CN115971798A

CN115971798A - Method and system for machining rotary workpiece, electronic device, and storage medium

Info

Publication number: CN115971798A
Application number: CN202211586739.6A
Authority: CN
Inventors: 涂彬; 朱适琛; 李桐超
Original assignee: Suzhou Qianji Intelligent Technology Co ltd
Current assignee: Suzhou Qianji Intelligent Technology Co ltd
Priority date: 2022-12-09
Filing date: 2022-12-09
Publication date: 2023-04-18

Abstract

The application provides a method, a system, an electronic device and a storage medium for processing a rotary workpiece, wherein the method comprises the following steps: s1: roughly turning the air inlet side of the blank to remove large allowance of the air inlet side, reserving a process table at the hub of the air inlet side of the blank, milling the hub of the air inlet side of the blank to form an angular groove, and taking the angular groove as an angular reference; s2: roughly turning the air outlet side of the blank to remove large allowance of the air outlet side, milling the blank based on the angular reference to form a blade, and finely turning the air outlet side of the blank; s3: finely turning the air inlet side of the blank; s4: and removing the process table to obtain the rotary workpiece. In the process of processing the blank into the first-stage blade disc with the shaft diameter, the processing procedures are greatly reduced through the turning and milling composite machine tool, rapid model change among multiple procedures is realized, the processing qualification rate is high, the efficiency is high, and the processing is easy.

Description

Method and system for machining rotary workpiece, electronic device, and storage medium

Technical Field

The present application relates to the field of machining of aircraft engines and rotary workpieces, and in particular, to a method and a system for machining a rotary workpiece, an electronic device, and a storage medium.

Background

An Aircraft engine (Aircraft engine) refers to an engine device that is mainly used to generate a pulling force or a pushing force to advance an Aircraft. With the continuous improvement of the performance requirements of the aero-engine, the processing difficulty of parts of the aero-engine is also continuously improved.

In an aircraft engine, a method for machining a partially rotating workpiece (for example, a first-stage bladed disc with a shaft diameter) has problems of many processes, long manufacturing cycle, machining deformation, and the like.

In view of the foregoing, the present application provides a method, system, electronic device and storage medium for machining a rotating-type workpiece to improve the above-mentioned deficiencies of the prior art.

Disclosure of Invention

The application aims to provide a method and a system for processing a rotary workpiece, electronic equipment and a storage medium, which greatly reduce processing procedures through a turning and milling composite machine tool in the process of processing a blank into a first-stage blade disc with an axis diameter, realize rapid model change among multiple procedures, and have the advantages of high processing qualification rate, high efficiency and easiness in processing.

The purpose of the application is realized by adopting the following technical scheme:

in a first aspect, the present application provides a method for processing a rotary workpiece, which is used for processing a blank into the rotary workpiece by using a turn-milling compound device, wherein the rotary workpiece is a first-stage bladed disk with a shaft diameter, and the method includes:

s1: roughly turning the air inlet side of the blank to remove large allowance of the air inlet side, reserving a process table at the hub of the air inlet side of the blank, milling the hub of the air inlet side of the blank to form an angular groove, and taking the angular groove as an angular reference;

s2: roughly turning the air outlet side of the blank to remove large allowance of the air outlet side, milling the blank based on the angular reference to form a blade, and finely turning the air outlet side of the blank;

s3: finely turning the air inlet side of the blank;

s4: and removing the process table to obtain the rotary workpiece.

The technical scheme has the beneficial effects that: in the process of processing a blank into a first-stage blade disc with a shaft diameter, the processing procedures are greatly reduced through a turning and milling composite machine tool, rapid model change among multiple procedures is realized, the processing qualification rate is high, the efficiency is high, and the processing is easy.

Briefly, the whole blank processing process is as follows: firstly, roughly turning an air inlet side and milling an angular groove, and reserving a process table at the hub of the air inlet side to facilitate subsequent positioning; then, milling an angular groove on the hub surface on the air inlet side to provide an angular reference for subsequent blade profile milling; then, roughly turning the gas outlet side, milling to form a blade, and then finely turning the gas outlet side; and finally, finely turning the air inlet side and removing the process table to obtain the rotary workpiece.

That is to say, the process can be fused into one to two steps of rough turning air inlet side and milling angle to the groove, and the process can be fused into one to the three steps of rough turning gas outlet side, leaf profile milling, finish turning gas outlet side, has reduced benchmark deviation and the time cost that blank clamping alignment many times caused, has avoided the error that artifical alignment brought effectively, has reduced alignment clamping time, promotes machining efficiency.

In some optional embodiments, the step S1 includes:

the auxiliary main shaft of the turning and milling composite machine tool is close to the end face of the air outlet side of the blank, and the outer circle of the blank is held tightly by three claws, so that the blank is clamped for the first time;

after the first clamping is finished, roughly turning the air inlet side of the blank to remove large allowance on the air inlet side and reserving a process table at the hub of the air inlet side of the blank;

and milling the hub surface on the air inlet side of the blank by using the B shaft of the turning and milling composite machine tool to form an angular groove, and taking the angular groove as an angular reference.

The technical scheme has the beneficial effects that: the auxiliary main shaft of the turn-milling combined machine tool can be used for supporting the end face of the air outlet side of the blank, and the turn-milling combined machining is carried out on the air inlet side of the blank in one machining procedure, so that the machining efficiency is improved.

In some optional embodiments, the step S2 includes:

moving the blank to a main shaft from a secondary main shaft of the turning and milling composite machine tool, supporting a hub surface on the air inlet side of the blank by using a chuck fixture arranged on the main shaft and clamping a shaft diameter circular surface of the blank, and arranging a key on a key groove of the main shaft for key positioning so as to realize secondary clamping of the blank;

after the second clamping is finished, roughly turning the air outlet side of the blank to remove the large allowance of the air outlet side to form an inner groove, and forming a process groove at the position of the inner groove;

milling the blank based on the angular reference to form a blade;

finely turning the air outlet side end face of the blank to form an air outlet side end face reference;

based on the reference of the air outlet side end face, roughly machining the inner hole of the blank and the process groove, and then finely machining the inner hole of the blank and the process groove;

and threading the inner hole of the blank.

The technical scheme has the beneficial effects that: the chuck clamp arranged on the main shaft of the turning and milling combined machine tool can be used for supporting the hub surface at the air inlet side of the blank, the air outlet side of the blank is subjected to turning and milling combined processing in one processing procedure, and the processing efficiency is improved.

In some optional embodiments, the step S3 includes:

moving the blank to an auxiliary main shaft from a main shaft of the turning and milling composite machine tool, and supporting the axial diameter end face of the blank by using a double-expansion clamp arranged on the auxiliary main shaft so as to expand the inner wall face of the blank and realize the third clamping of the blank;

after the third clamping is finished, finely turning the end face of the air inlet side of the blank to form a reference of the end face of the air inlet side;

and based on the air inlet side end face reference, roughly machining the angular groove and the excircle of the blank, and then finely machining the angular groove and the excircle of the blank.

