JPS59185896A - Centrifugal impeller - Google Patents

Centrifugal impeller

Info

Publication number
JPS59185896A
JPS59185896A JP6072283A JP6072283A JPS59185896A JP S59185896 A JPS59185896 A JP S59185896A JP 6072283 A JP6072283 A JP 6072283A JP 6072283 A JP6072283 A JP 6072283A JP S59185896 A JPS59185896 A JP S59185896A
Authority
JP
Japan
Prior art keywords
blade
labyrinth
groove
face
gap
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.)
Pending
Application number
JP6072283A
Other languages
Japanese (ja)
Inventor
Takashi Nagaoka
隆司 長岡
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.)
Hitachi Ltd
Original Assignee
Hitachi 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 Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP6072283A priority Critical patent/JPS59185896A/en
Publication of JPS59185896A publication Critical patent/JPS59185896A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To reduce leaking loss, by forming a suitable number of grooves in the end face of a blade which faces a shroud section in a casing so that labyrinthes are formed. CONSTITUTION:A blade 4B is formed in its end face with a groove 7 forming a labyrinth 8. With this arrangement the flow of leak is small in comparison with a blade having no groove in its end face due to the labyrinth effect by which the kinetic energy of the flow entering into the groove 7 through a gap 6 is converted into the heat energy. In order to exhibit the labyrinth effect the width (l) of the labyrinth 8 is made substantially equal to the size epsilon of the gap 6. Further, if more than two grooves 7 are formed in the end face of the balde 4B to provide a plurality of labyrinthes 8, the labyrinth effect may be moreover enhanced.

Description

【発明の詳細な説明】 〔発明の利用分野〕 本発明は遠心圧縮機、斜流圧縮機およびラジアルタービ
ンなどに用いられる開放型の遠心羽根車従来、産業用圧
縮機に用いられる遠心羽根車は第1図に示すように、石
板2、側板3およびこの両者2,3に固着された羽根4
とからなシ、この遠心羽根車1はケーシング5内に収納
されている。
[Detailed Description of the Invention] [Field of Application of the Invention] The present invention relates to an open-type centrifugal impeller used in centrifugal compressors, mixed flow compressors, radial turbines, etc. Conventionally, centrifugal impellers used in industrial compressors are As shown in FIG. 1, a stone plate 2, a side plate 3 and a blade 4 fixed to both 2 and 3.
In other words, this centrifugal impeller 1 is housed within a casing 5.

前記羽根車lは高効率の機械に好適であるが、高周速の
機械には適用することができない。
The impeller 1 is suitable for high efficiency machines, but cannot be applied to high peripheral speed machines.

このため、高周速の機械では、第2図(a)Cb)に示
すように石板1と羽根4とからなる開放型遠心羽根車I
Aが用ぬられる。この羽根車IAは側板を必要としない
が、これに代シケーシング5にシュラウド部5aを設け
る必要がある。
For this reason, in high peripheral speed machines, an open centrifugal impeller I consisting of a stone plate 1 and blades 4 is used, as shown in Fig. 2(a)Cb).
A is used. Although this impeller IA does not require a side plate, it is necessary to provide a shroud portion 5a in the shroud casing 5 instead.

遠心圧縮機の羽根車に関する損失としては、衝突損失、
摩擦損失、漏れ損失および二次流れ損失などがある。前
記漏れ損失は羽根車の羽根で区切られた隣り合う流路間
に生ずる漏れによるものでアシ、この漏れは第1図に示
す側板付羽根車1では生じない。
Losses related to centrifugal compressor impellers include collision loss,
These include friction losses, leakage losses, and secondary flow losses. The leakage loss is due to leakage occurring between adjacent flow paths separated by the blades of the impeller, and this leakage does not occur in the impeller 1 with side plates shown in FIG.

一方、第2図(a)に示す開放型羽根車IAでは、羽根
4Aの平面状先端部とケーシングのシュラウド部5aと
の間のすき間6において、第2図(b)に示すように羽
根4Aの圧力面側Xから負圧面側Yに向う漏れを生ずる
ため、漏れ損失が増加するから効率の低下を招く恐れが
ある。
On the other hand, in the open type impeller IA shown in FIG. 2(a), in the gap 6 between the planar tip of the blade 4A and the shroud part 5a of the casing, the blade 4A is Since leakage occurs from the pressure side X to the negative pressure side Y, leakage loss increases, which may lead to a decrease in efficiency.

一般的に上記漏れ損失は漏れ量に比例し、その漏れ量は
羽根4Aとケーシングシュラウド部5aとの間のすき間
6に比例する。このため前記すき間6を極力小さくする
必要があるが、そのすき間6を小さくすることは、回転
中の羽根車の変形および軸の振動などを考慮すると限界
があるので、余シ小さくすることは不可能である。
Generally, the leakage loss is proportional to the amount of leakage, and the amount of leakage is proportional to the gap 6 between the blade 4A and the casing shroud portion 5a. For this reason, it is necessary to make the gap 6 as small as possible, but there is a limit to making the gap 6 small considering deformation of the impeller during rotation, vibration of the shaft, etc., so it is not necessary to make the gap 6 small. It is possible.

〔発明の目的〕[Purpose of the invention]

本発明は上記にかんがみ、漏れ損失を低減して効率の向
上をはかることを目的とするものでおる。
In view of the above, it is an object of the present invention to reduce leakage loss and improve efficiency.

〔発明の概要〕[Summary of the invention]

本発明は上記目的を達成するために、石板と複数枚の羽
根とからなる開放型遠心羽根車において、ケーシングに
設けたシュラウド部に対向する前記羽根の端面に、任意
数の溝を設けてラビリンスを形成したことを特徴とする
ものである。
In order to achieve the above object, the present invention provides an open centrifugal impeller consisting of a stone plate and a plurality of blades, in which an arbitrary number of grooves are provided on the end surface of the blades facing a shroud portion provided in a casing. It is characterized by the formation of

〔発明の実施例〕[Embodiments of the invention]

以下本発明の実施例を図面について説明する。 Embodiments of the present invention will be described below with reference to the drawings.

