CN110677972A - Plasma generator for SiC optical mirror processing and application method thereof - Google Patents
Plasma generator for SiC optical mirror processing and application method thereof Download PDFInfo
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Abstract
Description
技术领域technical field
本发明涉及光学材料制造领域,具体涉及一种用于SiC光学镜面加工的等离子体发生器及其应用方法。The invention relates to the field of optical material manufacturing, in particular to a plasma generator used for SiC optical mirror processing and an application method thereof.
背景技术Background technique
SiC光学材料具有化学稳定性高、密度低、强度及弹性模量高、抗辐射性强、比刚度大、热变形系数小,可进行高反射率镀膜等良好特性。因此,SiC反射镜被越来越广泛地应用于空间天文光学、卫星遥感技术和大型地基光学系统。随着SiC反射镜应用领域越来越广泛,其与日剧增的需求量给SiC反射镜的高效加工提出全新挑战。目前,SiC反射镜的传统加工流程是粗磨成形、研磨、改性、抛光等几道工序。改性前是对SiC基体的加工,改性后是对改性层的加工。改性前对基体的磨削和研磨加工中,占了整个加工周期一半以上的时间。并且SiC材料硬度大,传统靠机械研磨抛光方式加工材料去除效率非常低、加工周期长。SiC optical materials have good characteristics such as high chemical stability, low density, high strength and elastic modulus, strong radiation resistance, high specific stiffness, small thermal deformation coefficient, and high reflectivity coating. Therefore, SiC mirrors are more and more widely used in space astronomical optics, satellite remote sensing technology and large-scale ground-based optical systems. As the application fields of SiC mirrors become more and more extensive, its increasing demand has brought new challenges to the efficient processing of SiC mirrors. At present, the traditional processing flow of SiC mirror is rough grinding, grinding, modification, polishing and other processes. Before the modification is the processing of the SiC matrix, and after the modification is the processing of the modified layer. Grinding and grinding of the substrate before modification accounted for more than half of the entire processing cycle. In addition, the hardness of SiC material is high, and the traditional mechanical grinding and polishing method is very low in material removal efficiency and long in processing cycle.
针对SiC材料硬度大,加工效率低的特点,国内外有研究采用超声振动磨削和了大气等离子体加工。超声振动磨削,虽然能一定程度上提高加工效率,但存在砂轮磨损的问题。然而,大气等离子体加工方式,利用等离子体激发出的高活性反应原子与被加工元件表面原子发生化学反应,生成强挥发性的气体生成物,从而实现工件材料原子量级去除的加工方式。以加工SiC材料为例,反应气体NF3,CF4,O2或者SF6在等离子体氛围中被激发成各种具有活性的自由基和激发态的F*或O*原子,自由基和F*原子或O*扩散到SiC材料表面,反应生成气态CO2,SiF4等气态生成物从工件表面逸出,达到SiC材料表面材料高效去除的目的。大气等离子体加工是可控化学反应过程,去除函数稳定,不存在传统加工砂轮磨损、磨头磨损等问题,是一种无损伤的加工方式。同时通过研究发现大气等离子体加工还具备去损伤能力,能有效去除机械加工后残留的表面及亚表面损伤。因此,近年来世界各国研究的大气等离子体加工技术有:日本大阪大学的等离子体化学蒸发加工技术(PCVM)、哈尔滨工业大学的大气等离子体抛光方法(APPP),美国Lawrence Livermore实验室的反应原子等离子体抛光技术(RAPT)和国防科技大学公布了专利号为CN103456610的一种SiC光学材料加工设备。常用的等离子体发生器类型可以分为电容耦合型等离子体(CCP)和电感耦合型等离子体(ICP)。其中,PCVM和APPP均是采用CCP等离子体发生方法产生可用于加工的等离子体,并研制了相应的等离子体发生器和加工设备,而RAPT和国防科技大学的SiC光学材料加工设备则采用普通ICP等离子体发生器产生等离子体。In view of the characteristics of high hardness and low processing efficiency of SiC materials, ultrasonic vibration grinding and atmospheric plasma processing have been studied at home and abroad. Although ultrasonic vibration grinding can improve the processing efficiency to a certain extent, there is the problem of grinding wheel wear. However, the atmospheric plasma processing method utilizes the chemical reaction between the highly active reactive atoms excited by the plasma and the surface atoms of the workpiece to be processed to generate highly volatile gaseous products, thereby realizing the processing method of removing the workpiece material at the atomic level. Taking the processing of SiC materials as an example, the reactive gases NF3, CF4, O2 or SF6 are excited into various active free radicals and excited F* or O* atoms, free radicals and F* atoms or O in the plasma atmosphere. *Diffusion to the surface of the SiC material, reacting to generate gaseous CO2, SiF4 and other gaseous products escaping from the surface of the workpiece to achieve the purpose of efficient removal of the surface material of the SiC material. Atmospheric plasma machining is a controllable chemical reaction process, the removal function is stable, and there are no problems such as traditional machining grinding wheel wear and grinding head wear, and it is a non-destructive machining method. At the same time, it was found through research that atmospheric plasma processing also has the ability to remove damage, which can effectively remove the residual surface and sub-surface damage after machining. Therefore, in recent years, the atmospheric plasma processing technologies studied by countries around the world include: the plasma chemical vaporization processing technology (PCVM) of Osaka University, Japan, the atmospheric plasma polishing method (APPP) of Harbin Institute of Technology, and the reactive atom of the Lawrence Livermore laboratory in the United States. Plasma Polishing Technology (RAPT) and National University of Defense Technology announced a SiC optical material processing equipment with patent number CN103456610. Commonly used plasma generator types can be divided into capacitively coupled plasma (CCP) and inductively coupled plasma (ICP). Among them, PCVM and APPP both use the CCP plasma generation method to generate plasma that can be used for processing, and have developed corresponding plasma generators and processing equipment, while the SiC optical material processing equipment of RAPT and National University of Defense Technology uses ordinary ICP A plasma generator produces plasma.
