JP2011177869A - End mill and machining method using the same - Google Patents

End mill and machining method using the same Download PDF

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JP2011177869A
JP2011177869A JP2010046847A JP2010046847A JP2011177869A JP 2011177869 A JP2011177869 A JP 2011177869A JP 2010046847 A JP2010046847 A JP 2010046847A JP 2010046847 A JP2010046847 A JP 2010046847A JP 2011177869 A JP2011177869 A JP 2011177869A
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umbrella
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end mill
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JP5260580B2 (en
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Mitsuhiro Matsuzaka
充浩 松坂
Koichiro Kuji
広一郎 久慈
Ryosuke Hoshina
良祐 保科
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Mitsubishi Heavy Industries Ltd
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Abstract

<P>PROBLEM TO BE SOLVED: To provide a machining method reducing machining man-hour by reducing centering work of a half-annular member and an umbrella-like end mill to half in every replacement of the half-annular member by machining an inclination surface with reverse slope only by movement of the umbrella-like end mill using the umbrella-like end mill when the inclination surface of a joint surface of an annular member formed in a ring-like shape by opposing the half-annular members of the same shape is machined. <P>SOLUTION: A first joint surface 11 having a first C inclination surface 113 extending along an annular axis direction is provided on one end of a half-annular turbine stationary blade 1 of the same shape, and a second joint surface 12 formed in a shape corresponding to the first joint surface 11 shape and having a second C inclination surface 123 is provided on the other end. The umbrella-like end mill 4 attached with a roughing tip 5 on an inclination part 41 having the same inclination as the respective inclination surfaces 11, 12 is moved along a surface plate 2. Thereby, the first C inclination surface 113 and the second inclination surface 123 can be cutting-machined. <P>COPYRIGHT: (C)2011,JPO&INPIT

Description

本発明は、半環状部材を対向させて、環状に継ぎ合せる合せ面を加工するエンドミルとそれを用いて加工する方法に関する。   The present invention relates to an end mill for processing a mating surface to be joined in an annular manner by facing semi-annular members and a method of processing using the end mill.

直径の大きいタービンの静翼を製造する場合、半割りの同一形状の部品を製造して、それを対向させて環状に継ぎ合せる構造としている。
従って、半割り形状のタービン静翼を継ぎ合せる継ぎ合せ面は、組立時における合せ面のずれを防止するために、立体形状の合せ面にの凹凸が倣うような形状にする場合が多い。
In the case of manufacturing a turbine vane having a large diameter, a structure in which halved parts having the same shape are manufactured and joined in an annular shape facing each other is produced.
Accordingly, the joining surface for joining the half-shaped turbine stationary blades is often shaped so that the unevenness of the three-dimensional joining surface follows the three-dimensional joining surface in order to prevent the joining surface from being displaced during assembly.

半環状部材の一端は半環状部材を組合せて環状にしたときの軸線を含む面に沿って形成された第一A面と、該A面に連続して軸線方向に沿って延在する第一傾斜面と、該第一傾斜面に連続して第一A面と平行に配置された第一B面とを有する第一接合面が形成されている。
一方、他端には第一接合面を倣うように当接する面が形成されている。
即ち、他端の第二接合面には、第一A面と当接する第二A面と、第一傾斜面に添った面の第二傾斜面及び第一B面と当接する第二B面とを有している。
第一A面と第二A面及び、第一B面と第二B面とが夫々凹凸の関係にある。
その結果、半割り状の同一形状の部品2個を対向させて、環状に継ぎ合せることが可能となる。
One end of the semi-annular member is a first A surface formed along a plane including an axis when the semi-annular members are combined into an annular shape, and a first extending continuously along the axial direction to the A surface. A first joint surface having an inclined surface and a first B surface arranged in parallel with the first A surface in succession to the first inclined surface is formed.
On the other hand, a surface that abuts on the other end so as to follow the first joint surface is formed.
That is, the second joining surface at the other end includes a second A surface that comes into contact with the first A surface, a second inclined surface that follows the first inclined surface, and a second B surface that comes into contact with the first B surface. And have.
The first A surface and the second A surface, and the first B surface and the second B surface are in an uneven relationship.
As a result, two halved parts having the same shape can be made to face each other and joined together in an annular shape.

ところが、第一傾斜面と第二傾斜面は傾斜の方向が異なっているため、図5に示すように、半環状部材01の接合面の加工は、基準加工面として、一端の第一A面011及び第一B面012と、第一A面011及び第一B面012を水平状に連続する水平部014(2点鎖線部)からなる鉤状に形成される。次の工程で、他端の第二A面、第二B面及び、第二A面と第二B面とを接続する水平部が形成される。(図示省略)
その後、エンドミル02によって水平部014を切削して第一傾斜面013が階段状に加工される。
ところが、エンドミルで第一傾斜面013の切削加工が完了すると、定盤上の半環状部材を反転する必要があり、半環状部材を反転後にエンドミルと半環状部材との芯合せを行い、固定する必要がある。
この反転作業は、第二A面と第二B面を接続する水平部(下向き面)に形成される第二傾斜面が下向き傾斜状態の切削加工となるため、加工精度が確保し難いためである。
特に、発電用等に使用される大型の静翼タービンの場合には、クレーン等を使用して2人がかりでセットしなければならず、その作業に多大な工数を必要とし、コストが高くなる要因となっていた。
However, since the first inclined surface and the second inclined surface are different in the direction of the inclination, as shown in FIG. 5, the processing of the joint surface of the semi-annular member 01 is the first A surface at one end as a reference processing surface. The first A surface 011 and the first B surface 012, and the first A surface 011 and the first B surface 012 are formed in a bowl shape including horizontal portions 014 (two-dot chain line portions) that are horizontally continuous. In the next step, the second part A, the second part B, and the horizontal part connecting the second part A and the second part B are formed. (Not shown)
Thereafter, the horizontal portion 014 is cut by the end mill 02 to process the first inclined surface 013 into a step shape.
However, when the cutting of the first inclined surface 013 is completed by the end mill, it is necessary to reverse the semi-annular member on the surface plate, and after reversing the semi-annular member, the end mill and the semi-annular member are aligned and fixed. There is a need.
This inversion work is because it is difficult to ensure the machining accuracy because the second inclined surface formed on the horizontal portion (downward surface) connecting the second A surface and the second B surface is a cutting operation in a downward inclined state. is there.
In particular, in the case of a large stationary blade turbine used for power generation or the like, it must be set by two persons using a crane or the like, which requires a large number of man-hours for the work and increases the cost. It was a factor.

