JP3129587B2 - Centrifugal low-temperature compressor impeller mounting structure - Google Patents

Centrifugal low-temperature compressor impeller mounting structure

Info

Publication number
JP3129587B2
JP3129587B2 JP05229545A JP22954593A JP3129587B2 JP 3129587 B2 JP3129587 B2 JP 3129587B2 JP 05229545 A JP05229545 A JP 05229545A JP 22954593 A JP22954593 A JP 22954593A JP 3129587 B2 JP3129587 B2 JP 3129587B2
Authority
JP
Japan
Prior art keywords
impeller
rotating shaft
bush
mounting structure
centrifugal
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 - Lifetime
Application number
JP05229545A
Other languages
Japanese (ja)
Other versions
JPH0763193A (en
Inventor
大策 加藤
脩好 佐治
博志 大矢
啓 朝倉
俊二 長井
Original Assignee
石川島播磨重工業株式会社
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 by 石川島播磨重工業株式会社 filed Critical 石川島播磨重工業株式会社
Priority to JP05229545A priority Critical patent/JP3129587B2/en
Publication of JPH0763193A publication Critical patent/JPH0763193A/en
Application granted granted Critical
Publication of JP3129587B2 publication Critical patent/JP3129587B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/266Rotors 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)

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【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 floating from a rotating shaft due to centrifugal force caused by high-speed rotation or ultra-high-speed rotation, and facilitates installation and removal. It was made.

【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 mount an impeller on a rotating shaft which is connected to and driven by a driving source. For example, the material of the impeller is thermally expanded from the rotating shaft. When the impeller is in a low temperature state during operation, a tightening force is automatically applied (self-tightening) by utilizing the fact that the amount of heat shrinkage is larger than that of the rotating shaft.

【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。
[0003] When the impeller is operated at a high speed rotation or a very high speed rotation, the mounting portion of the impeller to the rotating shaft is deformed by centrifugal force, and the impeller tends to float up from the rotating shaft. As shown before and after, the diameter of the mounting portion of the impeller 2 with respect to the rotating shaft 1 is set small,
Interference S exceeding the amount of deformation of the inner circumference of impeller 2 due to centrifugal force
To shrink-fit the impeller 2 to the rotating 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。
[0004] In such a centrifugal low-temperature compressor, it is necessary to remove the impeller 2 from the rotating shaft 1 to disassemble the compressor for inspection or repair.
In a state where the impeller 2 is shrink-fitted to the rotating shaft 1, only the rotating 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。
However, the impeller 2
Is heated at the same time, the rotating shaft 1 is also heated. Therefore, it is necessary to heat the rotating shaft 1 only, and to heat the impeller 2 to a much higher temperature than at the time of assembly, in which only the impeller 2 can be heated.

【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。
[0006] However, if the heating temperature is increased, the impeller 2 and other parts of the compressor are affected by heat, so that the heating temperature is naturally limited, and as a result, the firing between the rotary shaft 1 and the impeller 2 is reduced. And the deformation due to the centrifugal force caused by high-speed rotation cannot be suppressed, and the impeller 2 floats up with respect to the rotating shaft 1 and cannot be operated in a stable state. There is 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。
SUMMARY OF THE INVENTION The present invention has been made in view of the above-mentioned problems of the prior art, and it is possible to prevent a centrifugal force generated by high-speed rotation from floating from a rotating shaft, and to facilitate installation and removal of a centrifugal low-temperature compressor impeller. 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。
According to a first aspect of the present invention, there is provided an impeller mounting structure for a centrifugal low-temperature compressor, comprising a bush fitted between an impeller and a rotary shaft. It is formed using a material having the same coefficient of thermal expansion as the rotating shaft, and its inner diameter is formed so that it can be attached to the rotating shaft at room temperature with no gap. The centrifugal force generated at the outer diameter of this bush during operation of the impeller While shrink-fitting the impeller with a closing allowance to offset the deformation due to
The impeller is mounted on a rotating shaft having a threaded portion at the tip via the bush and tightened with a nut to restrict axial movement.