The technical scheme has the beneficial effects that: the blank can be moved to the auxiliary main shaft from the main shaft of the turning and milling combined machine tool, the turning and milling combined machining is carried out on the air inlet side of the blank again, and the machining efficiency is improved.

In some optional embodiments, before step S1, the method further comprises:

detecting whether the blank meets a first preset condition or not, wherein the first preset condition comprises a first preset design condition and/or a first preset surface condition;

the step S1 includes:

and when the blank is detected to meet the first preset condition, roughly turning the air inlet side of the blank.

The technical scheme has the beneficial effects that: before rough turning is carried out on the inner cavity of the blank, indexes such as the size, the material grade, the hardness and the surface state of the blank can be checked, the matching of the indexes such as the size, the material grade and the hardness of the blank and design requirements is ensured (namely, a first preset design condition is met), and the surface of the blank has no defects such as cracks, impurities and residues (namely, the first preset surface condition is met).

In some optional embodiments, the rotating workpiece is a bladed disk, and after step S6 and before step S7, the method further includes:

performing first clamping repair treatment on the blank to remove burrs on the surface of the blank and polish the blade;

and polishing the blank by taking the process table as a positioning reference so as to remove the tool marks and the clamp repairing marks of the blank.

The technical scheme has the beneficial effects that: the gyration type work piece that this application was suitable for can be the blade disc, and the blade disc is aeroengine's important rotating parts, and the surface quality requirement of blade disc processing is higher, and generally speaking, the blade disc is the horizontal processing vestige that does not allow to appear in certain distance of trailing edge in the front, and blade body profile, runner face and blade root fillet need smooth and slick and sly switching.

Considering the higher surface quality requirement of the bladed disk, after the air inlet side is finely turned and before the process table is removed, the blank can be subjected to surface treatment in the following two stages, namely a first stage: removing burrs on the surface of the blank through primary clamping and repairing treatment, thereby polishing the blade; and a second stage: and polishing the blank by taking the process table as a positioning basis so as to remove the tool marks and the clamp repairing marks of the blank and smoothen the surface of the blade so as to meet the surface quality requirement.

In some alternative embodiments, the polishing process is performed by abrasive flow polishing.

The technical scheme has the beneficial effects that: abrasive flow polishing is an advanced surface processing technology and is mainly characterized in that viscoelastic fluid abrasive particles are utilized to achieve the purposes of removing inner cavity burrs, finely processing and polishing the inner surface and processing round corners, deburring, rounding and polishing of different regions (including regions difficult to enter) of a workpiece can be completed simultaneously and at one time, and the roughness of the processed surface can reach Ra0.01 micrometer.

Compared with the traditional polishing method, the abrasive flow polishing technology can utilize the fluidity of the abrasive medium to polish holes with complex structures and deeper cavities, and can select different abrasive media to polish workpieces according to the material and application requirements of the workpieces so as to obtain different polishing effects to meet the requirements of the workpieces.

In some optional embodiments, the step S7 includes:

turning the blank to remove the process platform;

and carrying out secondary clamping and repairing treatment on the blank to obtain the rotary workpiece.

The technical scheme has the beneficial effects that: the process table can be removed by turning, after the process table is removed, tool marks generated by turning are also required to be removed so as to ensure the surface quality requirement of the blade disc, and at the moment, the blank can be subjected to secondary clamping and repairing treatment, so that the tool marks of turning are removed, and the rotary workpiece (namely the blade disc) is obtained.

In some optional embodiments, after the step S7, the method further comprises:

detecting defects of the rotary workpiece to judge whether the rotary workpiece meets a second preset condition, wherein the second preset condition comprises a second preset design condition and/or a second preset surface condition;

when the rotary workpiece does not meet the second preset condition, detecting whether the rotary workpiece meets a preset grinding condition;

and when the rotary workpiece does not meet the preset coping conditions, the rotary workpiece is scrapped or recycled.

The technical scheme has the beneficial effects that: after the rotary workpiece is obtained through processing, the defect detection can be carried out on the rotary workpiece, and whether the rotary workpiece meets a second preset condition or not is judged. When the rotary workpiece does not meet the second preset condition, the workpiece is not directly determined to be a waste product, whether the workpiece meets the preset polishing condition is detected, the workpiece is determined to be the waste product only if the workpiece does not meet the second preset condition or the preset polishing condition, and the waste product is correspondingly scrapped or recycled.

Through setting up preset coping conditions, can recycle the gyration type work piece that partly can be coping again, and then reduced manufacturing cost, practiced thrift the expenditure of raw and other materials, it is just the benefit to change original passive saving into "saving", is more suitable for popularizing the processing method of this application in the assembly line of productivity enterprise.

In some optional embodiments, the method further comprises:

determining grinding equipment corresponding to the rotary workpiece based on the defect detection result of the rotary workpiece;

and when the rotary workpiece meets the preset grinding condition, the rotary workpiece is sent into the grinding equipment for grinding treatment.

The technical scheme has the beneficial effects that: according to different defect conditions of the workpiece, different grinding equipment can be configured to grind the workpiece, and the mode of adaptively configuring the grinding equipment according to the defect conditions can improve the grinding efficiency and success rate of the workpiece, so that the whole processing flow is accelerated.

In a second aspect, the present application provides a system for processing a rotary workpiece, which is used for processing a blank into the rotary workpiece by using a turning and milling composite apparatus, wherein the rotary workpiece is a first-stage bladed disk with a shaft diameter, and the system includes:

the rough turning module at the air inlet side is used for rough turning the air inlet side of the blank so as to remove large allowance at the air inlet side, reserving a process table at the hub of the air inlet side of the blank, milling the hub of the air inlet side of the blank so as to form an angular groove, and taking the angular groove as an angular reference;

the air outlet side machining module is used for roughly turning the air outlet side of the blank to remove large allowance of the air outlet side, milling the blank based on the angular reference to form a blade and finely turning the air outlet side of the blank;

the air inlet side finish turning module is used for finish turning the air inlet side of the blank;

and the process table removing module is used for removing the process table to obtain the rotary workpiece.

In some optional embodiments, the intake side rough turning module is configured to:

after the first clamping is finished, roughly turning the air inlet side of the blank to remove large allowance of the air inlet side and reserving a process table at the hub of the air inlet side of the blank;

In some optional embodiments, the gas exit side processing module is to:

moving the blank to a main shaft from a secondary main shaft of the turning and milling composite machine tool, supporting the hub surface on the air inlet side of the blank by using a chuck clamp arranged on the main shaft and clamping the shaft diameter circular surface of the blank, and arranging a key on a key groove of the main shaft for key positioning so as to realize secondary clamping on the blank;

after the second clamping is finished, roughly turning the air outlet side of the blank to remove large allowance of the air outlet side to form an inner groove, and forming a process groove at the inner groove;

milling the blank based on the angular reference to form a blade;

and threading the inner hole of the blank.

