JPH0218317B2 - - Google Patents
Info
- Publication number
- JPH0218317B2 JPH0218317B2 JP59222574A JP22257484A JPH0218317B2 JP H0218317 B2 JPH0218317 B2 JP H0218317B2 JP 59222574 A JP59222574 A JP 59222574A JP 22257484 A JP22257484 A JP 22257484A JP H0218317 B2 JPH0218317 B2 JP H0218317B2
- Authority
- JP
- Japan
- Prior art keywords
- sintered body
- sliding member
- silicon carbide
- decomposition
- sliding
- 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
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims description 43
- 229910010271 silicon carbide Inorganic materials 0.000 claims description 43
- 238000000354 decomposition reaction Methods 0.000 claims description 35
- 239000003112 inhibitor Substances 0.000 claims description 11
- 238000000034 method Methods 0.000 claims description 11
- 238000000576 coating method Methods 0.000 claims description 10
- 238000003754 machining Methods 0.000 claims description 10
- 238000002844 melting Methods 0.000 claims description 10
- 230000008018 melting Effects 0.000 claims description 10
- 239000011248 coating agent Substances 0.000 claims description 9
- 238000005461 lubrication Methods 0.000 claims description 9
- 230000003647 oxidation Effects 0.000 claims description 5
- 238000007254 oxidation reaction Methods 0.000 claims description 5
- 239000000126 substance Substances 0.000 claims description 4
- 238000010438 heat treatment Methods 0.000 description 13
- 229910052799 carbon Inorganic materials 0.000 description 10
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 9
- 239000000463 material Substances 0.000 description 9
- 238000000859 sublimation Methods 0.000 description 7
- 230000008022 sublimation Effects 0.000 description 6
- 238000005245 sintering Methods 0.000 description 5
- 238000010304 firing Methods 0.000 description 4
- OKKJLVBELUTLKV-UHFFFAOYSA-N Methanol Chemical compound OC OKKJLVBELUTLKV-UHFFFAOYSA-N 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 3
- 238000005260 corrosion Methods 0.000 description 3
- 239000012530 fluid Substances 0.000 description 3
- 238000007789 sealing Methods 0.000 description 3
- 150000001875 compounds Chemical class 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000010687 lubricating oil Substances 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- KXGFMDJXCMQABM-UHFFFAOYSA-N 2-methoxy-6-methylphenol Chemical compound [CH]OC1=CC=CC([CH])=C1O KXGFMDJXCMQABM-UHFFFAOYSA-N 0.000 description 1
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 229910004298 SiO 2 Inorganic materials 0.000 description 1
- 235000021355 Stearic acid Nutrition 0.000 description 1