【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 the second aspect of the present invention, in addition to the structure of the first aspect, the impeller mounting structure of the centrifugal low-temperature compressor is formed on the annular projection provided on the back surface of the impeller when the impeller is operated. A rear ring made of a material having a thermal expansion coefficient equal to or higher than that of the impeller is shrink-fitted by giving a margin for restricting deformation of the inner diameter of the rear 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 the first aspect, the bush to be fitted into the impeller is made of a material having the same coefficient of thermal expansion as that of the rotating shaft, and the bushing rises even when a centrifugal force is applied to the outer periphery of the bush. The impeller is shrink-fitted with no interference, so that the bush and the impeller can be securely mounted 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 mounted on the rotary shaft via a bush without any gap, and a nut is fastened to a screw portion at the tip of the rotary shaft to restrict axial movement. The expansion coefficient allows operation without gaps even at low temperatures, and enables attachment and detachment 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 the second aspect, in addition to the above configuration, a back ring made of a material having a coefficient equal to or higher than the thermal expansion coefficient of the impeller is used, and this is used during operation of the impeller. A shrink fit is applied to the back of the impeller by giving a tightening that regulates the deformation of the inner diameter of the back of the impeller due to the generated centrifugal force. This prevents the vehicle from running 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 below in detail with reference to the drawings. FIG. 1 is a sectional view showing an impeller mounting structure of a centrifugal low-temperature compressor according to one embodiment of the present invention before and after assembly. In the impeller mounting structure 10 of the centrifugal low-temperature compressor, the rotating shaft 11 driven and rotated has a step 11a.
Are formed to form a small-diameter impeller mounting portion 11b, and a screw portion 12 having a smaller diameter than the impeller mounting portion 11b is formed at the tip.

【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 rotating 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 the same thermal expansion coefficient β2 (= β1) as the thermal expansion coefficient β1 of the rotating shaft 11, and has an inner diameter of the impeller mounting portion 11b of the rotating shaft 11 during assembly. It is machined so that it can be installed with no gap between the outer diameter and the impeller 14 at the rear end in the axial direction.
Is formed to secure a predetermined 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 impeller 14 attached to the outer diameter portion of the bush 13 has an inner diameter of the attachment portion smaller than the outer diameter of the bush 13. In order to restrict the deformation due to the centrifugal force that occurs during the operation of S1, the interference S1 is set.

【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。
The impeller 14 fitted on the bush 13 is mounted on the impeller mounting portion 11b of the rotary shaft 11 and the axial movement is tightened by the step 11a of the rotary shaft 11 with the screw portion 12 of the rotary shaft 11. A nut 15 for screwing is provided.

【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 operating at a high rotational speed, the outer periphery of the rear surface 14a of the impeller 14 is restricted in order to prevent the inner diameter from rising due to the centrifugal force generated during the operation of the rear surface 14a of the impeller 14. A rear ring 16 to be shrink-fitted is provided to prevent the inner diameter from rising due to the interference S2 by shrink-fitting, and the rear ring 16 itself is connected to the thermal expansion coefficient β3 of the impeller 16.
It is made of a material with a thermal expansion coefficient β4 (≧ β3) equal to or higher than that of.

【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。
The impeller 1 of such a centrifugal low-temperature compressor
4 is mounted on the rotating 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, the back ring 16 is further shrink-fitted to the back surface 14 a of the impeller 14. Are kept 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 of the bush 13 is fitted into the impeller mounting portion 11b of the rotating 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, the impeller mounting portion 11b of the rotary shaft 11 and the inner diameter portion of the bush 14, which have the same thermal expansion coefficient, are machined so that no gap is formed at room temperature during assembly, so that 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。
Then, the threaded portion 12 at the tip of the rotating shaft 11
The bush 13 is pressed against the step 11a of the rotating shaft 11 by using a nut 15, and is tightened with a tightening torque that does not cause relative displacement 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 attaching the impeller 14 to the rotating shaft 11 via the bush 13 in this manner, it is possible to reliably support the impeller 14.

【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 of the centrifugal low-temperature compressor, even when the temperature of the low-temperature fluid in contact with the impeller 14 is lower than the temperature of the rotary shaft 11, the rotary 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 of 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。
Further, 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 thermal expansion coefficient (β
4 ≧ β3), the interference is increased, and it is possible to prevent the inner diameter of the rear surface 14a of the impeller 14 from rising during operation.

【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 impeller 14 in the assembled state is to be removed from the rotating shaft 11, the nut 15 at the tip of the rotating shaft 11 is loosened and the impeller 14 is pulled out together with the bush 13, thereby eliminating the need for heating and cooling. It 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 a high speed, which has conventionally been caused by assembly problems, and the degree of freedom in the design of the impeller 14 is increased, resulting in high efficiency and compactness. 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, shrink-fitting is required when the impeller is mounted on the rotating shaft. In this mounting structure 10, the impeller 14 can be shrink-fitted on the bush 13 in advance. Therefore, final assembly can be easily performed, and 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。
Furthermore, when disassembling the compressor or replacing the impeller 14, it has conventionally been necessary to remove the impeller by applying high heat, but with this mounting structure 10, the impeller can be easily mounted without heating or cooling. In addition, the impeller 14 can be removed together with the bush 13 and can be used repeatedly with little risk of damage at the time of removal.

