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CN115091145A - A kind of supercharger casting turbine processing method - Google Patents

A kind of supercharger casting turbine processing method Download PDF

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Publication number
CN115091145A
CN115091145A CN202210910185.4A CN202210910185A CN115091145A CN 115091145 A CN115091145 A CN 115091145A CN 202210910185 A CN202210910185 A CN 202210910185A CN 115091145 A CN115091145 A CN 115091145A
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turbine
outer circle
blank
welding
face
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柯益
李成科
鲁建于
蒋中亮
周开松
刘国成
姚元润
杨意松
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Chongqing Jiangjin Shipbuilding Industry Co Ltd
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Chongqing Jiangjin Shipbuilding Industry Co Ltd
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/006Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine wheels

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Abstract

本发明涉及机械加工技术领域,具体涉及一种增压器铸造涡轮加工方法,包括粗车涡轮毛坯焊接端外圆及端面;软三爪夹涡轮毛坯焊接端外圆,端面拿平;粗车端面打中心孔;以中心孔为基准对涡轮毛坯进行磨削;切割粗车涡轮毛坯焊接端外圆长度;精车涡轮毛坯焊接端,得到成品涡轮,该涡轮加工方法,采用软三爪装夹涡轮毛坯焊接端,并采用与粗车焊接面外圆同样的要求,对加工非焊接端的外圆及端面粗车加工,同时在非焊接端的端面上加工出中心孔,并以中心孔为基准进行后续的加工操作,保证涡轮的中心与后续摩擦焊接时的中心一致,解决涡轮加工时,焊接端没有装夹,导致涡轮中心与后续摩擦焊接时的中心不一致的问题。

Figure 202210910185

The invention relates to the technical field of machining, in particular to a supercharger casting turbine machining method, including roughing the outer circle and end face of the welding end of the turbine blank; Punch the center hole; grind the turbine blank based on the center hole; cut the outer circle length of the welding end of the rough turning turbine blank; finish the welding end of the turbine blank to obtain the finished turbine. The turbine processing method adopts a soft three-jaw clamping turbine The welding end of the blank shall be rough-turned with the same requirements as the outer circle of the welding surface for rough turning. The outer circle and end face of the non-welding end shall be rough-turned, and a center hole shall be machined on the end face of the non-welding end, and the follow-up shall be carried out based on the center hole. It can ensure that the center of the turbine is consistent with the center of the subsequent friction welding, and solve the problem that the welding end is not clamped when the turbine is processed, resulting in the inconsistency between the center of the turbine and the center of the subsequent friction welding.

Figure 202210910185

Description

一种增压器铸造涡轮加工方法A kind of supercharger casting turbine processing method

技术领域technical field

本发明涉及机械加工技术领域,尤其涉及一种增压器铸造涡轮加工方法。The invention relates to the technical field of machining, in particular to a method for machining a supercharger casting turbine.

背景技术Background technique

涡轮作为船舶主要动力装置的船用柴油机的重要部件,增压器铸造涡轮的技术水平直接影响船用柴油机的工作效率。Turbine is an important part of marine diesel engine which is the main power unit of ship, and the technical level of supercharger casting turbine directly affects the working efficiency of marine diesel engine.

现有涡轮加工非焊接面时,涡轮焊接面端没有装夹,导致涡轮中心与后续摩擦焊接时的中心不一致。When the non-welded surface of the existing turbine is processed, the welding surface end of the turbine is not clamped, resulting in the inconsistency between the center of the turbine and the center of the subsequent friction welding.

发明内容SUMMARY OF THE INVENTION

本发明的目的在于提供一种增压器铸造涡轮加工方法,旨在解决涡轮加工时,焊接端没有装夹,导致涡轮中心与后续摩擦焊接时的中心不一致的问题。The purpose of the present invention is to provide a supercharger casting turbine processing method, which aims to solve the problem that the welding end is not clamped during turbine processing, resulting in the inconsistency between the turbine center and the center during subsequent friction welding.

