JPH0210821Y2 - - Google Patents

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Publication number
JPH0210821Y2
JPH0210821Y2 JP10424284U JP10424284U JPH0210821Y2 JP H0210821 Y2 JPH0210821 Y2 JP H0210821Y2 JP 10424284 U JP10424284 U JP 10424284U JP 10424284 U JP10424284 U JP 10424284U JP H0210821 Y2 JPH0210821 Y2 JP H0210821Y2
Authority
JP
Japan
Prior art keywords
elastic member
enclosure
rotating shaft
movable body
gas
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
Application number
JP10424284U
Other languages
Japanese (ja)
Other versions
JPS6119130U (en
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed filed Critical
Priority to JP10424284U priority Critical patent/JPS6119130U/en
Publication of JPS6119130U publication Critical patent/JPS6119130U/en
Application granted granted Critical
Publication of JPH0210821Y2 publication Critical patent/JPH0210821Y2/ja
Granted legal-status Critical Current

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Description

【考案の詳細な説明】 〔考案の利用分野〕 本考案は、高速回転する高温の回転軸を空気、
窒素あるいはヘリウムなどの気体膜により浮上さ
せた状態で回転可能に支持する動圧式の気体軸受
に関する。
[Detailed description of the invention] [Field of application of the invention] The invention uses a high-temperature rotating shaft that rotates at high speed to
This invention relates to a hydrodynamic gas bearing that is rotatably supported in a suspended state by a film of gas such as nitrogen or helium.

〔考案の背景〕[Background of the idea]

先ず、従来例を第9図に基いて説明する(例え
ば特開昭56−35816号公報参照)。同図において、
1はホルダーで該ホルダー1は円筒体形状に形成
され、空洞部2の内面に有端かつ波板形状の弾性
部材3が周設されている。そして、この弾性部材
3に有端かつ平面形状のトツプ・ホイル(top
foil)すなわち囲い体4が固着されている。該囲
い体4は、回転軸5と離間状態で該回転軸5を全
周にわたつて囲つている。該囲い体4及び弾性部
材3の同一側の一端がホルダー1の内面に圧入さ
れたキー6により挟持固定されている。ホルダー
1の外側面は、外側のケーシング7と面接触状態
で保持されている。
First, a conventional example will be explained based on FIG. 9 (see, for example, Japanese Patent Laid-Open No. 56-35816). In the same figure,
Reference numeral 1 denotes a holder, and the holder 1 is formed into a cylindrical shape, and an elastic member 3 having an end and a corrugated plate shape is provided around the inner surface of a hollow portion 2. A top foil (top foil) having an end and a planar shape is attached to this elastic member 3.
foil), that is, the enclosure 4 is fixed. The enclosure 4 surrounds the entire circumference of the rotating shaft 5 while being spaced apart from the rotating shaft 5. One end of the enclosure 4 and the elastic member 3 on the same side are clamped and fixed by a key 6 press-fitted into the inner surface of the holder 1. The outer surface of the holder 1 is held in surface contact with the outer casing 7.

