JPH0210817Y2 - - Google Patents

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Publication number
JPH0210817Y2
JPH0210817Y2 JP10352984U JP10352984U JPH0210817Y2 JP H0210817 Y2 JPH0210817 Y2 JP H0210817Y2 JP 10352984 U JP10352984 U JP 10352984U JP 10352984 U JP10352984 U JP 10352984U JP H0210817 Y2 JPH0210817 Y2 JP H0210817Y2
Authority
JP
Japan
Prior art keywords
elastic member
rotating shaft
movable body
holder
cavity
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
JP10352984U
Other languages
Japanese (ja)
Other versions
JPS6119126U (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 JP10352984U priority Critical patent/JPS6119126U/en
Publication of JPS6119126U publication Critical patent/JPS6119126U/en
Application granted granted Critical
Publication of JPH0210817Y2 publication Critical patent/JPH0210817Y2/ja
Granted legal-status Critical Current

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  • Support Of The Bearing (AREA)

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8図に基づいて説明する(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の内面に波板形状の弾性部材
3が周接されている。そして、この弾性部材3に
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の一端がホルダー1の内
面に固定されたキー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. 8 (see, for example, Japanese Patent Laid-Open No. 56-35816). In the figure, reference numeral 1 denotes a holder, and the holder 1 is formed into a cylindrical shape, and a corrugated elastic member 3 is circumferentially attached to the inner surface of a cavity 2. A top foil or enclosure 4 is fixed to the elastic member 3. 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 are clamped and fixed by a key 6 fixed to the inner surface of the holder 1. The outer surface of the holder 1 is connected to the outer casing 7.
is held in surface contact with.

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。
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.

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9
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10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。
In the case of a gas bearing having an elastic member 3, the rotating shaft 5
The rotating shaft 5 is deviated from the axis position due to the dynamic load, impact load, etc. caused by the rotation of the 9th axis.
As shown in the figure, since the elastic member 3 deforms to a certain extent in response to the deflection of the rotating shaft 5 (see the lower end of the figure), the thickness of the gas film changes with respect to the deflection of the rotating shaft 5. Therefore, the influence of the above-mentioned impact etc. is 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. 10 shows the pressure distribution with respect to the deviation from the axis 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 area where the gas film thickness is uniform is narrow and is likely to be adversely affected by impacts and the like.

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. . In general, in a gas bearing, the distance between the enclosure 4 and the rotating shaft 5 is very small, so 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, resulting in seizure. There was a risk of this happening.

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.

〔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
償機能を有する気体軸受を提供するのが目的であ
る。
The present invention was devised in view of the above circumstances, and it is an object of the present invention to provide a gas bearing having a compensating function to maintain a constant gas film thickness against thermal expansion of a rotating shaft.

〔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
内側面に前記弾性部材の適宜位置を固定すると共
に、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, the elastic member is fixed at an appropriate position on the inner surface of the movable body, and the movable body is By disposing a compensating elastic member having a smaller elastic constant than the elastic member between the outer surface and the inner surface of the cavity, when the rotating shaft thermally expands, the gas film thickness decreases, and the pressure increases, This increased pressure causes the movable body to move in a direction away from the rotating shaft, thereby keeping the gas film thickness constant.

〔考案の実施例〕[Example of idea]

以下、本考案を図面の実施例に基づいて詳細に
説明する。第1図は本考案に係る気体軸受の断面
図、第2図は実際の使用状態を示す要部断面図を
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。この可動体8の内側円弧面9に
弾性部材3の一端10が溶接固定されている。ま
た、可動体8の外側円弧面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
が空洞部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。空洞
部2の内面は、異なる曲率の2つの内面13,1
4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。
第2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 a gas bearing according to the present invention, and FIG. 2 is a sectional view of a main part showing the actual usage state. 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. One end 10 of the elastic member 3 is welded and fixed to the inner arcuate surface 9 of the movable body 8. Further, a corrugated plate-shaped compensating elastic member 12 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. The inner surface of the cavity 2 has two inner surfaces 13, 1 with different curvatures.
4. 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 seats 15, 15, . . . of the elastic member 3 are in contact with a portion of the inner surface 14. 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, an appropriate bearing gap is created over the entire circumference of the bearing. It is formed.
In FIG. 2, 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。
Next, the action 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.

第3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の形状を前記実施例の如く波板
形状ではなく、平面折曲形状にしたものであり、
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. 3 is a sectional view showing another embodiment of the present invention, in which the shape of the compensating elastic member 12 is not a corrugated plate shape as in the previous embodiment, but a plane bent 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.

