JP2011144846A - Dynamic pressure gas bearing - Google Patents

Dynamic pressure gas bearing Download PDF

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JP2011144846A
JP2011144846A JP2010004575A JP2010004575A JP2011144846A JP 2011144846 A JP2011144846 A JP 2011144846A JP 2010004575 A JP2010004575 A JP 2010004575A JP 2010004575 A JP2010004575 A JP 2010004575A JP 2011144846 A JP2011144846 A JP 2011144846A
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foil
bearing housing
bearing
shaft
underfoil
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JP5333246B2 (en
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Koji Horikawa
浩司 堀川
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Shimadzu Corp
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Shimadzu Corp
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    • 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
    • F16C17/02—Sliding-contact bearings for exclusively rotary movement for radial load only
    • F16C17/024—Sliding-contact bearings for exclusively rotary movement for radial load only with flexible leaves to create hydrodynamic wedge, e.g. radial 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
    • F16C2360/00—Engines or pumps
    • 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
    • F16C43/00—Assembling bearings
    • F16C43/02—Assembling sliding-contact bearings

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Support Of The Bearing (AREA)

Abstract

<P>PROBLEM TO BE SOLVED: To further surely obtain a damping effect, when the amplitude of foils is increased by sliding the plurality of foils in reverse directions in a dynamic pressure gas bearing provided on an inner wall of a cylindrical bearing housing and including a plurality of foils. <P>SOLUTION: In the dynamic pressure gas bearing which is provided on the inner wall 1a of the bearing housing 1 and includes a plurality of foils 3, projections 33 for positioning each foil 3 to the bearing housing 1 are provided at axial end portions in the circumferential middle of the foil 3. <P>COPYRIGHT: (C)2011,JPO&INPIT

Description

本発明は、航空機のエアサイクルマシン、ヘリウム液化装置の膨張タービン、自動車のターボチャージャ等の高速回転機械に使用される軸受に関し、特に、軸を取り付ける対象である固定部材と軸に設けた回転受圧部との間に形成された気体膜により荷重を支持する動圧気体軸受に関する。   The present invention relates to bearings used in high-speed rotating machines such as aircraft air cycle machines, helium liquefaction equipment expansion turbines, automobile turbochargers, etc., and in particular, a fixed member to which a shaft is attached and a rotational pressure provided on the shaft. The present invention relates to a dynamic pressure gas bearing that supports a load by a gas film formed between the first and second portions.

高速回転機械用に使用される軸受として、軸を取り付ける対象である固定部材と軸に設けた回転受圧部との間に形成した空間により両部材間に薄い気体膜を生じさせ、この気体膜の潤滑作用により荷重を支持する動圧気体軸受が従来知られている。   As a bearing used for a high-speed rotating machine, a thin gas film is formed between both members by a space formed between a fixed member to which the shaft is attached and a rotary pressure receiving portion provided on the shaft. Conventionally known is a dynamic pressure gas bearing that supports a load by a lubricating action.

このような従来の動圧気体軸受の一例として、複数枚のフォイルを固定部材にそれぞれ係止するとともに、互いに隣接するフォイルを重ね合わせ、軸に近い側のフォイルをたわませて固定部材に近い側のフォイルに支持させる構成のものが知られている（特許文献１参照）。   As an example of such a conventional dynamic pressure gas bearing, a plurality of foils are respectively locked to a fixing member, and the foils adjacent to each other are overlapped, and the foil on the side close to the shaft is bent to be close to the fixing member. The thing of the structure supported by the foil of the side is known (refer patent document 1).

特開平４−５４３０９号公報JP-A-4-54309

しかして、前記特許文献１のもののような構成では、複数枚のフォイルそれぞれの下流側端部を順次固定部材に取り付けるようにしているので、フォイルに過大な押さえつけ力が作用した際には、気体膜からの圧力を受けた際にアッパーフォイルとアンダーフォイルとが同じ方向に延伸しようとする。すると、アッパーフォイルとアンダーフォイルとが互いに摺動する際の相対移動の量が小さくダンピング効果を得にくいので、フォイルに過大な押さえつけ力が作用した際に振動や騒音が発生しやすくなるという不具合が存在する。   In the configuration such as that of Patent Document 1, the downstream end of each of the plurality of foils is sequentially attached to the fixing member. Therefore, when an excessive pressing force acts on the foil, When subjected to pressure from the membrane, the upper foil and the underfoil tend to stretch in the same direction. Then, since the amount of relative movement when the upper foil and the underfoil slide against each other is small, it is difficult to obtain a damping effect. Exists.