次に動作を説明する。回転軸5が回転すると、
回転軸5の外側面と囲い体4の間の微少隙間に周
囲の気体がその粘性により引き込まれ、いわゆる
くさび膜作用により圧力が発生し、回転軸5は前
記圧力に基づく気体膜により回転可能に支持され
る。この気体膜の圧力は、回転軸5と囲い体4と
の間隔すなわち気体膜の厚さによつて決まる。弾
性部材3を有する気体軸受の場合、回転軸5の回
転によつて生じる動荷重や衝撃荷重等によつて当
該回転軸5が軸芯位置から偏位するが、第10図
に示した如く、該回転軸5の偏位に対応して弾性
部材3がある程度まで変形(同図の下端部)する
ため、回転軸5の偏位に対して気体膜の厚さの一
様な領域が広くなり、従つて、前記衝撃等の影響
は緩和吸収され、負荷容量の大きい気体軸受とな
つている。そして、通常の運転では、大きい気体
膜厚で作動することができ、信頼性の高い軸受と
なつている。参考までに、弾性部材3を有しない
型式の気体軸受における回転軸5の軸芯位置から
の偏位に対する圧力分布を第11図に示す。同図
から解るように気体膜厚さの一様な領域は狭く、
衝撃等により悪影響を受けやすいと言える。
Next, the operation will be explained. When the rotating shaft 5 rotates,
The surrounding gas is drawn into the minute gap between the outer surface of the rotating shaft 5 and the enclosure 4 due to its viscosity, and pressure is generated by a so-called wedge film action, and the rotating shaft 5 is made rotatable by the gas film based on the pressure. Supported. The pressure of this gas film is determined by the distance between the rotating shaft 5 and the enclosure 4, that is, the thickness of the gas film. In the case of a gas bearing having an elastic member 3, the rotating shaft 5 deviates from its axis position due to dynamic loads, impact loads, etc. generated by the rotation of the rotating shaft 5, but as shown in FIG. Since the elastic member 3 deforms to a certain extent (lower end in the figure) in response to the deviation of the rotating shaft 5, the region where the thickness of the gas film is uniform becomes wider with respect to the deviation of the rotating shaft 5. Therefore, the effects of the above-mentioned shocks and the like are relaxed and absorbed, resulting in a gas bearing with a large load capacity. During normal operation, the bearing can operate with a large gas film thickness, making it a highly reliable bearing. For reference, FIG. 11 shows the pressure distribution with respect to the deviation from the axial center position of the rotating shaft 5 in a type of gas bearing that does not have the elastic member 3. As can be seen from the figure, the region where the gas film thickness is uniform is narrow;
It can be said that it is easily affected by adverse effects such as shock.

上記の如く、弾性部材3を設けたことにより、
回転軸5に作用する衝撃等に対しては悪影響を受
けにくく信頼性の高い気体軸受となつているが、
従来は回転軸5の熱膨張に対しては全く考慮され
ていなかつた。すなわち、高温の温度場で気体軸
受を使用する場合、回転軸5にタービンの熱が伝
熱され、その結果、該回転軸5が熱膨張し、囲い
体4と回転軸5との隙間が小さくなる。一般に、
気体軸受では囲い体4と回転軸5との間隔は非常
に小さいため、回転軸5の回転時に気体膜ができ
ず、当該回転軸5と囲い体4とが、直接固体接触
して焼き付きを起こすおそれがあつた。
As mentioned above, by providing the elastic member 3,
Although it is a highly reliable gas bearing that is not susceptible to adverse effects such as impacts acting on the rotating shaft 5,
Conventionally, no consideration was given to thermal expansion of the rotating shaft 5. That is, when using a gas bearing in a high temperature field, the heat of the turbine is transferred to the rotating shaft 5, and as a result, the rotating shaft 5 thermally expands, and the gap between the enclosure 4 and the rotating shaft 5 becomes smaller. Become. in general,
In a gas bearing, since the distance between the enclosure 4 and the rotating shaft 5 is very small, a gas film is not formed when the rotating shaft 5 rotates, and the rotating shaft 5 and the enclosure 4 come into direct solid contact, causing seizure. I was afraid.

他の従来例として、特公昭55−17851号公報や
特開昭55−166525号公報に記載された流体軸受が
提供されているが、これらも回転軸の熱膨張につ
いては考慮されておらず、上記従来例と同様の欠
点を有している。
As other conventional examples, fluid bearings described in Japanese Patent Publication No. 55-17851 and Japanese Patent Application Laid-open No. 55-166525 have been provided, but these also do not take into account the thermal expansion of the rotating shaft. It has the same drawbacks as the conventional example described above.