【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-described embodiment, and each component may be modified without changing the gist of the present 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 the embodiment, according to the impeller mounting structure of the centrifugal low-temperature compressor according to the first aspect of the present invention, the bush fitted into the impeller has the same heat as the rotating shaft. The bushing is made of a material with an expansion coefficient, and the outer periphery of the bush is shrink-fitted by giving an interference that does not float even when centrifugal force is applied, so that the bush and the impeller are not hindered during operation. You can do so.

【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, the impeller is attached to the rotating shaft via a bush without any gap, and a nut is fastened to the threaded portion at the tip of the rotating shaft to restrict the movement in the axial direction. Even when the temperature is low, the device can be operated without any gaps due to the expansion coefficient, and can be easily mounted and removed 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 of the centrifugal low-temperature compressor according to the second aspect of the present invention, in addition to the above-described structure, a back ring made of a material equal to or more than the coefficient of thermal expansion of the impeller is used, and this is used. The impeller is shrink-fitted to the back of the impeller by giving a tightening that regulates the deformation of the inner diameter of the back of the impeller due to the centrifugal force generated during the operation of the impeller. It is possible to operate the vehicle in a stable rotation state by preventing the floating due to the lifting.

【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 the design of the impeller is increased as compared with the conventional structure.

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

【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 sectional view showing an impeller mounting structure of a centrifugal low-temperature compressor according to an embodiment of the present invention before and after assembling.

【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 a conventional centrifugal low-temperature compressor before and after assembling according to an impeller mounting structure.

【符号の説明】[Explanation of symbols]

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 DESCRIPTION OF SYMBOLS 10 Impeller mounting structure of a centrifugal compressor 11 Rotating shaft 12 Thread part 13 Bush 14 Impeller 15 Nut 16 Back ring S1 Shrink fit of shrink fit of impeller and back ring S2 Shrink fit of shrink fit of impeller and back ring

───────────────────────────────────────────────────── フロントページの続き (72)発明者 大矢 博志 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 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 (58)調査した分野(Int.Cl.7,DB名) F04D 29/28 F04D 29/30 ──────────────────────────────────────────────────続 き Continuing on the front page (72) Inventor Hiroshi Oya 3-2-16-1 Toyosu, Koto-ku, Tokyo Ishikawa-jima-Harima Heavy Industries, Ltd. Toyosu General Office (72) Inventor Kei Asakura 3-chome, Toyosu, Koto-ku, Tokyo No. 2-16 Ishikawajima-Harima Heavy Industries, Ltd. Toyosu Sogo Office (72) Inventor Shunji Nagai 3-2-1 Toyosu, Koto-ku, Tokyo Ishikawa Shima-Harima Heavy Industries Toyosu Sogo Office (58) (Int.Cl. 7 , DB name) F04D 29/28 F04D 29/30

Claims (2)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 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. A bush fitted between an impeller and a rotating shaft is formed using a material having the same coefficient of thermal expansion as the rotating shaft, and the inner diameter thereof can be mounted at room temperature with no gap between the rotating shaft and the rotating shaft. The shrink fit of the outer diameter portion of the bush is given to the outer diameter portion of the bush by canceling the deformation due to the centrifugal force generated during the operation of the impeller, and the impeller is threaded at the tip portion through the bush. An impeller mounting structure for a centrifugal low-temperature compressor, wherein the impeller is mounted on a rotating shaft provided, restricting movement in the axial direction, and tightened with a nut.
【請求項2】 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. An interference protrusion formed on a rear surface of the impeller, which is formed of a material having a thermal expansion coefficient equal to or higher than that of the impeller, and restricts deformation of the inner diameter of the impeller due to centrifugal force generated during operation of the impeller. 2. The impeller mounting structure for a centrifugal compressor according to claim 1, wherein the rear ring is shrink-fitted.
JP05229545A 1993-08-23 1993-08-23 Centrifugal low-temperature compressor impeller mounting structure Expired - Lifetime JP3129587B2 (en)

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 JPH0763193A (en) 1995-03-07
JP3129587B2 true 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)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014196214A1 (en) * 2013-06-04 2014-12-11 三菱重工業株式会社 Impeller, rotating machine, and method for assembling rotating machine