In some optional embodiments, the intake side finishing module is to:

In some optional embodiments, the system further comprises:

the blank detection module is used for detecting whether the blank meets a first preset condition, wherein the first preset condition comprises a first preset design condition and/or a first preset surface condition;

the air inlet side rough turning module is used for: and when the blank is detected to meet the first preset condition, roughly turning the air inlet side of the blank.

In some optional embodiments, the system further comprises:

the first clamping module is used for carrying out first clamping treatment on the blank so as to remove burrs on the surface of the blank and polish the blade;

and the polishing module is used for polishing the blank by taking the process table as a positioning reference so as to remove the tool mark and the clamp repairing mark of the blank.

In some optional embodiments, the process platen removal module comprises:

the process platform turning unit is used for turning the blank to remove the process platform;

and the second clamping unit is used for carrying out secondary clamping treatment on the blank so as to obtain the rotary workpiece.

In some optional embodiments, the system further comprises:

the workpiece detection module is used for detecting defects of the rotary workpiece to judge whether the rotary workpiece meets a second preset condition, wherein the second preset condition comprises a second preset design condition and/or a second preset surface condition;

the grinding detection module is used for detecting whether the rotary workpiece meets the preset grinding condition or not when the rotary workpiece does not meet the second preset condition;

and the scrapping and recycling module is used for scrapping or recycling the rotary workpiece when the rotary workpiece does not meet the preset coping condition.

In some optional embodiments, the system further comprises:

the device configuration module is used for determining grinding devices corresponding to the rotary workpieces based on the defect detection results of the rotary workpieces;

and the workpiece grinding module is used for sending the rotary workpiece into the grinding equipment for grinding when the rotary workpiece meets the preset grinding condition.

In a third aspect, the present application provides an electronic device comprising a memory and at least one processor, the memory storing a computer program, the at least one processor implementing the steps of any of the above methods when executing the computer program.

In a fourth aspect, the present application provides a computer readable storage medium having stored thereon a computer program which, when executed by a processor, carries out the steps of any of the methods described above.

Drawings

The present application is further described below with reference to the drawings and embodiments.

Fig. 1 is a schematic flow chart of a machining method for a rotary workpiece according to an embodiment of the present disclosure.

Fig. 2 is a schematic structural diagram of a blank provided in an embodiment of the present application.

Fig. 3 is a schematic structural diagram of a rough turning blank on the air intake side according to an embodiment of the present application.

Fig. 4 is a schematic structural diagram of a blank after angular groove milling according to an embodiment of the present application.

Fig. 5 is a schematic view illustrating clamping of a blank according to an embodiment of the present disclosure.

Fig. 6 is a schematic structural diagram of a rough turning blank on the air outlet side according to an embodiment of the present application.

Fig. 7 is a schematic structural diagram of a blank after a blade profile is milled according to an embodiment of the present application.

Fig. 8 is a schematic structural diagram of a blank after finish turning of the air outlet side according to an embodiment of the present application.

Fig. 9 is a schematic view of another blank clamping provided in the embodiment of the present application.

Fig. 10 is a schematic structural diagram of a double-expansion clamp provided in an embodiment of the present application.

Fig. 11 is a schematic structural diagram of a blank after finish turning of an air intake side according to an embodiment of the present application.

Fig. 12 is a schematic structural diagram of a machining system for a rotary workpiece according to an embodiment of the present disclosure.

Fig. 13 is a block diagram of an electronic device according to an embodiment of the present application.

Fig. 14 is a schematic structural diagram of a program product provided in an embodiment of the present application.

Detailed Description

The technical solutions in the present application will be described below with reference to the drawings and the detailed description of the present application, and it should be noted that, in the present application, new embodiments can be formed by any combination of the following described embodiments or technical features without conflict.

In the present application, "at least one" means one or more, "a plurality" means two or more. "and/or" describes the association relationship of the associated object, indicating that there may be three relationships, for example, a and/or B, which may indicate: a exists alone, A and B exist simultaneously, and B exists alone, wherein A and B can be singular or plural. The character "/" generally indicates that the former and latter associated objects are in an "or" relationship. "at least one of the following" or similar expressions refer to any combination of these items, including any combination of the singular or plural items. For example, at least one (one) of a, b, or c, may represent: a, b, c, a and b, a and c, b and c, a and b and c, wherein a, b and c can be single or multiple. It is to be noted that "at least one item" may also be interpreted as "one or more items".

It is also noted that the terms "exemplary" or "such as" and the like are used herein to mean serving as an example, instance, or illustration. Any embodiment or design described herein as "exemplary" or "e.g.," is not necessarily to be construed as preferred or advantageous over other embodiments or designs. Rather, use of the word "exemplary" or "such as" is intended to present concepts related in a concrete fashion.

First, one of the application fields (aero-engine) of the embodiment of the present application will be briefly described below.

An Aircraft engine (Aircraft engine) refers to an engine device that is used primarily to generate a pulling or pushing force to advance an Aircraft. Besides generating forward force, the device can also provide electric power for electric equipment on the airplane and provide air source for air-using equipment such as air conditioning equipment. Generally, the design is relatively light due to flight requirements, but the design requires a relatively high use efficiency and a very low failure rate, so the process requirements for designing and producing the aircraft are relatively high. The main performance indexes of the aircraft engine include fuel consumption rate, thrust-weight ratio and the like. Air-dependent engines include piston engines, aero gas turbines, ramjet engines, detonation engines, and the like, wherein aero gas turbines include turbojet engines, turbofan engines, turboprop engines, paddle fan engines, turboshaft engines, and the like.

The blade disc is a novel structural member designed for meeting the requirements of high-performance aeroengines, and the blade disc integrates engine rotor blades and a wheel disc, so that tenons, mortises, locking devices and the like in the traditional connection are omitted, the structural weight and the number of workpieces are reduced, the tenon airflow loss is avoided, the pneumatic efficiency is improved, the engine structure is greatly simplified, and the blade disc is widely applied to military and civil aeroengines in various countries.

With the continuous improvement of the performance requirements of the aero-engine, the processing difficulty of parts of the aero-engine is also continuously improved. The existing machining method for the first-stage bladed disk with the shaft diameter has the technical problems of multiple working procedures, long manufacturing period, machining deformation and the like.