傾斜面を切削する特許文献1として、特開2004−34170号公報が知られている。図6に示すように特許文献1によると、案内ローラ070の周面070aとエンドミル010の刃部010aとでシート材020を挟み込み、エンドミル010の軸線を案内ローラ070の回転軸線Lに対し所定角度α分傾斜させて、案内ローラ070及びエンドミル010を所定の速度で回転させ傾斜面加工を行う技術が開示されている。
この場合でも、案内ローラ070の回転軸線Lに対し、エンドミル010の傾斜角度αを変更する場合は、傾斜角度αの調整と共に、傾斜角度αの変更に伴いエンドミル010とシート材020との相対位置関係がずれ、シート材020の切削加工範囲がずれるので、エンドミル010の軸線方向位置の修正も必要となり、調整作業に多数の工数を要する。
Japanese Patent Application Laid-Open No. 2004-34170 is known as Patent Document 1 for cutting an inclined surface. As shown in FIG. 6, according to Patent Document 1, the sheet material 020 is sandwiched between the peripheral surface 070a of the guide roller 070 and the blade portion 010a of the end mill 010, and the axis of the end mill 010 is set at a predetermined angle with respect to the rotation axis L of the guide roller 070. A technique is disclosed in which an inclined surface machining is performed by inclining α and rotating the guide roller 070 and the end mill 010 at a predetermined speed.
Even in this case, when the inclination angle α of the end mill 010 is changed with respect to the rotation axis L of the guide roller 070, the relative position between the end mill 010 and the sheet material 020 is changed along with the adjustment of the inclination angle α. Since the relationship is shifted and the cutting range of the sheet material 020 is shifted, it is necessary to correct the axial position of the end mill 010, and a large number of man-hours are required for the adjustment work.

また、エンドミル構造が特許文献2として、特開平7−195221号公報に開示されている。図7に示すように、工具本体080の外周部に複数の波形状の切れ刃081またはニックを有した切れ刃を設け、先端部にボール状のボール刃082を有したラフィングボールエンドミルが開示されている。
この場合、切れ刃が摩耗すると、工具全体080を交換する必要があり、材料価格の高価な高速度刃物鋼(俗称;ハイス)の無駄が大きくコスト的にも不利である。
An end mill structure is disclosed in Japanese Patent Laid-Open No. 7-195221 as Patent Document 2. As shown in FIG. 7, a roughing ball end mill is disclosed in which a plurality of wave-shaped cutting edges 081 or cutting edges having a nick are provided on the outer peripheral portion of a tool body 080, and a ball-shaped ball edge 082 is provided at the tip. ing.
In this case, if the cutting edge is worn, it is necessary to replace the entire tool 080, which is wasteful of expensive high-speed blade steel (common name; high speed), which is disadvantageous in terms of cost.

特開2004−34170号公報JP 2004-34170 A 特開平7−195221号公報JP-A-7-195221

本発明はかかる従来技術の課題に鑑み、同一形状の半環状部材を対向させて、環状に形成する環状部材の継ぎ合せ面の傾斜面を加工する際に、傘状エンドミルを使用して、勾配が逆の傾斜面を傘状エンドミルの移動のみで加工できるようにすることにより、半環状部材の反転毎に行う半環状部材と傘状エンドミルとの芯合せ作業を低減させて、加工工数の低減、継ぎ合せ面の加工精度向上を図った半環状部材の継ぎ合せ面を加工するエンドミルとそれを用いて加工する加工方法を提供することを目的とする。   In view of the problems of the prior art, the present invention uses an umbrella-shaped end mill to process the inclined surface of the joint surface of the annular member formed in an annular shape by facing the semi-annular members having the same shape to each other. By making it possible to machine the reverse inclined surface only by moving the umbrella-shaped end mill, the centering work between the semi-annular member and the umbrella-shaped end mill that is performed each time the semi-annular member is reversed is reduced, thereby reducing the number of processing steps. An object of the present invention is to provide an end mill for processing a joint surface of a semi-annular member and a processing method using the end mill for improving the processing accuracy of the joint surface.

本発明はかかる目的を達成するもので、同一形状の半環状部材を対向させて、環状に継ぎ合せる合せ面形状を有する前記半環状部材は、一端に前記環状の軸線方向に延在する第一傾斜面を有した第一継ぎ合せ面と、他端に前記第一継ぎ合せ面形状に倣う形状に形成され前記第一傾斜面と対向する形状を有する第二傾斜面とを有する第二継ぎ合せ面を有し、前記第一傾斜面と前記第二傾斜面の半環状部材の継ぎ合せ面加工方法において、
前記半環状部材を定盤上に固定して、前記半環状部材と、前記第一及び第二傾斜面と同じ傾斜を有する傾斜部に複数のラフィングチップが装着されている傘状エンドミルとの芯合せを行った後、前記傘状エンドミルにて前記第一傾斜面を形成する第一工程と、
前記傘状エンドミルを前記定盤に沿って前記他端に移動させ、前記傘状エンドミルにて前記第二継ぎ合せ面の前記第二傾斜面を形成する第二工程とを含む半環状部材の継ぎ合せ面の加工方法。
The present invention achieves such an object, and the semi-annular member having a mating surface shape in which the semi-annular members having the same shape are opposed to each other and joined in an annular shape is a first extending in the annular axial direction at one end. A second joint having a first joint surface having an inclined surface and a second inclined surface formed at the other end in a shape that follows the shape of the first joint surface and having a shape facing the first inclined surface. In the method for processing the joint surface of the semi-annular member of the first inclined surface and the second inclined surface,
The semi-annular member is fixed on a surface plate, and the core of the semi-annular member and an umbrella-shaped end mill having a plurality of luffing tips mounted on an inclined portion having the same inclination as the first and second inclined surfaces After performing the combination, a first step of forming the first inclined surface in the umbrella-shaped end mill,
A second step of moving the umbrella-shaped end mill to the other end along the surface plate and forming the second inclined surface of the second joint surface by the umbrella-shaped end mill; Processing method for mating surfaces.