为实现上述目的,本发明提供了一种增压器铸造涡轮加工方法,包括以下步骤:In order to achieve the above purpose, the present invention provides a supercharger casting turbine processing method, comprising the following steps:

粗车涡轮毛坯焊接端外圆及端面;The outer circle and end face of the welding end of the rough turning turbine blank;

软三爪夹所述涡轮毛坯焊接端外圆;The outer circle of the welding end of the turbine blank is clamped by the soft three-jaw clamp;

在粗车后的所述端面上顶中心孔;Top the center hole on the end face after rough turning;

以所述中心孔为基准对所述涡轮毛坯进行磨削;grinding the turbine blank based on the center hole;

切割所述粗车涡轮毛坯焊接端外圆长度;cutting the outer circle length of the welding end of the rough turning turbine blank;

精车所述涡轮毛坯焊接端,得到成品涡轮。Finish turning the welded end of the turbine blank to obtain a finished turbine.

其中,在步骤精车所述涡轮毛坯焊接端,得到成品涡轮之后,所述方法还包括:所述将主轴与所述成品涡轮焊接端焊接,并做动平衡处理。Wherein, after finishing the welding end of the turbine blank to obtain a finished turbine, the method further includes: welding the main shaft and the welding end of the finished turbine, and performing dynamic balancing treatment.

其中,所述粗车涡轮毛坯焊接端外圆及端面的具体方式:Wherein, the specific method of the outer circle and end face of the welding end of the rough turning turbine blank:

三爪夹所述涡轮毛坯焊接端外圆,找正外圆及端面;Three claws clamp the outer circle of the welding end of the turbine blank, and align the outer circle and end face;

光出端面打中心孔,粗车涡轮毛坯。Punch a center hole on the end face of the light, and rough the turbine blank.

其中,所述在粗车后的所述端面上顶中心孔的具体方式:Wherein, the specific method of topping the center hole on the end face after rough turning:

顶出中心孔,光出端面高点;Eject the center hole, and light out the high point of the end face;

光出外圆及端面。Light out the outer circle and end face.

其中,所述精车涡轮毛坯焊接端,得到成品涡轮的具体方式:Wherein, the detailed method of obtaining the finished turbine is the welding end of the finished turbine blank:

软三爪夹所述涡轮毛坯焊接端外圆;The outer circle of the welding end of the turbine blank is clamped by the soft three-jaw clamp;

找正非焊接端外圆和端面,精车。Align the outer circle and end face of the non-welded end, and finish turning.

本发明的一种增压器铸造涡轮加工方法,粗车涡轮毛坯焊接端外圆及端面;软三爪夹所述涡轮毛坯焊接端外圆;在粗车后的所述端面上顶中心孔;以所述中心孔为基准对所述涡轮毛坯进行磨削;切割所述粗车涡轮毛坯焊接端外圆长度;精车所述涡轮毛坯焊接端,得到成品涡轮,该涡轮加工方法,采用软三爪装夹涡轮毛坯焊接端,并采用与粗车焊接面外圆同样的要求,对加工非焊接端的外圆及端面粗车加工,同时在非焊接端的端面上加工出中心孔,并以中心孔为基准进行后续的加工操作,保证涡轮的中心与后续摩擦焊接时的中心一致,解决涡轮加工时,焊接端没有装夹,导致涡轮中心与后续摩擦焊接时的中心不一致的问题。The supercharger casting turbine processing method of the present invention includes rough turning of the outer circle and end face of the welding end of the turbine blank; the outer circle of the welding end of the turbine blank is clamped by soft three claws; Grinding the turbine blank based on the center hole; cutting the outer circle length of the welding end of the rough turning turbine blank; finishing turning the welding end of the turbine blank to obtain a finished turbine. The turbine processing method adopts a soft three The claw clamps the welded end of the turbine blank, and adopts the same requirements as the rough turning of the outer circle of the welding surface. The outer circle and end face of the non-welded end are rough-machined. At the same time, a center hole is machined on the end face of the non-welded end, and the center hole is used. Follow-up processing operations are carried out as the benchmark to ensure that the center of the turbine is consistent with the center of the subsequent friction welding, so as to solve the problem that the welding end is not clamped when the turbine is processed, resulting in the inconsistency between the center of the turbine and the center of the subsequent friction welding.