Method embodiment

A method, a system, an electronic device and a storage medium for machining a rotary workpiece are provided to reduce machining processes, achieve rapid prototyping among multiple processes, and achieve high machining yield, high efficiency and easy machining.

Fig. 1 is a schematic flow chart of a method for processing a rotary workpiece according to an embodiment of the present disclosure.

The method is used for processing a blank into a rotary workpiece by using turning and milling composite equipment, wherein the rotary workpiece is a first-stage blade disc with a shaft diameter, and the method comprises the steps of S1-S4.

S1: roughly turning the air inlet side of the blank to remove large allowance of the air inlet side, reserving a process table at the hub of the air inlet side of the blank, milling the hub of the air inlet side of the blank to form an angular groove, and taking the angular groove as an angular reference.

The blank is a raw material which is not processed yet, can also refer to a part before the finished product is finished, and can be a casting part, a forging part or a material obtained by sawing, gas cutting and the like, such as blank ceramics and the like. In the embodiment of the present application, the blank refers to a blank of a rotary body (for example, an alloy material may be used) for machining a rotary workpiece, a product obtained after performing all machining processes on the blank is referred to as a rotary workpiece (for example, a blade disc), and the names of the "blank" and the "rotary workpiece" are used only for distinguishing the states of the workpiece before and after machining, and the blank gradually approaches the final shape of the rotary workpiece during machining. Of course, the initial blank may be referred to as a "blank", and the intermediate product in the machining process and the final product obtained by the final machining may be referred to as a "rotary workpiece", which is not limited in the embodiments of the present application.

Referring to fig. 2 and fig. 3, fig. 2 is a schematic structural diagram of a blank provided in an embodiment of the present application, and fig. 3 is a schematic structural diagram of a blank after rough turning of an air intake side provided in an embodiment of the present application, where the blank in the embodiment of the present application may be a blank of a rotary body.

In the present application, the chain line in fig. 2, 3, 4, 6, 7, 8, 11 indicates the axis of rotation of the blank, and the thick solid line in fig. 3, 4, 6, 7, 8, 11 indicates the workpiece processing line.

The embodiment of the application does not limit the processing equipment adopted in the processing process, and the processing equipment can be a five-axis processing center or a turning and milling composite machine tool.

Five-axis machining centers combine high speed and high rigidity, with multi-faceted machining capabilities that allow complex workpieces to be machined in a single setup. The five axes of a five-axis machining center generally refer to the ability of a numerically controlled machine tool to move a workpiece or tool on five different CN C axes simultaneously. Wherein standard 3-axis milling is performed on the X, Y and Z axes. These three linear axes are directions in which the spindle or the workpiece can move, and the five-axis machining center also uses two rotation axes out of the following three axes: axis a, axis B and axis C. An A axis: rotation about X-axis, B-axis: rotation around the Y-axis, C-axis: rotating around the Z-axis.

A turning and milling combined machine tool (also called a turning and milling combined machining center) is a machine tool capable of turning and milling, and can complete all or most of machining of a workpiece on the turning and milling combined machine tool, so that the turning and milling combined machine tool is also called a small-sized production line. The machine tool not only can improve the precision of products and the efficiency of processing the products, but also greatly saves the occupied area of the machine tool for enterprises, and only one machine tool is needed to complete the processing of one workpiece in the past. Such machines can also be classified into vertical milling and turning combined and horizontal milling and turning combined machines.

Generally speaking, a five-axis machining center can only perform milling but not turning, so that there are many limitations in machining. That is to say, the turning and milling combined machine tool can cover the processing function of the five-axis machining center, but the five-axis machining center cannot perform the turning and milling combined processing.

Compared with the conventional numerical control machining process, the turning and milling composite machining has the following outstanding advantages:

(1) The manufacturing process chain of the product is shortened, and the production efficiency is improved. The special tool can be installed, the tool changing time is reduced, the machining efficiency is improved, and the turning and milling combined machining can realize one-time clamping to complete all or most machining processes, so that the product manufacturing process chain is greatly shortened. Therefore, on one hand, the production auxiliary time caused by clamping change is reduced, and meanwhile, the manufacturing period and waiting time of the tool fixture are also reduced, and the production efficiency can be obviously improved.

(2) The clamping frequency is reduced, and the processing precision is improved. The reduction of clamping times avoids the accumulation of errors caused by the conversion of the positioning reference. Meanwhile, most turning and milling composite machine tools have an online detection function, so that online detection and precision control of key data in the manufacturing process can be realized, and the processing precision of products is improved; in addition, the high-strength integrated lathe bed design is adopted, and the processing capacity of difficult-to-cut materials is improved.

In some embodiments, the machining device used in the examples of the present application is a turn-milling compound machine tool having a main spindle, a sub-main spindle, and a B-axis.

The B axis of the turning and milling composite machine tool is a servo axis rotating around the Y axis and is a tool rotating shaft with indexing positioning and linkage functions.

The B shaft is matched with other shafts to realize the multi-shaft linkage function of the machine tool, not only can drill inclined holes or mill inclined planes, but also can be used as an interpolation shaft to finish the processing of complex space curved surfaces, and has absolute advantages for processing high-precision complex workpieces. When a workpiece needs to be turned and bored or drilled, tapped, grooved or milled at a certain angle, the indexing positioning function of the B axis is needed, and locking can be required after indexing, otherwise, the cutting force can cause vibration or displacement, thereby affecting the machining precision. The B-axis fixation is generally divided into fixed angle fixation and arbitrary angle fixation. Therefore, the B shaft is provided with two sets of locking mechanisms, one set is locked at a fixed angle (generally 2.5 degrees or integral multiple of 5 degrees), and the other set is locked at any angle. The fixed angle locking is used for meeting the requirements of strong turning, milling and the like on a specified angle plane; the locking at any angle is used for realizing the processing requirement at any angle.

In step S1, rough turning is performed on the air intake side of the blank to remove the large allowance on the air intake side and reserve a process table at the hub of the air intake side of the blank, which may include:

and the auxiliary main shaft of the turning and milling composite machine tool is abutted against the end face of the air outlet side of the blank, and the excircle of the blank is held tightly by three claws to realize the first clamping of the blank.

After the first clamping is completed, roughly turning the air inlet side of the blank to remove the large allowance of the air inlet side and reserving a process table at the hub of the air inlet side of the blank.

Referring to fig. 3, in a specific application, after rough turning of the air inlet side, 2mm of margin may be left at the blade of the blank, 4mm of margin may be left at the process table, and 1.5mm of margin may be left at the rest.

Referring to fig. 4, fig. 4 is a schematic structural diagram of a blank after angular groove milling according to an embodiment of the present application.

In the step S1, milling the air inlet side hub of the blank to form an angular groove, and using the angular groove as an angular reference may include:

and milling the hub surface on the air inlet side of the blank by using the B shaft of the turning and milling compound machine tool to form an angular groove. The angular grooves can be used as angular references for subsequent milling of the blade profile (blade profile).