かかる発明において、半環状部材の両端の形状が環状部材の軸線方向において対称形状となり、半環状部材両端の傾斜面切削を、傘状エンドミルを定盤に沿って、移動させることにより、傾斜面への切削押圧力方向が変わるだけで、半環状部材両端の傾斜面切削を行うことができるので、半環状部材を定盤上にてセットし直し(反転)、半環状部材とエンドミルとの芯合せ等の面倒な作業が低減でき、加工に要するコストが大幅に低減できる。   In such an invention, the shape of both ends of the semi-annular member is symmetrical in the axial direction of the annular member, and the inclined surface cutting of both ends of the semi-annular member is moved to the inclined surface by moving the umbrella-shaped end mill along the surface plate. Since the cutting surface of the semi-annular member can be cut only by changing the cutting pressure direction, the semi-annular member is reset on the surface plate (reversed), and the semi-annular member and the end mill are aligned. The troublesome work such as this can be reduced, and the cost required for processing can be greatly reduced.

また、本願発明において好ましくは、前記傘状エンドミルの先端部に装着されるラフィングチップは刃先の先端部にラフィング状のR形状刃部が形成されているとよい。   In the present invention, preferably, the luffing tip attached to the tip of the umbrella-shaped end mill is provided with a roughing R-shaped blade at the tip of the blade tip.

このような構成にすることにより、傾斜面に接続する面と傾斜面との角部のR加工及び、傾斜面の切削加工とが同時にできるので、加工工数が減少し、コスト低減が可能となる。   By adopting such a configuration, it is possible to simultaneously perform the R processing of the corner portion between the surface connected to the inclined surface and the inclined surface and the cutting processing of the inclined surface, thereby reducing the number of processing steps and reducing the cost. .

また、本願発明において好ましくは、前記傘状エンドミルは、前記傘状エンドミルの傾斜部に装着される前記ラフィング状の複数のチップが傘状円周上の回転方向前後位置で、前側の前記ラフィングチップの波形状位置と、後側の前記ラフィングチップの波形状位置とが前記傾斜部の傾斜に沿ってずらして装着されるとよい。 Preferably, in the invention of the present application, the umbrella-shaped end mill has a plurality of luffing-shaped chips mounted on an inclined portion of the umbrella-shaped end mill at a front-rear luffing chip at a front-rear position in a rotational direction on the umbrella-shaped circumference. It is preferable that the wave shape position of the rear side and the wave shape position of the luffing tip on the rear side are mounted while being shifted along the inclination of the inclined portion.

このような構成にすることにより、円周方向ラフィング状の切削残りの部分を、傘状の円周方向で回転方向後方に装着され、且つ傾斜部の傾斜に沿ってずらして装着されたラフィングチップがワークを切削するので、ずらした量によって傾斜部の表面粗さが調整でき、ずらし量を少なくすれば微細の加工面となり、仕様要求の荒さ程度によっては仕上げ工程が省略できる。
更に、緻密な仕上げ面が必要な場合は、仕上げ工程のハイスによる作業時間が短縮され、ハイスの摩耗量も減少して、ハイスの交換時期が延長でき工数低減によるコスト低減が可能となる。
By adopting such a configuration, the luffing tip is mounted with the remaining portion of the circumferential luffing cut attached in the rotational direction rearward in the umbrella-like circumferential direction and shifted along the inclination of the inclined portion. However, since the workpiece is cut, the surface roughness of the inclined portion can be adjusted by the amount of displacement, and if the amount of displacement is reduced, the surface becomes fine and the finishing process can be omitted depending on the degree of roughness required by the specification.
Furthermore, when a fine finish surface is required, the work time by the high speed of the finishing process is shortened, the amount of wear of the high speed is also reduced, the replacement time of the high speed can be extended, and the cost can be reduced by reducing the number of man-hours.

本発明において、前記第一傾斜面を、前記第一及び第二傾斜面と同じ傾斜を有する傾斜部に切削仕上げ用の刃部を有した傘状仕上げハイスで仕上げ加工する第三工程と、前記傘状仕上げハイスを前記定盤に沿って前記他端側に移動させ、前記第二傾斜面を仕上げ形成するとよい。   In the present invention, the third step of finishing the first inclined surface with an umbrella-shaped finishing high speed blade having a cutting edge on the inclined portion having the same inclination as the first and second inclined surfaces; It is preferable to move the umbrella-shaped finishing high speed along the surface plate to the other end side and finish the second inclined surface.

このような構成にすることにより、第一及び第二工程終了状態では加工された面が要求粗さを満たさない場合に、仕上げ加工を実施するが、仕上げ工程においても、該傘状エンドミルを定盤に沿って、移動させることにより、傾斜面への切削押圧力方向が変わるだけで、半環状部材両端の傾斜面切削を行うことができるので、半環状部材を定盤上にてセットし直し、半環状部材とエンドミルとの芯合せ等、面倒な作業が半減でき、加工に要するコストが大幅に低減できる。   With such a configuration, finishing is performed when the processed surface does not satisfy the required roughness in the finished state of the first and second steps, but the umbrella-shaped end mill is also defined in the finishing step. By moving along the plate, it is possible to cut the inclined surface at both ends of the semi-annular member only by changing the cutting pressure direction to the inclined surface, so set the semi-annular member on the surface plate again. The troublesome work such as centering of the semi-annular member and the end mill can be halved, and the cost required for processing can be greatly reduced.

本発明によれば、傘状エンドミルを定盤に沿って移動させることにより、半環状部材の両端の形状が環状部材の軸線方向において対称形状となっている傾斜面切削を、傘状エンドミルの傾斜面への切削押圧力方向が変わるだけで、両端の傾斜面切削を行うことができ、加工に要するコストが大幅に低減できる。
また、傘状エンドミルの先端部に装着されるラフィングチップは刃先の先端部にラフィング状のR形状の刃部が設けられているので、傾斜面の切削と同時に、傾斜面に接続する面と傾斜面との屈曲部のR加工が行えるため、加工工数が減少し、コスト低減が可能となる。
According to the present invention, by moving the umbrella-shaped end mill along the surface plate, the inclined surface cutting in which the shapes of both ends of the semi-annular member are symmetrical in the axial direction of the annular member is performed. By changing only the direction of the pressing force on the surface, it is possible to perform inclined surface cutting at both ends, and the cost required for processing can be greatly reduced.
Also, the luffing tip attached to the tip of the umbrella-shaped end mill is provided with a roughing R-shaped blade at the tip of the blade tip. Since the R processing of the bent portion with the surface can be performed, the number of processing steps is reduced, and the cost can be reduced.