本発明は、以上を踏まえ、アッパーフォイルとアンダーフォイルとを互いに大きく摺動させてより効果的にダンピング効果が得られるようにすることにより、振動や騒音の発生を抑制することを目的とする。   In view of the above, an object of the present invention is to suppress the generation of vibration and noise by sliding the upper foil and the underfoil greatly relative to each other so as to obtain a damping effect more effectively.

すなわち本発明に係る動圧気体軸受は、軸受ハウジングの内壁に設けられ、複数のフォイルを具備するものであって、フォイルの周方向中間部の軸方向端部に、該フォイルを軸受ハウジングに対して位置決めするための突起を設けているとともに、この突起を、前記フォイルを形成する部材の軸方向端部を屈曲させることにより形成していることを特徴とする。   That is, the dynamic pressure gas bearing according to the present invention is provided on the inner wall of the bearing housing, and includes a plurality of foils, and the foil is attached to the bearing housing at the axial end of the circumferential middle portion of the foil. And a protrusion for positioning, and the protrusion is formed by bending the axial end of the member forming the foil.

このような構成によれば、フォイルの上流側を軸受ハウジングの内壁に対向するアンダーフォイル、下流側をこのアンダーフォイルと軸との間に位置するアッパーフォイルとすることで、フォイルに過大な押さえつけ力が作用した際にアンダーフォイルとアッパーフォイルとが逆方向に移動し、これらの間の相対的な摺動量を大きくしてより確実にダンピング効果を得られる構成の動圧気体軸受を、より少ない手間で実現することができる。   According to such a configuration, an excessive pressing force is applied to the foil by making the upstream side of the foil an underfoil facing the inner wall of the bearing housing and the downstream side an upper foil positioned between the underfoil and the shaft. The hydrofoil gas bearing is configured to move the underfoil and upper foil in the opposite directions when they act and increase the relative sliding amount between them to obtain a more reliable damping effect. Can be realized.

また、前記突起が軸受ハウジングに接触するとともに、前記フォイルが軸受ハウジングに向けて押し付けられた際に前記突起が弾性変形するものであれば、アッパーフォイルがさらに軸受ハウジングに近接し、アンダーフォイルとアッパーフォイルとがさらに大きく相対移動するので、アンダーフォイルとアッパーフォイルとの間の摩擦を利用したダンピング効果をより大きく得ることができる。   If the protrusion contacts the bearing housing and the protrusion is elastically deformed when the foil is pressed against the bearing housing, the upper foil further approaches the bearing housing, and the underfoil and the upper Since the foil relatively moves relative to the foil, the damping effect using the friction between the under foil and the upper foil can be further increased.

本発明に係る動圧気体軸受の構造によれば、フォイルの上流側を軸受ハウジングの内壁に対向するアンダーフォイル、下流側をこのアンダーフォイルと軸との間に位置するアッパーフォイルとすることで、フォイルに過大な押さえつけ力が作用した際にアンダーフォイルとアッパーフォイルとが逆方向に移動するので、これらの間の相対的な摺動量を大きくしてより確実にダンピング効果を得ることができる。従って、より効果的に振動や騒音の発生を抑制することができる。   According to the structure of the dynamic pressure gas bearing according to the present invention, the upstream side of the foil is an underfoil facing the inner wall of the bearing housing, and the downstream side is an upper foil positioned between the underfoil and the shaft. When an excessive pressing force is applied to the foil, the underfoil and the upper foil move in the opposite directions, so that the relative sliding amount between them can be increased to obtain a damping effect more reliably. Therefore, generation of vibration and noise can be suppressed more effectively.

本発明の第一実施形態に係る動圧気体軸受を示す正面図。The front view which shows the dynamic pressure gas bearing which concerns on 1st embodiment of this invention. 同実施形態に係るフォイルを示す斜視図。The perspective view which shows the foil which concerns on the same embodiment. 同実施形態に係るフォイルを示す側面図。The side view which shows the foil which concerns on the same embodiment. 本発明の第二実施形態に係る動圧気体軸受を示す正面図。The front view which shows the dynamic pressure gas bearing which concerns on 2nd embodiment of this invention.

