JPH0763193A - Impeller installation structure for centrifugal type low temperature compressor - Google Patents
Impeller installation structure for centrifugal type low temperature compressorInfo
- Publication number
- JPH0763193A JPH0763193A JP5229545A JP22954593A JPH0763193A JP H0763193 A JPH0763193 A JP H0763193A JP 5229545 A JP5229545 A JP 5229545A JP 22954593 A JP22954593 A JP 22954593A JP H0763193 A JPH0763193 A JP H0763193A
- Authority
- JP
- Japan
- Prior art keywords
- impeller
- bush
- rotary shaft
- fitted
- centrifugal force
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/266—Rotors specially for elastic fluids mounting compressor rotors on shafts
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】この発明は、遠心式低温圧縮機の
インペラ取付構造に関し、高速回転や超高速回転による
遠心力で回転軸から浮き上がることを防止するととも
に、取付けや取外しが容易にできるようにしたものであ
る。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an impeller mounting structure for a centrifugal low-temperature compressor, which prevents the centrifugal shaft from being lifted by a centrifugal force due to high-speed rotation or ultra-high-speed rotation, and facilitates mounting and removal. It is the one.
【0002】[0002]
【従来の技術】低温気体の圧縮などに使用される遠心式
低温圧縮機では、駆動源に連結されて駆動される回転軸
にインペラを取付ける必要があり、たとえばインペラの
材質を回転軸より熱膨張率が大きい材質とし、運転時に
インペラが低温状態になると、回転軸に比べて熱収縮量
が多くなることを利用して自動的に締付力が加わる(自
緊)ようにしている。2. Description of the Related Art In a centrifugal low-temperature compressor used for compressing low-temperature gas, it is necessary to attach an impeller to a rotary shaft that is driven by being connected to a drive source. For example, the material of the impeller is thermally expanded from the rotary shaft. It is made of a material with a high rate, and when the impeller is in a low temperature state during operation, the amount of heat shrinkage is larger than that of the rotating shaft, so that the tightening force is automatically applied (self-tightening).
【0003】また、インペラが高速回転や超高速回転で
運転されると、遠心力によってインペラの回転軸への取
付部分が変形し、インペラが回転軸から浮き上がろうと
するため、図2に組立前後の状態を示すように、回転軸
1に対してインペラ2の取付部の径を小さくして置き、
遠心力によるインペラ2の内周の変形量を上回る締代S
でインペラ2を回転軸1に焼きばめするようにしてい
る。When the impeller is operated at high speed or ultra-high speed, centrifugal force deforms the part of the impeller that is attached to the rotary shaft, and the impeller tends to float up from the rotary shaft. As shown in the front and rear states, the diameter of the mounting portion of the impeller 2 is set to be small with respect to the rotary shaft 1,
The interference S that exceeds the amount of deformation of the inner circumference of the impeller 2 due to centrifugal force
Then, the impeller 2 is shrink-fitted to the rotary shaft 1.
【0004】このような遠心式低温圧縮機では、点検の
ためや修理などのため圧縮機を分解しようとすると、回
転軸1からインペラ2を取り外す必要があるが、一旦、
回転軸1にインペラ2を焼きばめした状態では、回転軸
1だけを冷却することが出来ず、インペラ2を加熱して
取り外すようにしなければならない。In such a centrifugal low-temperature compressor, when the compressor is disassembled for inspection or repair, it is necessary to remove the impeller 2 from the rotary shaft 1.
In the state where the impeller 2 is shrink-fitted to the rotary shaft 1, only the rotary shaft 1 cannot be cooled, and the impeller 2 must be heated and removed.
【0005】[0005]
【発明が解決しようとする課題】ところが、インペラ2
を加熱する場合には、回転軸1も同時に温まってしまう
ので、回転軸1のみを冷却でき、インペラ2のみを加熱
できる組立時に比べて大幅に高い温度まで加熱する必要
がある。DISCLOSURE OF THE INVENTION Problems to be Solved by the Invention
In the case of heating, since the rotary shaft 1 is also warmed at the same time, it is necessary to heat the rotary shaft 1 only, and to heat the impeller 2 to a significantly higher temperature than when assembled.