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6362295B2 (en) 1997-07-17 2002-03-26 Atofina Chemicals, Inc. Fluoropolymer powder coatings from modified thermoplastic vinylidene fluoride based resins
JP2000120588A (en) * 1998-10-16 2000-04-25 Nikkiso Co Ltd Impeller fixing structure of canned motor pump
JP2002315286A (en) * 2001-04-06 2002-10-25 Nidec Shibaura Corp Pump
JP4941855B2 (en) * 2005-04-22 2012-05-30 西芝電機株式会社 Electric blower
KR100690686B1 (en) * 2005-07-23 2007-03-09 엘지전자 주식회사 Reinforced impeller rotating at high speed
JP4053563B2 (en) * 2005-12-01 2008-02-27 ファナック株式会社 Fluid machinery
IT1394295B1 (en) 2009-05-08 2012-06-06 Nuovo Pignone Spa CENTRIFUGAL IMPELLER OF THE CLOSED TYPE FOR TURBOMACCHINE, COMPONENT FOR SUCH A IMPELLER, TURBOMACCHINA PROVIDED WITH THAT IMPELLER AND METHOD OF REALIZING SUCH A IMPELLER
IT1397058B1 (en) 2009-11-23 2012-12-28 Nuovo Pignone Spa CENTRIFUGAL IMPELLER MOLD, MOLD INSERTS AND METHOD TO BUILD A CENTRIFUGAL IMPELLER
KR101055801B1 (en) * 2010-12-17 2011-08-09 한국기계연구원 Structure for fixing impeller
ITCO20110064A1 (en) 2011-12-14 2013-06-15 Nuovo Pignone Spa ROTARY MACHINE INCLUDING A ROTOR WITH A COMPOSITE IMPELLER AND A METAL SHAFT
GB201200403D0 (en) * 2012-01-10 2012-02-22 Napier Turbochargers Ltd Connector
ITCO20130067A1 (en) 2013-12-17 2015-06-18 Nuovo Pignone Srl IMPELLER WITH PROTECTION ELEMENTS AND CENTRIFUGAL COMPRESSOR
JP6631094B2 (en) * 2015-08-26 2020-01-15 株式会社Ihi Rotating machinery
US11236767B2 (en) 2016-10-07 2022-02-01 Mitsubishi Electric Corporation Electric blower, electric vacuum cleaner and hand dryer
CN112253528A (en) * 2020-09-10 2021-01-22 安徽银龙泵阀股份有限公司 Wear-resisting high strength centrifugal pump impeller

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014196214A1 (en) * 2013-06-04 2014-12-11 三菱重工業株式会社 Impeller, rotating machine, and method for assembling rotating machine
JP2014234786A (en) * 2013-06-04 2014-12-15 三菱重工業株式会社 Blower impeller, rotary machine, and assembly method of the rotary machine
US10514045B2 (en) 2013-06-04 2019-12-24 Mitsubishi Heavy Industries Compressor Corporation Impeller, rotating machine, and method for assembling rotating machine

Also Published As

Publication number Publication date
JPH0763193A (en) 1995-03-07

Similar Documents

Publication Publication Date Title
JP3129587B2 (en) Centrifugal low-temperature compressor impeller mounting structure
KR960002024B1 (en) Impeller wheel lock in a drive assembly
US6443710B1 (en) Magnetic pump
US3019039A (en) Means for mounting a body on a rotating shaft
JP4339782B2 (en) Fixing device for fixing the impeller to the shaft
KR100937901B1 (en) Oil-free turbocharger assembly
EP3798434B1 (en) Exhaust turbo supercharger
US7008191B2 (en) Compressor wheel assembly
JP2006097585A (en) Mounting structure for air separator and gas turbine provided with the same
JPH102355A (en) Fan and fan drive assembly
US4836750A (en) Rotor assembly
US4363631A (en) Structural arrangement for oxide ceramic shafts
EP1413765B1 (en) Compressor wheel assembly
US6663343B1 (en) Impeller mounting system and method
JPH03503563A (en) Bearing assembly with thermal compensation
JPH03151525A (en) Structure for fixing and supporting axial flow gas turbine
CN115768985A (en) Compressor comprising a drive shaft assembly and method for assembling said compressor
US5769605A (en) Sealing device for a rotary shaft
JPH08223863A (en) Axial flow fan
US3825366A (en) Assembly for centrifugal blowers and the like
JP3978978B2 (en) Spindle motor
JPH0552356U (en) Turbomachine impeller mounting device
JP3258598B2 (en) Gas turbine air separator
JP4220870B2 (en) Bearing device, compressor, and sleeve mounting method
JPH08312373A (en) Sliding bearing of variable stator blade for gas turbine

Legal Events

Date Code Title Description
FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20071117

Year of fee payment: 7

S531 Written request for registration of change of domicile

Free format text: JAPANESE INTERMEDIATE CODE: R313531

S533 Written request for registration of change of name

Free format text: JAPANESE INTERMEDIATE CODE: R313533

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20071117

Year of fee payment: 7

R350 Written notification of registration of transfer

Free format text: JAPANESE INTERMEDIATE CODE: R350

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20081117

Year of fee payment: 8

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20091117

Year of fee payment: 9

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20091117

Year of fee payment: 9

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20101117

Year of fee payment: 10

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20111117

Year of fee payment: 11

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20121117

Year of fee payment: 12

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20131117

Year of fee payment: 13

EXPY Cancellation because of completion of term