The size (width and depth) of the angular groove is not limited, the width of the angular groove can be 4mm, 5mm, 6mm or 7mm, and the depth of the angular groove can be 2mm, 3mm, 4mm or 5mm.

S2: and roughly turning the air outlet side of the blank to remove the large allowance of the air outlet side, milling the blank based on the angular reference to form a blade, and finely turning the air outlet side of the blank.

Referring to fig. 5 and 6, fig. 5 is a schematic view of clamping a blank provided in an embodiment of the present application, and fig. 6 is a schematic view of a structure of a blank after rough turning of an air outlet side provided in an embodiment of the present application.

In step S2, rough turning is performed on the gas outlet side of the blank to remove the large allowance of the gas outlet side, and the rough turning may include:

moving the blank to a main shaft from an auxiliary main shaft of the turning and milling composite machine tool, supporting the air inlet side hub surface of the blank by using a (circular) chuck clamp arranged on the main shaft and clamping the shaft diameter circular surface of the blank, and arranging a key on a key groove of the main shaft to perform key positioning, so that the second clamping of the blank is realized (as shown in figure 5), and the positioning precision can reach 0.01mm;

after the second clamping is completed, rough turning is performed on the air outlet side of the blank to remove the large allowance of the air outlet side, an inner groove is formed, and a process groove is formed in the inner groove (as shown in fig. 6).

The embodiment of the present application does not limit the keys used for key positioning, and for example, a flat key, a semicircular key, a wedge key, a tangential key, a spline, and the like may be used. The width of the key may be, for example, 3mm, 5mm or 8mm.

The size (width and depth) of the process groove is not limited in the embodiment of the application, the width of the process groove can be 4mm, 5mm, 6.5mm or 7mm, and the depth of the process groove can be 12mm, 13mm, 14mm or 15mm.

In a specific application, after rough turning of the air outlet side, 2mm of allowance can be reserved at the blade of the blank, the width of the process groove is 6.5mm, the depth of the process groove is 13mm, and the allowance of 1.5mm is reserved on the other surfaces.

Referring to fig. 7, fig. 7 is a schematic structural diagram of a blank after a blade profile is milled according to an embodiment of the present disclosure.

In step S2, milling the blank based on the angular reference to form a blade, which may include:

and based on the angular reference, milling the blank by using a B shaft of the milling composite machine tool to form a blade. The number of the blades of the blank is not limited in the embodiment of the application, and the number of the blades can be 30, 36, 48 or 54.

Referring to fig. 8, fig. 8 is a schematic structural diagram of a blank after finish turning of the air outlet side according to an embodiment of the present application.

In step S2, finish turning the gas outlet side of the blank may include:

firstly, finely turning the air outlet side end face of the blank to form an air outlet side end face reference;

then, based on the reference of the end face of the air outlet side, roughly processing the inner hole of the blank and the process groove, reserving a margin of 0.2mm, and finely processing the inner hole of the blank and the process groove, so as to ensure the processing state of the blank;

and finally, threading the inner hole of the blank.

S3: and finely turning the air inlet side of the blank.

Referring to fig. 9 to 11, fig. 9 is a schematic view of clamping another blank provided in the embodiment of the present application, fig. 10 is a schematic view of a structure of a double-expansion fixture provided in the embodiment of the present application, and fig. 11 is a schematic view of a structure of a blank after finish turning of an air inlet side provided in the embodiment of the present application.

The step S3 may include:

after the gas outlet side and the blade profile are machined, the blank is moved to an auxiliary main shaft from a main shaft of the turning and milling composite machine tool, a double-expansion clamp arranged on the auxiliary main shaft is used for supporting against the axial diameter end face of the blank so as to expand the inner wall face of the blank, and the third clamping of the blank is realized (as shown in fig. 9 and 10, the positioning precision can reach 0.01mm, and the machining rigidity of the axial diameter position of a workpiece can be ensured by adopting a double-expansion clamping mode);

and after the third clamping is finished, finely turning the air inlet side (except the area of the process table) of the blank.

Referring to fig. 11, a specific process of finely turning the intake side may include:

firstly, finely turning the end surface of the air inlet side of the blank to ensure the total length of a workpiece and form a reference of the end surface of the air inlet side;

then, based on the air inlet side end face reference, performing rough machining on the angular groove and the excircle of the blank, and reserving a 0.2mm allowance;

and finally, performing finish machining on the angular groove and the excircle of the blank.

S4: and removing the process table to obtain the rotary workpiece.

Therefore, in the process of processing the blank into the first-stage blade disc with the shaft diameter, the processing procedures are greatly reduced through the turning and milling composite machine tool, rapid model change among multiple procedures is realized, the processing qualification rate is high, the efficiency is high, and the processing is easy.

Briefly, the whole blank processing process is as follows: firstly, roughly turning an air inlet side and milling an angular groove, and reserving a process table at the hub of the air inlet side to facilitate subsequent positioning; then, milling an angular groove on the hub surface on the air inlet side to provide an angular reference for subsequent blade profile milling; then, roughly turning the air outlet side, milling to form a blade, and then finely turning the air outlet side; and finally, finely turning the air inlet side and removing the process table to obtain the rotary workpiece.

That is to say, the two steps of rough turning air inlet side and milling the angle to the groove can be fused into a process, and the three steps of rough turning air outlet side, milling the leaf profile, finish turning air outlet side can be fused into a process, has reduced benchmark deviation and time cost that blank clamping alignment many times caused, has avoided the error that artifical alignment brought effectively, has reduced alignment clamping time, promotes machining efficiency.

According to the processing method of the first-stage blade disc with the shaft diameter, the rough turning air inlet side and the milling angle groove are integrated into one process through the turning and milling composite equipment, the rough turning air outlet side, the blade milling type and the finish turning air outlet side are integrated into one process, the reference deviation and the time cost caused by multiple clamping and aligning of the blade disc are reduced, through a special tool, the blade disc can be rapidly switched between the main shaft and the auxiliary main shaft after one process is completed, the clamping precision of the blade disc is guaranteed in the type changing process, errors caused by manual aligning are effectively avoided, the aligning and clamping time is greatly reduced, and automatic processing is also realized.

In some optional embodiments, before step S1, the method further comprises:

the step S1 includes:

The design parameters in the first preset design condition are not limited in the embodiments of the present application, and may include, for example, one or more of the indexes of blank size, material grade, hardness, and the like.

The surface parameters in the first predetermined surface condition are not limited in the embodiments of the present application, and may include, for example, one or more of indexes such as cracks, inclusions, residues, holes, burrs, and the like.