また、従来は囲い体4と弾性部材3の同一側の
端部を離間して別個に固定していたため、この端
部付近においては弾性部材3はその波板形状を保
持することができず、すなわち、波の高さが不揃
になり、また囲い体4も一様な平面形状を維持す
ることが、その結果、回転軸の全周にわたつて一
様な気体膜厚さを形成しにくいという欠点があつ
た。また、キー6の付近では軸芯方向(長手方
向)にわたつても軸受隙間が一様でなくなり、軸
受性能の低下さらにはキー6が空洞部2内に突出
することにより軸受の耐久性が低下するという欠
点があつた。
Furthermore, in the past, the ends of the enclosure 4 and the elastic member 3 on the same side were separated and fixed separately, so the elastic member 3 could not maintain its corrugated shape near this end. In other words, the height of the waves becomes uneven, and the enclosure 4 also has to maintain a uniform planar shape, which makes it difficult to form a uniform gas film thickness around the entire circumference of the rotation axis. There was a drawback. Furthermore, the bearing clearance is not uniform in the axial direction (longitudinal direction) in the vicinity of the key 6, resulting in a decrease in bearing performance, and furthermore, as the key 6 protrudes into the cavity 2, the durability of the bearing decreases. There was a drawback of doing so.

〔考案の目的〕[Purpose of invention]

本考案は、上記事情に鑑みなされたもので、回
転軸の熱膨張に対して気体膜厚さを一定に保つ補
償機能を有し、且つ囲い体及び弾性部材を回転軸
の全周にわたつて略一様な形状で形成できるよう
にして全周にわたつて気体膜厚さを一様にし、こ
れにより軸受性能を向上させると共に、耐久性を
向上させることのできる気体軸受を提供するのが
目的である。
The present invention has been developed in view of the above circumstances, and has a compensating function to keep the gas film thickness constant against thermal expansion of the rotating shaft, and also has an enclosure and an elastic member around the entire circumference of the rotating shaft. The purpose is to provide a gas bearing that can be formed into a substantially uniform shape so that the gas film thickness is uniform over the entire circumference, thereby improving bearing performance and durability. It is.

〔考案の概要〕[Summary of the idea]

本考案の特徴は、ホルダーの空洞部内面と弾性
部材との間の一部に可動体を配設し、該可動体の
外側面と前記空洞部内面との間に前記弾性部材よ
り弾性定数の小さい補償用弾性部材を配設し、前
記弾性部材及び囲い体の同一側の端部を重ね合
せ、該重ね合せ端部を可動体の内側面から外側面
に向けて穿設されたスリツトに差し込み固定する
ことにより、回転軸が熱膨張し、気体膜厚さが小
さくなつて圧力が上昇すると、この上昇圧力によ
つて可動体が回転軸より離反する方向に移動し、
気体膜厚さを一定に保つようにすると共に、囲い
体及び弾性部材の同一側の端部を上記の如く、重
ね合せてスリツトに差し込んで固定することによ
り、この固定端部近傍においても囲い体の一様な
平面形状及び弾性部材の一様な波板形状を保持で
きるようにした点にある。
A feature of the present invention is that a movable body is disposed in a part between the inner surface of the cavity of the holder and the elastic member, and the elastic constant is greater than that of the elastic member between the outer surface of the movable body and the inner surface of the cavity. A small compensating elastic member is provided, the ends of the elastic member and the enclosure on the same side are overlapped, and the overlapped end is inserted into a slit drilled from the inner surface to the outer surface of the movable body. By fixing the rotating shaft, the rotating shaft expands thermally, the gas film thickness decreases, and the pressure rises. This increased pressure causes the movable body to move away from the rotating shaft.
In addition to keeping the gas film thickness constant, by overlapping the ends of the enclosure and the elastic member on the same side and inserting them into the slits and fixing them as described above, the enclosure can be fixed even near the fixed end. It is possible to maintain a uniform planar shape of the elastic member and a uniform corrugated plate shape of the elastic member.