- 229910021431 alpha silicon carbide Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 230000003466 anti-cipated effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 230000001680 brushing effect Effects 0.000 description 1
- 150000001721 carbon Chemical class 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 239000013043 chemical agent Substances 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000005229 chemical vapour deposition Methods 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 229910003460 diamond Inorganic materials 0.000 description 1
- 239000010432 diamond Substances 0.000 description 1
- 238000007598 dipping method Methods 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 238000011010 flushing procedure Methods 0.000 description 1
- 239000013505 freshwater Substances 0.000 description 1
- 230000002209 hydrophobic effect Effects 0.000 description 1
- 230000000873 masking effect Effects 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- QIQXTHQIDYTFRH-UHFFFAOYSA-N octadecanoic acid Chemical compound CCCCCCCCCCCCCCCCCC(O)=O QIQXTHQIDYTFRH-UHFFFAOYSA-N 0.000 description 1
- OQCDKBAXFALNLD-UHFFFAOYSA-N octadecanoic acid Natural products CCCCCCCC(C)CCCCCCCCC(O)=O OQCDKBAXFALNLD-UHFFFAOYSA-N 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 239000005011 phenolic resin Substances 0.000 description 1
- 229920001568 phenolic resin Polymers 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000007639 printing Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 239000008117 stearic acid Substances 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Sliding-Contact Bearings (AREA)
- Mechanical Sealing (AREA)
- Ceramic Products (AREA)
Description
〔産業上の利用分野〕
この発明は高密度炭化珪素焼結体で構成された
ハイドロダイナミツクシール用高密度炭化珪素焼
結体製摺動部材およびその摺動部材の摺動端面に
おける溝加工方法に関するものである。
〔従来の技術〕
炭化珪素の高密度焼結体(以下SiC焼結体と略
す)は、よく知られているように、耐熱性、耐摩
耗性および耐腐食性に優れた特長を有し、例えば
ガスタービン材料などのために非常に期待されて
いるセラミツク材料であり、なかでも最も早く実
用化されたのは、メカニカルシールの摺動部材と
してゞあつて、現在ではその優れた特性の故に最
高の性能を発揮する摺動部材として位置づけられ
ているところである。
また一方、技術の発達に併せて、この種のメカ
ニカルシールとしての使用環境は、日毎に厳格さ
を増してきており、これに伴なつてより一層高度
なシール性能が要求され、シール構造についても
一層複雑化を増す傾向にある。そしてこのような
折から、摺動端面での潤滑性の向上、ならびに冷
却性の促進などを意図して、同摺動端面に溝加工
を施したところの、いわゆるハイドロダイナミツ
クシールの構成が、最先端のシール設計技術とし
て注目されており、このように現時点での最高級
の摺動部材であるSiC焼結体を、ハイドロダイナ
ミツクシールに使用することは、とりも直さず最
高級のメカニカルシールを提供することにほかな
らないものである。
〔発明が解決しようとする問題点〕
しかしながら、一方、この種の一般的に使用さ
れてSiC焼結体は、極めて高硬度で耐摩耗性に優
れた材料であるが故に、その機械加工が容易では
なく、また高硬度な性状から反面、脆性材料でも
あるために、これらの性状を無視した強引な機械
加工によつては、加工傷その他の欠陥を生じて、
破壊しかねない惧れがあり、さらには耐腐食性で
あることから、化学薬品処理によるエツチング加
工なども困難、もしくは不可能に近いという問題
点を有している。
従つて、この発明は、ハイドロダイナミツクシ
ール用高密度炭化珪素焼結体製の摺動部材と、そ
の摺動部材をハイドロダイナミツクシール用にす
るために、その摺動部材の摺動端面の溝加工を精
度よくしかも容易に施すことができる方法を提供
することにある。
〔問題点を解決するための手段〕
上記目的を達成するために、この発明は、高密