第4図も本考案の他実施例を示す断面図で、ホ
ルダー1を外側のケーシング7と多点接触構造と
して、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を設けたもので
ある。20,21,22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。第5図及び第6図は、
接点20のそれぞれ異なる実施例を示す要部斜視
図で、第5図ではホルダー1の幅方向の両端に設
けた突起20a,20bにより形成したもので、
第6図は突起20c,20dをホルダー1の幅方
向の両端より内側に突設させることにより形成さ
れている。いずれも該ホルダー1とケーシング7
との非接触部の大きさを増すための構造である。
その他の構成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。作用的には
タービン16からの伝熱が空隙である非接触部1
7,18,19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。
FIG. 4 is also a cross-sectional view showing another embodiment of the present invention, in which the holder 1 has a multi-point contact structure with the outer casing 7, and non-contact parts 17, 18, which form gaps between the holder 1 and the casing 7, 19. Reference numerals 20, 21, and 22 indicate contacts constituting the multi-point contact structure. The contacts 20, 21, 22 are divided into at least three equal parts in the circumferential direction to prevent rattling.
Create a contact structure with points or more. Figures 5 and 6 are
FIG. 5 is a perspective view of a main part showing different embodiments of the contact 20. In FIG.
In FIG. 6, projections 20c and 20d are formed by protruding inward from both ends of the holder 1 in the width direction. Both the holder 1 and the casing 7
This structure is designed to increase the size of the non-contact area.
The rest of the configuration is similar to that of the previous embodiment, so the same parts are given the same reference numerals and the explanation will be omitted. Operationally, the heat transfer from the turbine 16 is through the non-contact part 1, which is the air gap.
7, 18, and 19, the heat transfer to the gas bearing is significantly reduced, and thermal deterioration of the gas bearing can be prevented. Moreover, the elastic member 3,
Deterioration of the spring characteristics of the spring 12 and thermal deformation and oxidation of the enclosure 4 and the elastic member 3 can be prevented.

第7図は更に本考案の他実施例を示す断面図
で、第4図に示した実施例において、補償用弾性
部材12の形状を第3図に示した実施例と同様の
形状のものにしたもので、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
付して説明を省略する。
FIG. 7 is a sectional view showing another embodiment of the present invention. In the embodiment shown in FIG. 4, the shape of the compensating elastic member 12 is the same as that in the embodiment shown in FIG. 3. Since the other configurations and functions are the same as those of the previous embodiment, the same parts are denoted by the same reference numerals and the explanation thereof 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 which 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 kept constant even when the thermal expansion occurs. dripping 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.

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

第1図は本考案に係る気体軸受の断面図、第2
図は実際の使用状態を示す要部断面図、第2図は
実際の使用状態を示す要部断面図、第3図及び第
4図は本考案のそれぞれ異なる他実施例を示す断
面図、第5図及び第6図は第4図の実施例につい
てのそれぞれ異なる他実施例を示す要部斜視図、
第7図も本考案の他実施例を示す断面図、第8図
は従来例を示す断面図、第9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10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。
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;
Figure 2 is a sectional view of the main part showing the actual usage state, Figure 2 is a sectional view of the main part showing the actual usage state, Figures 3 and 4 are sectional views showing other different embodiments of the invention, 5 and 6 are perspective views of main parts showing different embodiments of the embodiment shown in FIG. 4,
Fig. 7 is also a sectional view showing another embodiment of the present invention, Fig. 8 is a sectional view showing a conventional example, and Fig. 9 is a pressure distribution of the gas film with respect to deviation from the axis of the rotating shaft in the conventional example. FIG. 10 is a reference diagram of 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.

Claims (1)

【実用新案登録請求の範囲】 (1) 筒形状の空洞部を有するホルダーの該空洞部
内面に弾性部材を介して回転軸を離間して囲う
囲い体を設け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、該可動体の内側面に前記弾性部材の適宜
位置を固定すると共に、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たことを特
徴とする気体軸受。 (2) 前記ホルダーと外側のケーシングとを多点接
触構造として該ホルダーとケーシングとの間に
非接触部を設けたことを特徴とする実用新案登
録請求の範囲第1項記載の気体軸受。
[Claims for Utility Model Registration] (1) In a gas bearing in which a holder having a cylindrical cavity is provided with an enclosure that surrounds the rotating shaft at a distance via an elastic member on the inner surface of the cavity, the inner surface of the cavity A movable body is disposed in a part between the movable body and the elastic member, and the elastic member is fixed at an appropriate position on the inner surface of the movable body, and between the outer surface of the movable body and the inner surface of the cavity. A gas bearing characterized in that a compensating elastic member having a smaller elastic constant than the elastic member is disposed at the elastic member. (2) The gas bearing according to claim 1, wherein the holder and the outer casing have a multi-point contact structure, and a non-contact portion is provided between the holder and the casing.
JP10352984U 1984-07-09 1984-07-09 gas bearing Granted JPS6119126U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10352984U JPS6119126U (en) 1984-07-09 1984-07-09 gas bearing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10352984U JPS6119126U (en) 1984-07-09 1984-07-09 gas bearing

Publications (2)

Publication Number Publication Date
JPS6119126U JPS6119126U (en) 1986-02-04
JPH0210817Y2 true JPH0210817Y2 (en) 1990-03-16

Family

ID=33429009

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10352984U Granted JPS6119126U (en) 1984-07-09 1984-07-09 gas bearing

Country Status (1)

Country Link
JP (1) JPS6119126U (en)

Also Published As

Publication number Publication date
JPS6119126U (en) 1986-02-04

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