〔考案の実施例〕[Example of idea]

以下、本考案を図面の実施例に基いて詳細に説
明する。第1図は本考案に係る気体軸受の断面
図、第2図及び第3図はそれぞれ同要部拡大平面
図、第4図は実際の使用状態を示す要部断面図、
第5図は囲い体の組付前の状態における要部拡大
斜視図、第6図は弾性部材の組付前の状態におけ
る要部拡大斜視図を示す。同図において、8は可
動体を示し、該可動体8は、断面が略三日月形状
に形成され、ホルダー1の空洞部2内面と弾性部
材3との間の一部に配設されている。可動体8の
外側面弧面11と空洞部2内面との間に波板形状
の補償用弾性部材12がその一部を空洞部2内面
に溶接固定されて配設されている。該補償用弾性
部材12は、その弾性定数が前記弾性部材3より
も小さく設定されている。更に、可動体8の外側
面弧面11には適宜間隔毎に複数個の突起23,
23,……が突設されている。該突起23,2
3,……は対向する内面13と離間して設けられ
ており、この離間寸法が可動体8の最大移動量と
なる。可動体8の略中央部分には内側面弧面9か
ら外側面弧面11に向けてスリツトが穿設されて
いる。囲い体4の端部に固定用舌片25が突設さ
れており(第5図)、また、弾性部材3の端にも
固定用舌片26が突設されており(第6図)、こ
れら両固定用舌片25,26及び両端部を重ね合
わせ、この重ね合せ端部の当該固定用舌片25,
26を前記スリツト24に差し込むことにより当
該囲い体4及び弾性部材3が可動体8に固定され
ている。このように端部重ね合せによる差し込み
固定構造にすることにより弾性部材3の波板形状
を固定部近傍まで形成することができ、また、囲
い体4の一様な平面形状を同じく固定部近傍まで
形成することができる。27はリセス部すなわち
凹部を示す。空洞部2の内面は、異なる曲率の2
つの内面13,14により形成されている。すな
わち、内面13の曲率は内面14よりも大きい。
内面14は120度の円弧角の範囲に形成され、該
内面14の部分に弾性部材3の座部15,15,
……が接触している。また、可動体8の内側円弧
面9の曲率は前記内面14の曲率より僅かに大き
く形成され、可動体8が外方に移動したときも、
軸受全周にわたつて適正な軸受隙間ができるよう
形成されている。ホルダー1と外側のケーシング
7とは多点接触構造により互いに接触し、該ホル
ダー1とケーシング7との間に空隙となる非接触
部17,18,19が形成されている。20,2
1,22は前記多点接触構造を構成する接点を示
す。該接点20,21,22はガタ防止のため周
方向に等分割された少なくとも3点以上の接触構
造にする。この構造により外部からの伝熱が空隙
である非接触部17,18,19により大幅に減
少されるため、気体軸受への伝熱が大幅に減少し
て当該気体軸受の熱劣化を防ぐことができる。ま
た、弾性部材3,12のばね特性の劣化や囲い体
4、弾性部材3の熱変形及び酸化を防ぐことがで
きる。第4図において、16はタービンを示す。
Hereinafter, the present invention will be explained in detail based on the embodiments shown in the drawings. FIG. 1 is a sectional view of the gas bearing according to the present invention, FIGS. 2 and 3 are enlarged plan views of the same main parts, and FIG. 4 is a sectional view of the main parts showing actual usage conditions.
FIG. 5 is an enlarged perspective view of the main part before the enclosure is assembled, and FIG. 6 is an enlarged perspective view of the main part before the elastic member is assembled. In the figure, reference numeral 8 indicates a movable body, and the movable body 8 has a substantially crescent-shaped cross section and is disposed in a part between the inner surface of the cavity 2 of the holder 1 and the elastic member 3. A compensating elastic member 12 in the form of a corrugated plate is disposed between the outer arcuate surface 11 of the movable body 8 and the inner surface of the cavity 2, with a part thereof being welded and fixed to the inner surface of the cavity 2. The compensating elastic member 12 is set to have a smaller elastic constant than the elastic member 3. Furthermore, a plurality of protrusions 23 are provided at appropriate intervals on the outer arcuate surface 11 of the movable body 8.
23,... are provided protrudingly. The protrusion 23,2
3, . . . are provided apart from the opposing inner surface 13, and this distance is the maximum amount of movement of the movable body 8. A slit is bored in a substantially central portion of the movable body 8 from an inner arcuate surface 9 to an outer arcuate surface 11. A fixing tongue piece 25 is protruded from the end of the enclosure 4 (FIG. 5), and a fixing tongue piece 26 is also protruded from the end of the elastic member 3 (FIG. 6). These both fixing tongue pieces 25, 26 and both ends are overlapped, and the fixing tongue piece 25,
26 into the slit 24, the enclosure 4 and elastic member 3 are fixed to the movable body 8. By adopting the insertion fixing structure by overlapping the ends in this way, the corrugated plate shape of the elastic member 3 can be formed to the vicinity of the fixed part, and the uniform planar shape of the enclosure 4 can also be formed to the vicinity of the fixed part. can be formed. 27 indicates a recessed portion or a recessed portion. The inner surface of the cavity 2 has two different curvatures.
It is formed by two inner surfaces 13 and 14. That is, the curvature of the inner surface 13 is greater than that of the inner surface 14.
The inner surface 14 is formed within a range of an arcuate angle of 120 degrees, and the seat portions 15, 15,
...is in contact. Further, the curvature of the inner circular arc surface 9 of the movable body 8 is formed to be slightly larger than the curvature of the inner surface 14, so that even when the movable body 8 moves outward,
The bearing is formed so that there is an appropriate bearing clearance around the entire circumference of the bearing. The holder 1 and the outer casing 7 are in contact with each other through a multi-point contact structure, and non-contact parts 17, 18, and 19 are formed between the holder 1 and the casing 7, which serve as gaps. 20,2
Reference numerals 1 and 22 indicate contacts constituting the multi-point contact structure. The contacts 20, 21, 22 have a contact structure of at least three points equally divided in the circumferential direction to prevent backlash. With this structure, heat transfer from the outside is significantly reduced by the non-contact parts 17, 18, and 19, which are voids, so heat transfer to the gas bearing is significantly reduced and thermal deterioration of the gas bearing can be prevented. can. Further, deterioration of the spring characteristics of the elastic members 3 and 12 and thermal deformation and oxidation of the enclosure 4 and the elastic member 3 can be prevented. In FIG. 4, 16 indicates a turbine.

