JPH01242816A - Dynamic pressure thrust fluid bearing - Google Patents
Dynamic pressure thrust fluid bearingInfo
- Publication number
- JPH01242816A JPH01242816A JP63065912A JP6591288A JPH01242816A JP H01242816 A JPH01242816 A JP H01242816A JP 63065912 A JP63065912 A JP 63065912A JP 6591288 A JP6591288 A JP 6591288A JP H01242816 A JPH01242816 A JP H01242816A
- Authority
- JP
- Japan
- Prior art keywords
- foil
- bearing
- pad
- fluid
- spring
- 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.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/04—Sliding-contact bearings for exclusively rotary movement for axial load only
- F16C17/042—Sliding-contact bearings for exclusively rotary movement for axial load only with flexible leaves to create hydrodynamic wedge, e.g. axial foil bearings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C27/00—Elastic or yielding bearings or bearing supports, for exclusively rotary movement
- F16C27/02—Sliding-contact bearings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C37/00—Cooling of bearings
- F16C37/002—Cooling of bearings of fluid bearings
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- Sliding-Contact Bearings (AREA)
- Support Of The Bearing (AREA)
Abstract
Description
【発明の詳細な説明】
[産業上の利用分野]
本発明は軸受面を弾性のあるフォイルで構成した動圧ス
ラスト流体軸受に係り、特にパッドによりテーパを付け
たテーパランド型軸受に関する。DETAILED DESCRIPTION OF THE INVENTION [Industrial Field of Application] The present invention relates to a hydrodynamic thrust fluid bearing whose bearing surface is made of an elastic foil, and particularly to a tapered land type bearing tapered by pads.
[従来の技術]
フォイルパッドによりテーバを付けてテーパランド型軸
受を構成することは、例えば特開昭61−165011
号公報により公知である。[Prior Art] The construction of a tapered land type bearing by attaching a taper with a foil pad is disclosed in, for example, Japanese Patent Laid-Open No. 61-165011.
It is known from the publication no.
しかし、この公知の軸受では、パッドがパッドフォイル
本体に一点で連結されているので、パッドフォイルの下
に積層されるバックフォイルにパッドの連結側端を溶接
してパッドの補強を行う必要がある。このため、工作が
面倒であると共に溶接に際しての位置決め精度も厳しく
なるという欠点があった。However, in this known bearing, the pad is connected to the pad foil body at one point, so it is necessary to reinforce the pad by welding the connecting end of the pad to the back foil laminated under the pad foil. . For this reason, there have been disadvantages in that the machining is troublesome and the positioning accuracy during welding is also difficult.
またパッドフォイルの下に積層されるバックフォイルは
連続したリング状で、スリットも孔もないので、r!J
擦によりパッドに発生する熱を下側に有効に逃がすこと
ができない。Also, the back foil laminated under the pad foil is in the form of a continuous ring and has no slits or holes, so r! J
The heat generated in the pad due to rubbing cannot be effectively dissipated downward.
このため、高速回転するとパッドが発熱により熱変形し
て、軸受性能が劣化するという欠点もあった。Therefore, when the bearing rotates at high speed, the pad is thermally deformed due to heat generation, resulting in deterioration of bearing performance.
[発明が解決しようとする課題]
上記したように従来のスラスト軸受によると、パッドを
溶接するため工作が面倒であり、またパッドに発生する
*m熱を有効に逃がすことができないという欠点があっ
た。[Problems to be Solved by the Invention] As mentioned above, conventional thrust bearings have the drawbacks that the pads are welded, which is cumbersome to work with, and that the heat generated in the pads cannot be effectively dissipated. Ta.
本発明の目的は、上記従来技術の問題点を解消し、溶接
を不要とし、しかも熱変形を有効に防止できる動圧スラ
スト流体軸受を提供することにある。SUMMARY OF THE INVENTION An object of the present invention is to provide a hydrodynamic thrust fluid bearing that eliminates the problems of the prior art described above, eliminates the need for welding, and can effectively prevent thermal deformation.
[課題を解決するための手段]
本発明の動圧スラスト流体軸受は、ばね機能を有するば
ねフォイルと、軸受i能を有する軸受フォイルと、バッ
クアップ機能を有するシムフォイルとを上から順に積層
して構成される。[Means for Solving the Problems] The hydrodynamic thrust fluid bearing of the present invention is constructed by laminating in order from above a spring foil having a spring function, a bearing foil having a bearing function, and a shim foil having a backup function. be done.
