JPH0353494B2 - - Google Patents
Info
- Publication number
- JPH0353494B2 JPH0353494B2 JP61242844A JP24284486A JPH0353494B2 JP H0353494 B2 JPH0353494 B2 JP H0353494B2 JP 61242844 A JP61242844 A JP 61242844A JP 24284486 A JP24284486 A JP 24284486A JP H0353494 B2 JPH0353494 B2 JP H0353494B2
- Authority
- JP
- Japan
- Prior art keywords
- composite
- spindle
- speed rotating
- forming material
- cutting
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Landscapes
- Turning (AREA)
- Grinding And Polishing Of Tertiary Curved Surfaces And Surfaces With Complex Shapes (AREA)
- Rolls And Other Rotary Bodies (AREA)
Description
[産業上の利用分野]
本発明は、超精密工作機械、超高速加工機、高
剛性工作機械などの工作機械の回転主軸として利
用するのに適した高速回転部品に関するものであ
る。
[従来の技術]
工作機械の基本機能は、所要の幾何学的形状を
有する加工物をできるだけ精密に、かつ高能率に
生産することであり、そのためには工作機械構造
の中でも特にスピンドルその他の高速回転部品の
静剛性・動剛性・熱特性を改善することが基本的
に重要になる。
現在、例えば、工作機械のスピンドルには、炭
素鋼やNi―Cr―Mo鋼に代表される金属系材料が
用いられているが、これらの金属系材料では密度
および線膨張係数が大きく、かつ弾性係数が小で
あるために、切削抵抗、遠心力、加工熱などによ
る変形量が大きく、また高速切削においては固有
振動数が低く、びびり振動の発生が避けられな
い。
そのような理由から、現状のスピンドル材料で
は、高性能の工作機械を実現するのに限界があ
る。スピンドル以外の高速回転部品についても同
様なことが言える。
ところで、従来の金属系材料に代えて、高速回
転部品用の材料として好適なカーボン/カーボ
ン・コンポジツト(以下、C/Cコンポジツトと
略記する。)を用い、静的・動的・熱的特性を改
善すると共に、高剛性、軽量化、高減衰性、低熱
変形化を実現することが考えられるが、C/Cコ
ンポジツトが加工性に難があつて、その切削や研
削が困難であるばかりでなく、使用にあたつて特
に他の部材と接触する部分については、表面付近
の空孔を埋めて表面の平滑化及びかたさの改善を
図る必要がある。
[発明が解決しようとする問題点]
本発明の目的は、高速回転部品の材料として、
それに好適な特性を有するC/Cコンポジツトを
使用可能にすることにあり、特にその加工性の問
題を解決すると共に表面の平滑化及び硬さの改善
を図ることにある。
[問題点を解決するための手段]
上記目的を達成するため、本発明の高速回転部
品は、C/Cコンポジツトからなる部材表面の少
なくとも他の部材と接触する部分に、それと弾性
係数、線膨張係数がほぼ等しい高硬度の表面形成
材を、接合強度を高めるための中間材を介してコ
ーテイングし、そのコーテイング層に、切削、研
削または研磨加工を施すことにより所要形状に形
成される。
[作 用]
素材として用いるC/Cコンポジツトは、比剛
性、比強度、振動減衰率が高く、線膨張係数、密
度が低い複合材料である。したがつて、高速回転
においても遠心力、その他の外力による変形が極
めて小さく寸法安定性に優れ、振動減衰能も大で
あるために、高剛性の高速回転部品が実現でき
る。加工熱、軸受発熱による熱変形も生じにく
い。また、C/Cコンポジツトにコーテイングし
た中間材は、そのC/Cコンポジツトの表面の空
孔を埋めると同時に表面形成材の接合強度を強化
する。表面形成材は、切削、研削または研磨加工
により、その表面を容易に平滑化でき、表面のか
たさも改善される。
[発明による効果]
上述した本発明の高速回転部品によれば、以下
に列挙するような効果を期待することができる。
(1) 素材として用いたC/Cコンポジツトは、線
膨張係数が鉄系材料の1/20以下であるため、熱
変形が極めて小さい。
(2) 上記C/Cコンポジツトは密度が鉄系材料の
1/4以下で非常に小さく、また弾性係数が1.5倍
以上で大きいため、遠心力による変形が小さ
く、危険速度も高いため高速回転が可能であ
る。
(3) C/Cコンポジツトは優れた耐疲労性、耐食
性、耐熱性を有し、熱衝撃に強く、高温での使
用にも耐えることができる。
(4) C/Cコンポジツトは内部減衰率が高いた
め、振動減衰能が高く、びびり振動の発生しに
くい高速回転部品を実現できる。
(5) C/Cコンポジツトにコーテイングした中間
材を介して強固に固定された表面形成材は、
C/Cコンポジツトに比べて比較的容易に加工
できるため、実質的にC/Cコンポジツトで形
成し且つ所要形状に加工した高速回転部品を得
ることができる。
(6) 中間材によつてC/Cコンポジツトの空孔を
埋めると同時に表面形成材の接合強度を高め、
その表面形成材の加工により表面を平滑化する
と共にかたさを改善することができる。
[実施例]
第1図は本発明を工作機械用スピンドルに適用
した場合の実施例を示す。その一部を拡大して示
す第2図において、1はC/Cコンポジツトで構
成されるスピンドル素材で、クロス積層材、また
はフイラメント・ワインデイング成形、三次元構
造材等のC/Cコンポジツトが用いられる。
上記スピンドル素材1の表面は、プラズマ溶射
またはレーザ溶射、反応拡散法などにより、
Mo,WやNbを数十μm程度の厚さにコーテイン