附图说明Description of drawings

为了更清楚地说明本发明实施例或现有技术中的技术方案,下面将对实施例或现有技术描述中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图仅仅是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。In order to explain the embodiments of the present invention or the technical solutions in the prior art more clearly, the following briefly introduces the accompanying drawings that need to be used in the description of the embodiments or the prior art. Obviously, the accompanying drawings in the following description are only These are some embodiments of the present invention. For those of ordinary skill in the art, other drawings can also be obtained according to these drawings without creative efforts.

图1是本发明提供的一种增压器铸造涡轮加工方法的流程图。FIG. 1 is a flow chart of a method for machining a supercharger cast turbine provided by the present invention.

图2是粗车涡轮毛坯焊接端外圆及端面的示意图。Figure 2 is a schematic diagram of the outer circle and end face of the welded end of the rough-turned turbine blank.

图3是软三爪夹所述涡轮毛坯焊接端外圆和在粗车后的所述端面上顶中心孔的示意图。3 is a schematic diagram of the outer circle of the welding end of the turbine blank and the top center hole on the end face after rough turning of the soft three-jaw clamp.

图4是以所述中心孔为基准对所述涡轮毛坯进行磨削的示意图。FIG. 4 is a schematic diagram of grinding the turbine blank based on the center hole.

图5是精车所述涡轮毛坯焊接端,得到成品涡轮的示意图。Figure 5 is a schematic diagram of finishing the welded end of the turbine blank to obtain a finished turbine.

图6是涡轮加工示意图。Figure 6 is a schematic diagram of turbine processing.

图7是将主轴与所述成品涡轮焊接端焊接,并做动平衡处理的示意图。FIG. 7 is a schematic diagram of welding the main shaft and the welded end of the finished turbine and performing dynamic balancing treatment.

图8是机械加工工艺过程卡片。Figure 8 is a machining process card.

具体实施方式Detailed ways

下面详细描述本发明的实施例,所述实施例的示例在附图中示出,其中自始至终相同或类似的标号表示相同或类似的元件或具有相同或类似功能的元件。下面通过参考附图描述的实施例是示例性的,旨在用于解释本发明,而不能理解为对本发明的限制。The following describes in detail the embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein the same or similar reference numerals refer to the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are exemplary, and are intended to explain the present invention and should not be construed as limiting the present invention.

请参阅图1至图8,本发明提供一种增压器铸造涡轮加工方法,包括以下步骤:Please refer to FIG. 1 to FIG. 8 , the present invention provides a supercharger casting turbine processing method, which includes the following steps:

S1粗车涡轮毛坯焊接端外圆及端面;The outer circle and end face of the welding end of the S1 rough turning turbine blank;

具体的,为控制涡轮旋转中心与涡轮质量中心的偏差,减小焊接后涡轮轴的残余不平衡量,加工所述涡轮毛坯外圆时主要找正流道处外圆,即以流道为找正基准(主要原因为根据涡轮结构分析,涡轮大部分质量均在流道以内的实体部分,以流道为找正基准能尽量减小涡轮旋转中心与质量中心的偏差),同时在所述涡轮毛坯端面上加工出中心孔。Specifically, in order to control the deviation between the center of rotation of the turbine and the center of mass of the turbine and reduce the residual unbalance of the turbine shaft after welding, when machining the outer circle of the turbine blank, the outer circle at the runner is mainly aligned, that is, the runner is used for alignment. Benchmark (the main reason is that according to the turbine structure analysis, most of the mass of the turbine is in the solid part of the flow channel, and using the flow channel as the alignment benchmark can minimize the deviation between the turbine rotation center and the mass center), and at the same time in the turbine blank A center hole is machined on the end face.

具体方式:Specific way:

S11三爪夹所述涡轮毛坯焊接端外圆,找正外圆及端面;S11 three-jaw clamps the outer circle of the welding end of the turbine blank, and aligns the outer circle and end face;

S12光出端面打中心孔,粗车所述涡轮毛坯。The S12 light-emitting end face is punched with a center hole, and the turbine blank is rough-machined.