度炭化珪素焼結体製摺動部材にあつて、その摺動
端面所要部分に潤滑用の溝を形成してハイドロダ
イナミツクシール用高密度炭化珪素焼結体製摺動
部材に構成してあるものである。
また、このハイドロダイナミツクシール用高密
度炭化珪素焼結体製摺動部材の摺動端面溝加工方
法は、その摺動部材の摺動端面の被加工溝形成部
分を除く全表面に、高密度炭化珪素焼結体の分解
点より高い融点をもつ分解防止剤でコーテイング
被覆し、次いでコーテイング被覆された摺動部材
を、高密度炭化珪素焼結体の分解点より高い温度
で且つ分解防止剤の融点より低い温度で熱処理し
て、前記コーテイング被覆されていない被加工溝
形成部分を所定深さに亘り昇華分解させて溝加工
をなし、その後、酸化または薬品処理若しくは機
械処理によつて、前記コーテイング被覆を除去す
るようにしたものである。
〔実施例〕
以下、この発明に係る摺動端面溝を有するハイ
ドロダイナミツクシール用高密度SiC焼結体製摺
動部材、および同摺動部材の摺動端面溝加工方法
につき、第1図aないしdを参照して詳細に説明
する。
一般的に高密度SiC焼結体は、例えば、高純度
に精製された炭化珪素の微粉末原料に、焼結促進
材としての所定量のホウ素系化合物または/およ
びアルミ系化合物と、焼結助材としての所定量の
炭素とを添加混合し、かつ成形して2000℃以上の
高温で不活性雰囲気下に焼成することによつて構
成される。
そしてこのように構成される高密度SiC焼結体
を、メカニカルシールの摺動部材とする場合は、
その摺動端面をラツプ仕上げして使用するように
している。一方、この種のメカニカルシールの摺
動部材においては、高負荷における使用条件下で
所定のシール特性、すなわち高圧、高速下での
PV値、また高温下でのPVT値などを向上させる
のに、単なるシール摺動端面間での境界潤滑のみ
では不充分であつて、このために多少のシール漏
洩を許容しても、摺動端面に潤滑用の溝形成をな
すようにした、いわゆるハイドロダイナミツクシ
ール構造を採用しているが、さきにも述べたよう
に、この摺動部材としての高密度SiC焼結体は、
その焼結後の二次加工が極めて困難であり、前記
のハイドロダイナミツクシール構造のための摺動
端面への潤滑用の溝形成についても例外ではな
い。
そこで発明者はこの高密度SiC焼結体による摺
動部材をハイドロダイナミツクシール構造とする
ための溝加工形成について鋭意検討した結果、次
のような手段を見出した。
すなわち、一旦焼成後の高密度SiC焼結体は、
通常、2000℃以上で自己昇華分解を生じ、かつ真
空減圧下では1900℃位から分解し始めるから、こ
の昇華分解反応(SiC−→Si↑
+C)を利用し
て、摺動端面に所望の凹凸形状などの溝加工を施
すようにしたものであり、またこのように昇華分
解反応を効果的に利用するために、摺動端面の被
加工溝形成部分を除く全表面を、高密度SiC焼結
体の分解点より高い融点をもつ分解防止剤でコー
テイング被覆したのち、高密度SiC焼結体の分解
点より高い温度で且つ分解防止剤の融点より低い
温度で熱処理して、コーテイング被覆されていな
い被加工溝形成部分を、所定の深さ範囲に亘り昇
華分解して溝加工をなす新規な技術手段である。
次にこの発明の望ましい一実施例につき、第1
図aないしdを参照して詳細に説明する。
この実施例では、所定の摺動部材形状に成形
し、所定の焼結温度で焼成された高密度SiC焼結
体を用いる。そしてまず、第1図aに示されてい
るように、この所定形状に成形された高密度SiC
焼結体からなる摺動部材1は、全表面、こゝでは
少なくとも摺動端面2を含む所定表面をラツプ仕
上げする。
ついで同図bに示されているように、前記摺動
端面2の被加工溝形成部分2aを除い全表面に対
し、高融点を有していて、かつ焼結温度、こゝで
は例えば2000℃以下では蒸気圧が低くて昇華分解
作用を生じない物質による分解防止剤3をコーテ
イング被覆させる。こゝで分解防止剤3として
は、カーボンとかB4C、TiCなどのような炭化
物、またはTiB2、ZrB2などのようなホウ化物、
さらにはタングステン、モリブデンなどを用いる
ことができ、またコーテイング方法としては、ス
プレーコーテイング法、浸漬法、印刷付着法と
か、あるいはCVD法、PVD法などであつてよ
い。
そして次に、前記コーテイング被覆処理した摺
動部材1を、真空炉中において、減圧下に1900℃
以上の温度で熱処理する。すなわち、この熱処理
によつて、同図cに示すように、摺動部材1のコ
ーテイング被覆処理されていない被加工溝形成部
分2aに、昇華分解反応(SiC−→Si↑
+C)を
生じて、同部分2aに凹状溝4が形成される。
こゝで前記熱処理温度としては、1900℃以上で望
ましくは同摺動部材1としての高密度SiC焼結体
の焼結温度を越えないように制御するのがよいも
ので、これは焼結温度を越える場合、同焼結体の
内部組織に変化をきたす惧れを避けるためであ
る。また前記凹状溝4の形成深さは、熱処理温度
と熱処理時間とを制御することによつて自由に調
整可能である。
その後、同図dに示すように、前記コーテイン
グ被覆した分解防止剤3を、酸化処理とか、薬品
によるエツチング処理、その他の機械的処理など
により除去して、目的とするところの、摺動端面
2に潤滑用の溝4を形成した摺動部材1を得るの
である。
こゝでコーテイング被覆をなす分解防止剤3と
して、カーボンを用いるのが効果的であり、この
カーボンを用いるときは、熱処理時のマスキング
作用に有効であるほかに、熱処理後の除去を酸化
処理により容易に実行でき、また必要に応じて、
摺動端面2のみの昇華分解による凹凸溝4の加工
であれば、単なるラツプ処理によつても機械的除
去処理が容易である。
またこの摺動部材1をハイドロダイナミツクシ
ールにしているが故に、シール対象流体が油系の
場合には、溝4部に潤滑油をより一層安定に保持
させるために、昇華分解によつて生ずる溝4部内
のカーボン層はこれが親油性であることから、そ
のまゝで残す方がよく、またシール対象流体が水
系の場合は、逆に昇華分解によつて生ずる溝4部