ばねフォイルは回転軸のランナの回転方向に沿って表裏
に交互に配列される線状突起を有すると共に、線状突起
を中断するパッド挿通用の窓が適宜間隔を隔てて設けら
れる。The spring foil has linear protrusions arranged alternately on the front and back sides along the rotational direction of the runner of the rotating shaft, and windows for inserting pads that interrupt the linear protrusions are provided at appropriate intervals.
軸受フォイルは切り起し可能なパッド片を一体的に有し
、このパッド片をばねフォイルの窓から挿通してばねフ
ォイルの線状突起に支承され得るテーパランドとする。The bearing foil integrally has a pad piece that can be cut and bent, and this pad piece is inserted through a window of the spring foil to form a tapered land that can be supported by a linear projection of the spring foil.
シムフォイルはばねフォイルの線状突起を支承してテー
パランドを補強する枕状突起を有すると共に、パッド片
間の切起し間隙を介して窓に連通ずる流体供給孔が設け
られる。The shim foil has a pillow-like projection that supports the linear projection of the spring foil and reinforces the taper land, and is also provided with a fluid supply hole that communicates with the window through the cut-and-raised gap between the pad pieces.
[作 用]
パッド片をばねフォイルの窓から挿通すると、パッド片
は傾斜した格好でばねフォイルに乗り上げるので、構造
上ランナとの間にくさび状隙間が形成される。[Function] When the pad piece is inserted through the window of the spring foil, the pad piece rides on the spring foil in an inclined manner, so that a structural wedge-shaped gap is formed between the pad piece and the runner.
ランナが回転すると流体がその粘性でひきずられ、くさ
び状隙間に押し込められて圧力を生じる。As the runner rotates, the fluid is dragged by its viscosity and forced into the wedge-shaped gap, creating pressure.
傾斜しているパッド片はこの圧力により下層側へ押え付
けられて平らになろうとうするが、ばねフォイルの線状
突起及びシムフォイルの枕状突起に支承されるため、テ
ーパランドを維持する。The inclined pad piece is pressed toward the lower layer side by this pressure and tries to become flat, but it maintains its tapered land because it is supported by the linear projection of the spring foil and the pillow-like projection of the shim foil.
また、各パッド片は、パッド片間の切起し間隙を介して
窓に連通ずる流体供給孔により独立に分割されて、恰度
独立軸受の機能を発揮するから、ランナが偏荷重を受け
て傾いてもテーパランドの復原力があり角度剛性が大き
い。In addition, each pad piece is independently divided by the fluid supply hole that communicates with the window through the cut-and-raised gap between the pad pieces, so that it functions as an independent bearing, so the runner will not tilt due to unbalanced loads. However, the tapered land has a restoring force and high angular rigidity.
一方、ランナの回転が速くなればなる程流体摩擦による
発熱が大きくなるが、これと比例して、流体供給孔から
流入する流体も増加するため、この流体によってパッド
片が有効に冷却される。On the other hand, as the rotation speed of the runner increases, heat generation due to fluid friction increases, but the amount of fluid flowing in from the fluid supply hole also increases in proportion to this, so that the pad piece is effectively cooled by this fluid.
[実施例]
以下、本発明の実施例を第1図〜第4図を用いて説明す
る。[Example] Hereinafter, an example of the present invention will be described using FIGS. 1 to 4.
第2図は本発明の動圧スラスト流体軸受例の分解図を示
す。本軸受は図から分るように回転軸孔を中心に打ち抜
いた円盤状の3枚のフォイルから成り、上層から下層に
向かって順に、ばねフォイル10.軸受フォイル20.
シムフォイル30が積層される。FIG. 2 shows an exploded view of an example of the dynamic pressure thrust fluid bearing of the present invention. As can be seen from the figure, this bearing consists of three disc-shaped foils punched out around the rotating shaft hole, and the spring foils 10. Bearing foil 20.
Shim foil 30 is laminated.
ばねフォイル10は、その表裏に表と裏とて互い違いに
配列され、径方向に延びた多数の線状突起1を回転軸の
ランナ(図示せず)の回転方向(矢印ω)に沿って有し
ている。線状突起1はホトエツチングによりランド部分
を掘り下げて形成する。エツチング箇所を梨地で示しで
ある。また、ばねフォイル10には線状突起1を中断す
るような形で、適宜間隔を隔ててパッド片挿通用の窓2
が同じくホトエツチングにより複数個打ち扱かれている
。図示例では6個の窓2が設けられ、また窓2間には恰
度4本の線状突起1が設けられているが、これらの数は
図示例のものに限定されない。The spring foil 10 has a large number of linear protrusions 1 arranged alternately on the front and back sides and extending in the radial direction along the rotation direction (arrow ω) of a runner (not shown) of the rotation shaft. are doing. The linear protrusion 1 is formed by digging into the land portion by photoetching. The etched areas are shown in matte finish. Further, the spring foil 10 is provided with windows 2 for inserting pad pieces at appropriate intervals in a shape that interrupts the linear protrusion 1.