As an example, the first preset condition includes a first preset design condition and a first preset surface condition, wherein the first preset design condition is "blank size: 140 mm (diameter), 190 mm (diameter); material designation: 7075 aluminum alloy; hardness: HB 150", the first predetermined surface condition is" no crack, no inclusion, no residue on the blank surface ".

Therefore, before rough turning is carried out on the inner cavity of the blank, indexes such as the size, the material grade, the hardness and the surface state of the blank can be checked, the matching of the indexes such as the size, the material grade and the hardness of the blank and design requirements (namely, the first preset design condition is met) is ensured, and the surface of the blank has no defects such as cracks, impurities and residues (namely, the first preset surface condition is met).

In some optional embodiments, after step S6 and before step S7, the method further comprises:

carrying out first-time clamp repairing treatment on the blank to remove burrs on the surface of the blank and polish the blade;

Therefore, the rotary workpiece applicable to the application can be a blade disc which is an important rotating part of an aeroengine, the surface quality requirement of the blade disc is high, generally speaking, transverse processing marks are not allowed to appear in a certain distance between the front edge and the rear edge of the blade disc, and the blade body profile, the flow passage surface and the blade root fillet need smooth and smooth switching.

Considering the higher surface quality requirement of the bladed disk, after the air inlet side is finely turned and before the process platform is removed, the surface treatment of the blank can be divided into the following two stages, namely a first stage: removing burrs on the surface of the blank through primary clamping and repairing treatment, thereby polishing the blade; and a second stage: and polishing the blank by taking the process table as a positioning basis so as to remove the tool marks and the clamp repairing marks of the blank and smoothen the surface of the blade so as to meet the surface quality requirement.

Therefore, abrasive particle flow polishing is an advanced surface processing technology and is mainly characterized in that viscoelastic fluid abrasive particles are used for achieving the purposes of removing inner cavity burrs, finely processing and polishing the inner surface and processing round corners, the deburring, rounding and polishing of different regions (including regions difficult to enter) of a workpiece can be completed at the same time, and the roughness of the processed surface can reach Ra0.01 micrometer.

In one particular application, the process of abrasive flow polishing the blank may comprise:

and (3) pressing the axial diameter end surface of the blank by utilizing a double-expansion clamp of the auxiliary main shaft to support against the process table, polishing the blank by abrasive flow, removing tool marks and clamp repairing marks, and smoothening the surface of the blade.

In some optional embodiments, the step S7 includes:

turning the blank to remove the process platform;

Therefore, the process table can be removed through turning, after the process table is removed, tool marks generated by turning are required to be removed so as to ensure the surface quality requirement of the bladed disk, and at the moment, the blank can be subjected to secondary clamping and repairing treatment so as to remove the tool marks generated by turning, so that a rotary workpiece (namely the bladed disk) is obtained.

In one embodiment, the process of removing the process platen may comprise:

mounting the blank on a double-expansion clamp on a main shaft of a turning and milling composite machine tool, and supporting against the axial diameter end face of the blank so as to expand the inner wall face of the blank and clamp and position the blank;

and (4) turning to remove the workblank.

At the moment, the main body of the blank is processed in place, the rigidity of the blank is reduced, and the cutting parameters can be properly adjusted, so that the processing state of the blank is ensured.

In some optional embodiments, after the step S7, the method further comprises:

when the rotary workpiece does not meet the second preset condition, detecting whether the rotary workpiece meets a preset grinding condition or not;

Therefore, after the rotary workpiece is machined, the defect of the rotary workpiece can be detected, and whether the rotary workpiece meets the second preset condition or not is judged. When the rotary workpiece does not meet the second preset condition, the workpiece is not directly determined to be a waste product, whether the workpiece meets the preset polishing condition is detected, the workpiece is determined to be the waste product only if the workpiece does not meet the second preset condition or the preset polishing condition, and the waste product is correspondingly scrapped or recycled.

Through setting up preset coping conditions, can recycle the gyration type work piece that partly can regrind again, and then reduced manufacturing cost, practiced thrift the expenditure of raw and other materials, change original passive saving into "practice thrift just benefit", be more suitable for popularizing the processing method of this application in the assembly line of productivity enterprise.

The design parameters in the second preset design condition are not limited in the embodiments of the present application, and may include, for example, the workpiece size and/or form and location tolerance.

The surface parameters in the second predetermined surface condition are not limited in the embodiments of the present application, and may include, for example, one or more of roughness, index, crack, and the like.

As an example, the second preset condition includes a second preset design condition and a second preset surface condition, wherein the second preset design condition is "workpiece size: 110 mm (diameter), 120 mm (diameter); form and position tolerance: the roundness is 0.02 ', and the second preset surface condition is that the surface of the workpiece has no cracks and the roughness Ra0.1'.

The preset grinding condition is not limited, and the preset grinding condition can be that the defect depth of the workpiece is not larger than a preset depth threshold value, or the defect length of the workpiece is not larger than a preset length threshold value. The defect depth can be a scratch depth or a gouge depth, and the defect length can be a scratch length or a gouge length.

The preset depth threshold is, for example, 0.1mm, 0.5mm or 0.8mm and the preset length threshold is, for example, 0.8mm, 1mm or 2mm.

In some optional embodiments, the method further comprises:

Therefore, different grinding equipment can be configured to grind the workpiece according to different defect conditions of the workpiece, and the mode of adaptively configuring the grinding equipment according to the defect conditions can improve the efficiency and success rate of grinding the workpiece, so that the whole processing flow is accelerated.

In some embodiments, when the defect detection result of the revolving-type workpiece indicates that the workpiece is not polished well, the corresponding polishing apparatus may be a polishing machine;

when the defect detection result of the rotary workpiece indicates that the workpiece is scratched, the corresponding grinding equipment can be a spraying machine.

Aiming at the technical problems of multiple working procedures, long manufacturing period, processing deformation and the like of the existing first-stage bladed disk machining method with the shaft diameter, the embodiment of the application also provides a machining method of a rotary workpiece, wherein the rotary workpiece is a bladed disk (such as the first-stage bladed disk of an aircraft engine), the corresponding machining equipment is a turning and milling composite machine tool, and the turning and milling composite machine tool and a special tool are adopted, so that the machining procedures are reduced, the rapid model change among the multiple working procedures is realized, the machining qualification rate is high, the efficiency is high, and the machining is easy.

The method comprises a first step to a ninth step.

The method comprises the following steps: and (6) inspecting incoming materials.

And the size, the grade, the hardness and the surface state of the blank are inspected to ensure that the size, the grade and the hardness of the blank are matched with the design requirements, and the surface of the blank has no defects of cracks, impurities, residues and the like.

Step two: rough turning of the air inlet side + groove milling (first fusion process).