具体的,光出:采用机械加工的方式将需加工的面或外圆全部加工出,加工后整个端面或外圆不允许有未加工前的原始痕迹。Specifically, light out: all surfaces or outer circles to be machined are machined out by machining, and the entire end surface or outer circle after machining is not allowed to have original traces before processing.

S2软三爪夹所述涡轮毛坯焊接端外圆;S2 soft three-jaw clamps the outer circle of the welding end of the turbine blank;

S3在粗车后的所述端面上顶中心孔;S3 tops the center hole on the end face after rough turning;

具体方式:Specific way:

S31顶出中心孔,光出端面高点;S31 pushes out the center hole, and light out the high point of the end face;

S32光出外圆及端面。S32 light out the outer circle and end face.

S4以所述中心孔为基准对涡轮毛坯进行磨削;S4 grinds the turbine blank based on the center hole;

具体的,以粗车加工出的所述中心孔为装夹定位基准,顶两端中心孔,磨非焊接端外圆、叶片处大外圆及焊接端叶片端面。磨非焊接端外圆主要用于后续精车焊接端时装夹基准;磨焊接端叶片端面主要用于后续精车焊接端时找正基准;磨叶片处大外圆主要用于后续精车焊接面时找正基准以及摩擦焊接时工装定位用(保证焊接时涡轮与光轴同心,以减小焊接后涡轮轴的不平衡量。此外圆涡轮加工图纸要求加工,但作为精车的加工基准以及后续涡轮与光轴摩擦焊接定位基准需要,此外圆需进行加工)。Specifically, the center hole processed by rough turning is used as the clamping and positioning reference, and the center holes at the top two ends are ground for the outer circle of the non-welding end, the large outer circle at the blade and the end face of the blade at the welding end. Grinding the outer circle of the non-welding end is mainly used for the clamping datum of the welding end of the subsequent finishing; grinding the end face of the blade at the welding end is mainly used for aligning the datum in the welding end of the subsequent finishing; grinding the large outer circle of the blade is mainly used for the welding surface of the subsequent finishing It is used for alignment reference and tooling positioning during friction welding (to ensure that the turbine and the optical axis are concentric during welding to reduce the unbalance of the turbine shaft after welding. In addition, the machining drawing of the circular turbine requires processing, but it is used as the machining benchmark for finishing and subsequent turbines. The positioning datum is required for friction welding with the optical axis, and the other circle needs to be processed).

S5切割粗车涡轮毛坯焊接端外圆长度;S5 cutting the outer circle length of the welding end of the rough turning turbine blank;

具体的,采用线切割方式割去所述涡轮毛坯焊接端外圆多余长度(即割去铸造时预留的工艺夹头,工艺夹头约20mm长)。预留此工艺夹头的主要目的时用于车削非焊接端外圆及端面的装夹用,按照涡轮加工图要求,焊接端外圆最终长度只有1mm长,而在加工非焊接端外圆及端面时只能装夹焊接端,叶片由于不连续且为毛坯状态,无法装夹,故只能夹持焊接面处外圆,但按图纸尺寸来说夹持长度是不够的,故铸造时将焊接面处外圆进行加长,预留工艺夹头来夹持。同时,由于涡轮为高温合金材质,车削时加工效率很低,为生产周期及加工成本考虑,采用线切割的方式来去掉工艺夹头,只留1mm余量来精车。Specifically, the excess length of the outer circle of the welded end of the turbine blank is cut off by wire cutting (ie, the process chuck reserved during casting is cut off, and the process chuck is about 20 mm long). The main purpose of reserving this process chuck is for the clamping of the outer circle and end face of the non-welded end. According to the requirements of the turbine processing drawing, the final length of the outer circle of the welded end is only 1mm long, while the outer circle of the non-welded end and When the end face is used, only the welding end can be clamped. The blade cannot be clamped because it is discontinuous and in a blank state, so it can only clamp the outer circle of the welding surface. However, according to the size of the drawing, the clamping length is not enough. The outer circle of the welding surface is lengthened, and the process chuck is reserved for clamping. At the same time, because the turbine is made of superalloy, the processing efficiency during turning is very low. Considering the production cycle and processing cost, the process chuck is removed by wire cutting, leaving only a 1mm margin for finishing.

