JP2006231472A - Electrolytic abrasive polishing method for blade member having three-dimensional free-form surfaces - Google Patents
Electrolytic abrasive polishing method for blade member having three-dimensional free-form surfaces Download PDFInfo
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Abstract
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本発明は複数の3次元曲面を有する翼部材の研磨方法に関するものである。 The present invention relates to a method for polishing a wing member having a plurality of three-dimensional curved surfaces.
3次元自由曲面を有する部材を、電解砥粒研磨により鏡面研磨する方法が提案されている。該3次元自由曲面を部材の研磨例として、人工心臓用ポンプが記載されている。
(特許文献1参照)。
(See Patent Document 1).
しかしながら、上記の従来技術は、3次元曲面を有する翼の複数で構成されている翼部材を具体的に電解砥粒研磨する場合の課題、課題を解決するための手段は開示されていない。
すなわち、該3次元曲面を有する翼の複数で構成されている翼部材を電解砥粒研磨するに際し、翼部材の単体では複雑な形状を有しているので固定が難しい、また、翼は厚みが薄肉のところがあり、翼の先端は片持ちになるので研磨に際し力を加えると変形してしまい、十分な研磨できない。更に、図2−(b)に示すように、研磨工具が逃げてしまって、均一な研磨できないという問題点を有する。
However, the above prior art does not disclose a problem or a means for solving the problem when specifically polishing electrolytic abrasive grains on a blade member composed of a plurality of blades having a three-dimensional curved surface.
That is, when electrolytic blade polishing is performed on a blade member composed of a plurality of blades having a three-dimensional curved surface, the blade member alone has a complicated shape and is difficult to fix. Since the tip of the blade is cantilevered, it is deformed when a force is applied during polishing, and sufficient polishing cannot be performed. Further, as shown in FIG. 2B, the polishing tool escapes and there is a problem that uniform polishing cannot be performed.
そこで、本発明は上述した点に鑑み、翼部材がしっかりとした固定ができ、研磨に際し翼の先端が片持ちにならないようにし、研磨工具が逃げてしまうこともなく、均一な電解砥粒研磨できる研磨方法を提供することを目的とするものである。 Therefore, in view of the above points, the present invention makes it possible to firmly fix the wing member, prevent the tip of the wing from being cantilevered during polishing, and prevent the polishing tool from escaping, and uniform electrolytic abrasive polishing. An object of the present invention is to provide a polishing method that can be used.
本発明の3次元自由曲面を有する翼部材の電解砥粒研磨方法は、複数の翼からなり、該複数の翼の面はそれぞれ複数の3次元自由曲面で構成されている翼部材をブロック内に複数の接続箇所を有して形成し、該ブロック内に形成されている該翼部材の3次元自由曲面を電解砥粒研磨したのち、複数の接続箇所から翼部材を切り離すことを特徴とする。 The method for polishing electrolytic abrasive grains of a wing member having a three-dimensional free-form surface according to the present invention comprises a plurality of wings, each of which has a plurality of three-dimensional free-form surfaces. The wing member is formed with a plurality of connection portions, and after the three-dimensional free-form surface of the wing member formed in the block is subjected to electrolytic abrasive polishing, the wing member is separated from the plurality of connection portions.
上記の構成によれば、翼部材はブロックの内部に形成されている翼部材を研磨するので、翼部材が研磨に際し、研磨工具の押し付け圧力により変形したりすることがなく安定した研磨が可能となる。また、翼部材とブロックの接続箇所を翼の先端にすれば、片持ちによる翼の変形もなくなる。また、翼部材単体では自動で研磨する場合は固定が難しいが、ブロックでの固定はしっかりとしたものとなる。また、翼部品を機械加工で加工するのにも、ブロック内に形成することが安定した機械加工が可能となる。 According to the above configuration, since the wing member polishes the wing member formed inside the block, the wing member can be stably polished without being deformed by the pressing pressure of the polishing tool when the wing member is polished. Become. Further, if the connecting portion between the wing member and the block is the tip of the wing, the wing will not be deformed by cantilevering. In addition, it is difficult to fix the wing member alone when it is automatically polished, but the fixing with the block is firm. In addition, when machining the wing parts by machining, forming in the block enables stable machining.