目前,从等离子体加工效率来说,普通ICP等离子体加工方法可以使用更大的功率,因此等离子体的电离程度更高,活性粒子的浓度更高,可实现效率高于CCP等离子体的加工,同时,无电极存在可以避免电极的腐蚀对加工材料的污染;然而,对于SiC这种高硬度材料,普通ICP等离子体的加工效率还是偏低的。从ICP等离子体发生器结构来说,普通ICP等离子体发生器采用一体式石英炬管;一体式石英炬管会因为ICP等离子体加工时的热量累积导致炬管易炸裂而报废,很难适应长时间加工,而且维护难度和成本都很高。At present, in terms of plasma processing efficiency, the ordinary ICP plasma processing method can use higher power, so the plasma ionization degree is higher, the concentration of active particles is higher, and the processing efficiency is higher than that of the CCP plasma. At the same time, the absence of electrodes can prevent the corrosion of electrodes from contaminating the processing materials; however, for high-hardness materials such as SiC, the processing efficiency of ordinary ICP plasma is still low. In terms of the structure of the ICP plasma generator, the common ICP plasma generator adopts an integrated quartz torch; the integrated quartz torch will be scrapped due to the heat accumulation during ICP plasma processing, which will cause the torch to burst easily, and it is difficult to adapt to long-term Time processing, and maintenance is difficult and costly.
发明内容SUMMARY OF THE INVENTION
本发明要解决的技术问题:针对现有技术的上述问题,提供一种用于SiC光学镜面加工的等离子体发生器及其应用方法,本发明能够降低ICP等离子体加工过程的维护难度,提高SiC光学镜面加工效率与长时间稳定性,具有加工效率高,结构简单、成本低廉、便于维护、长时间稳定性高的优点。The technical problem to be solved by the present invention: in view of the above-mentioned problems of the prior art, a plasma generator for SiC optical mirror surface processing and an application method thereof are provided. The present invention can reduce the maintenance difficulty of the ICP plasma processing process and improve the The optical mirror surface processing efficiency and long-term stability have the advantages of high processing efficiency, simple structure, low cost, easy maintenance, and high long-term stability.
为了解决上述技术问题,本发明采用的技术方案为:In order to solve the above-mentioned technical problems, the technical scheme adopted in the present invention is:
本发明提供一种用于SiC光学镜面加工的等离子体发生器,包括外壳和安装于外壳内的组合式炬管,所述组合式炬管包括外管和依次嵌套在外管入口端的中管和内管,所述外管的中部外壁上套设有电感耦合线圈,所述外管的出口端设有拉瓦尔喷嘴,所述外管、中管之间的空隙形成冷却气体流入通道,所述中管、内管之间的空隙形成激发气体流入通道,所述内管的内腔形成反应气体流入通道。The invention provides a plasma generator for SiC optical mirror processing, comprising a casing and a combined torch mounted in the casing, the combined torch comprising an outer tube, a middle tube nested in sequence at the inlet end of the outer tube, and In the inner tube, an inductive coupling coil is sleeved on the outer wall of the middle part of the outer tube, the outlet end of the outer tube is provided with a Laval nozzle, the gap between the outer tube and the middle tube forms a cooling gas inflow channel, the The space between the middle tube and the inner tube forms an inflow channel of excitation gas, and the inner cavity of the inner tube forms an inflow channel of reaction gas.
可选地,所述组合式炬管的外壁上套设固定有炬管安装板,所述外管、中管、内管分别安装固定在炬管安装板上,所述组合式炬管通过炬管安装板安装在外壳的内腔中轴线上。Optionally, a torch mounting plate is sleeved and fixed on the outer wall of the combined torch, the outer pipe, the middle pipe, and the inner pipe are respectively mounted and fixed on the torch mounting plate, and the combined torch passes through the torch. The tube mounting plate is mounted on the central axis of the inner cavity of the housing.
可选地,所述电感耦合线圈为内部带有第一水冷循环通道的铜管,且通过炬管安装板安装在组合式炬管出口端外围且两者之间留有隔热间隙。Optionally, the inductively coupled coil is a copper tube with a first water-cooling circulation channel inside, and is mounted on the periphery of the outlet end of the combined torch through a torch mounting plate with a thermal insulation gap therebetween.
可选地,所述拉瓦尔喷嘴采用铜质材料制成。Optionally, the Laval nozzle is made of copper material.
可选地,所述拉瓦尔喷嘴的外侧设有喷嘴外壳,所述喷嘴外壳上固定有喷嘴安装板,所述拉瓦尔喷嘴通过喷嘴安装板固定在喷嘴外壳的内腔中轴线上、且通过喷嘴安装板与外壳密封连接并与组合式炬管保持中心轴共线。Optionally, a nozzle housing is provided on the outer side of the Laval nozzle, a nozzle mounting plate is fixed on the nozzle housing, and the Laval nozzle is fixed on the central axis of the inner cavity of the nozzle housing through the nozzle mounting plate, and passes through the nozzle. The mounting plate is sealingly connected to the housing and maintains a central axis co-linear with the modular torch.
可选地,所述拉瓦尔喷嘴的外壁和喷嘴外壳的内壁之间形成冷却空腔,所述外壳中设有壳体空腔,所述壳体空腔、冷却空腔连通形成第二水冷循环通道。Optionally, a cooling cavity is formed between the outer wall of the Laval nozzle and the inner wall of the nozzle shell, the shell is provided with a shell cavity, and the shell cavity and the cooling cavity are connected to form a second water cooling cycle aisle.