は本発明の実施形態にかかる切削加工状況の概略図を示す。These show the schematic of the cutting condition concerning embodiment of this invention. は加工工程の加工形状とその順序を表す工程図をで、(A)は加工基準面の荒加工、(B)は基準平面仕上げ加工と、傾斜面荒加工、(C)は傾斜面仕上げ加工及び(D)はR部仕上げ加工図を示す。Is a process diagram showing the machining shape and sequence of machining processes, (A) rough machining of the machining reference surface, (B) reference flat surface finishing machining and inclined surface rough machining, (C) inclined surface finishing machining. And (D) shows the R section finishing process drawing. 本発明の実施形態にかかる傘状ラフィングチップ装着のエンドミル斜視図を示す。The end mill perspective view of the umbrella-like luffing tip mounting concerning the embodiment of the present invention is shown. 本発明の実施形態にかかり、(A)はラフィングチップの斜視図、(B)はラフィングR部の平面視拡大図を示す。1A is a perspective view of a luffing tip, and FIG. 2B is an enlarged plan view of a luffing R portion according to an embodiment of the present invention. 従来技術における傾斜面の切削加工形態図を示す。The cutting process figure of the inclined surface in a prior art is shown. 従来技術のおける他の切削加工形態図を示す。(特許文献1)The other cutting form figure in a prior art is shown. (Patent Document 1) 従来技術のおける他のラフィングエンドミルの外観図を示す。(特許文献2)The external view of the other roughing end mill in a prior art is shown. (Patent Document 2)

以下、本発明を図に示した実施形態を用いて詳細に説明する。
但し、この実施形態に記載されている構成部品の寸法、材質、形状、その相対配置などは特に特定的な記載がない限り、この発明の範囲をそれのみに限定する趣旨ではなく、単なる説明例にすぎない。
Hereinafter, the present invention will be described in detail with reference to embodiments shown in the drawings.
However, the dimensions, materials, shapes, relative arrangements, and the like of the components described in this embodiment are not intended to limit the scope of the present invention only to specific examples unless otherwise specifically described. Only.

図1は半環状部材である半環状タービン静翼1を定盤2上にセット用ブロック3を介して、固定用クランプ(図示省略)にて固定した状態である。エンドミル4は半環状タービン静翼1の傾斜面を切削加工する工具である。
エンドミル4を固定すると共に回転駆動させるヘッド部8は図示されない工作機械の摺動ベッド上を定盤2に沿って移動(摺動)可能に保持されている。工作機械の摺動ベッドと定盤2との相対位置関係は精密に維持されている。
また、ヘッド部8は摺動ベッドの移動方向に対し、直角方向(定盤2との距離)、及び上下方向への移動が高精度に調整できる装置を有している。
尚、図において、半環状タービン静翼1は各個所の説明を明確にするため、継ぎ合せ部の形状は切削加工終了状態の形状を記載してある。
FIG. 1 shows a state where a semi-annular turbine stationary blade 1 which is a semi-annular member is fixed on a surface plate 2 via a setting block 3 by a fixing clamp (not shown). The end mill 4 is a tool for cutting the inclined surface of the semi-annular turbine stationary blade 1.
A head portion 8 that fixes and rotates the end mill 4 is held so as to be movable (slidable) along a surface plate 2 on a sliding bed of a machine tool (not shown). The relative positional relationship between the sliding bed of the machine tool and the surface plate 2 is maintained precisely.
The head unit 8 has a device that can adjust the movement in the direction perpendicular to the moving direction of the sliding bed (distance from the surface plate 2) and the vertical direction with high accuracy.
In the drawing, in order to clarify the explanation of each part of the semi-annular turbine stationary blade 1, the shape of the joining portion is the shape in the cutting finished state.

図1に示すように、半環状タービン静翼1は半環状に形成され、一端には第一継ぎ合せ面11と、他端の第二継ぎ合せ面12とがA矢視方向で、図面上の上下方向において上下対称に形成されている。
半環状タービン静翼1は外周部となる外輪101と、タービンの出力軸であるロータ(図示省略)を外嵌する内輪102と、外輪101と内輪102との間にタービンの動翼に蒸気流が効率よく当たるように案内するノズル板103(翼)が固着されている。
As shown in FIG. 1, the semi-annular turbine vane 1 is formed in a semi-annular shape, and a first seaming surface 11 at one end and a second seaming surface 12 at the other end are in the direction of arrow A, Are formed symmetrically in the vertical direction.
The semi-annular turbine stationary blade 1 has an outer ring 101 as an outer periphery, an inner ring 102 that externally fits a rotor (not shown) that is an output shaft of the turbine, and a steam flow between the outer ring 101 and the inner ring 102 on the rotor blades of the turbine. The nozzle plate 103 (blade) is guided so as to guide it efficiently.

半環状タービン静翼1の一端の第一継ぎ合せ面11は軸線(環状に形成されたときの軸線)を含む面に沿って外輪101に形成された第一A面111、該第一A面111に連続して前記軸線方向に延在する傾斜面である第一C傾斜面113、該第一C傾斜面113に連続して前記第一A面111と平行に配置された第一B面112と、内輪102に形成され、第一A面111、第一C傾斜面113、及び第一B面112夫々と同一平面内に位置した、第一A´面114、第一C´傾斜面116、及び第一B´面115とで構成されている。
尚、以後説明の煩雑を防ぐため、第一A面111と第一A´面114とを併せて第一A面111と総称し、第一B面112と第一B´面115とを併せて第一B面112と総称し、第一C傾斜面113と第一C´傾斜面116とを併せて第一C傾斜面113と総称する。
A first seaming surface 11 at one end of the semi-annular turbine vane 1 includes a first A surface 111 formed on the outer ring 101 along a surface including an axis (axis when formed annularly), the first A surface. A first C inclined surface 113 that is an inclined surface extending in the axial direction continuously to 111, and a first B surface arranged in parallel to the first A surface 111 continuously to the first C inclined surface 113 112 and the first A ′ surface 114 and the first C ′ inclined surface formed on the inner ring 102 and located in the same plane as the first A surface 111, the first C inclined surface 113, and the first B surface 112, respectively. 116 and the first B ′ surface 115.
In addition, in order to prevent the following description from being complicated, the first A surface 111 and the first A ′ surface 114 are collectively referred to as the first A surface 111, and the first B surface 112 and the first B ′ surface 115 are combined. The first B surface 112 is collectively referred to, and the first C inclined surface 113 and the first C ′ inclined surface 116 are collectively referred to as a first C inclined surface 113.