内のカーボン層が疎水性として作用し、水潤滑が
妨げられるから、分解処理後、この溝4部内のカ
ーボン層を酸化処理などによつて除去すると共
に、同溝4部内には親水性のSiO2などの酸化膜
を形成させるようにして、水潤滑の効果を向上さ
せるのがよい。
つぎに、さらに具体的な実施例について説明す
る。
実施例 1
平均粒子径0.7μmのα−SiC粉(1000g)と、
平均粒子径0.5μmのB4C(5g)をボールミルに
とり、更に、残炭率50%のフエノール樹脂40g、
PEG20g、ステアリン酸10gをメタノール溶媒
として添加混合した。ついでスプレードライヤー
にて乾燥造粒した後、金型にて1500Kg/cm2の成形
圧力にて、70φ×50φ×10tの成形体10ケを製作し
た。
この成形体を焼成炉にセツトした後、真空下
(10-1Torr以下)で1600℃まで昇温した後、Arガ
スを導入し、大気圧下で2100℃に昇温、1時間保
持して焼成を終了した。冷却後、この高密度SiC
焼結体はいずれも3.15〜3.16g/cm3の密度を有し
ており、約18%の線収縮率を示した。
また、この高密度SiC焼結体の内部組織は、5
〜10μmの結晶粒で構成され、特に巨大な粒成長
組織は認められなかつた。
上記高密度SiC焼結体より、54φ×41φ×7tのシ
ールリングに研磨加工し、摺動端面は、ダイヤモ
ンドペーストでラツプ、ポリツシユ仕上げをし
た。
このようにして得られた摺動端面に、第2図で
示す摺動端面2に形成されているような溝4…を
形成すべく、ハイドロ加工用のゾスクリーンを用
いて、分解防止剤としてのカーボンペーストを摺
動端面に印刷し、他の面はハケ塗りによりカーボ
ンペーストをコーテイングした。上記の処理品を
下記表−1に示す条件で、分解熱処理した。
[Industrial Application Field] The present invention relates to a sliding member made of a high-density silicon carbide sintered body for a hydrodynamic seal, and a method for machining grooves on the sliding end surface of the sliding member. It is related to. [Prior Art] As is well known, high-density sintered bodies of silicon carbide (hereinafter referred to as SiC sintered bodies) have excellent heat resistance, wear resistance, and corrosion resistance. Ceramic materials are highly anticipated as materials for gas turbines, for example, and the earliest material to be put into practical use was as a sliding member for mechanical seals, and is now considered the best material due to its excellent properties. It is positioned as a sliding member that exhibits the following performance. On the other hand, along with the development of technology, the usage environment for this type of mechanical seal is becoming more and more severe day by day. There is a tendency for things to become even more complex. At this time, the structure of the so-called hydrodynamic seal, in which grooves were machined on the sliding end face with the intention of improving lubricity on the sliding end face and promoting cooling performance, was developed. It is attracting attention as a cutting-edge seal design technology, and the use of SiC sintered bodies, which are currently the highest-grade sliding components, in hydrodynamic seals is of course the highest-grade mechanical component. It is nothing more than providing a seal. [Problems to be solved by the invention] However, this type of commonly used SiC sintered body is a material with extremely high hardness and excellent wear resistance, so machining is not easy. Although it has high hardness, it is also a brittle material, so aggressive machining that ignores these properties can result in machining scratches and other defects.
