Fungus-Shaped Blade Root CAM Software Based on VB
CN207239671U (en) Steel construction joint ball Five-axis NC Machining Center
CN102079059B (en) Method for realizing curved surface machining by means of track of closed controllable space mechanism connecting rod

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C53 Correction of patent for invention or patent application
CB02 Change of applicant information

Address after: 214174 Huishan Road, Huishan Economic Development Zone, Jiangsu, No. 1800, No.

Applicant after: Wuxi Turbine Blade Co., Ltd.

Address before: Nanchang District 214023 in Jiangsu province Wuxi City Qingyang Road No. 305

Applicant before: Wuxi Turbine Blade Co., Ltd.

C14 Grant of patent or utility model
GR01 Patent grant