一方、他端の外輪101には第二継ぎ合せ面12が第一継ぎ合せ面11の形状に倣う形状に形成され、第一A面111と対向する形状を有する第二A面121、第一C傾斜面113と対向する形状を有する第二C傾斜面123、第一B面112と対向する形状を有する第二B面122と、内輪102に形成され、第一A面121、第一C傾斜面123、及び第一B面122夫々と同一平面内に位置した、第一A´面124、第一C´傾斜面126、及び第二B´面125とで構成されている。
尚、以後説明の煩雑を防ぐため、第二A面121と第二A´面124とを併せて第二A面121と総称し、第二B面122と第二B´面125とを併せて第二B面122と総称し、第二C傾斜面123と第二C´傾斜面126とを併せて第二C傾斜面123と総称する。
従って、半環状タービン静翼1は同一形状の物を2個対向させて、第一継ぎ合せ面11と、第二継ぎ合せ面12とを互いに当接させて固着させることにより環状に形成される。
このように半環状に形成することにより、製造設備の大きさを半分にして、設備投資を半減させることができると共に、取扱いが容易となりコスト低減効果も有している。
On the other hand, the second joining surface 12 is formed on the outer ring 101 at the other end so as to follow the shape of the first joining surface 11, and the second A surface 121 having a shape facing the first A surface 111, the first A second C inclined surface 123 having a shape facing the C inclined surface 113, a second B surface 122 having a shape facing the first B surface 112, and the inner ring 102, the first A surface 121, the first C The first A ′ surface 124, the first C ′ inclined surface 126, and the second B ′ surface 125 are located in the same plane as the inclined surface 123 and the first B surface 122.
In addition, in order to prevent the following description from being complicated, the second A surface 121 and the second A ′ surface 124 are collectively referred to as a second A surface 121, and the second B surface 122 and the second B ′ surface 125 are combined. The second B surface 122 is collectively referred to, and the second C inclined surface 123 and the second C ′ inclined surface 126 are collectively referred to as a second C inclined surface 123.
Therefore, the semi-annular turbine stationary blade 1 is formed in an annular shape by causing two identically shaped objects to face each other and bringing the first seaming surface 11 and the second seaming surface 12 into contact with each other and fixing them together. .
By forming the semicircular ring in this way, the size of the manufacturing facility can be halved, the capital investment can be halved, the handling is facilitated, and the cost can be reduced.

第一継ぎ合せ面11及び第二継ぎ合せ面12の切削加工方法は、
半環状タービン静翼1がセット用ブロック3を介して定盤2上に載置され、固定用クランプ(図示省略)にて固定される。次に、半環状タービン静翼1の第一継ぎ合せ面11及び第二継ぎ合せ面12と切刃を有した切削工具(図示省略)との前後、左右、上下方向の芯合せを行い、切削加工の基準位置をセットする第1工程。
第2工程として、切削工具にて、第一継ぎ合せ面11の第一A面111を切削後、第一B面112を切削して、第一A面111と第一B面112間を鉤状に切削加工して、切削加工の基準面を形成する工程。(図2―Aの形状。斜線部を切削)
第3工程として、切削工具を定盤2に沿って他端である第二継ぎ合せ面12側に移動させ、第二継ぎ合せ面側12の第二A面121を切削後、第二B面122を切削して、第二A面121と第二B面122間を鉤状に切削加工して、切削加工の基準面を形成する工程。
尚、第二A面121と第二B面122の切削加工順序はどちらが先でも特別の理由はない。(図2―Aの形状。斜線部相当部を切削。)
The cutting method of the first joint surface 11 and the second joint surface 12 is as follows:
The semi-annular turbine stationary blade 1 is placed on the surface plate 2 via the setting block 3 and fixed by a fixing clamp (not shown). Next, the first and second joint surfaces 11 and 12 of the semi-annular turbine vane 1 are aligned with the cutting tool (not shown) having a cutting edge in the front-rear, left-right, and vertical directions to perform cutting. A first step of setting a processing reference position.
As a 2nd process, after cutting the 1st A surface 111 of the 1st splicing surface 11 with a cutting tool, the 1st B surface 112 is cut, and a gap between 1st A surface 111 and 1st B surface 112 is made. Process to form a reference surface for cutting. (Shape of Fig. 2-A. Cutting the shaded area)
As a third step, the cutting tool is moved along the surface plate 2 to the second joining surface 12 side, which is the other end, and after cutting the second A surface 121 on the second joining surface side 12, the second B surface The process of cutting 122, cutting between the 2nd A surface 121 and the 2nd B surface 122 in a bowl shape, and forming the reference surface of cutting.
Note that there is no special reason for the cutting order of the second A surface 121 and the second B surface 122 whichever comes first. (The shape of Fig. 2-A. The part corresponding to the shaded area is cut.)

第4工程として、複数のラフィングチップ5が装着されているエンドミル02(図5参照。この行程は従来と同じ。)にて、第一継ぎ合せ面11の第一A面111と第一B面112間の鉤状に切削加工された部分を荒引き加工して、第一C傾斜面113を形成する。(図2―Bの形状に切削)
第5工程として、エンドミル02を定盤2に沿って第二継ぎ合せ面12の側に移動させ、エンドミル02を第一C傾斜面113に押圧した切削圧力方向をエンドミル02の軸線に対し、反対側に押圧して、第二継ぎ合せ面12の第二A面121と第二B面122間の鉤状に切削加工された部分を荒引き加工して、第二C傾斜面123を形成する。(図2―Bの形状に切削)
As a fourth step, the first A surface 111 and the first B surface of the first joining surface 11 are obtained in an end mill 02 (see FIG. 5, this process is the same as the conventional one) on which a plurality of luffing tips 5 are mounted. The first C inclined surface 113 is formed by roughing a portion cut into a bowl shape between 112. (Cutting into the shape of Fig. 2-B)
As a fifth step, the end mill 02 is moved along the surface plate 2 toward the second joining surface 12, and the cutting pressure direction in which the end mill 02 is pressed against the first C inclined surface 113 is opposite to the axis of the end mill 02. The second C inclined surface 123 is formed by roughing the portion of the second joint surface 12 that has been cut into a bowl shape between the second A surface 121 and the second B surface 122. . (Cutting into the shape of Fig. 2-B)

第6行程として、第一継ぎ合せ面11の第一A面111と第一B面112をスローアウェイ式フライス工具で仕上げ加工をする。
第7工程として、フライス工具を定盤2に沿って第二継ぎ合せ面12の側に移動させ、同様に第二A面121と第二B面122の仕上げ加工を実施する。
As the sixth step, the first A surface 111 and the first B surface 112 of the first joint surface 11 are finished with a throw-away milling tool.
As a seventh step, the milling tool is moved along the surface plate 2 to the second joining surface 12 side, and finishing of the second A surface 121 and the second B surface 122 is similarly performed.