可选地,所述外管的外壁上还设有第一通气入口,所述第一通气入口形成冷却气体流入通道,所述中管的外壁上还设有第二通气入口,所述第二通气入口形成激发气体流入通道,所述内管的外壁上还设有第三通气入口,所述第三通气入口形成反应气体流入通道。Optionally, the outer wall of the outer pipe is further provided with a first ventilation inlet, the first ventilation inlet forms a cooling gas inflow channel, and the outer wall of the middle pipe is further provided with a second ventilation inlet, the second ventilation inlet is The ventilation inlet forms an inflow channel for excitation gas, and a third ventilation inlet is further provided on the outer wall of the inner tube, and the third ventilation inlet forms an inflow channel for reaction gas.
本发明还提供一种前述用于SiC光学镜面加工的等离子体发生器的应用方法,实施步骤包括:The present invention also provides an application method of the aforementioned plasma generator for SiC optical mirror processing, the implementation steps comprising:
1)将所述用于SiC光学镜面加工的等离子体发生器安装于三轴联动功能的数控运动平台上,运用等离子体直线扫描SiC工件的表面得出去除函数的材料去除量,通过提取和拟合材料去除量沟槽截面形状获得去除函数实验模型;1) The plasma generator used for SiC optical mirror processing is installed on a numerically controlled motion platform with three-axis linkage function, and the surface of the SiC workpiece is scanned linearly by the plasma to obtain the material removal amount of the removal function. The experimental model of the removal function was obtained by combining the material removal amount and the groove section shape;
2)根据去除函数实验模型计算驻留时间分布,设置加工路径;2) Calculate the residence time distribution according to the experimental model of the removal function, and set the processing path;
3)通过所述用于SiC光学镜面加工的等离子体发生器对SiC工件的表面进行迭代加工。3) Iteratively process the surface of the SiC workpiece by the plasma generator for SiC optical mirror machining.
可选地,步骤1)中获取去除函数实验模型的详细步骤包括:Optionally, the detailed steps for obtaining the experimental model of the removal function in step 1) include:
1.1)通过所述用于SiC光学镜面加工的等离子体发生器以指定的运动速度v沿SiC工件的表面的Y轴方向直线扫描加工出一条沟槽,通过立式干涉仪得出测量沟槽的截面形状数据;1.1) A groove is processed by linear scanning along the Y-axis direction of the surface of the SiC workpiece at a specified motion speed v by the plasma generator used for SiC optical mirror processing, and the measurement groove is obtained by a vertical interferometer. Section shape data;
1.2)在得到沟槽的截面形状数据的基础上拟合式(4)得到沟槽截面形状深度Ax、去除函数实验模型的高斯分布参数σx的值,然后再根据式(5)得出在运动速度v下的去除函数实验模型;1.2) Fitting formula (4) on the basis of the obtained groove cross-sectional shape data to obtain the groove cross-sectional shape depth A x , the value of the Gaussian distribution parameter σ x of the removal function experimental model, and then according to formula (5) to obtain The experimental model of the removal function under the motion speed v;
式(4)中,G(x)为X轴方向上的沟槽截面形状函数,Ax为沟槽截面形状深度,σx为去除函数实验模型的高斯分布参数,x为坐标(x,y)处的横坐标;In formula (4), G(x) is the shape function of the groove section in the X-axis direction, Ax is the depth of the groove section shape, σx is the Gaussian distribution parameter of the experimental model of the removal function, and x is the coordinate (x, y) ) at the abscissa;
式(5)中,R(x,y)表示坐标(x,y)处的材料去除量,Ax为沟槽截面形状深度,v为等离子体发生器的运动速度,σx为去除函数实验模型的高斯分布参数。In formula (5), R(x,y) represents the material removal amount at the coordinate (x,y), Ax is the depth of the groove cross-sectional shape, v is the moving speed of the plasma generator, σx is the removal function experiment Gaussian distribution parameters for the model.
可选地,步骤2)中根据去除函数实验模型计算驻留时间分布具体是指运用脉冲迭代法计算驻留时间分布τ(x,y),且运用脉冲迭代法计算驻留时间分布τ(x,y)的详细步骤包括:Optionally, calculating the residence time distribution according to the removal function experimental model in step 2) specifically refers to using the pulse iteration method to calculate the residence time distribution τ(x, y), and using the pulse iteration method to calculate the residence time distribution τ(x). ,y) The detailed steps include:
2.1)根据SiC工件的已知面形的材料去除量分布建立材料去除量矩阵R,在得到去除函数实验模型的基础上确定去除函数矩阵G和去除函数强度Br;2.1) According to the material removal amount distribution of the known surface shape of the SiC workpiece, a material removal amount matrix R is established, and the removal function matrix G and the removal function intensity B r are determined on the basis of obtaining the removal function experimental model;
2.2)设置初始驻留时间T0的值为R/Br、残差为E0的值为其中,R为材料去除量矩阵,Br为去除函数强度,G为去除函数矩阵;2.2) Set the value of the initial dwell time T 0 as R/B r and the residual as the value of E 0 Among them, R is the material removal amount matrix, B r is the removal function strength, and G is the removal function matrix;
2.3)计算k个驻留点的驻留时间校正量Δk的值为Ek/Br;其中,Ek为k个驻留点的残差矩阵,Br为去除函数强度;2.3) Calculate the value of the dwell time correction Δk of the k dwell points as E k /B r ; wherein, E k is the residual matrix of the k dwell points, and B r is the removal function strength;
2.4)校正k+1个驻留点的驻留时间Tk+1的值为Tk+ζ·Δk;其中,Tk为k个驻留点的驻留时间,ζ为松弛因子,Δk为k个驻留点的驻留时间校正量;2.4) The value of the dwell time T k+1 of the correction k+1 dwell points is T k +ζ·Δ k ; where T k is the dwell time of k dwell points, ζ is the relaxation factor, Δ k is the dwell time correction amount of k dwell points;
2.5)计算残差矩阵Ek+1的值为其中,Ek+1为k+1个驻留点的残差矩阵,Br为去除函数强度,R为材料去除量矩阵,Tk+1为k+1个驻留点的驻留时间,G为去除函数矩阵;2.5) Calculate the value of the residual matrix E k+1 as Among them, E k+1 is the residual matrix of k+1 dwell points, B r is the strength of the removal function, R is the material removal matrix, T k+1 is the dwell time of k+1 dwell points, G is the removal function matrix;
2.6)判断k+1个驻留点的驻留时间Tk+1和残差矩阵Ek+1是否满足要求,不满足则重复步骤2.3);否则迭代结束,得到所有驻留点的驻留时间构成的驻留时间分布τ(x,y)。2.6) Determine whether the dwell time T k+1 of k+1 dwell points and the residual matrix E k+1 meet the requirements, if not, repeat step 2.3); otherwise, the iteration ends, and the dwell of all dwell points is obtained The dwell time distribution τ(x,y) formed by time.