更に、3次元自由曲面を有する翼部材の電解砥粒研磨方法は、上記の請求項1において、上記のブロック内に形成されている複数の翼部材はブロック内に該翼面と対向して所定の間隔を置いてブロック壁面が形成され、かつ、該ブロック壁面は該翼の3次元自由曲面に対して等距離になるように形成され、該研磨工具を用いて翼部材の3次元自由曲面を電解砥粒研磨するに際し、研磨工具中心が該所定の間隔の中心になるよう電解砥粒研磨をすることを特徴とする。
Furthermore, the electrolytic abrasive polishing method for a wing member having a three-dimensional free-form surface is the method of claim 1, wherein the plurality of wing members formed in the block are opposed to the wing surface in the block. And the block wall surface is formed so as to be equidistant with respect to the three-dimensional free-form surface of the blade, and the polishing tool is used to form the three-dimensional free-form surface of the blade member. When electrolytic polishing is performed, electrolytic polishing is performed such that the center of the polishing tool is the center of the predetermined interval.
上記の構成によれば、ブロック内に該翼面と対向して所定の間隔を置いてブロック壁面が形成され、かつ、該ブロック壁面は該翼の3次元自由曲面に対して等距離になるように形成され、研磨工具の中心が所定の間隔の中心になるように研磨するので、研磨工具の逃げがなくなり、翼部材の研磨面のどの場所でも均一な力で研磨が可能となり、均一な電解砥粒研磨が達成することができる。 According to the above configuration, the block wall surface is formed at a predetermined interval in the block so as to face the blade surface, and the block wall surface is equidistant with respect to the three-dimensional free-form surface of the blade. Since the polishing tool is polished so that the center of the polishing tool is at the center of the predetermined interval, the polishing tool can be prevented from escaping, and polishing can be performed with uniform force anywhere on the polishing surface of the wing member. Abrasive polishing can be achieved.
以下、本発明の実施形態を説明する。 Embodiments of the present invention will be described below.
本発明は、請求項1に基づく第1の特徴と、請求項2に基づく第2の特徴を有するものである。
図1−(a)〜(c)は、上記の本発明の第1の特徴を説明するためのものである。
図1−(a)〜(c)に基づき上記の第1の特徴を詳しく説明をする。
図1−(a)は、ブロック2内に翼部材1を形成した具体例を示したものである。同図において、翼部材1が接続箇所3でブロック2に連結されている。同図から明らかなのように、ブロック2は四角な長方体であるので、ブロック2内に翼部材1を機械加工により製作するのに、ブロック2に形成されたブロック固定案内溝7を基準に翼部材1が固定できるので、翼部材1の座標が正確に読み取ることができ、翼部材1の製造が寸法精度よく加工することができる。
図1−(b)は、図1−(a)に示されたブロック2内に形成された翼部材1を電解砥粒研磨する様子を示すものである。研磨の様子は、図2(a)に基づき、後で詳述するが、電解砥粒研磨に際しても、ブロック2に形成された固定案内溝7を基準に翼部材1が固定できるので、翼部材1の座標が正確に読み取ることができ、均一な研磨が可能となる。又、翼部材1の先端は接続箇所3でブロック2に固定されているので、翼部材1の翼1−1の先端を研磨するに際し、片持ちにならないので変形をしないで研磨することが可能となる。
図1−(c)は、翼部材1を接続箇所3でブロック2から切り離した、電解砥粒研磨が終了した翼部材1を示す。同図から明らかのように、切り離し作業は通常の機械加工により簡単にできる。
上記の如く、本発明の請求項1に基づく第1の特徴、すなわち、翼部材1はブロック2の内部に形成されている翼部材1を研磨するので、翼部材1が研磨に際し、研磨工具4の押し付け圧力により変形したりすることがなく安定した研磨が可能となる。また、翼部材1とブロックの接続箇所3を翼1−1の先端にすれば、片持ちによる翼の変形もなくなる。また、翼部材1単体では自動で研磨する場合は固定が難しいが、ブロック2での固定はしっかりとしたものとなる。また、翼部材1を機械加工で加工するのにも、ブロック2内に形成することが安定した機械加工が可能となる。
なお、上記において、図1−(c)に示す翼部材1は一例であり、翼1−1が複数のものであれば、その形状は問わない。
また、ブロック2と翼部材1は同じ材質であり、翼部材1はチタン(Ti)、ステンレス、モリブデン(Mo)、タンタル(Ta)、タングステン(W)などが適用できる。
The present invention has a first feature based on claim 1 and a second feature based on claim 2.