以下、本発明の第一実施形態を、図面を参照して説明する。   Hereinafter, a first embodiment of the present invention will be described with reference to the drawings.

本実施形態に係る軸受は、図１に概略正面図、図２に要部の中央横断面図をそれぞれ示すようなジャーナル軸受であり、軸２を取り付ける対象である軸受ハウジング１と軸２との間に設けられる。すなわち、前記軸受ハウジング１の内壁１ａに設けられる。また、この軸受は、複数のフォイル３を具備するものであって、これら複数のフォイル３を軸２と前記軸受ハウジング１との間に配した際に、一のフォイル３と、他のフォイル３とが重なり合い、各フォイル３の一部が軸２に対向するアッパーフォイル３１として機能するとともに、各フォイル３の他の一部が前記アッパーフォイル３１と前記内壁１ａとの間に位置し、内壁１ａに対向するアンダーフォイル３２として機能する。そして、前記フォイル３と前記軸２との間に図示しない気体膜を形成し、この気体膜の気圧を利用して軸２を支持する。すなわち、本実施形態に係る軸受は、フォイル型のジャーナル気体軸受である。なお、前記図１及び図２では、フォイル３は形状の理解を容易にするため、一定の厚さで示されているが、実際には、例えば０．１〜０．２ｍｍの板状であり、かつ軸２を巻回する環状に形成されている。   The bearing according to the present embodiment is a journal bearing having a schematic front view in FIG. 1 and a central cross-sectional view of the main part in FIG. 2, and includes a bearing housing 1 and a shaft 2 to which the shaft 2 is attached. Between. That is, it is provided on the inner wall 1 a of the bearing housing 1. The bearing includes a plurality of foils 3. When the plurality of foils 3 are arranged between the shaft 2 and the bearing housing 1, one foil 3 and another foil 3 are provided. And a part of each foil 3 functions as an upper foil 31 opposed to the shaft 2, and the other part of each foil 3 is located between the upper foil 31 and the inner wall 1a, and the inner wall 1a It functions as an underfoil 32 opposite to. A gas film (not shown) is formed between the foil 3 and the shaft 2, and the shaft 2 is supported using the pressure of the gas film. That is, the bearing according to the present embodiment is a foil-type journal gas bearing. In FIG. 1 and FIG. 2, the foil 3 is shown to have a constant thickness in order to facilitate understanding of the shape. And is formed in an annular shape around which the shaft 2 is wound.

さらに詳述すると、前記フォイル３は、本実施形態ではいずれも板状をなし、前記内壁１ａに沿って配置される。また、このフォイル３の周方向中間部の軸方向端部には、該フォイル３を軸受ハウジング１に対して位置決めするための突起３３を設けているとともに、この突起３３を、前記フォイル３を形成する部材の軸方向端部を屈曲させることにより形成している。さらに詳述すると、この突起３３は、図２に示すように、フォイル３の周方向中間部の軸方向両端部からそれぞれ軸方向に突出する接続部３３ａと、この接続部３３ａの端部を軸２から離間する方向に折り返して形成してなるとともに前記軸受ハウジング１に設けた凹部１ｘに挿入させてなる突出部３３ｂとを有する。そして、本実施形態では、各フォイル３の下流側ほぼ半分を、周方向に隣接するフォイル３の上流側ほぼ半分の軸２側に重ね合わせた状態で、前記突起３３の突出部３３ｂを軸受ハウジング１に設けた凹部１ｘに挿入することによりフォイル３を軸受ハウジング１に取り付けるようにしている。すなわち、前記図１及び図４に示すように、各フォイル３の下流側ほぼ半分が、軸２に対向するアッパーフォイル３１として機能するとともに、各フォイル３の上流側ほぼ半分が、前記内壁１ａと他方のフォイル３の前記アッパーフォイル３１として機能する部分との間に位置するアンダーフォイル３２として機能するようにしている。   More specifically, in the present embodiment, the foil 3 has a plate shape and is disposed along the inner wall 1a. Further, a projection 33 for positioning the foil 3 with respect to the bearing housing 1 is provided at an axial end portion of the intermediate portion in the circumferential direction of the foil 3, and the projection 33 is formed with the projection 33. It is formed by bending the axial end portion of the member to be operated. More specifically, as shown in FIG. 2, the protrusion 33 includes a connection portion 33 a that protrudes in the axial direction from both axial end portions of the intermediate portion in the circumferential direction of the foil 3, and an end portion of the connection portion 33 a as a shaft. 2 and a protrusion 33b that is formed by being folded back in a direction away from 2 and inserted into a recess 1x provided in the bearing housing 1. In the present embodiment, the protrusion 33b of the protrusion 33 is placed in the bearing housing in a state in which approximately half of the downstream side of each foil 3 is superimposed on the shaft 2 side of the upstream half of the foil 3 adjacent in the circumferential direction. The foil 3 is attached to the bearing housing 1 by being inserted into a recess 1x provided in the bearing 1. That is, as shown in FIGS. 1 and 4, almost half of the downstream side of each foil 3 functions as the upper foil 31 facing the shaft 2, and almost half of the upstream side of each foil 3 is connected to the inner wall 1a. It functions as an underfoil 32 positioned between the other foil 3 and the portion functioning as the upper foil 31.

