JP2706347B2 - Radiation turbine - Google Patents

Radiation turbine

Info

Publication number
JP2706347B2
JP2706347B2 JP2070832A JP7083290A JP2706347B2 JP 2706347 B2 JP2706347 B2 JP 2706347B2 JP 2070832 A JP2070832 A JP 2070832A JP 7083290 A JP7083290 A JP 7083290A JP 2706347 B2 JP2706347 B2 JP 2706347B2
Authority
JP
Japan
Prior art keywords
scroll
radiation
divided
rotating shaft
turbine
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 - Fee Related
Application number
JP2070832A
Other languages
Japanese (ja)
Other versions
JPH03271506A (en
Inventor
栄人 松尾
圭介 園田
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP2070832A priority Critical patent/JP2706347B2/en
Publication of JPH03271506A publication Critical patent/JPH03271506A/en
Application granted granted Critical
Publication of JP2706347B2 publication Critical patent/JP2706347B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Description

【発明の詳細な説明】 産業上の利用分野 本発明は、輻流タービンに関し、具体的には、回転軸
の軸端に輻流羽根車が取付けられ、該輻流羽根車の外周
にこれを囲繞するようスクロールが設けられていると共
に、輻流羽根車の下流側にはディフューザが設けられて
なる輻流タービンの改良に係る。
Description: BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a radiation turbine, and more specifically, a radiation impeller is attached to a shaft end of a rotating shaft, and the radiation impeller is mounted on an outer periphery of the radiation impeller. The present invention relates to an improvement of a radiation turbine in which a scroll is provided so as to surround and a diffuser is provided downstream of the radiation impeller.

従来の技術 従来のこの種の輻流タービンには、第2図に示すよう
に、回転軸1の軸端に取付けられた輻流羽根車2と、該
輻流羽根車2の外周にこれを囲繞するように設けられて
いるスクロール3と、前記輻流羽根車2の下流側に設け
られているディフューザ5とを主要部材として構成され
るものがある。
2. Description of the Related Art As shown in FIG. 2, a conventional radiation turbine of this type includes a radiation impeller 2 attached to a shaft end of a rotating shaft 1 and an outer periphery of the radiation impeller 2. Some scrolls are provided so as to surround them, and the diffuser 5 provided downstream of the radiation impeller 2 is a main member.

この輻流タービンでは、流体入口よりスクロール3内
へ入った流体はスクロール3内を増速しながら流れ、大
きな周方向速度をもつ流れとなって動翼4へと入る。
In this radiation turbine, the fluid that has entered the scroll 3 from the fluid inlet flows while increasing the speed in the scroll 3 and flows into the rotor blade 4 as a flow having a large circumferential speed.

発明が解決しようとする課題 しかし、このとき、流体が軽い気体と重い液滴とで構
成されているような場合には、大きな重い液滴は加速さ
れず、気体に比べ遅い速度で流れ、動翼4と衝突すると
ともに、気体の流れに乗ることのできない数十μ以上の
液滴は、動翼の翼面に付着し、集積されて大きな液滴と
なり、スクロール3内へと遠心力によって飛ばされる。
このように常に、スクロール3と動翼4との間に一定量
の液滴が滞留し、動翼4の回転エネルギを消費し、効率
を低下させる。
However, at this time, when the fluid is composed of a light gas and heavy droplets, the large heavy droplets are not accelerated, flow at a lower speed than the gas, and move. Droplets of several tens μm or more that cannot collide with the wing 4 and cannot get on the flow of gas adhere to the wing surface of the moving blade and are accumulated as large droplets, which are blown into the scroll 3 by centrifugal force. It is.
In this way, a fixed amount of liquid droplets always stay between the scroll 3 and the moving blade 4, consuming the rotational energy of the moving blade 4 and lowering the efficiency.

さらに、多量の液滴が入ってきた場合、動翼4の回転
を低下させ、多量の液滴がディフューザ5へと流出する
ことになる。
Furthermore, when a large amount of droplets enter, the rotation of the bucket 4 is reduced, and a large amount of droplets flow out to the diffuser 5.

本発明は、このような従来技術の問題点を解決するた
めに創案されたもので、液滴による効率低下の防止と、
多量の液滴の輻流タービンへの通過の防止を図ることの
できる新規な輻流タービンを提供することを目的とす
る。
The present invention has been conceived in order to solve such problems of the prior art, and prevents the efficiency from being reduced by droplets,
It is an object of the present invention to provide a new radiant turbine capable of preventing a large amount of droplets from passing through the turbulent turbine.