本发明用于SiC光学镜面加工的等离子体发生器具有下述优点:本发明的等离子体发生器包括外壳和安装于外壳内的组合式炬管,组合式炬管包括外管和依次嵌套在外管入口端的中管和内管,外管的中部外壁上套设有电感耦合线圈,外管的出口端设有拉瓦尔喷嘴,可在拉瓦尔喷嘴处形成电弧增强等离子体,能够降低ICP等离子体加工过程的维护难度,提高SiC光学镜面加工效率与长时间稳定性,具有加工效率高,结构简单、成本低廉、便于维护、长时间稳定性高的优点。The plasma generator used for SiC optical mirror processing of the present invention has the following advantages: the plasma generator of the present invention includes a casing and a combined torch installed in the casing, and the combined torch includes an outer tube and is sequentially nested in the outer casing. The middle tube and inner tube at the inlet end of the tube, an inductive coupling coil is set on the outer wall of the middle part of the outer tube, and a Laval nozzle is arranged at the outlet end of the outer tube, which can form arc-enhanced plasma at the Laval nozzle, which can reduce the ICP plasma The maintenance difficulty of the processing process improves the processing efficiency and long-term stability of the SiC optical mirror surface, and has the advantages of high processing efficiency, simple structure, low cost, easy maintenance, and high long-term stability.
本发明用于SiC光学镜面加工的等离子体发生器的应用方法具有下述优点:本发明用于SiC光学镜面加工的等离子体发生器的应用方法的特点是应用于SiC光学镜面加工时能产生电弧增强的等离子体,获得峰值去除率高且半峰全宽小的去除函数。该方法利用直线扫描实验方法获取去除函数实验模型,运用脉冲迭代法计算出精确驻留时间分布,然后设置加工路径,提高单次加工收敛比,从而提高整个迭代加工过程的效率。The application method of the plasma generator for SiC optical mirror processing of the present invention has the following advantages: the application method of the plasma generator for SiC optical mirror processing of the present invention is characterized in that an arc can be generated when applied to SiC optical mirror processing Enhanced plasma, high peak removal rate and small full width at half maximum removal function are obtained. The method uses the linear scanning experimental method to obtain the experimental model of the removal function, uses the pulse iteration method to calculate the precise residence time distribution, and then sets the machining path to improve the single machining convergence ratio, thereby improving the efficiency of the entire iterative machining process.
附图说明Description of drawings
图1为本发明实施例等离子体发生器的原理结构示意图。FIG. 1 is a schematic diagram of the principle structure of a plasma generator according to an embodiment of the present invention.
图2为本发明实施例等离子体发生器的立体结构示意图。FIG. 2 is a schematic three-dimensional structure diagram of a plasma generator according to an embodiment of the present invention.
图3为本发明实施例等离子体发生器的主视结构示意图。FIG. 3 is a schematic front view of the structure of a plasma generator according to an embodiment of the present invention.
图4为图3的A-A剖视结构示意图。FIG. 4 is a schematic view of the cross-sectional structure taken along the line A-A of FIG. 3 .
图5为本发明实施例中组合式炬管的立体结构示意图。FIG. 5 is a schematic three-dimensional structure diagram of a combined torch in an embodiment of the present invention.
图6为现有技术的普通ICP等离子体直线扫描实验获得的材料去除量。FIG. 6 is the material removal amount obtained by the conventional ICP plasma linear scanning experiment in the prior art.
图7为现有技术的普通ICP等离子体直线扫描实验获得的去除深度(横截面沟槽)。FIG. 7 shows the removal depth (cross-sectional groove) obtained by the conventional ICP plasma linear scanning experiment of the prior art.
图8为本发明实施例等离子体发生器直线扫描获得的材料去除量。FIG. 8 is the material removal amount obtained by the linear scanning of the plasma generator according to the embodiment of the present invention.
图9为本发明实施例等离子体发生器直线扫描获得的去除深度(横截面沟槽)。FIG. 9 is the removal depth (cross-sectional groove) obtained by linear scanning of the plasma generator according to the embodiment of the present invention.
图10为本发明实施例中得到的去除函数实验模型。FIG. 10 is an experimental model of the removal function obtained in the embodiment of the present invention.
图11为本发明实施例中得到的驻留时间分布。FIG. 11 is the residence time distribution obtained in the embodiment of the present invention.
图12为现有的普通光栅加工路径。Fig. 12 shows the conventional ordinary grating processing path.
图13为本发明实施例中的中嵌套式光栅加工路径。FIG. 13 is the inner-nested grating processing path in the embodiment of the present invention.
图14为SiC光学镜面采用现有技术的普通ICP等离子体加工的初始面形。FIG. 14 is the initial surface shape of the SiC optical mirror surface processed by conventional ICP plasma processing.
图15为SiC光学镜面采用现有技术的普通ICP等离子体加工后的面形。FIG. 15 is the surface shape of the SiC optical mirror surface processed by the conventional ICP plasma.
图16为本发明实施例中SiC光学镜面电弧增强等离子体加工的初始面形。FIG. 16 is the initial surface shape of the arc-enhanced plasma processing of the SiC optical mirror surface in the embodiment of the present invention.