第8工程として、複数のラフィングチップ5が第一C及び第二C傾斜面113,123と同じ傾斜で、且つ傾斜と同じか、又は、若干長い長さ(A面からB面方向の長さ)を有する傾斜部41(図3)に装着された所謂、総型形状の傘状エンドミル4の先端部を、第一A面111と第一C傾斜部との屈曲部に芯合せを行う。傘状エンドミル4にて第一C傾斜面113を形成する。(いわゆる第一工程。)
第9工程として、傘状エンドミル4を定盤2に沿って第二継ぎ合せ面12側に移動させ、傘状エンドミル4の切削圧力方向を傘状エンドミルの軸線に対し、第一C傾斜面113に押圧した方向と反対側に押圧して、第二継ぎ合せ面12の第二A面121と第二B面122間の第二C傾斜面123を形成する。(いわゆる第二工程。)
As an eighth step, the plurality of luffing chips 5 have the same inclination as the first C and second C inclined surfaces 113 and 123, and the same length as the inclination, or a slightly longer length (length from the A surface to the B surface direction). The tip of the so-called general-shaped umbrella-shaped end mill 4 mounted on the inclined portion 41 (FIG. 3) having the) is aligned with the bent portion of the first A surface 111 and the first C inclined portion. The first C inclined surface 113 is formed by the umbrella-shaped end mill 4. (So-called first step)
As a ninth step, the umbrella-shaped end mill 4 is moved to the second joining surface 12 side along the surface plate 2, and the cutting pressure direction of the umbrella-shaped end mill 4 is set to the first C inclined surface 113 with respect to the axis of the umbrella-shaped end mill. The second C inclined surface 123 between the second A surface 121 and the second B surface 122 of the second joining surface 12 is formed by pressing to the opposite side to the direction pressed. (So-called second step)

本実施形態において、傘状エンドミル4を保持しているヘッド部8は工作機械の摺動ベッド上を定盤2に沿って、定盤2との相対位置関係を高精度に維持しながら移動できるようになっており、且つ、第一及び第二C傾斜面113,123の傾斜と同じ傾斜を有する傘状エンドミル4の切削圧力方向がかわる構成なので、半環状タービン静翼1を反転させる従来の工法に比べ、加工精度を高くすることが容易となる。
また、半環状タービン静翼1を反転させる作業が省略できるので、半環状タービン静翼1と傘状エンドミル4との芯合せ作業が半減でき、加工工数減に伴うコスト低減が可能となる。
In the present embodiment, the head portion 8 holding the umbrella-shaped end mill 4 can move on the sliding bed of the machine tool along the surface plate 2 while maintaining the relative positional relationship with the surface plate 2 with high accuracy. Since the cutting pressure direction of the umbrella-shaped end mill 4 having the same inclination as the inclinations of the first and second C inclined surfaces 113 and 123 is changed, the conventional semi-annular turbine stator blade 1 is inverted. Compared to the construction method, it becomes easy to increase the processing accuracy.
Further, since the work of inverting the semi-annular turbine stationary blade 1 can be omitted, the centering work of the semi-annular turbine stationary blade 1 and the umbrella-shaped end mill 4 can be halved, and the cost can be reduced along with the reduction in the number of processing steps.

本実施形態では、傘状エンドミル4に装着される複数のラフィングチップ5を図4に示すように、コーナ部にR形状の刃部を有したラフィングR部51を設け、少なくとも図3のB部に配置した。
これにより第一A面111と第一C傾斜面113との凹状の屈曲部の面取り第一Rを第一C傾斜面113切削加工と同時に行えるようにした。
また、コーナ部のR形状の刃部は他の平面部よりラフィングのピッチを小さくして、凹状の屈曲部の面取り第一Rの面粗さを小さくすることにより、コーナ部に発生しやすい応力を低減させる効果を有している。
In the present embodiment, as shown in FIG. 4, a plurality of luffing tips 5 attached to the umbrella-shaped end mill 4 are provided with a roughing R portion 51 having an R-shaped blade portion at a corner portion, and at least a portion B in FIG. 3. Arranged.
As a result, the first chamfering of the concave bent portion between the first A surface 111 and the first C inclined surface 113 can be performed simultaneously with the cutting of the first C inclined surface 113.
In addition, the R-shaped blade portion of the corner portion is less likely to generate stress in the corner portion by reducing the luffing pitch than other flat portions and reducing the chamfered first R surface roughness of the concave bent portion. Has the effect of reducing.

更に、傘状エンドミル4の傾斜面41に配置した複数のラフィングチップ5の配置を、
傾斜面41の円周上において、傘状エンドミル4の回転方向の前後位置で、前側のラフィングチップ5の波形状位置に対し、後側のラフィングチップ5の波形状位置が傾斜面41に沿ってずらして装着されている。
ずらす量を1/4ピッチ(ラフィング)にすると、ラフィングピッチの1/4の切削荒さになり、1/2ピッチにすると1/4ピッチの倍の荒さに切削される。
従って、ずらす量を少なくすることにより研削される第一C傾斜面(含む第二C傾斜面)の切削表面粗さを微細にすることができ、要求仕様によっては仕上げ工程を省略できる可能性もある。
また、前の工程では切削表面粗さが、要求仕様を満たさない場合は、更に、以下の工程を追加する。
Furthermore, the arrangement of the plurality of luffing tips 5 arranged on the inclined surface 41 of the umbrella-shaped end mill 4 is as follows.
On the circumference of the inclined surface 41, the wave shape position of the rear luffing tip 5 is along the inclined surface 41 with respect to the wave shape position of the front luffing tip 5 at the front and rear positions in the rotational direction of the umbrella-shaped end mill 4. It is installed with a shift.
When the shift amount is set to 1/4 pitch (roughing), the cutting roughness becomes 1/4 of the luffing pitch, and when it is set to 1/2 pitch, the cutting is performed to a roughness twice the 1/4 pitch.
Therefore, the cutting surface roughness of the first C inclined surface (including the second C inclined surface) to be ground can be made fine by reducing the amount of shifting, and the finishing process may be omitted depending on the required specifications. is there.
Moreover, when the cutting surface roughness does not satisfy the required specifications in the previous step, the following steps are further added.