グして、中間材2を形成し、この中間材2上に同
様な手段で表面形成材3がコーテイングされる。
上記スピンドル素材1は、スピンドルにかかる
切削抵抗、遠心力を考慮して繊維方向の配向を決
定することが変形防止の上で有効である。また、
中間材2は、スピンドル素材1の表面の空孔を埋
めると共に、スピンドル素材1と表面形成材3と
を高強度に接合させる作用をするものである。
上記表面形成材3としては、素材1を形成する
C/Cコンポジツトと、弾性係数、線膨張係数が
ほぼ等しく、しかも高硬度の材料、例えば、WC
―Coサーメツト等を用い、それを数百μmの厚さ
にコーテイングし、第2図中に鎖線Aで示すよう
に、その表面を超精密切削や研削、研磨加工によ
り所要の形状および平滑さに仕上げられる。
上述したコーテイングや加工は、スピンドルに
おける表面全体に施こす必要はなく、少なくとも
他の部材と接触する部分に施こせばよい。
なお、図中、4はころがり軸受を示している
が、上記スピンドルは、ころがり軸受ばかりでな
く、すべり軸受、空気軸受などで支持することが
できる。
第1表は、上記C/Cコンポジツトの物性を従
来から使用されてきた鉄系材料のそれとの比較に
おいて示したものである。
第1表から、C/Cコンポジツトは鉄系材料と
の比較において弾性係数が大きく、かつ密度およ
び線膨張係数が小さいことが明らかである。した
がつて、上記C/Cコンポジツトを用いたスピン
ドルにおいては、切削抵抗や遠心力、その他の外
力の作用下においても変形量が極めて小さく、ま
た熱変形量も少なくなる。
[Industrial Application Field] The present invention relates to a high-speed rotating component suitable for use as a rotating spindle of a machine tool such as an ultra-precision machine tool, an ultra-high-speed processing machine, or a high-rigidity machine tool. [Prior Art] The basic function of a machine tool is to produce workpieces with a desired geometric shape as precisely and efficiently as possible. It is fundamentally important to improve the static stiffness, dynamic stiffness, and thermal properties of rotating parts. Currently, for example, metallic materials such as carbon steel and Ni-Cr-Mo steel are used for spindles of machine tools, but these metallic materials have high density and coefficient of linear expansion, and have low elasticity. Since the coefficient is small, the amount of deformation due to cutting resistance, centrifugal force, processing heat, etc. is large, and in high-speed cutting, the natural frequency is low, and the occurrence of chatter vibration is unavoidable. For these reasons, current spindle materials have limitations in realizing high-performance machine tools. The same can be said of high-speed rotating parts other than the spindle. By the way, instead of conventional metal-based materials, carbon/carbon composites (hereinafter abbreviated as C/C composites), which are suitable as materials for high-speed rotating parts, are used to improve static, dynamic, and thermal properties. It is possible to achieve high rigidity, weight reduction, high damping performance, and low thermal deformation by improving the C/C composite, but it is difficult to process the C/C composite, and cutting and grinding it is difficult. During use, it is necessary to smooth the surface and improve hardness by filling voids near the surface, especially in areas that come into contact with other members. [Problems to be Solved by the Invention] The purpose of the present invention is to use a material for high-speed rotating parts.