Similarly, multiple pieces are etched by photoetching. In the illustrated example, six windows 2 are provided, and four linear protrusions 1 are provided between the windows 2, but these numbers are not limited to the illustrated example.
線状突起1間のピッチは窓2間において回転方向に向か
って徐々に狭くなるようにして、剛性を高めである。The pitch between the linear protrusions 1 is gradually narrowed in the direction of rotation between the windows 2 to increase rigidity.
軸受フォイル20は上記窓2に対応して6枚のパッド片
11を有している。このパッド片11は扇形で、その長
さの凡そ2/3を切り起し可能とするように、略逆口字
形のスリット溝をパッド片11のまわりにエツチングで
切って形成される。The bearing foil 20 has six pad pieces 11 corresponding to the windows 2. This pad piece 11 is fan-shaped, and is formed by etching a substantially inverted opening-shaped slit groove around the pad piece 11 so that about two-thirds of its length can be cut and raised.
パッド片11のティリングエツジと隣接するパッド片1
1のリーディングエツジとの間の切起し間隙としてのス
リット溝12は、流体導入孔として使うために伯のスリ
ット溝よりやや幅広にとっである。フォイルを積層した
とき、シムフォイル30の枕状突起21を有効なものと
するために、パッド片11を除くフォイルのランド部分
をエツチングにより掘り下げである。Pad piece 1 adjacent to the tilling edge of pad piece 11
The slit groove 12, which serves as a cut-and-raised gap between the leading edge 1 and the leading edge 1, is made slightly wider than the slit groove 12 in order to be used as a fluid introduction hole. When the foils are laminated, in order to make the pillow-like protrusions 21 of the shim foil 30 effective, the land portion of the foil except for the pad piece 11 is dug out by etching.
シムフォイル30は、その表面に軸受フォイル20のパ
ッド片11をばねフォイル10の線状突起1を介して支
承するための6個の枕状突起21を有する。この枕状突
起21はばねフォイル10によってはパッド片11を支
承できないような荷重に対抗するために設けられる。枕
状突起21のパッド片11に対する位置は流体膜圧が最
大値を示すところに置かれる。既述したようにホトエツ
チングによりランド部分を掘り下げて枕状突起21を形
成する。またシムフォイル30には軸受外部から軸受内
部へ流体を積極的に供給するための流体供給孔22が設
けられる。流体供給孔22は径方向に延びた長孔であり
、その径方向外方端は円盤状シムフォイル30の外円よ
りも外側に突出させた取付片23の取付孔24にまで延
びている。また流体供給孔22の位置は、ばねフォイル
10の窓2の反回転方向側とパッド片11間のスリット
溝12とに一致連通させ、流体供給孔22より供給した
流体をスリット溝12を通って窓2内に導入できるよう
になっている。The shim foil 30 has six pillow-like protrusions 21 on its surface for supporting the pad pieces 11 of the bearing foil 20 via the linear protrusions 1 of the spring foil 10. This pillow-shaped protrusion 21 is provided to counteract loads that cannot be supported by the spring foil 10 on the pad piece 11. The position of the pillow-shaped protrusion 21 relative to the pad piece 11 is located where the fluid film pressure exhibits the maximum value. As described above, the land portion is dug down by photoetching to form the pillow-like protrusion 21. Further, the shim foil 30 is provided with a fluid supply hole 22 for actively supplying fluid from the outside of the bearing to the inside of the bearing. The fluid supply hole 22 is a long hole extending in the radial direction, and its radially outer end extends to the attachment hole 24 of the attachment piece 23 that projects outward from the outer circle of the disc-shaped shim foil 30. Further, the position of the fluid supply hole 22 is such that the counter-rotation direction side of the window 2 of the spring foil 10 and the slit groove 12 between the pad pieces 11 are aligned and communicated with each other, so that the fluid supplied from the fluid supply hole 22 is passed through the slit groove 12. It can be installed within Windows 2.