【0006】しかし、加熱温度を高くすると、インペラ
2や圧縮機の他の部分へ熱影響が及ぶことから加熱温度
には自ずから限界があり、これによって回転軸1とイン
ペラ2との間の焼きばめ時の締代Sにも限界が生じ、高
速回転よって生じる遠心力による変形を抑えることがで
きず、インペラ2が回転軸1に対して浮き上がってしま
い、安定した状態で運転することができない等の問題が
ある。However, when the heating temperature is increased, the impeller 2 and other parts of the compressor are thermally affected, so that the heating temperature naturally has a limit, and as a result, the burn-off between the rotary shaft 1 and the impeller 2 is limited. The tightening margin S at the time of tightening also has a limit, deformation due to centrifugal force caused by high-speed rotation cannot be suppressed, and the impeller 2 floats up with respect to the rotary shaft 1 and cannot be operated in a stable state. I have a problem.
【0007】この発明は、かかる従来技術の問題点に鑑
みてなされたもので、高速回転による遠心力で回転軸か
ら浮き上がることを防止でき、取付けや取外しが容易に
できる遠心式低温圧縮機のインペラ取付構造を提供しよ
うとするものである。The present invention has been made in view of the above-mentioned problems of the prior art, and it is possible to prevent the centrifugal shaft from being lifted up by a centrifugal force due to high-speed rotation and to easily mount and remove the impeller of a centrifugal low-temperature compressor. It is intended to provide a mounting structure.
【0008】[0008]
【課題を解決するための手段】上記従来技術が有する課
題を解決するためこの発明の請求項1の遠心式低温圧縮
機のインペラ取付構造は、インペラと回転軸との間に嵌
め込まれるブッシュを当該回転軸と同一熱膨張率を有す
る材質を用いて形成するとともに、その内径を常温で回
転軸との間に隙間無く装着可能に形成し、このブッシュ
の外径部にインペラの運転時に生じる遠心力による変形
を相殺する締代を与えてインペラを焼きばめする一方、
このインペラを前記ブッシュを介して先端部にねじ部を
備えた回転軸に装着しナットで締付けて軸方向の移動を
規制したことを特徴とするものである。In order to solve the problems of the above-mentioned prior art, the impeller mounting structure for a centrifugal low-temperature compressor according to claim 1 of the present invention has a bush fitted between the impeller and the rotary shaft. It is made of a material that has the same coefficient of thermal expansion as the rotating shaft, and its inner diameter can be mounted at room temperature without any gap between it and the rotating shaft. While giving a tightening margin that offsets the deformation due to
This impeller is mounted on a rotary shaft having a threaded portion at its tip through the bush and is tightened with a nut to restrict movement in the axial direction.
【0009】また、この発明の請求項2の遠心式低温圧
縮機のインペラ取付構造は、上記請求項1の構成に加
え、前記インペラの背面に設けられた環状の突起に、イ
ンペラの運転時に生じる遠心力によるインペラ背面の内
径の変形を規制する締代を与えてインペラと同等以上の
熱膨張率を有する材質で形成される背面リングを焼きば
めしたことを特徴とするものである。According to a second aspect of the present invention, in addition to the structure of the first aspect, the impeller mounting structure for a centrifugal low-temperature compressor is formed on an annular protrusion provided on the back surface of the impeller during operation of the impeller. The back ring made of a material having a coefficient of thermal expansion equal to or higher than that of the impeller is shrink-fitted by giving a tightening margin for restricting deformation of the inner diameter of the back surface of the impeller due to centrifugal force.