There is a risk of destruction, and furthermore, since it is corrosion resistant, it is difficult or almost impossible to perform etching processes using chemical agents. Therefore, the present invention provides a sliding member made of high-density silicon carbide sintered body for hydrodynamic sealing, and a sliding end face of the sliding member in order to use the sliding member for hydrodynamic sealing. It is an object of the present invention to provide a method by which groove machining can be performed accurately and easily. [Means for Solving the Problems] In order to achieve the above object, the present invention provides a sliding member made of a high-density silicon carbide sintered body, in which a groove for lubrication is formed in a required portion of the sliding end surface. This is a sliding member made of high-density silicon carbide sintered body for hydrodynamic seals. In addition, this method of machining grooves on the sliding end face of a sliding member made of high-density silicon carbide sintered body for hydrodynamic seals has a high density The sliding member is coated with a decomposition inhibitor having a melting point higher than the decomposition point of the silicon carbide sintered body, and then the coated sliding member is coated at a temperature higher than the decomposition point of the high-density silicon carbide sintered body and without the decomposition inhibitor. Heat treatment is performed at a temperature lower than the melting point to sublime and decompose the groove-forming portion to be processed to a predetermined depth by heat treatment at a temperature lower than the melting point, and then the coating is removed by oxidation, chemical treatment, or mechanical treatment. The coating is removed. [Example] Hereinafter, a sliding member made of a high-density SiC sintered body for a hydrodynamic seal having a sliding end groove according to the present invention, and a method of machining the sliding end groove of the sliding member are shown in Fig. 1a. This will be explained in detail with reference to d to d. Generally, high-density SiC sintered bodies are made by adding a predetermined amount of a boron-based compound and/or an aluminum-based compound as a sintering accelerator to a finely powdered raw material of highly purified silicon carbide. It is constructed by adding and mixing a predetermined amount of carbon as a material, molding, and firing in an inert atmosphere at a high temperature of 2000°C or higher. When the high-density SiC sintered body configured in this way is used as a sliding member of a mechanical seal,
The sliding end surface is lapped for use. On the other hand, the sliding member of this type of mechanical seal has certain sealing characteristics under high load usage conditions, that is, under high pressure and high speed.
To improve the PV value and the PVT value at high temperatures, mere boundary lubrication between the seal sliding end faces is insufficient, and even if some seal leakage is allowed, the sliding It uses a so-called hydrodynamic seal structure with grooves for lubrication formed on the end face, but as mentioned earlier, this high-density SiC sintered body as a sliding member is
Secondary processing after sintering is extremely difficult, and the formation of lubrication grooves on the sliding end surface for the hydrodynamic seal structure is no exception. Therefore, the inventors conducted intensive studies on forming grooves in order to make the sliding member made of the high-density SiC sintered body into a hydrodynamic seal structure, and as a result, they discovered the following means. In other words, once fired, the high-density SiC sintered body is
Normally, self-sublimation decomposition occurs at temperatures above 2000℃, and decomposition starts at around 1900℃ under vacuum and reduced pressure.Using this sublimation decomposition reaction (SiC-→Si↑+C), desired unevenness can be created on the sliding end surface. In order to effectively utilize the sublimation decomposition reaction in this way, the entire surface of the sliding end surface, except for the groove forming part, is made of high-density SiC sintered material. After coating with a decomposition inhibitor that has a melting point higher than the decomposition point of the high-density SiC sintered body, heat treatment is performed at a temperature higher than the decomposition point of the high-density SiC sintered body and lower than the melting point of the decomposition inhibitor, so that the material is not coated. This is a novel technical means for forming grooves by sublimating and decomposing the groove-forming portion to be processed over a predetermined depth range. Next, regarding a preferred embodiment of this invention, the first
This will be explained in detail with reference to figures a to d. In this embodiment, a high-density SiC sintered body formed into a predetermined sliding member shape and fired at a predetermined sintering temperature is used. First, as shown in Figure 1a, high-density SiC molded into a predetermined shape
The entire surface of the sliding member 1 made of a sintered body, in this case, a predetermined surface including at least the sliding end surface 2, is lapped. Next, as shown in Figure b, the entire surface of the sliding end surface 2 except for the groove forming portion 2a has a high melting point and is heated at a sintering temperature of, for example, 2000°C. In the following, a decomposition inhibitor 3 made of a substance having a low vapor pressure and not causing a sublimation decomposition effect is coated. Here, as the decomposition inhibitor 3, carbon, carbide such as B 4 C, TiC, etc., or boride such as TiB 2 , ZrB 2, etc.
Furthermore, tungsten, molybdenum, etc. can be used, and the coating method may be a spray coating method, a dipping method, a printing deposition method, a CVD method, a PVD method, or the like. Next, the coating-treated sliding member 1 is placed in a vacuum furnace at 1900°C under reduced pressure.