上述した各フォイル10,20.30の外周には取付孔
4.14.24を開けた取付片3.13゜23がそれぞ
れ突設されている。実施例では6個設けられているが、
各フォイル10.20.30間でこれらを一致させれば
、フォイル間の位置決めがなされる。Attachment pieces 3.13.degree. 23 with attachment holes 4, 14 and 24 are provided protruding from the outer periphery of each of the foils 10, 20.30 described above. In the example, six are provided, but
By matching these between each foil 10, 20, 30, positioning between the foils is achieved.
なお、取付孔のための取付片は図示例のような突片では
なく、フォイル外円をもう少し径方向外方へ大きくして
形成される円外縁部であってもよい。Note that the attachment piece for the attachment hole may not be a projecting piece as in the illustrated example, but may be a circular outer edge portion formed by enlarging the outer circle of the foil a little more radially outward.
第3図は組立図であり、2層目の軸受フォイル20のパ
ッド片11を、1層目のばねフォイル10の窓2から挿
通させ、最上層に乗っけるようにする。挿通は切り起し
可能なパッド片11全長の約273まで行う。ここまで
挿通すると、第1図に示すように、挿通バッド片11は
窓2のエツジに乗りトげて、ばねフォイル10の上方に
傾斜平面ないしはテーパランドを当初から構造的に形成
する。FIG. 3 is an assembled view in which the pad piece 11 of the second layer of bearing foil 20 is inserted through the window 2 of the first layer of spring foil 10 and placed on the top layer. The insertion is performed up to about 273 of the total length of the pad piece 11 which can be cut and raised. When inserted this far, the insertion pad piece 11 rides on the edge of the window 2, as shown in FIG. 1, and structurally forms an inclined plane or tapered land above the spring foil 10.
第4図に示すように、上記積層フォイルは軸受ケース4
0上に支承されるが、流体供給孔22位置に対応する軸
受ケース40面に、流体案内用のtM41を設けると、
パッド片11への流体供給がより円滑になされる。As shown in FIG. 4, the laminated foil is attached to the bearing case 4.
0, but if a fluid guide tM41 is provided on the surface of the bearing case 40 corresponding to the fluid supply hole 22 position,
Fluid can be supplied to the pad piece 11 more smoothly.
また荷重Wを受けたランナ50が矢印方向に移動すると
、パッド片11はばねフォイル20とシムフォイル30
とに支承されて図示するようなテーパランドAを形成し
て、枕状突起21位置でピークを持ら、流体供給孔22
ないし溝41位置で大気圧を呈するくさび状の流体膜圧
力が生じる。Further, when the runner 50 receiving the load W moves in the direction of the arrow, the pad piece 11 moves between the spring foil 20 and the shim foil 30.
A tapered land A as shown in the figure is formed by being supported by the fluid supply hole 22 and has a peak at the position of the pillow-like protrusion 21.
A wedge-shaped fluid film pressure exhibiting atmospheric pressure is generated at the groove 41 position.
このとぎ、溝41から導込され流体供給孔22より供給
された外部流体はパッド片11を積極的に冷知するクー
リング作用をする。At this time, the external fluid introduced from the groove 41 and supplied from the fluid supply hole 22 has a cooling effect that actively cools the pad piece 11.
[発明の効果] 本発明によれば次の効果がある。[Effect of the invention] According to the present invention, there are the following effects.
(1) ばねフォイルの窓から軸受フォイルのパッド
片を挿通するだけで、くさび状隙間が形成されるので、
溶接を必要とした従来のものに比較して、はるかに工作
が容易である。また、窓から挿通したパッド片はばねフ
ォイルの線状突起及びシムフォイルの枕状突起によって
支承されるので、回転速度が上昇してもテーパランドが
確保でき、優れた高速安定性を発揮する。(1) A wedge-shaped gap is created by simply inserting the pad piece of the bearing foil through the window of the spring foil.
It is much easier to work with than conventional ones that require welding. Furthermore, since the pad piece inserted through the window is supported by the linear protrusion of the spring foil and the pillow-like protrusion of the shim foil, a tapered land can be secured even when the rotational speed increases, and excellent high-speed stability is achieved.
(2) 各パッド片は、パッド片間の切起し間隙を介
して窓に連通ずる流体供給孔により独立に分割されるの
で、偏荷重がランチにかかっても容易に復原力が出るこ
とになり、角度剛性がきわめて大きい。また、流体供給
孔から積極的に流体が供給されるので、冷却作用が働き
熱変形にきわめて強い。(2) Each pad piece is divided independently by a fluid supply hole that communicates with the window through the cut-and-raised gap between the pad pieces, so even if an uneven load is applied to the launch, restoring force can be easily generated. Therefore, the angular rigidity is extremely large. Furthermore, since fluid is actively supplied from the fluid supply hole, a cooling effect is exerted and the device is extremely resistant to thermal deformation.