ここで、軸２が回転すると、軸２とフォイル３との隙間の空気等の気体が気体の粘性により引張られ、この隙間に形成してなる気体膜Ｓの圧力が上昇する。この圧力上昇によって、まず、各フォイル３のアッパーフォイル３１として機能する部分が軸受ハウジング１側に向かう作用を受ける。この際、前記アッパーフォイル３１として機能する部分は、隣接するフォイル３のアンダーフォイル３２として機能する部分に圧接し、前記アンダーフォイル３２として機能する部分が軸受ハウジング１側に向かう作用を受ける。そして、気体膜Ｓの形状が、例えば、入口部分から下流側に進むにつれ幅が小さくなるなど、適切な形状に維持され、前記アッパーフォイル３１の下流側端縁近傍すなわち自由端近傍で気体の圧力上昇が生じる。この圧力上昇により軸受は軸２を非接触で支えることになる。   Here, when the shaft 2 rotates, a gas such as air in the gap between the shaft 2 and the foil 3 is pulled by the viscosity of the gas, and the pressure of the gas film S formed in the gap increases. Due to this pressure increase, first, the portion functioning as the upper foil 31 of each foil 3 receives an action toward the bearing housing 1 side. At this time, the portion functioning as the upper foil 31 is pressed against the portion functioning as the underfoil 32 of the adjacent foil 3, and the portion functioning as the underfoil 32 is subjected to the action toward the bearing housing 1. The shape of the gas film S is maintained in an appropriate shape, for example, the width is reduced as it proceeds from the inlet portion to the downstream side, and the pressure of the gas near the downstream edge of the upper foil 31, that is, near the free end. An increase occurs. This pressure rise causes the bearing to support the shaft 2 in a non-contact manner.

ここで、フォイル３に気体膜Ｓによる押さえつけ力が作用した際には、アンダーフォイル３２は上流側に向かい移動する。一方、アッパーフォイル３１は下流側に向かい移動する。すなわち、フォイル３に過大な押さえつけ力が作用した際には、これらアッパーフォイル３１及びアンダーフォイル３２は互いに逆方向に摺動し、この摺動の際に振動エネルギーを熱エネルギー等に変換して振動を抑制する効果であるダンピング効果が得られる。   Here, when the pressing force by the gas film S acts on the foil 3, the underfoil 32 moves toward the upstream side. On the other hand, the upper foil 31 moves toward the downstream side. That is, when an excessive pressing force is applied to the foil 3, the upper foil 31 and the underfoil 32 slide in opposite directions, and vibration energy is converted into heat energy or the like during the sliding. The damping effect which is the effect which suppresses is acquired.

以上に述べたように、本実施形態に係る軸受の構成によれば、フォイル３の上流側を軸受ハウジング１の内壁１ａに対向するアンダーフォイル３２、下流側をこのアンダーフォイル３２と軸２との間に位置するアッパーフォイル３１とすることで、フォイル３に過大な押さえつけ力が作用した際にアンダーフォイル３２とアッパーフォイル３１とが逆方向に移動し、これらの間の相対的な摺動量を大きくしてより確実にダンピング効果を得られる構成の動圧気体軸受を、より少ない手間で実現することができる。   As described above, according to the configuration of the bearing according to the present embodiment, the upstream side of the foil 3 is the underfoil 32 facing the inner wall 1a of the bearing housing 1, and the downstream side is the underfoil 32 and the shaft 2. By using the upper foil 31 positioned between them, when an excessive pressing force acts on the foil 3, the under foil 32 and the upper foil 31 move in the opposite directions, and the relative sliding amount between them is increased. Thus, it is possible to realize a dynamic pressure gas bearing having a configuration that can obtain a damping effect more reliably with less effort.