Heat treatment is performed at a temperature higher than that. That is, by this heat treatment, as shown in FIG. A concave groove 4 is formed in the same portion 2a.
Here, the heat treatment temperature is preferably controlled at 1900°C or higher, preferably so as not to exceed the sintering temperature of the high-density SiC sintered body as the sliding member 1; This is to avoid the risk of causing changes in the internal structure of the sintered body if it exceeds this range. Furthermore, the depth of the concave groove 4 can be freely adjusted by controlling the heat treatment temperature and heat treatment time. Thereafter, as shown in FIG. Thus, a sliding member 1 having a groove 4 for lubrication formed therein is obtained. In this case, it is effective to use carbon as the decomposition inhibitor 3 that forms the coating.When using this carbon, it is effective for masking action during heat treatment, and it can also be removed after heat treatment by oxidation treatment. It is easy to perform and, if necessary,
If the uneven grooves 4 are processed by sublimation and decomposition of only the sliding end surface 2, mechanical removal can be easily performed even by a simple lapping process. In addition, since this sliding member 1 is a hydrodynamic seal, when the fluid to be sealed is oil-based, in order to more stably retain the lubricating oil in the groove 4, the lubricating oil is generated by sublimation and decomposition. Since the carbon layer in groove 4 is lipophilic, it is better to leave it as is.If the fluid to be sealed is aqueous, conversely, the carbon layer in groove 4, which is generated by sublimation and decomposition, is hydrophobic. Therefore, after the decomposition process, the carbon layer in the groove 4 is removed by oxidation treatment, etc., and an oxide film such as hydrophilic SiO 2 is formed in the groove 4. It is preferable to improve the effectiveness of water lubrication. Next, more specific examples will be described. Example 1 α-SiC powder (1000 g) with an average particle size of 0.7 μm,
B 4 C (5 g) with an average particle size of 0.5 μm was placed in a ball mill, and 40 g of phenolic resin with a residual carbon content of 50% was added.
20 g of PEG and 10 g of stearic acid were added and mixed as a methanol solvent. Then, after drying and granulating with a spray dryer, 10 molded bodies of 70φ×50φ×10 t were manufactured using a mold at a molding pressure of 1500Kg/cm 2 . After setting this compact in a firing furnace, the temperature was raised to 1600°C under vacuum (below 10 -1 Torr), then Ar gas was introduced, the temperature was raised to 2100°C under atmospheric pressure, and the temperature was maintained for 1 hour. Firing has finished. After cooling, this high-density SiC
All of the sintered bodies had a density of 3.15 to 3.16 g/cm 3 and exhibited a linear shrinkage rate of about 18%. Moreover, the internal structure of this high-density SiC sintered body is 5
It was composed of crystal grains of ~10 μm, and no particularly large grain growth structure was observed. The high-density SiC sintered body was polished into a 54φ x 41φ x 7t seal ring, and the sliding end surface was lapped and polished with diamond paste. In order to form grooves 4 on the sliding end surface obtained in this way, such as those formed on the sliding end surface 2 shown in FIG. Carbon paste was printed on the sliding end surface, and the other surfaces were coated with carbon paste by brushing. The above treated product was subjected to decomposition heat treatment under the conditions shown in Table 1 below.
【表】
以上の様に、摺動端面溝加工法としての分解処
理条件は、真空下1900℃〜2000℃が好ましい。
2000℃を越えると分解が促進されコーテイング部
からも一部分解が生じ、正確な溝加工が困難にな
る。一方、1900℃以下では、ほとんど分解が抑制
され溝加工ができない。
特に、比較品3に示す様に高密度SiC焼結体の
焼成温度まで処理温度を高めると、分解が著しい
だけでなく、焼結体組織に粒成長を伴い、摺動材
としては好ましくない。
実験例 2
上記本発明品1、4、5に基づくシールリング
をメカニカルシール試験機に組み込み下記の条件
で回転テストした結果、下記表−2に示す如く、
いずれもモレ量が若干増したが摩擦係数が著しく
低下し、また摩耗もほとんど認められなかつた。
[条件]
流体(清水)、圧力(10Kg/cm2)、回転数
3600rpm(8.9m/s)、フラツシング量(3/
min)[Table] As mentioned above, the decomposition treatment conditions for the sliding end face groove processing method are preferably 1900°C to 2000°C under vacuum.