第1図は本発明による動圧スラスト流体軸受の一実施例
を示す周方向の要部展間断面図、第2図は第1図に示す
スラスト流体軸受の全体分解平面図、第3図は同じく組
立平面図、第4図は高速時のスラストフォイル状態図及
び流体膜圧力特性図である。
図中、1は線状突起、2は窓、10はばねフォイル、1
1はパッド片、12は切起し間隙としてのスリット溝、
20は軸受フォイル、21は枕状突起、22は流体供給
孔、30はシムフォイル、50はランナ、Aはテーパラ
ンドである。
特 許 出 願 人 石川島播磨重工業株式会社代理
人弁理士 絹 谷 信 雄
第3図
第4図FIG. 1 is a circumferential cross-sectional view showing an embodiment of a hydrodynamic thrust fluid bearing according to the present invention, FIG. 2 is an exploded plan view of the entire thrust fluid bearing shown in FIG. 1, and FIG. FIG. 4, which is also an assembly plan view, is a thrust foil state diagram and a fluid film pressure characteristic diagram at high speed. In the figure, 1 is a linear projection, 2 is a window, 10 is a spring foil, 1
1 is a pad piece, 12 is a slit groove as a cut and raised gap,
20 is a bearing foil, 21 is a pillow-shaped projection, 22 is a fluid supply hole, 30 is a shim foil, 50 is a runner, and A is a tapered land. Patent Applicant: Ishikawajima Harima Heavy Industries Co., Ltd. Representative Patent Attorney Nobuo Kinuya Figure 3 Figure 4
Claims (1)
列される線状突起を有するばねフォイルを備え、該ばね
フォイルは線状突起を中断する窓を適宜間隔を隔てて設
けられるようにし、切り起し可能なパッド片を一体的に
有する軸受フォイルをばねフォイルの下層に備え、パッ
ド片はばねフォイルの窓から挿通してばねフォイルの線
状突起に支承され得るテーパランドを形成するようにし
、ばねフォイルの線状突起を支承してテーパランドを補
強する枕状突起を有するシムフオイルを軸受フォイルの
下層に備え、シムフォイルはパッド片間の切起し間隙を
介して窓に連通する流体供給孔が設けられるようにした
動圧スラスト流体軸受。1. A spring foil having linear protrusions arranged alternately on the front and back sides along the rotation direction of the runner of the rotating shaft, and the spring foil is provided with windows interrupting the linear protrusions at appropriate intervals. A bearing foil integrally having a pad piece that can be cut and raised is provided below the spring foil, and the pad piece is inserted through a window of the spring foil to form a tapered land that can be supported by a linear protrusion of the spring foil. The lower layer of the bearing foil is equipped with a shim foil having a pillow-like projection that supports the linear projection of the spring foil and reinforces the taper land, and the shim foil has a fluid supply that communicates with the window through the cut and raised gap between the pad pieces. A hydrodynamic thrust fluid bearing with holes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP63065912A JPH0742980B2 (en) | 1988-03-22 | 1988-03-22 | Hydrodynamic thrust fluid bearing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP63065912A JPH0742980B2 (en) | 1988-03-22 | 1988-03-22 | Hydrodynamic thrust fluid bearing |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH01242816A true JPH01242816A (en) | 1989-09-27 |
| JPH0742980B2 JPH0742980B2 (en) | 1995-05-15 |
Family
ID=13300655
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP63065912A Expired - Lifetime JPH0742980B2 (en) | 1988-03-22 | 1988-03-22 | Hydrodynamic thrust fluid bearing |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0742980B2 (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR100585587B1 (en) * | 1999-02-22 | 2006-06-07 | 삼성테크윈 주식회사 | Air Foil Bearing |
| US20150275967A1 (en) * | 2012-10-17 | 2015-10-01 | Borgwarner Inc. | Oil-free turbocharger bearing assembly having conical shaft supported on compliant gas bearings |
| WO2016153201A1 (en) * | 2015-03-20 | 2016-09-29 | 주식회사 티앤이코리아 | Thrust foil air bearing |
| EP3036409A4 (en) * | 2013-08-20 | 2017-04-19 | Borgwarner Inc. | Air bearing arrangement |
| EP3385553A4 (en) * | 2015-12-01 | 2019-09-11 | NTN Corporation | Foil bearing |