S6精车涡轮毛坯焊接端,得到成品涡轮。S6 finish turning the welded end of the turbine blank to obtain the finished turbine.

具体的,将主轴与所述成品涡轮焊接端焊接,并做动平衡处理,具体操作为,把主轴放置于支承位置上,在TT和V平面做动平衡,去重位置为x所指处,去重范围见机械加工工艺过程卡片,已做过动平衡的主轴用彩笔标明,加工时采用软三爪夹持已磨非焊接端外圆,靠平已磨非焊接端端面,精车焊接面外圆、端面及内孔,同时精车后续涡轮与光轴摩擦焊接所定位用的台阶平面,加工时复校找正叶片处已磨外圆,保证涡轮加工时的中心与后续摩擦焊接时的中心一致,减小摩擦焊接时涡轮与光轴不同心造成涡轮轴的不平衡量。Specifically, the main shaft is welded to the welded end of the finished turbine, and dynamic balance processing is performed. The specific operation is as follows: place the main shaft on the support position, perform dynamic balance on the TT and V planes, and the deweighting position is the position indicated by x, See the machining process card for the range of deduplication. The spindle that has been dynamically balanced is marked with colored pens. During processing, soft three claws are used to hold the outer circle of the ground non-welding end, and the non-welding end face is flat and ground. The outer circle of the face, the end face and the inner hole, and at the same time, the step plane used for the positioning of the friction welding between the subsequent turbine and the optical axis is finished, and the outer circle at the blade is re-calibrated during processing to ensure that the center of the turbine is processed and the subsequent friction welding. The center is consistent, reducing the unbalance of the turbine shaft caused by the misalignment of the turbine and the optical axis during friction welding.

具体方式:Specific way:

S61软三爪夹所述涡轮毛坯焊接端外圆;S61 soft three-jaw clamps the outer circle of the welding end of the turbine blank;

S62找正非焊接端外圆和端面,精车。S62 Align the outer circle and end face of the non-welded end, and finish turning.

以上所揭露的仅为本发明一种专利名称较佳实施例而已,当然不能以此来限定本发明之权利范围,本领域普通技术人员可以理解实现上述实施例的全部或部分流程,并依本发明权利要求所作的等同变化,仍属于发明所涵盖的范围。The above disclosure is only a preferred embodiment of the present invention, and of course, it cannot limit the scope of rights of the present invention. Those of ordinary skill in the art can understand that all or part of the process of realizing the above embodiment can be implemented according to the present invention. The equivalent changes made by the invention claims still belong to the scope covered by the invention.

Claims (5)