次いで、本発明の第二実施形態を、図４を参照して説明する。なお、上述した第一実施形態におけるものと共通の部位には、共通の名称及び符号を付している。以下、上述した第一実施形態との相違点についてのみ述べる。   Next, a second embodiment of the present invention will be described with reference to FIG. In addition, the common name and code | symbol are attached | subjected to the site | part common in the thing in 1st embodiment mentioned above. Only differences from the first embodiment described above will be described below.

本実施形態においては、図４に示すように、突起３３の突出部３３ｂの突出端を折り返して折り返し部３３ｘを設けるとともに、突出端すなわち折り返し部３３ｘを前記軸受ハウジング１の凹部１ｘに当接させ、フォイル３が軸受ハウジング１に向けて押し付けられた際にこの折り返し部３３ｘが弾性変形するようにしている。   In the present embodiment, as shown in FIG. 4, the protruding end of the protruding portion 33 b of the protrusion 33 is folded to provide a folded portion 33 x, and the protruding end, that is, the folded portion 33 x is brought into contact with the concave portion 1 x of the bearing housing 1. The folded portion 33x is elastically deformed when the foil 3 is pressed toward the bearing housing 1.

このように構成することにより、上述した第一実施形態に係る構成の効果に加えて、以下のような作用効果が得られる。すなわち、フォイル３が軸受ハウジング１に大きな力で押し付けられ前記突起３３の折り返し部３３ｘが弾性変形した際に、アッパーフォイル３１がさらに軸受ハウジング１に近接し、アンダーフォイル３２とアッパーフォイル３１とがさらに大きく相対移動するので、アンダーフォイル３２とアッパーフォイル３１との間の摩擦を利用したダンピング効果をより大きく得ることができるという効果が得られる。   By comprising in this way, in addition to the effect of the structure which concerns on 1st embodiment mentioned above, the following effects are obtained. That is, when the foil 3 is pressed against the bearing housing 1 with a large force and the folded portion 33x of the projection 33 is elastically deformed, the upper foil 31 further approaches the bearing housing 1, and the underfoil 32 and the upper foil 31 further Since the relative movement is large, an effect that a damping effect using friction between the underfoil 32 and the upper foil 31 can be obtained can be obtained.

なお、本発明は以上に述べた実施形態に限らない。   The present invention is not limited to the embodiment described above.

例えば、軸受ハウジングの内壁に対向するアンダーフォイルとなるべき部位に、軸方向に延伸する突条を設ける等の手段により、アッパーフォイルとなるべき部位を軸に向かう方向に付勢するバネとしての機能を付与させてもよい。   For example, a function as a spring that urges the portion to be the upper foil in the direction toward the shaft by means such as providing a protrusion extending in the axial direction at the portion to be the underfoil facing the inner wall of the bearing housing. May be given.

また、ジャーナル軸受だけでなく、スラスト軸受に本発明を適用してもよい。   Moreover, you may apply this invention not only to a journal bearing but to a thrust bearing.

その他、本発明の趣旨を損ねない範囲で種々に変更してよい。   In addition, various changes may be made without departing from the spirit of the present invention.

１…軸受ハウジング
２…軸
３…フォイル
３３…突起 DESCRIPTION OF SYMBOLS 1 ... Bearing housing 2 ... Shaft 3 ... Foil 33 ... Protrusion

Claims (2)