图17为本发明实施例中SiC光学镜面电弧增强等离子体加工后的面形。FIG. 17 is the surface shape of the SiC optical mirror surface after arc-enhanced plasma processing in the embodiment of the present invention.
图例说明:1、外壳;11、壳体空腔;2、组合式炬管;20、炬管安装板;21、外管;211、第一通气入口;22、中管;221、第二通气入口;23、内管;231、第三通气入口;24、电感耦合线圈;25、拉瓦尔喷嘴;26、喷嘴外壳;261、喷嘴安装板;262、冷却空腔;3、射频电源;4、功率匹配器。Legend description: 1. Housing; 11. Housing cavity; 2. Combined torch; 20. Torch mounting plate; 21. Outer tube; 211, First vent inlet; 22, Middle tube; Inlet; 23, inner pipe; 231, third ventilation inlet; 24, inductively coupled coil; 25, Laval nozzle; 26, nozzle housing; 261, nozzle mounting plate; 262, cooling cavity; 3, RF power supply; 4, power matcher.
具体实施方式Detailed ways
如图1、图2、图3和图4所示,本实施例提供一种用于SiC光学镜面加工的等离子体发生器,包括外壳1和安装于外壳1内的组合式炬管2,组合式炬管2包括外管21和依次嵌套在外管21入口端的中管22和内管23,外管21的中部外壁上套设有电感耦合线圈24,外管21的出口端设有拉瓦尔喷嘴25,外管21、中管22之间的空隙形成冷却气体流入通道(图1中a所示),中管22、内管23之间的空隙形成激发气体流入通道(图1中b所示),内管23的内腔形成反应气体流入通道(图1中c所示),本实施例提用于SiC光学镜面加工的等离子体发生器可在拉瓦尔喷嘴25处形成电弧增强等离子体(图1中d所示)。As shown in FIG. 1 , FIG. 2 , FIG. 3 and FIG. 4 , this embodiment provides a plasma generator for SiC optical mirror processing, including a
本实施例中,外壳1为铝材料,设置为空腔结构。In this embodiment, the
如图4所示,组合式炬管2的外壁上套设固定有炬管安装板20,外管21、中管22、内管23分别安装固定在炬管安装板20上,组合式炬管2通过炬管安装板20安装在外壳1的内腔中轴线上,简单方便,易于装卸,便于外管21、中管22、内管23单独更换和维护。As shown in FIG. 4 , a torch mounting plate 20 is sleeved and fixed on the outer wall of the combined
本实施例中,外管21为石英材料,耐高温效果良好,提高组合式炬管2高温加工的稳定性。中管22采用不锈钢材料且下端开口设置成喇叭状,提高管道内部气流速度,进而使得激发气体更加容易电离。在等离子体束接触SiC工件表面时,不锈钢的中管22和SiC光学镜面会形成电极,产生放电现象,而放电使得SiC材料的Si-C键更容易断裂,Si-F键更容易形成,降低了反应所需要的能量,使得反应更加容易进行,从而提高了材料去除率,进而提高了加工效率。实验验证得出,这种放电现象可以大幅提高等离子加工的效率,在相同条件下,电弧增强的等离子体加工效率高出普通等离子体加工效率的几倍,如图6~图9所示,相同加工条件下,普通等ICP离子体直线扫描实验去除深度为89.5nm,半峰全宽为15.73mm,去除效率为0.27μ/min;而电弧增强等离子体直线扫描实验去除深度为604.7nm,半峰全宽为5.27mm,体积去除率为5.36μ/min;因此,本实施例设备所产生的电弧增强等离子体可实现SiC光学镜面较普通等ICP离子体更高效的加工。本实施例中,内管23为刚玉材料,而刚玉不与活性F*发生反应,与提高了内管抗F*的腐蚀能力。In this embodiment, the
本实施例中,电感耦合线圈24为内部带有第一水冷循环通道的铜管,且通过炬管安装板20安装在组合式炬管2出口端外围且两者之间留有隔热间隙。第一水冷循环通道用来冷却射频功率耦合产热,能够防止组合式炬管2炸裂、提高电弧增强等离子体加工的稳定性并且可延长炬管的使用寿命,能够抑制等离子体加工过程热量的累积,降低等离子体温度,防止温度过高影响等离子体加工的稳定性;电感耦合线圈24通过炬管安装板20安装在组合式炬管2出口端外围且两者之间留有隔热间隙,能够避免电感耦合线圈24工作产生的热量直接传导给外管21引起炸裂。In this embodiment, the
本实施例中,拉瓦尔喷嘴25采用铜质材料制成,可避免射频电磁场功率耦合至拉瓦尔喷嘴25上而导致激发的等离子体熄灭,从而提高等离子体加工的稳定性。In this embodiment, the
如图4所示,拉瓦尔喷嘴25的外侧设有喷嘴外壳26,喷嘴外壳26上固定有喷嘴安装板261,拉瓦尔喷嘴25通过喷嘴安装板261固定在喷嘴外壳26的内腔中轴线上、且通过喷嘴安装板261与外壳1密封连接并与组合式炬管2保持中心轴共线。As shown in FIG. 4 , the outer side of the
本实施例中,喷嘴外壳26为铝材料。In this embodiment, the
如图4所示,拉瓦尔喷嘴25的外壁和喷嘴外壳26的内壁之间形成冷却空腔262,外壳1中设有壳体空腔11,壳体空腔11、冷却空腔262连通形成第二水冷循环通道。第二水冷循环通道用来冷却等离子体发生器整体产热,能够抑制等离子体加工过程热量的累积,降低等离子体温度,防止温度过高影响等离子体加工的稳定性。作为一种可选的实施特例,本实施例中壳体空腔11、冷却空腔262之间通过塑料管保持连通。As shown in FIG. 4 , a
如图5所示,外管21的外壁上还设有第一通气入口211,第一通气入口211形成冷却气体流入通道,中管22的外壁上还设有第二通气入口221,第二通气入口221形成激发气体流入通道,内管23的外壁上还设有第三通气入口231,第三通气入口231形成反应气体流入通道,通过上述结构能够增加通气量,提高加工性能。本实施例中,外管21、中管22之间的空隙以及第一通气入口211共同形成冷却气体流入通道,向外管21通入大流量的冷却气体Ar,使等离子体产生的热量随着气流排出;中管22、内管23之间的空隙以及第二通气入口221共同形成激发气体流入通道,向中管22中通入小流量的等离子激发气体Ar;第三通气入口231和内管23的内腔6向内管23通入反应气体SF6与小流量Ar混合气体。As shown in FIG. 5 , the outer wall of the
本实施例中,电感耦合线圈24连接有激励单元,激励单元还包括射频电源3和功率匹配器4,射频电源3的输出端通过功率匹配器4与电感耦合线圈24的线圈端子相连。系统工作时,功率匹配器4将射频电源3输出功率匹配到电感耦合线圈24上,然后电感耦合线圈24产生高频感应电磁场使激发气体Ar激发反应气体SF6产生稳定得等离子体。In this embodiment, the