課題を解決するための手段 上記目的を達成するために、本発明は、回転軸の軸端
に輻流羽根車が取付けられ、該輻流羽根車の外周にこれ
を囲繞するようスクロールが設けられている輻流タービ
ンにおいて、前記スクロールを、回転軸の軸線にほぼ直
交する方向に延びる隔壁によって2つの分割スクロール
部分に分割し、その一方の分割スクロール部分の開口部
を動翼入口の開口部とほぼ一致させ、動翼入口と重なら
ないよう回転軸の軸線方向にずれて位置する他方の分割
スクロール部分には流体入口を設け、かつ前記隔壁の内
周側には各分割スクロール部分を連通させる連通流路を
設けたことを特徴とする。
Means for Solving the Problems To achieve the above object, according to the present invention, a radiation impeller is attached to a shaft end of a rotating shaft, and a scroll is provided around the radiation impeller to surround the same. In the radiation turbine, the scroll is divided into two divided scroll portions by a partition extending in a direction substantially perpendicular to the axis of the rotating shaft, and an opening of one of the divided scroll portions is formed as an opening of a blade inlet. A fluid inlet is provided in the other divided scroll portion, which is positioned so as to be substantially coincident and is shifted in the axial direction of the rotating shaft so as not to overlap with the rotor blade inlet, and a communication is provided in which the divided scroll portion communicates with the inner peripheral side of the partition wall. A flow path is provided.

作用 上記手段において、動翼入口と重ならないよう回転軸
の軸線方向にずれて位置する他方の分割スクロール部分
に導入される流体はその分割スクロール部分での遠心力
を利用し、液滴を分離するとともに、その分割スクロー
ル部分での加速によって作り出された周方向速度を維持
したまま、連通流路を経て、一方の分割スクロール部分
内へと導かれ、さらに、動翼へと導かれる。
In the above means, the fluid introduced into the other divided scroll portion, which is shifted in the axial direction of the rotating shaft so as not to overlap with the blade entrance, utilizes the centrifugal force at the divided scroll portion to separate liquid droplets. At the same time, while maintaining the circumferential velocity created by the acceleration in the divided scroll portion, the fluid is guided into one of the divided scroll portions via the communication flow path, and further guided to the moving blade.

実施例 以下、本発明の好適な一実施例を図面を参照しながら
詳細に説明する。なお、従来のものと共通する構成要素
については同一符号を使用するものとする。
Hereinafter, a preferred embodiment of the present invention will be described in detail with reference to the drawings. Note that the same reference numerals are used for components common to those of the related art.

第1図は、本発明の輻流タービン要部の概略縦断面図
である。
FIG. 1 is a schematic longitudinal sectional view of a main part of a radiant flow turbine of the present invention.

図示するように、この輻流タービンでは回転軸1の軸
端に輻流羽根車2が取付けられ、該輻流羽根車2の外周
にこれを囲繞するようスクロール3が設けられていると
共に、輻流羽根車2の下流側にはディフューザ5が設け
られている点で従来のものと同様であるが、そのスクロ
ール3が回転軸1の軸線にほぼ直交して延びる隔壁6に
よって二分割され、その一方の分割スクロール部分7は
動翼入口8とほぼ一致するよう開口され、他方の分割ス
クロール部分9は動翼入口8と重ならないよう回転軸1
の軸線方向にずらして位置されるとともに図示しない流
体入口が設けられ、スクロール3を二分割する隔壁6に
各分割スクロール部分7,9を連通する連通流路10が設け
られている点で従来のものと異なる。この連通流路10は
隔壁6の内周側に設けられる。
As shown in the figure, in this radiation turbine, a radiation impeller 2 is attached to a shaft end of a rotating shaft 1, and a scroll 3 is provided around the radiation impeller 2 so as to surround the radiation impeller 2. Although the diffuser 5 is provided on the downstream side of the flow impeller 2 in the same manner as the conventional one, the scroll 3 is divided into two by a partition wall 6 extending substantially perpendicular to the axis of the rotating shaft 1. One of the divided scroll portions 7 is opened so as to substantially coincide with the moving blade inlet 8, and the other divided scroll portion 9 is rotated so as not to overlap with the moving blade inlet 8.
A fluid inlet (not shown) is provided at a position shifted in the axial direction, and a communication channel 10 for communicating the divided scroll portions 7 and 9 is provided in a partition wall 6 for dividing the scroll 3 into two parts. Different from the ones. The communication channel 10 is provided on the inner peripheral side of the partition 6.

従って、この実施例の輻流タービンによれば、下記の
作用を奏する。
Therefore, the radiation turbine of this embodiment has the following operations.