【0010】[0010]
【作用】請求項1の遠心式低温圧縮機のインペラ取付構
造によれば、インペラに嵌め込むブッシュを回転軸と同
一の熱膨張率の材質とし、このブッシュの外周に遠心力
が加わっても浮き上がらない締代を与えてインペラを焼
きばめするようにしており、ブッシュとインペラとの取
付けを運転時に支障がないようにしている。According to the impeller mounting structure of the centrifugal low-temperature compressor of claim 1, the bush fitted in the impeller is made of a material having the same coefficient of thermal expansion as that of the rotating shaft, and the bush is floated even if a centrifugal force is applied to the outer circumference of the bush. The impeller is shrink-fitted with no interference, so that the bush and the impeller can be installed without any hindrance during operation.
【0011】また、回転軸にはブッシュを介してインペ
ラを隙間無く取付け、回転軸の先端のねじ部にナットを
締付けて軸方向の移動を規制するようにしており、ブッ
シュと回転軸の等しい熱膨張率によって低温時でも隙間
のない状態で運転でき、加熱や冷却の必要を無くして取
付けや取外しができるようになる。Further, an impeller is attached to the rotary shaft via a bush without a gap, and a nut is fastened to a threaded portion at the tip of the rotary shaft to restrict axial movement. Due to the expansion coefficient, it can be operated without gaps even at low temperatures, and can be installed or removed without the need for heating or cooling.
【0012】さらに、請求項2の遠心式低温圧縮機のイ
ンペラ取付構造によれば、上記の構成に加え、インペラ
の熱膨張率と同等以上の材質の背面リングを用い、これ
をインペラの運転時に生じる遠心力によるインペラ背面
の内径の変形を規制する締代を与えてインペラの背面に
焼きばめするようにしており、低温時の熱収縮を利用し
て一層確実にインペラの遠心力による浮き上がりを防止
して安定した回転状態で運転できるようにしている。Further, according to the impeller mounting structure of the centrifugal low-temperature compressor of claim 2, in addition to the above-mentioned structure, a back ring made of a material having a coefficient of thermal expansion equal to or higher than that of the impeller is used, which is used during operation of the impeller. The shrinkage is applied to the back surface of the impeller by restricting the deformation of the inner diameter of the back surface of the impeller due to the generated centrifugal force, and the shrinkage at the low temperature is used to more reliably lift the impeller due to the centrifugal force. It prevents it so that it can be operated in a stable rotation state.
【0013】[0013]
【実施例】以下、この発明の一実施例を図面に基づき詳
細に説明する。図1はこの発明の遠心式低温圧縮機のイ
ンペラ取付構造の一実施例にかかる組立前および組立後
の断面図である。この遠心式低温圧縮機のインペラ取付
構造10では、駆動回転される回転軸11に段差11a
が形成されて小径とされたインペラ装着部11bが形成
され、先端部にインペラ装着部11bより小径のねじ部
12が形成してある。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of the present invention will be described in detail below with reference to the drawings. 1 is a cross-sectional view of an impeller mounting structure for a centrifugal low-temperature compressor according to an embodiment of the present invention before and after assembly. In this impeller mounting structure 10 for a centrifugal low-temperature compressor, a step 11a is formed on a rotating shaft 11 that is driven and rotated.
Is formed to form a small diameter impeller mounting portion 11b, and a threaded portion 12 having a smaller diameter than the impeller mounting portion 11b is formed at the tip end portion.
【0014】この回転軸11のインペラ装着部11bに
は、ブッシュ13を介してインペラ14が取付けられる
ようになっている。An impeller 14 is attached to the impeller mounting portion 11b of the rotary shaft 11 via a bush 13.
【0015】このブッシュ13は回転軸11の熱膨張率
β1 と同一の熱膨張率β2 (=β1)を有する材質でほ
ぼ円筒状に作られ、内径が組立時に回転軸11のインペ
ラ装着部11bの外径と隙間のない状態で装着できるよ
うに加工されるとともに、軸方向後端部にインペラ14
が係止される大径部13aが形成されて所定の肉厚を確
保して形成してある。The bush 13 is made of a material having a coefficient of thermal expansion β2 (= β1) which is the same as the coefficient of thermal expansion β1 of the rotating shaft 11, and is formed into a substantially cylindrical shape. It is machined so that it can be installed without a gap with the outer diameter, and the impeller 14 is attached to the axial rear end.