If the temperature exceeds 2000℃, decomposition will be accelerated and some decomposition will occur from the coating, making accurate groove machining difficult. On the other hand, at temperatures below 1900°C, decomposition is almost suppressed and grooving cannot be performed. In particular, when the treatment temperature is raised to the firing temperature of a high-density SiC sintered body, as shown in Comparative Product 3, not only is the decomposition significant, but grain growth occurs in the structure of the sintered body, making it undesirable as a sliding material. Experimental Example 2 Seal rings based on the above-mentioned products 1, 4, and 5 of the present invention were installed in a mechanical seal tester and a rotation test was performed under the following conditions. As a result, as shown in Table 2 below,
In both cases, the amount of leakage increased slightly, but the coefficient of friction decreased significantly, and almost no wear was observed. [Conditions] Fluid (fresh water), pressure (10Kg/cm 2 ), rotation speed
3600rpm (8.9m/s), flushing amount (3/
min)
【表】
(発明の効果)
以上のようにこの発明によれば、高密度炭化珪
素焼結体製摺動部材にあつて、その摺動端面所要
部分に潤滑用の溝を形成したから、耐熱性、耐摩
耗性および耐腐食性に優れていることは勿論のこ
と、摺動端面での潤滑性ならびに冷却性なども大
幅に向上し得、このため高負荷条件下でも好適に
使用できるハイドロダイナミツクシール用高密度
炭化珪素焼結体製摺動部材を提供できるものであ
る。また、この発明のハイドロダイナミツクシー
ル用高密度炭化珪素焼結体製摺動部材の摺動端面
の溝加工方法によれば、高密度SiC焼結体による
摺動部材において、摺動端面の被加工溝形成部分
を除く全表面を、高密度SiC焼結体の分解点より
高い融点をもつ分解防止剤でコーテイング被覆
し、次いでコーテイング被覆された摺動部材を、
高密度SiC焼結体の分解点より高い温度で且つ分
解防止剤の融点より低い温度で熱処理して、前記
コーテイング被覆されていない被加工溝形成部分
を所定深さに亘り昇華分解させて溝加工をなし、
その後、酸化または薬品処理若しくは機械的処理
によつて、前記コーテイング被覆を除去するよう
にしたから、従来、極めて困難であつた高密度炭
化珪素焼結体による摺動部材への潤滑用の溝加工
を頗る容易に行うことができ、しかも熱処理時の
温度および時間を制御することで、その加工溝深
さなどを精密に調整することができるなどの特徴
を有するものである。[Table] (Effects of the Invention) As described above, according to the present invention, in the sliding member made of high-density silicon carbide sintered body, a groove for lubrication is formed in the required portion of the sliding end surface, so that the heat resistant Hydrodyna not only has excellent wear resistance, wear resistance, and corrosion resistance, but also has significantly improved lubricity and cooling performance on the sliding end surface, making it suitable for use even under high load conditions. It is possible to provide a sliding member made of high-density silicon carbide sintered body for a mix seal. Further, according to the method of grooving the sliding end face of a sliding member made of a high-density silicon carbide sintered body for a hydrodynamic seal of the present invention, in the sliding member made of a high-density SiC sintered body, the sliding end face is covered. The entire surface except the part where the processed grooves are formed is coated with a decomposition inhibitor having a melting point higher than the decomposition point of the high-density SiC sintered body, and then the coated sliding member is
Grooving is performed by heat treatment at a temperature higher than the decomposition point of the high-density SiC sintered body and lower than the melting point of the decomposition inhibitor to sublimate and decompose the groove-forming portion to be processed that is not coated over a predetermined depth. and
After that, the coating was removed by oxidation, chemical treatment, or mechanical treatment, so it was difficult to create grooves for lubrication on sliding members made of high-density silicon carbide sintered body, which was extremely difficult in the past. It is characterized by being extremely easy to perform, and by controlling the temperature and time during heat treatment, the depth of the processed groove can be precisely adjusted.