1.一种增压器铸造涡轮加工方法,其特征在于,包括以下步骤:1. a supercharger casting turbine processing method, is characterized in that, comprises the following steps: 粗车涡轮毛坯焊接端外圆及端面;The outer circle and end face of the welding end of the rough turning turbine blank; 软三爪夹所述涡轮毛坯焊接端外圆;The outer circle of the welding end of the turbine blank is clamped by the soft three-jaw clamp; 在粗车后的所述端面上顶中心孔;Top the center hole on the end face after rough turning; 以所述中心孔为基准对所述涡轮毛坯进行磨削;grinding the turbine blank based on the center hole; 切割所述粗车涡轮毛坯焊接端外圆长度;cutting the outer circle length of the welding end of the rough turning turbine blank; 精车所述涡轮毛坯焊接端,得到成品涡轮。Finish turning the welded end of the turbine blank to obtain a finished turbine. 2.如权利要求1所述的一种增压器铸造涡轮加工方法,其特征在于,2. A kind of supercharger casting turbine processing method as claimed in claim 1 is characterized in that, 在步骤精车所述涡轮毛坯焊接端,得到成品涡轮之后,所述方法还包括:After finishing the welding end of the turbine blank to obtain a finished turbine, the method further includes: 将主轴与所述成品涡轮焊接端焊接,并做动平衡处理。Weld the main shaft and the welded end of the finished turbine, and do dynamic balancing treatment. 3.如权利要求1所述的一种增压器铸造涡轮加工方法,其特征在于,3. A kind of supercharger casting turbine processing method as claimed in claim 1 is characterized in that, 所述粗车涡轮毛坯焊接端外圆及端面的具体方式:The specific method of the outer circle and end face of the welding end of the rough turning turbine blank: 三爪夹所述涡轮毛坯焊接端外圆,找正外圆及端面;Three claws clamp the outer circle of the welding end of the turbine blank, and align the outer circle and end face; 光出端面打中心孔,粗车所述涡轮毛坯。Punch a center hole on the end face of the light, and rough the turbine blank. 4.如权利要求1所述的一种增压器铸造涡轮加工方法,其特征在于,4. a kind of supercharger casting turbine processing method as claimed in claim 1 is characterized in that, 所述在粗车后的所述端面上顶中心孔的具体方式:The specific method of topping the center hole on the end face after rough turning: 顶出中心孔,光出端面高点;Eject the center hole, and light out the high point of the end face; 光出外圆及端面。Light out the outer circle and end face. 5.如权利要求1所述的一种增压器铸造涡轮加工方法,其特征在于,5. A kind of supercharger casting turbine processing method as claimed in claim 1 is characterized in that, 所述精车涡轮毛坯焊接端,得到成品涡轮的具体方式:The concrete method of obtaining the finished turbine from the welding end of the finished turbine blank: 软三爪夹所述涡轮毛坯焊接端外圆;The outer circle of the welding end of the turbine blank is clamped by the soft three-jaw clamp; 找正非焊接端外圆和端面,精车。Align the outer circle and end face of the non-welded end, and finish turning.
CN202210910185.4A 2022-07-29 2022-07-29 A kind of supercharger casting turbine processing method Pending CN115091145A (en)

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Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1134358A2 (en) * 2000-03-13 2001-09-19 Ishikawajima Mass-Produced Machinery Co., Ltd. Method of machining the turbine rotor shaft of a supercharger
JP2004052616A (en) * 2002-07-18 2004-02-19 Ndk Kako Center Kk Method of machining turbine blade of supercharger
CN1693675A (en) * 2005-05-17 2005-11-09 江津增压器厂 Manufacturing method of small sized turbine shaft
CN1693677A (en) * 2005-05-17 2005-11-09 江津增压器厂 Manufacturing method of small sized turbine
KR20110017667A (en) * 2009-08-14 2011-02-22 두산중공업 주식회사 Grinding method for bucket tip of the turbine-rotor
WO2015087907A1 (en) * 2013-12-13 2015-06-18 昭和電工株式会社 Formed material for turbo-compressor wheel made of aluminum alloy, and method of manufacturing turbo-compressor wheel
CN113020899A (en) * 2020-12-28 2021-06-25 重庆江增船舶重工有限公司 Method for processing compressed air impeller of ZR series supercharger
KR20220099232A (en) * 2021-01-06 2022-07-13 주식회사 삼정터빈 A vacuum investment casting system and method of turbine wheel for a turbocharger

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1134358A2 (en) * 2000-03-13 2001-09-19 Ishikawajima Mass-Produced Machinery Co., Ltd. Method of machining the turbine rotor shaft of a supercharger
JP2004052616A (en) * 2002-07-18 2004-02-19 Ndk Kako Center Kk Method of machining turbine blade of supercharger
CN1693675A (en) * 2005-05-17 2005-11-09 江津增压器厂 Manufacturing method of small sized turbine shaft
CN1693677A (en) * 2005-05-17 2005-11-09 江津增压器厂 Manufacturing method of small sized turbine
KR20110017667A (en) * 2009-08-14 2011-02-22 두산중공업 주식회사 Grinding method for bucket tip of the turbine-rotor
WO2015087907A1 (en) * 2013-12-13 2015-06-18 昭和電工株式会社 Formed material for turbo-compressor wheel made of aluminum alloy, and method of manufacturing turbo-compressor wheel
CN113020899A (en) * 2020-12-28 2021-06-25 重庆江增船舶重工有限公司 Method for processing compressed air impeller of ZR series supercharger
KR20220099232A (en) * 2021-01-06 2022-07-13 주식회사 삼정터빈 A vacuum investment casting system and method of turbine wheel for a turbocharger

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