The object of the present invention is to make it possible to use a C/C composite having properties suitable for this purpose, and in particular, to solve the problem of its workability and to improve its surface smoothness and hardness. [Means for Solving the Problems] In order to achieve the above object, the high-speed rotating component of the present invention has a C/C composite member surface that has a modulus of elasticity, a linear expansion coefficient, A desired shape is formed by coating high-hardness surface-forming materials with approximately the same coefficients through an intermediate material to increase bonding strength, and cutting, grinding, or polishing the coating layer. [Function] The C/C composite used as the material is a composite material that has high specific rigidity, specific strength, and vibration damping rate, and has a low coefficient of linear expansion and low density. Therefore, even during high-speed rotation, deformation due to centrifugal force and other external forces is extremely small, the dimensional stability is excellent, and the vibration damping ability is also large, so that a highly rigid high-speed rotating component can be realized. Heat deformation due to processing heat and bearing heat generation is also less likely to occur. Further, the intermediate material coated on the C/C composite fills the pores on the surface of the C/C composite and at the same time strengthens the bonding strength of the surface forming material. The surface of the surface forming material can be easily smoothed by cutting, grinding, or polishing, and the hardness of the surface can also be improved. [Effects of the Invention] According to the above-described high-speed rotating component of the present invention, the following effects can be expected. (1) The C/C composite used as the material has a coefficient of linear expansion less than 1/20 that of iron-based materials, so thermal deformation is extremely small. (2) The above C/C composite has a very low density, less than 1/4 of that of iron-based materials, and a large elastic modulus of more than 1.5 times, so deformation due to centrifugal force is small, and the critical speed is high, so high-speed rotation is not possible. It is possible. (3) C/C composites have excellent fatigue resistance, corrosion resistance, and heat resistance, are resistant to thermal shock, and can withstand use at high temperatures. (4) C/C composites have a high internal damping rate, so they have high vibration damping ability and can create high-speed rotating parts that are less prone to chatter vibrations. (5) The surface forming material is firmly fixed to the C/C composite via the intermediate material coated.
Since it can be processed relatively easily compared to C/C composites, it is possible to obtain high-speed rotating parts substantially made of C/C composites and processed into desired shapes. (6) The intermediary material fills the pores in the C/C composite and at the same time increases the bonding strength of the surface forming material,
By processing the surface forming material, the surface can be smoothed and the hardness can be improved. [Embodiment] FIG. 1 shows an embodiment in which the present invention is applied to a spindle for a machine tool. In Fig. 2, which shows a part of the spindle on an enlarged scale, 1 is a spindle material made of C/C composite. It will be done. The surface of the spindle material 1 is coated by plasma spraying, laser spraying, reaction diffusion method, etc.
An intermediate material 2 is formed by coating Mo, W, or Nb to a thickness of about several tens of micrometers, and a surface forming material 3 is coated on this intermediate material 2 by the same means. For the spindle material 1, it is effective to determine the fiber orientation in consideration of the cutting resistance and centrifugal force applied to the spindle in order to prevent deformation. Also,
The intermediate material 2 serves to fill the pores on the surface of the spindle material 1 and to bond the spindle material 1 and the surface forming material 3 with high strength. As the surface forming material 3, a material having almost the same elastic modulus and linear expansion coefficient as the C/C composite forming the material 1 and high hardness, such as WC.
- Using Co cermet, etc., it is coated to a thickness of several hundred μm, and the surface is cut into the desired shape and smoothness by ultra-precision cutting, grinding, and polishing, as shown by the chain line A in Figure 2. It will be finished. The coating and processing described above need not be applied to the entire surface of the spindle, but may be applied to at least the portion that comes into contact with other members. Although numeral 4 indicates a rolling bearing in the figure, the spindle can be supported not only by a rolling bearing but also by a sliding bearing, an air bearing, or the like. Table 1 shows the physical properties of the above C/C composite in comparison with those of conventionally used iron-based materials. From Table 1, it is clear that the C/C composite has a large elastic modulus and a small density and linear expansion coefficient when compared with iron-based materials. Therefore, in a spindle using the above C/C composite, the amount of deformation is extremely small even under the action of cutting resistance, centrifugal force, and other external forces, and the amount of thermal deformation is also small.