A large-diameter portion 13a is formed to secure the predetermined wall thickness.
【0016】このブッシュ13の外径部に取付けられる
インペラ14は、その取付部の内径がブッシュ13の外
径より小さくしてあり、この径の差がブッシュ13に焼
きばめしたときにインペラ14の運転時に生じる遠心力
による変形を規制する締代S1 となるようにしてある。The inner diameter of the mounting portion of the impeller 14 mounted on the outer diameter portion of the bush 13 is smaller than the outer diameter of the bush 13, and the difference in this diameter when the bush 13 is shrink fitted into the impeller 14. The tightening margin S1 is set so as to regulate the deformation due to the centrifugal force generated during the operation.
【0017】そして、ブッシュ13に焼きばめしたイン
ペラ14ごと回転軸11のインペラ装着部11bに装着
して軸方向の移動を回転軸11の段差11aとで締付け
るため回転軸11のねじ部12にねじ込むナット15が
用意してある。Then, the impeller 14 shrunk to the bush 13 is mounted on the impeller mounting portion 11b of the rotary shaft 11 so as to tighten the axial movement with the step 11a of the rotary shaft 11, so that the threaded portion 12 of the rotary shaft 11 is secured. A nut 15 for screwing is prepared.
【0018】さらに、回転数が高い状態で運転するイン
ペラの場合には、インペラ14の背面14aの運転時に
生じる遠心力による変形に伴う内径の浮き上がりを規制
するため、インペラ14の背面14aの外周に焼きばめ
される背面リング16が用意してあり、焼きばめによる
締代S2 によって内径の浮き上がりを防止するととも
に、背面リング16自体をインペラ16の熱膨張率β3
と同等以上の熱膨張率β4 (≧β3 )の材質で作ってあ
る。Further, in the case of an impeller that operates at a high rotational speed, in order to restrict the rise of the inner diameter due to the deformation of the back surface 14a of the impeller 14 due to the centrifugal force generated during operation, the outer circumference of the back surface 14a of the impeller 14 is restricted. A back ring 16 to be shrink-fitted is prepared, and the tightening margin S2 due to shrink-fitting prevents the inner diameter from rising, and the back ring 16 itself is fitted with a coefficient of thermal expansion β3 of the impeller 16.
It is made of a material with a coefficient of thermal expansion β4 (≧ β3) that is equal to or higher than.
【0019】このような遠心式低温圧縮機のインペラ1
4の回転軸11への取付けは、次のようにして行われ
る。Impeller 1 of such a centrifugal low-temperature compressor
4 is attached to the rotary shaft 11 as follows.
【0020】予め、インペラ14をブッシュ13の外径
部に焼きばめするとともに、高速回転で使用されるイン
ペラ14の場合には、さらに背面リング16をインペラ
14の背面14aに焼きばめしてこれらを一体にしてお
く。In advance, the impeller 14 is shrink-fitted to the outer diameter portion of the bush 13, and in the case of the impeller 14 used at high speed rotation, the back ring 16 is further shrink-fitted to the back surface 14a of the impeller 14 and these Keep together.
【0021】このインペラ14、ブッシュ13および背
面リング16が一体とした状態で、回転軸11のインペ
ラ装着部11bにブッシュ13の内径部を嵌め込む。With the impeller 14, the bush 13 and the back ring 16 integrated, the inner diameter portion of the bush 13 is fitted into the impeller mounting portion 11b of the rotary shaft 11.
【0022】このとき、熱膨張率が等しい回転軸11の
インペラ装着部11bとブッシュ14の内径部を組立時
に常温で隙間ができない状態に加工してあるので、簡単
に装着することができる。At this time, since the impeller mounting portion 11b of the rotary shaft 11 and the inner diameter portion of the bush 14 having the same coefficient of thermal expansion are machined so that no gap can be formed at room temperature during assembly, they can be easily mounted.