軸受ハウジングと、この軸受ハウジングと軸との間に設けてなる複数のフォイルとを具備するものであって、フォイルの周方向中間部の軸方向端部に、該フォイルを軸受ハウジングに対して位置決めするための突起を設けているとともに、この突起を、前記フォイルを形成する部材の軸方向端部を屈曲させることにより形成していることを特徴とする動圧気体軸受。 A bearing housing and a plurality of foils provided between the bearing housing and the shaft, wherein the foil is positioned with respect to the bearing housing at an axial end of a circumferential intermediate portion of the foil. A hydrodynamic gas bearing characterized in that a protrusion for forming the protrusion is formed, and the protrusion is formed by bending an axial end portion of the member forming the foil. 前記突起が軸受ハウジングに接触するとともに、前記フォイルが軸受ハウジングに向けて押し付けられた際に前記突起が弾性変形する請求項１記載の動圧気体軸受。 The hydrodynamic gas bearing according to claim 1, wherein the protrusion contacts the bearing housing, and the protrusion is elastically deformed when the foil is pressed toward the bearing housing.
JP2010004575A 2010-01-13 2010-01-13 Dynamic pressure gas bearing Expired - Fee Related JP5333246B2 (en)

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WO2013069682A1 (en) * 2011-11-09 2013-05-16 株式会社Ihi Radial foil bearing
JP2014020463A (en) * 2012-07-18 2014-02-03 Ihi Corp Radial foil bearing
EP2740950A1 (en) * 2011-08-01 2014-06-11 IHI Corporation Radial foil bearing
JP2014122708A (en) * 2014-03-25 2014-07-03 Ntn Corp Foil bearing
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RU2658260C2 (en) * 2015-02-04 2018-06-19 Сергей Иванович Сигачев Radial flap gas dynamic bearing
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CN113710908A (en) * 2019-04-04 2021-11-26 株式会社Ihi Radial foil bearing
WO2022107534A1 (en) * 2020-11-17 2022-05-27 株式会社Ihi Thrust air bearing

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EP2740950A1 (en) * 2011-08-01 2014-06-11 IHI Corporation Radial foil bearing
WO2013054613A1 (en) * 2011-10-13 2013-04-18 株式会社Ihi Radial foil bearing
JP2013087789A (en) * 2011-10-13 2013-05-13 Ihi Corp Radial foil bearing
KR101564355B1 (en) * 2011-10-13 2015-10-29 가부시키가이샤 아이에이치아이 Radial foil bearing
US8944688B2 (en) 2011-10-13 2015-02-03 Ihi Corporation Radial foil bearing
JP2013100885A (en) * 2011-11-09 2013-05-23 Ihi Corp Radial foil bearing
KR101559860B1 (en) * 2011-11-09 2015-10-13 가부시키가이샤 아이에이치아이 Radial foil bearing
WO2013069682A1 (en) * 2011-11-09 2013-05-16 株式会社Ihi Radial foil bearing
US9206840B2 (en) 2011-11-09 2015-12-08 Ihi Corporation Radial foil bearing
JP2014020463A (en) * 2012-07-18 2014-02-03 Ihi Corp Radial foil bearing
US9568042B2 (en) 2012-07-18 2017-02-14 Ihi Corporation Radial foil bearing
US9551375B2 (en) 2012-08-14 2017-01-24 Ihi Corporation Radial foil bearing
US9784307B2 (en) 2012-12-19 2017-10-10 Ntn Corporation Foil bearing
US9631556B2 (en) 2012-12-19 2017-04-25 Ntn Corporation Foil bearing
JP2014122708A (en) * 2014-03-25 2014-07-03 Ntn Corp Foil bearing
RU2658260C2 (en) * 2015-02-04 2018-06-19 Сергей Иванович Сигачев Radial flap gas dynamic bearing
WO2017169676A1 (en) * 2016-03-30 2017-10-05 Ntn株式会社 Foil bearing
WO2019017134A1 (en) * 2017-07-19 2019-01-24 Ntn株式会社 Foil bearing
WO2019172370A1 (en) * 2018-03-07 2019-09-12 株式会社Ihi Radial foil bearing
JP2019157899A (en) * 2018-03-07 2019-09-19 株式会社Ihi Radial foil bearing
US11319987B2 (en) 2018-03-07 2022-05-03 Ihi Corporation Radial foil bearing
CN113710908A (en) * 2019-04-04 2021-11-26 株式会社Ihi Radial foil bearing
EP3951198A4 (en) * 2019-04-04 2022-12-07 IHI Corporation Radial foil bearing
US11940005B2 (en) 2019-04-04 2024-03-26 Ihi Corporation Radial foil bearing
WO2022107534A1 (en) * 2020-11-17 2022-05-27 株式会社Ihi Thrust air bearing

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