第10工程として、複数のラフィングチップ5を装着した傘状エンドミル4に換え、第一C及び第二C傾斜面113,123と同じ傾斜で、且つ傾斜と同じか、又は、若干長い長さ(A面からB面方向の長さ)を有した傾斜部の傾斜面に切削刃61を有した総型形状の傘状仕上げハイス6にて第一継ぎ合せ面11側の第一C傾斜面113を仕上げ加工するいわゆる第三工程。(図2−Cの形状)
第11工程として、傘状の仕上げハイス6を定盤2に沿って第二継ぎ合せ面12側に移動させ、第二継ぎ合せ面12側の第二C傾斜面123を仕上げ加工するいわゆる第四工程。(図2−Cの形状)
As a tenth step, instead of the umbrella-shaped end mill 4 equipped with a plurality of luffing tips 5, the same inclination as the first C and second C inclined surfaces 113 and 123 and the same as the inclination or a slightly longer length ( The first C inclined surface 113 on the first joining surface 11 side by the umbrella-shaped finishing high speed 6 having a cutting blade 61 on the inclined surface of the inclined portion having a length from the A surface to the B surface direction). So-called third process of finishing. (Shape of Fig. 2-C)
As an eleventh step, the umbrella-shaped finishing high speed 6 is moved along the surface plate 2 to the second joining surface 12 side, and the second C inclined surface 123 on the second joining surface 12 side is finished so-called fourth. Process. (Shape of Fig. 2-C)

第12工程として、傘状の仕上げハイス6に換え、切刃が凹状になったR状ハイス7(図2―D参照)にて、第一継ぎ合せ面11側の第一C傾斜面113と第一B面との凸状屈曲部の第二Rを面取りする仕上げ工程。(図2−Dの形状)
第13工程として、R状ハイス7を定盤2に沿って第二継ぎ合せ面12側に移動させて、第二継ぎ合せ面12側の第二C傾斜面123と第二B面122との凸状屈曲部の第二Rを面取りする仕上げ工程。(図2−Dの形状)
As a twelfth step, in place of the umbrella-shaped finishing high speed 6, an R-shaped high speed 7 having a concave cutting edge (see FIG. 2D), the first C inclined surface 113 on the first joining surface 11 side, A finishing step of chamfering the second R of the convex bent portion with the first B surface. (Shape of Fig. 2-D)
As a thirteenth step, the R-shaped high speed 7 is moved along the surface plate 2 to the second joining surface 12 side, and the second C inclined surface 123 and the second B surface 122 on the second joining surface 12 side are A finishing step of chamfering the second R of the convex bent portion. (Shape of Fig. 2-D)

以上の工程を経て半環状タービン静翼1の第一継ぎ合せ面11及び第二継ぎ合せ面12の合せ面の切削加工が終了する。
尚、本実施形態では、加工工程の始りを第一継ぎ合せ面11側から実施するように記載したが、第二継ぎ合せ面12側で終了し、次の形状の切削工程に移る場合、第二継ぎ合せ面12側で次の形状の切削工程を始め、切削工程終了後に、第一継ぎ合せ面11側に工具を移動させて、第一継ぎ合せ面11側において同じ形状の切削工程を実施するようにすることも可能であることは当然である。
The cutting process of the mating surfaces of the first seaming surface 11 and the second seaming surface 12 of the semi-annular turbine stationary blade 1 is completed through the above steps.
In the present embodiment, the start of the machining process is described to be performed from the first joining surface 11 side, but when the process ends at the second joining surface 12 side and the process proceeds to the cutting process of the next shape, The cutting process of the next shape is started on the second joining surface 12 side, and after the cutting process is finished, the tool is moved to the first joining surface 11 side, and the cutting process of the same shape is performed on the first joining surface 11 side. Of course, it is also possible to implement.

本実施形態によると、半環状タービン静翼1の両端に傾斜部を有した形状が、半環状タービン静翼1の軸線方向において対称形状となっている半環状タービン静翼1両端の第一及び第二傾斜面113,123の切削を、傘状エンドミル4を定盤に沿って、移動させることにより、第一及び第二傾斜面113,123への切削押圧力方向が変わるだけで、半環状タービン静翼1の両端の第一及び第二傾斜面113,123切削を可能としたので、半環状タービン静翼1を定盤2上にて反転させて、半環状タービン静翼1とエンドミルとの芯合せ等の面倒な作業が半減でき、加工工数の低減によるコスト低減ができる。
また、傘状エンドミル5の先端部に装着されるラフィングチップ5の刃先の先端部にラフィング状のR形状刃部を形成したので、第一A面111と第一傾斜面113及び第二A面と第二傾斜面123との屈曲部の第一R加工が、傾斜面加工と同時に行えるため、加工工数が減少し、コスト低減が可能となる。
尚、ラフィングチップ5の刃先の先端部にラフィング状のR形状刃部を形成したラフィングチップ5は傘状エンドミル4の先端部だけに使用するものではなく、傾斜部41の他の部分に装着して使用することにより、ラフィングチップ5の共通化、部品管理点数の増加抑制によるコスト低減効果を図れる。
According to the present embodiment, the first and the second ends of the semi-annular turbine stationary blades 1 are configured so that the shapes having the inclined portions at both ends of the semi-annular turbine stationary blade 1 are symmetrical in the axial direction of the semi-annular turbine stationary blade 1. By moving the umbrella-shaped end mill 4 along the surface plate to cut the second inclined surfaces 113 and 123, only the cutting pressure direction on the first and second inclined surfaces 113 and 123 is changed, so that the semi-annular shape is changed. Since the first and second inclined surfaces 113 and 123 at both ends of the turbine vane 1 can be cut, the semi-annular turbine vane 1 is reversed on the surface plate 2, and the semi-annular turbine vane 1 and the end mill The troublesome work such as centering can be cut in half, and the cost can be reduced by reducing the number of processing steps.
Further, since the luffing R-shaped blade portion is formed at the tip portion of the cutting edge of the luffing tip 5 attached to the tip portion of the umbrella-shaped end mill 5, the first A surface 111, the first inclined surface 113, and the second A surface Since the first R processing of the bent portion between the second inclined surface 123 and the second inclined surface 123 can be performed simultaneously with the inclined surface processing, the number of processing steps can be reduced and the cost can be reduced.
The luffing tip 5 in which the luffing R-shaped blade portion is formed at the tip of the cutting edge of the luffing tip 5 is not used only at the tip of the umbrella-shaped end mill 4, and is attached to the other portion of the inclined portion 41. The cost reduction effect can be achieved by using the luffing chip 5 in common and suppressing the increase in the number of parts management points.