【0023】そして、回転軸11の先端部のねじ部12
にナット15を用い、ブッシュ13を回転軸11の段差
11aに押し付けるようにし、運転時にも接触面で相対
変位が生じないような締付けトルクで締付ける。The threaded portion 12 at the tip of the rotary shaft 11
A nut 15 is used to press the bush 13 against the step 11a of the rotating shaft 11, and the bushing 13 is tightened with a tightening torque such that relative displacement does not occur on the contact surface even during operation.
【0024】こうしてインペラ14をブッシュ13を介
して回転軸11に取付けることで、確実に支持すること
ができる。By mounting the impeller 14 on the rotary shaft 11 via the bush 13 in this manner, the impeller 14 can be reliably supported.
【0025】このような遠心式低温圧縮機のインペラ取
付構造10によれば、インペラ14が接する低温流体の
温度が回転軸11の温度より低くなる場合でも、回転軸
11とブッシュ13とが同一熱膨張率(β1 =β2 )を
有する材質であるので、、軸方向の相対変位が小さく、
ナット15による締付けトルクを予め増やしておくこと
によってインペラ14を確実にブッシュ13を介して回
転軸11に取付けることができる。According to the impeller mounting structure 10 for such a centrifugal low-temperature compressor, even when the temperature of the low temperature fluid contacting the impeller 14 becomes lower than the temperature of the rotating shaft 11, the rotating shaft 11 and the bush 13 have the same heat. Since the material has an expansion coefficient (β1 = β2), the relative displacement in the axial direction is small,
By increasing the tightening torque by the nut 15 in advance, the impeller 14 can be securely attached to the rotating shaft 11 via the bush 13.
【0026】また、インペラ14が接する気体の温度が
インペラ14の組立時の温度より低くなる場合でも、背
面リング16がインペラ14と同等以上の熱膨張率(β
4 ≧β3 )を有する材質であるので、締代が増加し、運
転中のインペラ14の背面14aの内径の浮き上がりを
防止することができる。Even when the temperature of the gas in contact with the impeller 14 becomes lower than the temperature at the time of assembling the impeller 14, the rear ring 16 has a coefficient of thermal expansion (β that is equal to or higher than that of the impeller 14).
Since it is a material having 4 ≧ β 3), the tightening margin is increased, and it is possible to prevent the inner diameter of the rear surface 14a of the impeller 14 during operation from rising.
【0027】一方、組み立てた状態のインペラ14を回
転軸11から取り外す場合には、回転軸11の先端部の
ナット15を緩めてブッシュ13ごとインペラ14を引
き抜くことで、加熱や冷却の必要もなく簡単に取り外す
ことができる。On the other hand, when the assembled impeller 14 is removed from the rotary shaft 11, the nut 15 at the tip of the rotary shaft 11 is loosened and the impeller 14 is pulled out together with the bush 13 so that heating and cooling are not necessary. Can be easily removed.
【0028】したがって、従来、組立上の問題から生じ
ていた超高速回転する遠心式低温圧縮機の設計限界を上
げることができ、インペラ14の設計上の自由度が大き
くなり、高効率、コンパクトな遠心式低温圧縮機を設計
することができる。Therefore, it is possible to raise the design limit of the centrifugal low-temperature compressor that rotates at an extremely high speed, which has conventionally been caused by an assembly problem, and the degree of freedom in designing the impeller 14 is increased, which is highly efficient and compact. A centrifugal low temperature compressor can be designed.
【0029】また、従来構造では、回転軸へのインペラ
の取付けの際、焼きばめが必要であったが、この取付構
造10では、予めインペラ14をブッシュ13に焼きば
めしておくことができるので、簡単に最終組立を行うこ
とができ、組立性も向上する。Further, in the conventional structure, when the impeller is attached to the rotary shaft, shrink fitting is necessary, but in the mounting structure 10, the impeller 14 can be shrink fitted to the bush 13 in advance. Therefore, the final assembly can be easily performed, and the assemblability is improved.