1- (a) to (c) are for explaining the first feature of the present invention.
The first feature will be described in detail based on FIGS. 1- (a) to (c).
FIG. 1- (a) shows a specific example in which the wing member 1 is formed in the block 2. In the figure, a wing member 1 is connected to a block 2 at a connection point 3. As is apparent from the figure, since the block 2 is a rectangular rectangular parallelepiped, the block fixing guide groove 7 formed in the block 2 is used as a reference to manufacture the wing member 1 in the block 2 by machining. Since the wing member 1 can be fixed, the coordinates of the wing member 1 can be read accurately, and the manufacture of the wing member 1 can be processed with high dimensional accuracy.
FIG. 1- (b) shows a state where the blade member 1 formed in the block 2 shown in FIG. 1- (a) is subjected to electrolytic abrasive polishing. The state of the polishing will be described in detail later with reference to FIG. 2 (a), but the blade member 1 can be fixed on the basis of the fixed guide groove 7 formed in the block 2 during the electrolytic abrasive polishing. The coordinates of 1 can be read accurately, and uniform polishing is possible. Further, since the tip of the wing member 1 is fixed to the block 2 at the connection point 3, when the tip of the wing 1-1 of the wing member 1 is polished, it cannot be cantilevered and can be polished without deformation. It becomes.
FIG. 1- (c) shows the wing member 1 that has been subjected to electrolytic abrasive grain polishing, in which the wing member 1 is cut off from the block 2 at the connection point 3. As is clear from the figure, the separation work can be easily performed by ordinary machining.
As described above, the first feature based on the first aspect of the present invention, that is, the wing member 1 polishes the wing member 1 formed inside the block 2, and therefore, when the wing member 1 is polished, a polishing tool 4 is used. Stable polishing is possible without being deformed by the pressing pressure. Further, if the connecting portion 3 between the wing member 1 and the block is the tip of the wing 1-1, the wing is not deformed by cantilever. In addition, it is difficult to fix the blade member 1 alone when it is automatically polished, but the block 2 is firmly fixed. In addition, even when the wing member 1 is machined, forming it in the block 2 enables stable machining.
In addition, in the above, the wing | blade member 1 shown to FIG. 1- (c) is an example, and if the wing | blade 1-1 is a several thing, the shape will not ask | require.
The block 2 and the blade member 1 are made of the same material, and the blade member 1 can be made of titanium (Ti), stainless steel, molybdenum (Mo), tantalum (Ta), tungsten (W), or the like.
図2−(a)〜(b)は、本発明の請求項2に基づく、第2の特徴を説明するためのものである。
図2−(a)は、本発明の請求項2に基づく、本発明の第2の特徴を示すものである。
図2−(b)は、通常の研磨方法で翼部材1の翼面6を電解砥粒研磨する様子を示したものである。
図2−(b)に示す通常の研磨においては、研磨工具4が研磨圧力により、逃げてしまい均一な研磨ができない。
図2−(a)に示す本発明の電解砥粒研磨方法では、翼部材1の翼面6の対向する面には所定の間隔Xを置いて、ブロック壁面5が形成されており、且つ、所定の間隔Xはブロック壁面5と対向する翼面6のどこの場所でも同じ距離Xになるよう、等距離で形成されている
そして、電解砥粒研磨に際し、研磨工具5の径中心mが所定の間隔Xの中心nにくるように常に電解砥粒研磨を行う。そうすると、研磨工具4の研磨圧力は、翼の面6とブロック壁面5とで等しい値となり、翼の面が偏りなく均一な研磨が実現できる。
上記の如く、本発明の請求項2に基づく第2の特徴、すなわち、ブロック2内に該翼面6と対向して所定の間隔を置いてブロック壁面5が形成され、かつ、該ブロック壁面5は該翼の3次元自由曲面に対して等距離になるように形成され、研磨工具4の中心が所定の間隔の中心になるように研磨するので、研磨工具の逃げがなくなり、翼部材の研磨面のどの場所でも均一な力で研磨が可能となり、均一な電解砥粒研磨が達成することができる。
FIGS. 2A to 2B are for explaining the second feature based on claim 2 of the present invention.