本实施例前述用于SiC光学镜面加工的等离子体发生器的应用方法的实施步骤包括:The implementation steps of the above-mentioned application method of the plasma generator for SiC optical mirror processing in this embodiment include:
1)将所述用于SiC光学镜面加工的等离子体发生器安装于三轴联动功能的数控运动平台上,运用等离子体直线扫描SiC工件的表面得出去除函数的材料去除量,通过提取和拟合材料去除量沟槽截面形状获得去除函数实验模型;1) The plasma generator used for SiC optical mirror processing is installed on a numerically controlled motion platform with three-axis linkage function, and the surface of the SiC workpiece is scanned linearly by the plasma to obtain the material removal amount of the removal function. The experimental model of the removal function was obtained by combining the material removal amount and the groove section shape;
2)根据去除函数实验模型计算驻留时间分布,设置加工路径;2) Calculate the residence time distribution according to the experimental model of the removal function, and set the processing path;
3)通过用于SiC光学镜面加工的等离子体发生器对SiC工件的表面进行迭代加工。3) Iterative machining of the surface of the SiC workpiece by a plasma generator for SiC optical mirror machining.
将本实施例前述用于SiC光学镜面加工的等离子体发生器安装于三轴联动功能的数控运动平台上即可用于完成XYZ三轴联动加工,基于等离子体发生器加工SiC光学镜面时产生电弧增强的等离子体,获取高效率的去除函数,计算驻留时间,设置加工路径即可以实现SiC光学镜面电弧增强等离子体的高效加工。The plasma generator used for SiC optical mirror processing in this embodiment can be installed on a CNC motion platform with three-axis linkage function to complete XYZ three-axis linkage processing, and the arc enhancement is generated when processing SiC optical mirror surfaces based on the plasma generator. The high-efficiency removal function is obtained, the residence time is calculated, and the processing path is set to realize the high-efficiency processing of SiC optical mirror arc-enhanced plasma.
本实施例中,步骤1)中获取去除函数实验模型的详细步骤包括:In the present embodiment, the detailed steps of obtaining the experimental model of the removal function in step 1) include:
1.1)通过所述用于SiC光学镜面加工的等离子体发生器以指定的运动速度v沿SiC工件的表面的Y轴方向直线扫描加工出一条沟槽,通过立式干涉仪得出测量沟槽的截面形状数据,如图5所示;本实施例中,指定的运动速度v具体为50mm/min。1.1) A groove is processed by linear scanning along the Y-axis direction of the surface of the SiC workpiece at a specified motion speed v by the plasma generator used for SiC optical mirror processing, and the measurement groove is obtained by a vertical interferometer. The cross-sectional shape data is shown in Figure 5; in this embodiment, the specified movement speed v is specifically 50 mm/min.
参见图8和图9,可看出本实施例中通过等离子体发生器以指定的运动速度v沿SiC工件的表面的Y轴方向直线扫描加工出一条沟槽获得的材料去除量与去除深度。作为对比,图6为普通ICP等离子体直线扫描实验获得的材料去除量,图7为普通ICP等离子体直线扫描实验获得的去除深度。对比图6、7和图8、9可知,本实施例中通过等离子体发生器在SiC光学镜面产生的去除函数的峰值去除效高且半峰全宽较小。Referring to FIG. 8 and FIG. 9 , it can be seen that in this embodiment, the material removal amount and the removal depth obtained by linearly scanning and machining a groove along the Y-axis direction of the surface of the SiC workpiece by the plasma generator at a specified moving speed v. For comparison, Fig. 6 shows the material removal amount obtained by the ordinary ICP plasma linear scanning experiment, and Fig. 7 is the removal depth obtained by the ordinary ICP plasma linear scanning experiment. Comparing FIGS. 6 and 7 with FIGS. 8 and 9 , it can be seen that, in this embodiment, the removal function generated by the plasma generator on the SiC optical mirror surface has a high peak removal efficiency and a small full width at half maximum.