【0030】さらに、圧縮機を分解するときやインペラ
14を交換するときに、従来は高熱を加えてインペラを
取り外す必要があったが、この取付構造10では、加熱
や冷却を行うこと無く、簡単にブッシュ13ごとインペ
ラ14を取り外すことができるとともに、取外し時に損
傷する恐れも少なく繰返し使用することができる。Further, when disassembling the compressor or replacing the impeller 14, it has conventionally been necessary to remove the impeller by applying high heat, but this mounting structure 10 does not require heating or cooling and is simple. Further, the impeller 14 together with the bush 13 can be removed, and there is little risk of damage at the time of removal, and the bush can be used repeatedly.
【0031】なお、この発明は、上記実施例に限定する
ものでなく、この発明の要旨を変更しない範囲で各構成
要素に変更を加えるようにしても良い。The present invention is not limited to the above-mentioned embodiments, and each constituent element may be modified within the scope of the invention.
【0032】[0032]
【発明の効果】以上、一実施例とともに具体的に説明し
たようにこの発明の請求項1の遠心式低温圧縮機のイン
ペラ取付構造によれば、インペラに嵌め込むブッシュを
回転軸と同一の熱膨張率の材質とし、このブッシュの外
周にインペラを遠心力が加わっても浮き上がらない締代
を与えて焼きばめするようにしたので、ブッシュとイン
ペラとの取付けを運転時に浮き上がる等の支障がないよ
うにすることができる。As described above in detail with reference to the embodiment, according to the impeller mounting structure of the centrifugal low-temperature compressor according to claim 1 of the present invention, the bush fitted in the impeller has the same heat as the rotating shaft. As the material has a coefficient of expansion and the bush is fitted around the outer circumference of the bush by a shrinkage fit that does not float even if centrifugal force is applied, there is no obstacle such as lifting during operation of the bush and impeller. You can
【0033】また、回転軸にはブッシュを介してインペ
ラを隙間無く取付け、回転軸の先端のねじ部にナットを
締付けて軸方向の移動を規制するようにしたので、ブッ
シュと回転軸の等しい熱膨張率によって低温時でも隙間
のない状態で運転でき、加熱や冷却の必要を無くして取
付けや取外しを簡単に行うことができる。Further, since the impeller is attached to the rotary shaft through the bush without a gap and the nut is fastened to the screw portion at the tip of the rotary shaft to restrict the axial movement, the heat of the bush and the rotary shaft are equal. Due to the expansion coefficient, it can be operated without gaps even at low temperatures, and can be installed and removed easily without the need for heating or cooling.
【0034】さらに、この発明の請求項2の遠心式低温
圧縮機のインペラ取付構造によれば、上記の構成に加
え、インペラの熱膨張率と同等以上の材質の背面リング
を用い、これをインペラの運転時に生じる遠心力による
インペラ背面の内径の変形を規制する締代を与えてイン
ペラの背面に焼きばめするようにしたので、低温時の熱
収縮を利用して一層確実にインペラの遠心力による浮き
上がりを防止して安定した回転状態で運転することがで
きる。Further, according to the impeller mounting structure for a centrifugal low-temperature compressor of claim 2 of the present invention, in addition to the above-mentioned constitution, a back ring made of a material having a coefficient of thermal expansion equal to or higher than that of the impeller is used, and this is used for the impeller. The shrinkage of the inner diameter of the impeller back face due to the centrifugal force generated during the operation of the impeller is given to the back face of the impeller so that it is shrink-fitted. It is possible to operate in a stable rotating state by preventing the floating due to.
【0035】したがって、これまでの構造に比べてイン
ペラの設計上の自由度が大きくなるなどの利点がある。Therefore, there is an advantage that the degree of freedom in designing the impeller is increased as compared with the conventional structure.
【図1】この発明の遠心式低温圧縮機のインペラ取付構
造の一実施例にかかる組立前および組立後の断面図であ
る。FIG. 1 is a cross-sectional view before and after assembly according to an embodiment of an impeller mounting structure for a centrifugal low-temperature compressor of the present invention.