FIG. 2- (a) shows a second feature of the present invention based on claim 2 of the present invention.
FIG. 2- (b) shows a state where the blade surface 6 of the blade member 1 is electrolytically polished by a normal polishing method.
In the normal polishing shown in FIG. 2B, the polishing tool 4 escapes due to the polishing pressure, and uniform polishing cannot be performed.
In the electrolytic abrasive polishing method of the present invention shown in FIG. 2- (a), a block wall surface 5 is formed at a predetermined interval X on the opposing surface of the blade surface 6 of the blade member 1, and The predetermined interval X is formed at an equal distance so as to be the same distance X everywhere on the blade surface 6 facing the block wall surface 5. In the electrolytic abrasive polishing, the diameter center m of the polishing tool 5 is predetermined. Electrolytic abrasive polishing is always performed so as to be at the center n of the interval X. Then, the polishing pressure of the polishing tool 4 becomes equal between the blade surface 6 and the block wall surface 5, and uniform polishing can be realized without unevenness of the blade surface.
As described above, the second feature based on the second aspect of the present invention, that is, the block wall surface 5 is formed in the block 2 at a predetermined interval facing the blade surface 6, and the block wall surface 5 is formed. Is formed so as to be equidistant with respect to the three-dimensional free-form surface of the blade, and polishing is performed so that the center of the polishing tool 4 is centered at a predetermined interval. Polishing can be performed with a uniform force anywhere on the surface, and uniform electrolytic abrasive polishing can be achieved.
なお、上記の本発明の3次元自由曲面を有する翼部材1の電解砥粒研磨方法は、手動で研磨した場合、及び自動で研磨した場合でも、同じ効果を有するものである。手動で研磨する具体例としては、特開2004−299029号公報に示されたものであり、自動で研磨する具体例としては、特願2005−050619号公報に示されたものである。 In addition, the electrolytic abrasive grain polishing method of the wing member 1 having a three-dimensional free-form surface according to the present invention has the same effect even when it is manually polished and automatically polished. A specific example of manual polishing is disclosed in Japanese Patent Application Laid-Open No. 2004-299029, and a specific example of automatic polishing is disclosed in Japanese Patent Application No. 2005-050619.
本発明の翼部材1をブロック2内に形成し、かつ、翼部材1の翼面6の対向面にブロック壁面5を所定の等間隔で形成し、研磨工具4の工具径の中心mが該所定の等間隔の中心nにくるように電解砥粒研磨したので、翼1−1の研磨が均一に安定して研磨することができ、複数の3次元自由曲面を有する翼部品の精密研磨に寄与するところ大である。 The blade member 1 of the present invention is formed in the block 2, and the block wall surface 5 is formed at a predetermined equal interval on the surface of the blade member 1 facing the blade surface 6. Since the electrolytic abrasive grain polishing is performed so as to be at the center n at a predetermined equal interval, the blade 1-1 can be uniformly and stably polished, and the blade member having a plurality of three-dimensional free-form surfaces can be precisely polished. It is a great place to contribute.
1 3次元自由曲面を有する翼部材
1−1 翼部材の翼
2 ブロック
3 翼部材とブロックの接続箇所
4 研磨工具
5 ブロック壁面
6 翼部材の翼面
7 ブロック固定案内溝
m 研磨工具径の中心
n 翼面とブロック壁面との間隔の中心
X 所定の間隙長さ
DESCRIPTION OF SYMBOLS 1 Blade member which has a three-dimensional free-form surface 1-1 Blade of blade member 2 Block 3 Connection point of blade member and block 4 Polishing tool 5 Block wall surface 6 Blade surface of blade member 7 Block fixed guide groove m Center n of polishing tool diameter Center of clearance between blade surface and block wall surface X Predetermined gap length
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Cited By (1)
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US8420156B2 (en) | 2010-01-12 | 2013-04-16 | Samsung Display Co., Ltd. | Method of forming pattern and manufacturing method of organic light emitting device |
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Publication number | Priority date | Publication date | Assignee | Title |
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US8420156B2 (en) | 2010-01-12 | 2013-04-16 | Samsung Display Co., Ltd. | Method of forming pattern and manufacturing method of organic light emitting device |
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