次に作用を説明する。タービン16からの伝熱
により回転軸5が熱膨張し、囲い体4との隙間す
なわち気体膜厚さが小さくなると圧力が上昇す
る。すると囲い体4が拡がる方向に力を受け、こ
の力が可動体8を回転軸5より離反する方向に押
圧する。このとき、補償用弾性部材12の弾性定
数が弾性部材3より小さく設定されているため、
補償用弾性部材12が変形する。これにより回転
軸5の熱膨張分が可動体8の移動によつて補償さ
れ、気体膜厚さは一定に保たれる。また、弾性部
材3及び囲い体4の端部重ね合せ差し込み固定構
造により、この固定部近傍まで当該弾性部材3及
び囲い体4の波板形状及び平面形状の各形状を維
持して形成することができ、これにより、回転軸
全周にわたつて気体膜厚さを略一定に形成するこ
とができる。
Next, the effect will be explained. The rotating shaft 5 thermally expands due to heat transfer from the turbine 16, and when the gap with the enclosure 4, that is, the gas film thickness becomes smaller, the pressure increases. Then, the enclosure 4 receives a force in the direction of expansion, and this force presses the movable body 8 in a direction away from the rotating shaft 5. At this time, since the elastic constant of the compensating elastic member 12 is set smaller than that of the elastic member 3,
The compensating elastic member 12 is deformed. Thereby, the thermal expansion of the rotating shaft 5 is compensated for by the movement of the movable body 8, and the gas film thickness is kept constant. Furthermore, due to the overlapping insertion and fixing structure of the ends of the elastic member 3 and the enclosure 4, it is possible to maintain the corrugated plate shape and planar shape of the elastic member 3 and the enclosure 4 up to the vicinity of the fixed portion. As a result, the gas film thickness can be formed to be substantially constant over the entire circumference of the rotating shaft.