同一形状の半環状部材を対向させて、環状に継ぎ合せる合せ面形状を有する前記半環状部材の接合面が環状の軸線方向に対して対称形状に形成されている傾斜面を、該傾斜面の傾斜に沿った傘状エンドミル加工を要するタービン静翼等に適用できる。   An inclined surface in which the joining surface of the semi-annular member having a mating surface shape that faces the semi-annular members of the same shape and joins in an annular shape is formed symmetrically with respect to the annular axial direction is formed on the inclined surface. The present invention can be applied to turbine stationary blades that require umbrella-shaped end mill processing along an inclination.

1 半環状タービン静翼
2 定盤
3 セット用ブロック
4 傘状エンドミル
5 ラフィングチップ
6 仕上げハイス
7 R状ハイス
11 第一継ぎ合せ面
12 第二継ぎ合せ面
41 傾斜部
51 ラフィングR部
61 切削刃
101 外輪
102 内輪
103 ノズル板
111 第一A面
112 第一B面
113 第一C面
121 第二A面
122 第二B面
123 第二C面
DESCRIPTION OF SYMBOLS 1 Semi-annular turbine stationary blade 2 Surface plate 3 Block for set 4 Umbrella-shaped end mill 5 Roughing tip 6 Finishing high speed 7 R-shaped high speed 11 First joint surface 12 Second joint surface 41 Inclined portion 51 Roughing R portion 61 Cutting blade 101 Outer ring 102 Inner ring 103 Nozzle plate 111 First A surface 112 First B surface 113 First C surface 121 Second A surface 122 Second B surface 123 Second C surface

Claims (4)

同一形状の半環状部材を対向させて、環状に継ぎ合せる合せ面形状を有する前記半環状部材は、一端に前記環状の軸線方向に延在する第一傾斜面を有した第一継ぎ合せ面と、他端に前記第一継ぎ合せ面形状に倣う形状に形成され前記第一傾斜面と対向する形状を有する第二傾斜面とを有する第二継ぎ合せ面を有し、前記第一傾斜面と前記第二傾斜面の半環状部材の継ぎ合せ面加工方法において、前記半環状部材を定盤(定磐)上に固定して、前記半環状部材と、前記第一及び第二傾斜面と同じ傾斜を有する傾斜部に複数のラフィングチップが装着されている傘状エンドミルとの芯合せを行った後、前記傘状エンドミルにて前記第一傾斜面を形成する第一工程と、前記傘状エンドミルを前記定盤に沿って前記他端に移動させ、前記傘状エンドミルにて前記第二継ぎ合せ面の前記第二傾斜面を形成する第二工程とを含む半環状部材の継ぎ合せ面の加工方法。   The semi-annular member having a mating surface shape for facing the semi-annular members of the same shape and joining them in an annular shape includes a first seaming surface having a first inclined surface extending in the annular axial direction at one end. A second seam surface having a second sloped surface having a shape opposite to the first sloped surface and having a shape facing the first sloped surface at the other end, and the first sloped surface, In the joint surface processing method of the semi-annular member of the second inclined surface, the semi-annular member is fixed on a surface plate (fixed surface), and the same as the semi-annular member and the first and second inclined surfaces. A first step of forming the first inclined surface with the umbrella-shaped end mill after centering with an umbrella-shaped end mill having a plurality of luffing tips attached to an inclined portion having an inclination; and the umbrella-shaped end mill; Is moved to the other end along the surface plate, and the umbrella-shaped end Processing method of seaming surface of the semi-annular member and a second step of forming the second inclined surface of said second seaming surface at. 前記傘状エンドミルの先端部に装着されるラフィングチップは刃先の先端部にラフィング状のR形状刃部が形成されていることを特徴とする請求項1記載の半環状部材の継ぎ合せ面の加工方法。   2. The processing of the joining surface of the semi-annular member according to claim 1, wherein the roughing tip attached to the tip of the umbrella-shaped end mill has a roughing R-shaped blade at the tip of the blade tip. Method. 前記傘状エンドミルは、前記傘状エンドミルの傾斜部に装着される前記ラフィング状の複数のチップが傘状円周上の回転方向前後位置で、前側の前記ラフィングチップの波形状位置と、後側の前記ラフィングチップの波形状位置とが前記傾斜部の傾斜に沿ってずらして装着されていることを特徴とする請求項1又は2記載の半環状部材の継ぎ合せ面の加工方法。   In the umbrella-shaped end mill, the plurality of luffing-shaped tips attached to the inclined portion of the umbrella-shaped end mill are front and rear positions in the rotational direction on the umbrella-shaped circumference, the wave-shaped position of the luffing tip on the front side, and the rear side 3. The method for processing a joining surface of a semi-annular member according to claim 1, wherein the luffing tip is mounted with a wave shape position shifted along the inclination of the inclined portion. 本発明において、前記第一傾斜面を前記第一及び第二傾斜面と同じ傾斜を有する傾斜部に切削仕上げ用の刃部を有した傘状仕上げハイスで仕上げ加工する第三工程と、前記傘状仕上げハイスを前記定盤に沿って前記他端側に移動させ、前記傘状仕上げハイスを前記第一傾斜面に押圧した切削圧力方向を前記傘状仕上げハイスの軸線に対し、反対側に押圧して前記第二傾斜面を仕上げ形成する第四工程を含むことを特徴とする請求項1または3記載の半環状部材の継ぎ合せ面の加工方法。   In the present invention, the third step of finishing the first inclined surface with an umbrella-shaped finishing high speed blade having a cutting edge for an inclined portion having the same inclination as the first and second inclined surfaces, and the umbrella The shape finishing high speed is moved to the other end side along the surface plate, and the cutting pressure direction in which the umbrella shaped finishing high speed is pressed against the first inclined surface is pressed opposite to the axis of the umbrella shaped finishing high speed. The method for processing a joining surface of a semi-annular member according to claim 1 or 3, further comprising a fourth step of finishing the second inclined surface.
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CN114178780A (en) * 2020-09-15 2022-03-15 三菱重工压缩机有限公司 Method for manufacturing machine room

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