1.2)在得到沟槽的截面形状数据的基础上拟合式(4)得到沟槽截面形状深度Ax、去除函数实验模型的高斯分布参数σx的值,然后再根据式(5)得出在运动速度v下的去除函数实验模型;1.2) Fitting formula (4) on the basis of the obtained groove cross-sectional shape data to obtain the groove cross-sectional shape depth A x , the value of the Gaussian distribution parameter σ x of the removal function experimental model, and then according to formula (5) to obtain The experimental model of the removal function under the motion speed v;
式(4)中,G(x)为X轴方向上的沟槽截面形状函数,Ax为沟槽截面形状深度,σx为去除函数实验模型的高斯分布参数,x为坐标(x,y)处的横坐标;In formula (4), G(x) is the shape function of the groove section in the X-axis direction, Ax is the depth of the groove section shape, σx is the Gaussian distribution parameter of the experimental model of the removal function, and x is the coordinate (x, y) ) at the abscissa;
式(5)中,R(x,y)表示坐标(x,y)处的材料去除量,Ax为沟槽截面形状深度,v为等离子体发生器的运动速度,σx为去除函数实验模型的高斯分布参数。In formula (5), R(x,y) represents the material removal amount at the coordinate (x,y), Ax is the depth of the groove cross-sectional shape, v is the moving speed of the plasma generator, σx is the removal function experiment Gaussian distribution parameters for the model.
SiC工件的X轴方向上的沟槽截面形状函数G(x)的理论模型可描述为式(1);The theoretical model of the groove cross-sectional shape function G(x) in the X-axis direction of the SiC workpiece can be described as formula (1);
式(1)中,R(x,y)表示坐标(x,y)处的材料去除量,v为等离子体发生器的运动速度。In formula (1), R(x, y) represents the material removal amount at the coordinates (x, y), and v is the moving speed of the plasma generator.
而典型高斯形去除函数可以描述为式(2);The typical Gaussian-shaped removal function can be described as formula (2);
式(2)中,R(x,y)表示坐标(x,y)处的材料去除量,A是峰值去除速率,σ为去除函数的高斯分布参数。将式(3)代入式(1)则有式(3);In formula (2), R(x, y) represents the material removal amount at the coordinate (x, y), A is the peak removal rate, and σ is the Gaussian distribution parameter of the removal function. Substitute formula (3) into formula (1) to have formula (3);
式(3)中各参量可参见式(1)和式(2)。The parameters in formula (3) can be found in formula (1) and formula (2).
因此,沟槽截面形状函数G(x)经高斯拟合为式(4)。Therefore, the groove cross-sectional shape function G(x) is Gaussian fitted to Equation (4).
本实施例中,通过立式干涉仪得出测量沟槽截面形状数据后根据式(4)拟合得到的沟槽截面形状函数G(x)为:In the present embodiment, the groove cross-sectional shape function G(x) obtained by fitting the groove cross-sectional shape data according to the formula (4) after obtaining the measurement groove cross-sectional shape data by the vertical interferometer is:
即:沟槽截面形状深度Ax的值为0.604,去除函数实验模型的高斯分布参数σx的值为2.24。在此基础上,即可根据式(5)可得在运动速度v下的去除函数实验模型为:That is, the value of the groove cross-sectional shape depth A x is 0.604, and the value of the Gaussian distribution parameter σ x of the removal function experimental model is 2.24. On this basis, according to formula (5), the experimental model of the removal function under the motion speed v can be obtained as:
上述运动速度v下的去除函数实验模型如图10所示。The experimental model of the removal function at the above motion speed v is shown in Figure 10.
如图6~图9所示,针对本发明中等离子发生器在SiC光学镜面产生的去除函数的峰值去除效高,且半峰全宽较小,因此,可利用脉冲迭代法计算驻留时间分布τ(x,y)。本实施例中,步骤2)中根据去除函数实验模型计算驻留时间分布具体是指运用脉冲迭代法计算驻留时间分布τ(x,y),且运用脉冲迭代法计算驻留时间分布τ(x,y)的详细步骤包括:As shown in Fig. 6 to Fig. 9 , the peak removal efficiency of the removal function generated by the plasmon generator on the SiC optical mirror in the present invention is high, and the full width at half maximum is small. Therefore, the pulse iteration method can be used to calculate the residence time distribution. τ(x,y). In this embodiment, calculating the dwell time distribution according to the experimental model of the removal function in step 2) specifically refers to using the pulse iteration method to calculate the dwell time distribution τ(x,y), and using the pulse iteration method to calculate the dwell time distribution τ( The detailed steps of x,y) include:
2.1)根据SiC工件的已知面形的材料去除量分布(根据如图16所示的初始面形确定)建立材料去除量矩阵R,在得到去除函数实验模型的基础上确定去除函数矩阵G和去除函数强度Br;2.1) According to the material removal amount distribution of the known surface shape of the SiC workpiece (determined according to the initial surface shape as shown in Figure 16), the material removal amount matrix R is established, and the removal function matrix G and remove function strength B r ;
2.2)设置初始驻留时间T0的值为R/Br、残差为E0的值为其中,R为材料去除量矩阵,Br为去除函数强度,G为去除函数矩阵;2.2) Set the value of the initial dwell time T 0 as R/B r and the residual as the value of E 0 Among them, R is the material removal amount matrix, B r is the removal function strength, and G is the removal function matrix;
2.3)计算k个驻留点的驻留时间校正量Δk的值为Ek/Br;其中,Ek为k个驻留点的残差矩阵,Br为去除函数强度;2.3) Calculate the value of the dwell time correction Δk of the k dwelling points as E k /B r ; wherein, E k is the residual matrix of the k dwelling points, and B r is the removal function strength;
2.4)校正k+1个驻留点的驻留时间Tk+1的值为Tk+ζ·Δk;其中,Tk为k个驻留点的驻留时间,ζ为松弛因子,Δk为k个驻留点的驻留时间校正量;松弛因子ζ用来控制残留误差收敛的速率,松弛因子ζ越大,残差收敛越快,反之残差收敛较慢,松弛因子一般取ζ≤1。2.4) The value of the dwell time T k+1 of the correction k+1 dwell points is T k +ζ·Δ k ; where T k is the dwell time of k dwell points, ζ is the relaxation factor, Δ k is the dwell time correction of k dwell points; the relaxation factor ζ is used to control the rate of residual error convergence, the larger the relaxation factor ζ, the faster the residual error convergence, otherwise the residual error convergence is slower, the relaxation factor generally takes
2.5)计算残差矩阵Ek+1的值为其中,Ek+1为k+1个驻留点的残差矩阵,Br为去除函数强度,R为材料去除量矩阵,Tk+1为k+1个驻留点的驻留时间,G为去除函数矩阵;2.5) Calculate the value of the residual matrix E k+1 as Among them, E k+1 is the residual matrix of k+1 dwell points, B r is the strength of the removal function, R is the material removal matrix, T k+1 is the dwell time of k+1 dwell points, G is the removal function matrix;
2.6)判断k+1个驻留点的驻留时间Tk+1和残差矩阵Ek+1是否满足要求,不满足则重复步骤2.3);否则迭代结束,得到所有驻留点的驻留时间构成的驻留时间分布τ(x,y)。本实施例中最终计算得出的驻留时间如图11所示。2.6) Determine whether the dwell time T k+1 of k+1 dwell points and the residual matrix E k+1 meet the requirements, if not, repeat step 2.3); otherwise, the iteration ends, and the dwell of all dwell points is obtained The dwell time distribution τ(x,y) formed by time. The dwell time finally calculated in this embodiment is shown in FIG. 11 .