【表】
次に、本発明者らによる工作機械用スピンドル
の試作例について説明する。
スピンドルの試作に際し、第1図に示すような
段付部を有する中空円筒材を製作した。スピンド
ル素材1を構成するC/Cコンポジツトとして
は、0°/90°/45°の構成で成形した素材を用いた。
その上に中間材2としてMoをプラズマ溶射によ
つて50μm程度コーテイングし、さらにその上に、
表面形成材3としてWC―Coサーメツトを低圧プ
ラズマ溶射により700μmの厚さにコーテイングし
た。
その後、ダイヤモンド・ホイールにより、超精
密円筒研削を行い、表面形成材3の表面を仕上げ
て軸受けはめ合い部とした。
以上においては、工作機械用スピンドルについ
て説明したが、本発明はその他の高速回転部品に
適用することができ、その場合に、C/Cコンポ
ジツトの繊維配向を変化させれば、より合目的的
な高速回転部品の製作が可能である。[Table] Next, an example of a prototype spindle for a machine tool manufactured by the present inventors will be described. When making a prototype spindle, a hollow cylindrical member with a stepped part as shown in FIG. 1 was made. As the C/C composite constituting the spindle material 1, a material molded with a 0°/90°/45° configuration was used.
On top of that, as an intermediate material 2, Mo was coated with a thickness of about 50 μm by plasma spraying, and further on top of that,
As the surface forming material 3, WC-Co cermet was coated to a thickness of 700 μm by low-pressure plasma spraying. Thereafter, ultra-precision cylindrical grinding was performed using a diamond wheel to finish the surface of the surface forming material 3 to form a bearing fitting part. Although the above description has been given to spindles for machine tools, the present invention can be applied to other high-speed rotating parts, and in that case, by changing the fiber orientation of the C/C composite, a more suitable It is possible to manufacture high-speed rotating parts.
第1図は本発明の実施の一例を示す断面図、第
2図はその一部拡大断面図である。
1…スピンドル素材、2…中間材、3…表面形
成材。
FIG. 1 is a sectional view showing an example of the implementation of the present invention, and FIG. 2 is a partially enlarged sectional view thereof. 1... Spindle material, 2... Intermediate material, 3... Surface forming material.
Claims (1)
部材表面の少なくとも他の部材と接触する部分
に、それと弾性係数、線膨張係数がほぼ等しい高
硬度の表面形成材を、接合強度を高めるための中
間材を介してコーテイングし、そのコーテイング
層に、切削、研削または研磨加工を施すことによ
り所要形状に形成したことを特徴とする高速回転
部品。1. A high-hardness surface-forming material with approximately the same elastic coefficient and linear expansion coefficient as that of the carbon/carbon composite member is applied to at least the portion of the member surface that contacts other members via an intermediate material to increase bonding strength. A high-speed rotating part characterized by being coated and formed into a desired shape by cutting, grinding, or polishing the coating layer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP24284486A JPS6396311A (en) | 1986-10-13 | 1986-10-13 | High-speed rotary part |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP24284486A JPS6396311A (en) | 1986-10-13 | 1986-10-13 | High-speed rotary part |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6396311A JPS6396311A (en) | 1988-04-27 |
| JPH0353494B2 true JPH0353494B2 (en) | 1991-08-15 |
Family
ID=17095133
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP24284486A Granted JPS6396311A (en) | 1986-10-13 | 1986-10-13 | High-speed rotary part |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6396311A (en) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2756155B2 (en) * | 1988-09-26 | 1998-05-25 | 東芝機械株式会社 | Spindle of machine tool |
| JPH0574716U (en) * | 1992-03-17 | 1993-10-12 | 三井精機工業株式会社 | Hardened structure of spindle taper hole |
| JPH0572309U (en) * | 1992-03-17 | 1993-10-05 | 三井精機工業株式会社 | Hardening structure of spindle taper hole |
| KR20010067620A (en) * | 2001-02-23 | 2001-07-13 | 이해덕 | Manufacturing method of ceramic coated SPINDLE DISK using thermal spray |
| CN110605406A (en) * | 2018-06-14 | 2019-12-24 | 靖江斯贝得电机制造有限公司 | Self-draining sealed electric spindle |
| CN110815037B (en) * | 2018-08-08 | 2021-07-30 | 湖北鼎龙控股股份有限公司 | Polishing pad and preparation method and application thereof |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6041246B2 (en) * | 1980-02-20 | 1985-09-14 | 東レ株式会社 | Fiber-reinforced plastic propeller shaft |
-
1986
- 1986-10-13 JP JP24284486A patent/JPS6396311A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6396311A (en) | 1988-04-27 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EXPY | Cancellation because of completion of term |