第1図aないしdはこの発明に係る摺動端面溝
を有する高密度SiC焼結体製摺動部材の摺動端面
溝加工方法の一実施例を工程順に示すそれぞれ要
部の拡大断面図、第2図はハイドロダイナミツク
用摺動部材の一例を示す平面図である。
1……高密度炭化珪素焼結体製摺動部材、2…
…同摺動部材の摺動端面、2a……同摺動端面の
被加工溝形成部分、3……コーテイング被覆させ
た分解防止剤、4……摺動端面に形成された溝。
FIGS. 1a to 1d are enlarged sectional views of essential parts showing, in order of steps, an embodiment of the method for machining sliding end grooves of a high-density SiC sintered sliding member having sliding end grooves according to the present invention; FIG. 2 is a plan view showing an example of a hydrodynamic sliding member. 1...Sliding member made of high-density silicon carbide sintered body, 2...
...Sliding end face of the sliding member, 2a... Processed groove forming portion of the sliding end face, 3... Anti-decomposition agent coated, 4... Groove formed in the sliding end face.
Claims (1)
その摺動端面所要部分に潤滑用の溝を形成したこ
とを特徴とするハイドロダイナミツクシール用高
密度炭化珪素焼結体製摺動部材。 2 高密度炭化珪素焼結体で構成された摺動部材
を用い、その摺動部材の摺動端面の被加工溝形成
部分を除く全表面に、高密度炭化珪素焼結体の分
解点より高い融点をもつ分解防止剤でコーテイン
グ被覆し、次いでコーテイング被覆された摺動部
材を、高密度炭化珪素焼結体の分解点より高い温
度で且つ分解防止剤の融点より低い温度で熱処理
して、前記コーテイング被覆されていない被加工
溝形成部分を所定深さに亘り昇華分解させて溝加
工をなし、その後、酸化または薬品処理若しくは
機械処理によつて、前記コーテイング被覆を除去
することを特徴とするハイドロダイナミツクシー
ル用高密度炭化珪素焼結体製摺動部材の摺動端面
溝加工方法。[Claims] 1. Regarding a sliding member made of high-density silicon carbide sintered body,
A sliding member made of a high-density silicon carbide sintered body for a hydrodynamic seal, characterized in that a groove for lubrication is formed in a required portion of the sliding end surface. 2 A sliding member made of a high-density silicon carbide sintered body is used, and the entire surface of the sliding end face of the sliding member except for the groove forming part is heated to a temperature higher than the decomposition point of the high-density silicon carbide sintered body. The sliding member coated with a decomposition inhibitor having a melting point is then heat-treated at a temperature higher than the decomposition point of the high-density silicon carbide sintered body and lower than the melting point of the decomposition inhibitor. The groove forming portion to be machined which is not covered with the coating is sublimated and decomposed over a predetermined depth to form the groove, and then the coating is removed by oxidation, chemical treatment, or mechanical treatment. A method for machining grooves on the sliding end face of a sliding member made of high-density silicon carbide sintered body for dynamic seals.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP59222574A JPS61101480A (en) | 1984-10-22 | 1984-10-22 | Sliding member of high density silicon carbide sintered bodyand method of processing sliding side surface groove |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP59222574A JPS61101480A (en) | 1984-10-22 | 1984-10-22 | Sliding member of high density silicon carbide sintered bodyand method of processing sliding side surface groove |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS61101480A JPS61101480A (en) | 1986-05-20 |
| JPH0218317B2 true JPH0218317B2 (en) | 1990-04-25 |
Family
ID=16784598
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP59222574A Granted JPS61101480A (en) | 1984-10-22 | 1984-10-22 | Sliding member of high density silicon carbide sintered bodyand method of processing sliding side surface groove |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS61101480A (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0366919A (en) * | 1989-08-04 | 1991-03-22 | Eagle Ind Co Ltd | Sliding bearing and manufacture thereof |
| WO2001016655A1 (en) | 1999-08-26 | 2001-03-08 | Seiko Epson Corporation | Timepiece device |
| JP2006021986A (en) * | 2004-06-08 | 2006-01-26 | Fujitsu Ltd | Method for processing silicon carbide material |
-
1984
- 1984-10-22 JP JP59222574A patent/JPS61101480A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS61101480A (en) | 1986-05-20 |
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