【図2】従来の遠心式低温圧縮機のインペラ取付構造に
かかる組立前および組立後の断面図である。FIG. 2 is a cross-sectional view of an impeller mounting structure for a conventional centrifugal low-temperature compressor before and after assembly.
10 遠心式圧縮機のインペラ取付構造 11 回転軸 12 ねじ部 13 ブッシュ 14 インペラ 15 ナット 16 背面リング S1 ブッシュとインペラの焼きばめの締代 S2 インペラと背面リングの焼きばめの締代 10 Centrifugal compressor impeller mounting structure 11 Rotating shaft 12 Threaded portion 13 Bushing 14 Impeller 15 Nut 16 Rear ring S1 Shrinkage interference of bush and impeller S2 Impeller and interference shrinkage of rear ring
フロントページの続き (72)発明者 朝倉 啓 東京都江東区豊洲三丁目2番16号 石川島 播磨重工業株式会社豊洲総合事務所内 (72)発明者 長井 俊二 東京都江東区豊洲三丁目2番16号 石川島 播磨重工業株式会社豊洲総合事務所内Front page continuation (72) Inventor Kei Asakura 3-21-16 Toyosu, Koto-ku, Tokyo Ishikawajima Harima Heavy Industries Ltd. Toyosu General Office (72) Inventor Shunji Nagai 3-2-1-16 Toyosu, Koto-ku, Tokyo Ishikawajima Harima Heavy Industries Co., Ltd.Toyosu General Office
Claims (2)
ブッシュを当該回転軸と同一熱膨張率を有する材質を用
いて形成するとともに、その内径を常温で回転軸との間
に隙間無く装着可能に形成し、このブッシュの外径部に
インペラの運転時に生じる遠心力による変形を相殺する
締代を与えてインペラを焼きばめする一方、このインペ
ラを前記ブッシュを介して先端部にねじ部を備えた回転
軸に装着し軸方向の移動を規制してナットで締付けたこ
とを特徴とする遠心式低温圧縮機のインペラ取付構造。1. The bush fitted between the impeller and the rotary shaft is made of a material having the same coefficient of thermal expansion as the rotary shaft, and the inner diameter of the bush can be mounted at room temperature without any gap between the bush and the rotary shaft. The bush is formed on the outer diameter portion of the bush, and the impeller is shrink-fitted by giving a tightening margin to offset the deformation caused by centrifugal force generated during the operation of the impeller, while the impeller is screwed to the tip portion through the bush. An impeller mounting structure for a centrifugal low-temperature compressor, which is mounted on a rotating shaft provided and regulated in axial movement to be tightened with a nut.
突起に、インペラと同等以上の熱膨張率を有する材質で
形成されインペラの運転時に生じる遠心力によるインペ
ラの内径の変形を規制する締代を与えて背面リングを焼
きばめしたことを特徴とする請求項1記載の遠心式圧縮
機のインペラ取付構造。2. A tightening allowance for restricting deformation of the inner diameter of the impeller, which is formed on a ring-shaped projection provided on the back surface of the impeller and has a coefficient of thermal expansion equal to or higher than that of the impeller, due to centrifugal force generated during operation of the impeller. The impeller mounting structure for a centrifugal compressor according to claim 1, wherein the back ring is shrink-fitted by applying the above.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP05229545A JP3129587B2 (en) | 1993-08-23 | 1993-08-23 | Centrifugal low-temperature compressor impeller mounting structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP05229545A JP3129587B2 (en) | 1993-08-23 | 1993-08-23 | Centrifugal low-temperature compressor impeller mounting structure |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH0763193A true JPH0763193A (en) | 1995-03-07 |
JP3129587B2 JP3129587B2 (en) | 2001-01-31 |
Family
ID=16893848
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP05229545A Expired - Lifetime JP3129587B2 (en) | 1993-08-23 | 1993-08-23 | Centrifugal low-temperature compressor impeller mounting structure |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP3129587B2 (en) |
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