第7図は本考案の他実施例を示す断面図で、補
償用弾性部材12は波板形状ではなく、平面折曲
形状に形成したもので、その他の構成及び作用は
前記実施例と同様なので同一部分に同一符号を付
して説明は省略する。
FIG. 7 is a cross-sectional view showing another embodiment of the present invention, in which the compensating elastic member 12 is formed not in the shape of a corrugated plate but in a bent plane shape, and other configurations and functions are the same as in the previous embodiment. Identical parts are given the same reference numerals and explanations will be omitted.

第8図も本考案の他実施例を示す断面図で、ホ
ルダー1の外面を一様な円柱体面形状に形成した
ものである。その他の構成及び作用は前記実施例
と同様なので同一部分に同一符号を付して説明は
省略する。
FIG. 8 is also a sectional view showing another embodiment of the present invention, in which the outer surface of the holder 1 is formed into a uniform cylindrical shape. Other configurations and operations are similar to those of the previous embodiment, so the same parts are denoted by the same reference numerals and explanations will be omitted.

〔考案の効果〕[Effect of idea]

本考案によれば、回転軸の熱膨張に対して、そ
の膨張分を打ち消す方向に移動する補償機能を有
する可動体を設けたので、前記熱膨張があつても
気体膜厚さは常に一定に保たれる。従つて、高温
の温度場で気体軸受を使用しても、従来のように
焼き付き等による破損のおそれは少なく、信頼性
の高い気体軸受となる。
According to the present invention, a movable body is provided that has a compensating function of moving in a direction to cancel out the thermal expansion of the rotating shaft, so that the gas film thickness is always constant even when the thermal expansion occurs. It is maintained. Therefore, even if the gas bearing is used in a high-temperature field, there is less risk of damage due to seizure or the like as in conventional gas bearings, resulting in a highly reliable gas bearing.