实现SiC光学镜面的电弧增强等离子体反应高效加工,除需要求解准确的驻留时间分布τ(x,y)外,还需要合理规划加工路径,以提高等离子体高效加工方法的稳定性。电弧增强等离子体高效加工过程中,温度对加工效率影响较大,传统的光栅路径,如图12所示,普通光栅加工路径的路径间栅距很小,随着加工时间的推移,加工温度逐渐增大,造成去除函数加工效率升高。另一方面,随着加工时间的增加,SiC工件自身温度随之升高,继而将影响加工过程中的去除函数的加工效率稳定性。因此。针对这一问题,本实施例方法采用嵌套光栅扫描路径,如图13所示,本实施例中嵌套式光栅加工路径中相邻路径之间的栅距可以根据实际加工工件的大小尺寸调整,以利于平衡加工产热量,均衡加工时镜面的温度分布,继而提高电弧增强等离子体去除函数加工效率稳定性。In order to realize the efficient processing of arc-enhanced plasma reaction of SiC optical mirror, in addition to solving the accurate residence time distribution τ(x, y), it is also necessary to reasonably plan the processing path to improve the stability of the plasma efficient processing method. In the high-efficiency processing of arc-enhanced plasma, the temperature has a great influence on the processing efficiency. For the traditional grating path, as shown in Figure 12, the grating pitch between the paths of the ordinary grating processing path is very small. As the processing time goes on, the processing temperature gradually increases. increases, resulting in an increase in the processing efficiency of the removal function. On the other hand, as the machining time increases, the temperature of the SiC workpiece itself increases, which in turn affects the stability of the machining efficiency of the removal function during the machining process. therefore. In order to solve this problem, the method of this embodiment adopts a nested raster scanning path. As shown in FIG. 13 , the raster pitch between adjacent paths in the nested raster processing path in this embodiment can be adjusted according to the size of the actual workpiece to be processed. , in order to balance the heat production of processing, balance the temperature distribution of the mirror surface during processing, and then improve the stability of the processing efficiency of the arc-enhanced plasma removal function.
本实施例中,最终将计算的驻留时间和设置的光栅路径转化成为CNC数控代码,然后进行SiC光学镜面加工。根据加工后的面形收敛情况,如图14所示,SiC工件的初始面形为:PV 108.5nm,RMS 28.5nm,普通等离子体经过10分钟加工,如图15所示,加工后面形为:PV 72nm,RMS 15.2nm,因此加工面形28.5nm RMS到15.2nm RMS,收敛比为1.87。如图16所示,SiC工件的初始面形为:PV 220nm,RMS 58nm,用本实施例方法经过8分钟加工,如图17所示,加工后面形为:PV 166nm,RMS 19nm,面形从68nm RMS到19nm RMS,收敛比为3.58,面形不仅实现了快速收敛,而且收敛比提高了将近1倍。如果加工面形不收敛或者没有达到加工要求,再次设定材料去除量,计算驻留时间,设置光栅路径,进行迭代加工,直至加工结果满足加工要求。In this embodiment, the calculated dwell time and the set grating path are finally converted into CNC numerical control codes, and then SiC optical mirror processing is performed. According to the surface shape convergence after processing, as shown in Figure 14, the initial surface shape of the SiC workpiece is: PV 108.5nm, RMS 28.5nm, After 10 minutes of ordinary plasma processing, as shown in Figure 15, the shape after processing is: PV 72nm, RMS 15.2nm, so the processing surface shape is 28.5nm RMS to 15.2nm RMS, and the convergence ratio is 1.87. As shown in Figure 16, the initial surface shape of the SiC workpiece is: PV 220nm, RMS 58nm, After 8 minutes of processing by the method of this embodiment, as shown in Figure 17, the shape after processing is: PV 166nm, RMS 19nm, the surface shape is from 68nm RMS to 19nm RMS, the convergence ratio is 3.58, the surface shape not only achieves rapid convergence, but also The convergence ratio is nearly doubled. If the processing surface shape does not converge or does not meet the processing requirements, set the material removal amount again, calculate the dwell time, set the grating path, and perform iterative processing until the processing results meet the processing requirements.
以上所述仅是本发明的优选实施方式,本发明的保护范围并不仅局限于上述实施例,凡属于本发明思路下的技术方案均属于本发明的保护范围。应当指出,对于本技术领域的普通技术人员来说,在不脱离本发明原理前提下的若干改进和润饰,这些改进和润饰也应视为本发明的保护范围。The above are only the preferred embodiments of the present invention, and the protection scope of the present invention is not limited to the above-mentioned embodiments, and all technical solutions under the idea of the present invention belong to the protection scope of the present invention. It should be pointed out that for those skilled in the art, some improvements and modifications without departing from the principle of the present invention should also be regarded as the protection scope of the present invention.
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