The specific process is shown in fig. 2-4:

the outer circle of the workpiece is held tightly by three claws on the side end surface of the air outlet of the workpiece on an auxiliary main shaft of the turning and milling composite machine tool;

turning the air inlet side of a workpiece, removing large allowance of the air inlet side, reserving a process table at the hub of the air inlet side for convenient subsequent positioning, reserving 2mm allowance at a blade, reserving 4mm allowance at the process table, and reserving 1.5mm allowance at the rest surface;

then, an angular groove with the width of 5mm and the depth of 3mm is milled on the hub surface on the air inlet side through a B shaft of the turning and milling composite machine tool, and an angular reference is provided for subsequent blade profile milling.

Step three: turning the gas outlet side and milling the blade profile (second fusion process).

The specific process is shown in fig. 5-8:

after the second fusion process is completed, the workpiece is moved to the main shaft from the auxiliary main shaft, a circular chuck fixture is arranged on the main shaft, the circular chuck fixture is supported against the hub surface on the air inlet side of the workpiece to clamp the shaft diameter circular surface of the workpiece, and a 5mm key is arranged on the key groove for positioning. The rapid clamping and positioning of the workpiece are realized, and the positioning precision is 0.01mm.

Then, roughly turning the air outlet side, removing the large allowance of the air outlet side, leaving 2mm allowance at the blade, forming a process groove with the width of 6.5mm and the depth of 13mm at the inner groove, and leaving 1.5mm allowance at the rest surface.

Then, the blade is milled through the B shaft to a final state, and the gas outlet side of the workpiece is finely turned to the final state (the end face is turned first to form a final standard).

And finally, machining the inner hole and the process groove, reserving a 0.2mm allowance, then performing finish machining on the inner hole and the process groove, ensuring the machining state of the workpiece, and turning inner hole threads.

Step four: finely turning the air inlet side.

The specific process is shown in fig. 9-11:

after the air outlet side and the blade profile are machined, the workpiece is moved to the auxiliary main shaft from the main shaft, a double-expansion clamp is mounted on the auxiliary main shaft, the auxiliary main shaft abuts against the end face of the shaft diameter of the workpiece, the inner wall face of the workpiece is expanded, the workpiece is clamped and positioned quickly, the positioning accuracy is 0.01mm, and the machining rigidity of the shaft diameter of the workpiece can be guaranteed by adopting double expansion.

And (4) finely machining the air inlet side of the workpiece (the process table does not machine) to a final state (the end face is turned first to form a final reference).

Then, the angular groove and the outer circle are machined, a margin of 0.2mm is reserved, and finally the angular groove and the outer circle are subjected to finish machining. The process platform needs to clamp and position the subsequent abrasive flow and remove the abrasive flow.

Step five: and (4) performing clamping repair, removing machining burrs on the surface of the workpiece, polishing the blade and cleaning the workpiece.

Step six: and (4) polishing the abrasive flow, supporting against a process table, pressing the axial end surface of the workpiece tightly, polishing the workpiece by the abrasive flow, and removing tool marks and clamp repairing marks to smoothen the surface of the blade.

Step seven: and removing the process table, mounting the workpiece on a double-expansion clamp on an auxiliary main shaft of the turning and milling composite machine tool, supporting against the axial end surface of the workpiece, and expanding the inner wall surface of the workpiece. And (5) turning to remove the workpiece process platform.

At the moment, the workpiece main body is processed in place, the rigidity of the workpiece is reduced, the cutting parameters are adjusted, and the processing state of the workpiece is ensured.

Step eight: and (5) clamping, removing the machined burrs on the surface of the workpiece, and cleaning the workpiece.

Step nine: and (5) finally checking.

And (4) summarizing and checking the workpieces, checking all sizes and form and position tolerance requirements of the workpieces, checking the outer surfaces of the workpieces and marking requirements, forming summarizing records, and determining whether the design requirements of the workpieces are met.

By adopting the turning and milling combined machine tool, the rough turning air inlet side and the milling angle are integrated into a process, the rough turning air outlet side, the milling blade type and the finish turning air outlet side are integrated into a process, the reference deviation and the time cost caused by multiple clamping and alignment of the blade disc are reduced, the special tool is used for realizing process switching between the main shaft and the auxiliary main shaft quickly after one process is finished, the clamping precision of the blade disc is ensured in the shape changing process, the errors caused by manual alignment are effectively avoided, the alignment and clamping time is greatly reduced, the automatic processing is also realized, the double-expansion design and the chuck clamp greatly enhance the processing rigidity of workpieces, the processing deformation of the blade disc is small, the repeated positioning precision is high, and the processing efficiency is greatly improved.

System embodiment

Referring to fig. 12, fig. 12 is a schematic structural diagram of a machining system for a rotary workpiece according to an embodiment of the present disclosure.

The embodiment of the present application provides a machining system for a rotary workpiece, and a specific implementation manner of the machining system is consistent with the implementation manner and the achieved technical effect described in the above method embodiment, and some contents are not described again.

The embodiment of the application provides a system for processing of gyration type work piece for utilize the turning and milling multiple equipment to process the blank into gyration type work piece, gyration type work piece is the first order bladed disk of taking the shaft diameter, the system includes:

the rough turning module 101 at the air inlet side is used for roughly turning the air inlet side of the blank to remove large allowance at the air inlet side, reserving a process table at the hub of the air inlet side of the blank, and milling the hub of the air inlet side of the blank to form an angular groove, wherein the angular groove is used as an angular reference;

the gas outlet side machining module 102 is configured to roughly machine the gas outlet side of the blank to remove a large allowance of the gas outlet side, mill the blank based on the angular reference to form a blade, and finish-machine the gas outlet side of the blank;

an air inlet side finish turning module 103, which is used for finish turning the air inlet side of the blank;

and the process table removing module 104 is used for removing the process table to obtain the rotary workpiece.

In some optional embodiments, the system further comprises:

the intake side rough turning module 101 is configured to: and when the blank is detected to meet the first preset condition, roughly turning the air inlet side of the blank.

In some optional embodiments, the system further comprises:

In some alternative embodiments, the stage removal module 107 comprises:

In some optional embodiments, the system further comprises:

An embodiment of the present application further provides an electronic device, where the electronic device includes a memory and at least one processor, the memory stores a computer program, and the at least one processor implements the steps of any one of the methods when executing the computer program.

Apparatus embodiment

Referring to fig. 13, fig. 13 shows a block diagram of an electronic device according to an embodiment of the present application.

The electronic device may include, for example, at least one memory 210, at least one processor 220, and a bus 230 connecting the different platform systems.

The memory 210 may include readable media in the form of volatile memory, such as Random Access Memory (RAM) 211 and/or cache memory 212, and may further include Read Only Memory (ROM) 213.

Wherein the memory 210 further stores a computer program that can be executed by the processor 220 such that the processor 220 implements the steps of any of the methods described above.