| CN110360144A (en) * | 2019-08-30 | 2019-10-22 | 势加透博洁净动力如皋有限公司 | A two-stage air suspension centrifugal air compressor bearing assembly |
| CN116194681A (en) * | 2020-09-24 | 2023-05-30 | 株式会社Ihi | Thrust Foil Bearings |
-
1988
- 1988-03-22 JP JP63065912A patent/JPH0742980B2/en not_active Expired - Lifetime
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR100585587B1 (en) * | 1999-02-22 | 2006-06-07 | 삼성테크윈 주식회사 | Air Foil Bearing |
| US20150275967A1 (en) * | 2012-10-17 | 2015-10-01 | Borgwarner Inc. | Oil-free turbocharger bearing assembly having conical shaft supported on compliant gas bearings |
| US9394941B2 (en) * | 2012-10-17 | 2016-07-19 | Borgwarner Inc. | Oil-free turbocharger bearing assembly having conical shaft supported on compliant gas bearings |
| EP3036409A4 (en) * | 2013-08-20 | 2017-04-19 | Borgwarner Inc. | Air bearing arrangement |
| JP2018506687A (en) * | 2015-03-20 | 2018-03-08 | 株式会社ティーエヌイーコリアTne Korea Co., Ltd | Thrust foil air bearing |
| US9726220B2 (en) | 2015-03-20 | 2017-08-08 | Tne Korea Co., Ltd. | Thrust foil air bearing |
| WO2016153201A1 (en) * | 2015-03-20 | 2016-09-29 | 주식회사 티앤이코리아 | Thrust foil air bearing |
| EP3385553A4 (en) * | 2015-12-01 | 2019-09-11 | NTN Corporation | Foil bearing |
| US10487870B2 (en) | 2015-12-01 | 2019-11-26 | Ntn Corporation | Foil bearing |
| CN110360144A (en) * | 2019-08-30 | 2019-10-22 | 势加透博洁净动力如皋有限公司 | A two-stage air suspension centrifugal air compressor bearing assembly |
| CN116194681A (en) * | 2020-09-24 | 2023-05-30 | 株式会社Ihi | Thrust Foil Bearings |
| EP4219965A4 (en) * | 2020-09-24 | 2024-11-13 | IHI Corporation | PRINTING FILM WAREHOUSE |
| US12345293B2 (en) | 2020-09-24 | 2025-07-01 | Ihi Corporation | Thrust foil bearing |
| CN116194681B (en) * | 2020-09-24 | 2026-03-20 | 株式会社Ihi | Thrust foil bearing |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0742980B2 (en) | 1995-05-15 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| USRE39190E1 (en) | Compliant foil fluid film radial bearing | |
| EP1001180B1 (en) | Compliant fluid foil member for hydrodynamic fluid film thrust bearing | |
| JP4249822B2 (en) | Disk support method and compliant foil fluid film thrust bearing | |
| US5911510A (en) | Bi-directional foil bearings | |
| KR100604132B1 (en) | Foil air bearing | |
| JP2851097B2 (en) | Rotating anode X-ray tube | |
| JPS6319733B2 (en) | ||
| US5871284A (en) | Foil thrust bearing set | |
| US6224263B1 (en) | Foil thrust bearing with varying circumferential and radial stiffness | |
| US3375046A (en) | Foil thrust bearing arrangements | |
| JPH01242816A (en) | Dynamic pressure thrust fluid bearing | |
| JPH05322050A (en) | Noncontact mechanical seal | |
| JP4031614B2 (en) | Foil gas bearing | |
| WO2020130124A1 (en) | Thrust foil bearing | |
| JPH0193614A (en) | Underwater thrust bearing device | |
| JP3514958B2 (en) | Fluid bearing device | |
| JP2005155802A (en) | Thrust dynamic bearing | |
| US4171928A (en) | Foil bearing turbomachine | |
| JP3465288B2 (en) | Fluid bearing device | |
| JP2003269449A (en) | Foil bearing | |
| JPH0742981B2 (en) | Hydrodynamic journal fluid bearing | |
| JP2020115021A (en) | Thrust foil bearing device | |
| US12345293B2 (en) | Thrust foil bearing | |
| JPS626335Y2 (en) | ||
| CA3193679C (en) | Thrust foil bearing |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EXPY | Cancellation because of completion of term |