また、囲い体及び弾性部材の同一側の端部を上
記の如く、重ね合せて可動体に設けたスリツトに
差し込んで固定するようにしたので、この固定端
部近傍においても当該囲い体の一様な平面形状及
び弾性部材の一様な波板形状を維持して形成する
ことができるので、回転軸の全周にわたつて弾性
部材によるバネ剛性が略均一となり、気体膜厚さ
を一様にすることができ、これにより軸受性能を
向上させることができる。また、従来のようなキ
ーによる固定に比して、固定部近傍の信頼性及び
耐久性を向上させることもできる。
In addition, since the ends of the enclosure and the elastic member on the same side are overlapped and fixed by being inserted into the slit provided in the movable body as described above, the enclosure is uniform evenly near the fixed end. Since it is possible to maintain a flat planar shape and a uniform corrugated shape of the elastic member, the spring stiffness of the elastic member is approximately uniform over the entire circumference of the rotating shaft, and the gas film thickness can be made uniform. This allows the bearing performance to be improved. Furthermore, the reliability and durability of the vicinity of the fixing part can be improved compared to fixing with a conventional key.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本考案に係る気体軸受の断面図、第2
図及び第3図はそれぞれ同要部拡大平面図、第4
図は実際の使用状態を示す要部断面図、第5図は
囲い体の組付前の状態における要部拡大斜視図、
第6図は弾性部材の組付前の状態における要部拡
大斜視図、第7図及び第8図はそれぞれ本考案の
異なる他実施例を示す断面図、第9図は従来例を
示す断面図、第10図は同従来例における回転軸
の軸芯位置からの偏位に対する気体膜の圧力分布
を示す説明図、第11図は圧力分布の参考説明図
を示す。 1……ホルダー、2……空洞部、3……弾性部
材、4……囲い体、5……回転軸、7……ケーシ
ング、8……可動体、9……内側円弧面、11…
…外側円弧面、12……補償用弾性部材、17,
18,19……非接触部、24……スリツト。
Figure 1 is a sectional view of the gas bearing according to the present invention, Figure 2 is a cross-sectional view of the gas bearing according to the present invention;
Figures 3 and 3 are enlarged plan views of the same main parts, respectively.
The figure is a sectional view of the main part showing the actual usage state, FIG. 5 is an enlarged perspective view of the main part in the state before the enclosure is assembled,
FIG. 6 is an enlarged perspective view of the main part of the elastic member before assembly, FIGS. 7 and 8 are sectional views showing different embodiments of the present invention, and FIG. 9 is a sectional view showing a conventional example. , FIG. 10 is an explanatory diagram showing the pressure distribution of the gas film with respect to the deviation from the axial center position of the rotating shaft in the conventional example, and FIG. 11 is a reference explanatory diagram of the pressure distribution. DESCRIPTION OF SYMBOLS 1... Holder, 2... Cavity part, 3... Elastic member, 4... Enclosure, 5... Rotating shaft, 7... Casing, 8... Movable body, 9... Inner circular arc surface, 11...
...outer circular arc surface, 12...compensating elastic member, 17,
18, 19...non-contact part, 24...slit.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 筒形状の空洞部を有するホルダーの該空洞部内
面に有端かつ波板形状の弾性部材を周設し、該弾
性部材に有端かつ平面形状の囲い体を取り付けて
該囲い体により回転軸を離間して囲うようにした
気体軸受において、前記空洞部内面と前記弾性部
材との間の一部に可動体を配設し、該可動体の外
側面と前記空洞部内面との間に前記弾性部材より
弾性定数の小さい補償用弾性部材を配設し、前記
弾性部材及び囲い体の同一側の端部を重ね合せ、
該重ね合せ端部を可動体の内側面から外側面に向
けて穿設されたスリツトに差し込み固定したこと
を特徴とする気体軸受。
An elastic member with an end and a corrugated plate shape is provided around the inner surface of the hollow part of a holder having a cylindrical hollow part, and an enclosure body with an end and a planar shape is attached to the elastic member, and the rotation axis is controlled by the enclosure body. In the gas bearing that is separated and enclosed, a movable body is disposed in a part between the inner surface of the cavity and the elastic member, and the elastic member is disposed between the outer surface of the movable body and the inner surface of the cavity. disposing a compensating elastic member having a smaller elastic constant than the member, overlapping the ends of the elastic member and the enclosure on the same side;
A gas bearing characterized in that the overlapping ends are inserted and fixed into a slit bored from the inner surface to the outer surface of the movable body.
JP10424284U 1984-07-10 1984-07-10 gas bearing Granted JPS6119130U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10424284U JPS6119130U (en) 1984-07-10 1984-07-10 gas bearing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10424284U JPS6119130U (en) 1984-07-10 1984-07-10 gas bearing

Publications (2)

Publication Number Publication Date
JPS6119130U JPS6119130U (en) 1986-02-04
JPH0210821Y2 true JPH0210821Y2 (en) 1990-03-16

Family

ID=30663598

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10424284U Granted JPS6119130U (en) 1984-07-10 1984-07-10 gas bearing

Country Status (1)

Country Link
JP (1) JPS6119130U (en)

Also Published As

Publication number Publication date
JPS6119130U (en) 1986-02-04

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