Memory 210 may also include a utility 214 having at least one program module 215, such program modules 215 including, but not limited to: an operating system, one or more application programs, other program modules, and program data, each of which, or some combination thereof, may comprise an implementation of a network environment.

Accordingly, the processor 220 may execute the computer programs described above, and may execute the utility 214.

The processor 220 may employ one or more Application Specific Integrated Circuits (ASICs), DSPs, programmable Logic Devices (PLDs), complex Programmable Logic Devices (CPLDs), field Programmable Gate Arrays (FPGAs), or other electronic components.

Bus 230 may be one or more of any of several types of bus structures including a memory bus or memory controller, a peripheral bus, an accelerated graphics port, and a local bus using any of a variety of bus architectures.

The electronic device may also communicate with one or more external devices 240, such as a keyboard, pointing device, bluetooth device, etc., and may also communicate with one or more devices capable of interacting with the electronic device, and/or with any devices (e.g., routers, modems, etc.) that enable the electronic device to communicate with one or more other computing devices. Such communication may be through input-output interface 250. Also, the electronic device may communicate with one or more networks (e.g., a Local Area Network (LAN), a wide area network (WA N), and/or a public network, such as the internet) via the network adapter 260. The network adapter 260 may communicate with other modules of the electronic device via the bus 230. It should be appreciated that although not shown in the figures, other hardware and/or software modules may be used in conjunction with the electronic device, including but not limited to: microcode, device drivers, redundant processors, external disk drive arrays, RAID systems, tape drives, and data backup storage platforms, to name a few.

Media embodiments

An embodiment of the present application further provides a computer-readable storage medium, where a computer program is stored, and when the computer program is executed by a processor, the steps of any one of the methods are implemented, and a specific implementation manner of the method is consistent with the implementation manner and the achieved technical effect described in the foregoing method embodiment, and some details are not repeated.

Referring to fig. 14, fig. 14 shows a schematic structural diagram of a program product provided in an embodiment of the present application.

The program product is for implementing any of the methods described above. The program product may employ a portable compact disc read only memory (CD-ROM) and include program code, and may be run on a terminal device, such as a personal computer. However, the program product of the present invention is not limited thereto, and in the embodiments of the present application, the readable storage medium may be any tangible medium that can contain or store a program, which can be used by or in connection with an instruction execution system, apparatus, or device. The program product may employ any combination of one or more readable media. The readable medium may be a readable signal medium or a readable storage medium. A readable storage medium may be, for example, but not limited to, an electronic, magnetic, optical, electromagnetic, infrared, or semiconductor system, apparatus, or device, or any combination of the foregoing. More specific examples (a non-exhaustive list) of the readable storage medium include: an electrical connection having one or more wires, a portable disk, a hard disk, a Random Access Memory (RAM), a read-only memory (ROM), an erasable programmable read-only memory (EPROM or flash memory), an optical fiber, a portable compact disc read-only memory (CD-ROM), an optical storage device, a magnetic storage device, or any suitable combination of the foregoing.

A computer readable storage medium may include a propagated data signal with readable program code embodied therein, for example, in baseband or as part of a carrier wave. Such a propagated data signal may take many forms, including, but not limited to, electro-magnetic, optical, or any suitable combination thereof. A readable storage medium may also be any readable medium that can communicate, propagate, or transport the program for use by or in connection with the instruction execution system, apparatus, or device. Program code embodied on a readable storage medium may be transmitted using any appropriate medium, including but not limited to wireless, wireline, optical fiber cable, RF, etc., or any suitable combination of the foregoing. Program code for carrying out operations for aspects of the present invention may be written in any combination of one or more programming languages, including an object oriented programming language such as Java, C + + or the like and conventional procedural programming languages, such as the C language or similar programming languages. The program code may execute entirely on the user's computing device, partly on the user's device, as a stand-alone software package, partly on the user's computing device and partly on a remote computing device, or entirely on the remote computing device or server. In situations involving remote computing devices, the remote computing devices may be connected to the user computing device through any kind of network, including a Local Area Network (LAN) or a Wide Area Network (WAN), or may be connected to external computing devices (e.g., through the internet using an internet service provider).

While the present application is described in terms of various aspects, including exemplary embodiments, the principles of the invention should not be limited to the disclosed embodiments, but are also intended to cover various modifications, equivalents, and alternatives falling within the spirit and scope of the invention as defined by the appended claims.

Claims

1. A processing method of a rotary workpiece is used for processing a blank into the rotary workpiece by using a turning and milling composite device, wherein the rotary workpiece is a first-stage blade disc with a shaft diameter, and the method comprises the following steps:

s3: finely turning the air inlet side of the blank;

s4: and removing the process table to obtain the rotary workpiece.

2. The method for machining a rotating-type workpiece according to claim 1, wherein the step S1 includes:

the auxiliary main shaft of the turning and milling composite machine tool is close to the end face of the air outlet side of the blank through three claws, so that the blank is clamped for the first time;

3. The method for machining a rotating-type workpiece according to claim 1, wherein the step S2 includes:

milling the blank based on the angular reference to form a blade;

finely turning the air outlet side of the blank to form an air outlet side end face reference;

and threading the inner hole of the blank.

4. The method for machining a rotating-type workpiece according to claim 1, wherein the step S3 includes:

moving the blank to an auxiliary main shaft from a main shaft of the turning and milling combined machine tool, and supporting the axial end surface of the blank by using a double-expansion clamp arranged on the auxiliary main shaft so as to expand the inner wall surface of the blank to realize the third clamping of the blank;

5. The method for machining a rotating-type workpiece according to claim 1, wherein before step S1, the method further comprises:

the step S1 includes:

6. The method for machining a rotating-type workpiece according to claim 1, wherein after step S3 and before step S4, the method further comprises:

7. The method of machining a rotating-type workpiece according to claim 6, wherein the step S4 includes:

turning the blank to remove the process platform;

8. A system for processing a rotary workpiece, wherein the system is used for processing a blank into the rotary workpiece by using a turning and milling composite device, the rotary workpiece is a first-stage blade disc with a shaft diameter, and the system comprises:

the rough turning module at the air inlet side is used for roughly turning the air inlet side of the blank to remove large allowance at the air inlet side and reserve a process table at the hub of the air inlet side of the blank, and milling the hub of the air inlet side of the blank to form an angular groove which is used as an angular reference;

9. An electronic device, characterized in that the electronic device comprises a memory and at least one processor, the memory storing a computer program, the at least one processor implementing the steps of the method according to any of claims 1-7 when executing the computer program.

10. A computer-readable storage medium, characterized in that the computer-readable storage medium stores a computer program which, when being executed by a processor, carries out the steps of the method according to any one of claims 1 to 7.