すなわち、図示しない流路入口から分割スクロール部
分9に導入される流体は、周方向速度を与えられるとと
もに、遠心力を利用し、液滴を分離抽出し、同時に加速
によって作り出された周方向速度を維持したまま、連通
流路10を経て、隣の分割スクロール部分7内へと導か
れ、さらに動翼入口8から動翼4へと導かれ、その動翼
4を高効率で駆動する。そして、流体はディフューザ5
の出口へと排出される。
That is, the fluid introduced into the divided scroll portion 9 from the flow path inlet (not shown) is given a circumferential velocity, and separates and extracts droplets using centrifugal force, and at the same time, generates a circumferential velocity created by acceleration. While being maintained, it is guided into the adjacent divided scroll portion 7 through the communication flow path 10 and further guided from the moving blade inlet 8 to the moving blade 4, and the moving blade 4 is driven with high efficiency. And the fluid is diffuser 5
Is discharged to the exit.

発明の効果 以上、本発明によれば、輻流羽根車の外周に二分割さ
れて設けられたスクロールの一方を輻流羽根車入口部と
ほぼ一致するように開口し、動翼入口と重ならないよう
回転軸の軸線方向にずれて位置する他方の流体入口を設
け、スクロールを二分割する隔壁の内周側を連通流路に
よって連通している構造であるから、動翼に達する前に
作動流体中に含まれた液滴の分離回収が容易となり、作
動流体中の液滴に起因する効率の低下を防止し、かつエ
ロージョン防止を図ることができる。
As described above, according to the present invention, one of two scrolls provided on the outer periphery of the radiation impeller is opened so as to substantially coincide with the entrance of the radiation impeller, and does not overlap with the blade entrance. The other fluid inlet which is shifted in the axial direction of the rotating shaft is provided so that the inner peripheral side of the partition dividing the scroll into two is communicated by the communication flow path. Separation and recovery of the liquid droplets contained therein can be facilitated, the efficiency can be prevented from lowering due to the liquid droplets in the working fluid, and erosion can be prevented.

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

第1図は本発明の実施例に係る輻流タービン要部の概略
縦断面図、第2図は従来の輻流タービン要部の概略縦断
面図である。 1……回転軸、2……輻流羽根車、3……スクロール、
4……動翼、5……ディフューザ、6……隔壁、7,9…
…分割スクロール部分、8……動翼入口、10……連通流
路。
FIG. 1 is a schematic longitudinal sectional view of a main part of a radiation turbine according to an embodiment of the present invention, and FIG. 2 is a schematic longitudinal sectional view of a principal part of a conventional radiation turbine. 1 ... rotating shaft, 2 ... radiation impeller, 3 ... scroll,
4 ... rotor blade, 5 ... diffuser, 6 ... bulkhead, 7, 9 ...
... divided scroll part, 8 ... blade entrance, 10 ... communication flow path.

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】回転軸の軸端に輻流羽根車が取付けられ、
該輻流羽根車の外周にこれを囲繞するようスクロールが
設けられている輻流タービンにおいて、前記スクロール
を、回転軸の軸線にほぼ直交する方向に延びる隔壁によ
って2つの分割スクロール部分に分割し、その一方の分
割スクロール部分の開口部を動翼入口の開口部とほぼ一
致させ、動翼入口と重ならないよう回転軸の軸線方向に
ずれて位置する他方の分割スクロール部分には流体入口
を設け、かつ前記隔壁の内周側には各分割スクロール部
分を連通させる連通流路を設けたことを特徴とする輻流
タービン。
1. A radiating impeller is attached to a shaft end of a rotating shaft,
In a radiation turbine in which a scroll is provided so as to surround the outer periphery of the radiation impeller, the scroll is divided into two divided scroll portions by a partition extending in a direction substantially perpendicular to the axis of the rotating shaft, The opening of one of the divided scroll portions is made substantially coincident with the opening of the moving blade entrance, and the other divided scroll portion which is shifted in the axial direction of the rotating shaft so as not to overlap with the moving blade entrance is provided with a fluid inlet, A radial flow turbine, wherein a communication flow path for communicating each divided scroll portion is provided on an inner peripheral side of the partition wall.
JP2070832A 1990-03-20 1990-03-20 Radiation turbine Expired - Fee Related JP2706347B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2070832A JP2706347B2 (en) 1990-03-20 1990-03-20 Radiation turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2070832A JP2706347B2 (en) 1990-03-20 1990-03-20 Radiation turbine

Publications (2)

Publication Number Publication Date
JPH03271506A JPH03271506A (en) 1991-12-03
JP2706347B2 true JP2706347B2 (en) 1998-01-28

Family

ID=13442944

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2070832A Expired - Fee Related JP2706347B2 (en) 1990-03-20 1990-03-20 Radiation turbine

Country Status (1)

Country Link
JP (1) JP2706347B2 (en)

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4027994A (en) * 1975-08-08 1977-06-07 Roto-Master, Inc. Partially divided turbine housing for turbochargers and the like
JPS6188002U (en) * 1984-11-15 1986-06-09

Also Published As

Publication number Publication date
JPH03271506A (en) 1991-12-03

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