第3図(a)において、2は石板、4Bは羽根で、この
羽根4Bは第3図(b)に示すように、その端面に溝7
が一個設けられてラビリンス8を形成している。5aは
ケーシング5のシュラウド部、6は前記シュラウド部5
aと羽根4Bの端面すなわちラビリンス8との間に形成
されたすき間である。
In FIG. 3(a), 2 is a stone plate, 4B is a blade, and this blade 4B has a groove 7 on its end surface, as shown in FIG. 3(b).
One is provided to form a labyrinth 8. 5a is a shroud portion of the casing 5; 6 is the shroud portion 5;
a and the end face of the blade 4B, that is, the labyrinth 8.

上記のような構成からなる羽根車IBでは、漏れ流れは
、すき間6よシ溝7内に流入する時に、運動エネルギー
が熱エネルギーに変換されるラビリンス効果によシ、羽
根端面に溝を設けない従来の羽根車IA(第2図)に比
べて減少する。しかし、前記ラビリンス8の幅tがすき
間6の大きさεに比べて大きいときには、ラビリンス効
果が減少するため、tを6と同程度の大きさにする必要
がある。
In the impeller IB having the above configuration, the leakage flow is caused by the labyrinth effect in which kinetic energy is converted into thermal energy when it flows into the groove 7 through the gap 6, so no groove is provided on the end surface of the blade. This decreases compared to the conventional impeller IA (Fig. 2). However, when the width t of the labyrinth 8 is larger than the size ε of the gap 6, the labyrinth effect is reduced, so it is necessary to make t about the same size as 6.

前記溝7の加工は、羽根の厚さがおる程度以上の羽根車
に対してのみ可能で’1=Iy、Nc加工機を用いれば
容易に加工することができる。また羽根4Bの厚みが十
分に大きい場合には、第4図に示すように羽根4Bに2
個以上の溝7を設けてラビリンス8を多数段ければ、ラ
ビリンス効果をよシ一層に向上させることができる。ざ
らに第5図に示すようにラビリンス8の圧力面側tシャ
ープなエツジに形成してもよい、。・ 〔発明の効果〕 以上説明したように本発明に呵れば、漏れ損失を低減し
て効率を向上させることができる。
The groove 7 can be formed only on an impeller whose blade thickness is at least as thick as possible, and can be easily formed using a '1=Iy, Nc processing machine. In addition, if the thickness of the blade 4B is sufficiently large, the blade 4B has two
The labyrinth effect can be further improved by providing a plurality of grooves 7 to form a large number of labyrinths 8. As roughly shown in FIG. 5, the pressure surface side of the labyrinth 8 may be formed with a sharp edge. - [Effects of the Invention] As explained above, if the present invention is applied, leakage loss can be reduced and efficiency can be improved.

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

第1図および第2図(a)は従来の側板付遠心羽根車お
よび開放型遠心羽根車の子午面断面図、第2図(b)は
同図(a)のA−A断面図、第3図(a)(b)は本発
明の遠心羽根車の一実施例全示す子午面断面図および同
(a)のB−B断面図、第4図および第5図は本発明に
係わる遠心羽根車の変形例の部分断面図である。 2・・・石板、4B・・・羽根、5・・・ケーシング、
5a・・・シュラウド部、6・・・すき間、7・・・溝
、8・・・ラビリンス。 代理人 弁理士 高橋明夫 Z 1 図 第3図 x5図 581−
Figures 1 and 2 (a) are meridional cross-sectional views of a conventional centrifugal impeller with side plates and an open type centrifugal impeller, and Figure 2 (b) is a cross-sectional view taken along line A-A in Figure (a). 3(a) and 5(b) are a meridional plane sectional view showing an embodiment of the centrifugal impeller of the present invention, and a BB sectional view of FIG. 3(a), and FIGS. It is a partial sectional view of a modification of an impeller. 2...Stone plate, 4B...Blade, 5...Casing,
5a...Shroud part, 6...Gap, 7...Groove, 8...Labyrinth. Agent Patent Attorney Akio Takahashi Z 1 Figure 3 x 5 Figure 581-

Claims (1)

【特許請求の範囲】 1、石板と複数枚の羽根とからなる開放型遠心羽根車に
おいて、ケーシングに設けたシュラウド部に対向する前
記羽根の端面に、任意数の溝を設けてラビリンスを形成
したことを特徴とする遠心羽根車。 2、前記ラビリンスの厚さを、ケーシングのシュラウド
部と羽根の前記シュラウド側端面との間のすき間取下に
形成したことを特徴とする特許請求の範囲第1項記載の
遠心羽根車。
[Claims] 1. In an open centrifugal impeller consisting of a stone plate and a plurality of blades, a labyrinth is formed by providing an arbitrary number of grooves on the end surface of the blade facing a shroud portion provided in a casing. A centrifugal impeller characterized by: 2. The centrifugal impeller as set forth in claim 1, wherein the thickness of the labyrinth is determined by the clearance between the shroud portion of the casing and the shroud side end surface of the blade.
JP6072283A 1983-04-08 1983-04-08 Centrifugal impeller Pending JPS59185896A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6072283A JPS59185896A (en) 1983-04-08 1983-04-08 Centrifugal impeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6072283A JPS59185896A (en) 1983-04-08 1983-04-08 Centrifugal impeller

Publications (1)

Publication Number Publication Date
JPS59185896A true JPS59185896A (en) 1984-10-22

Family

ID=13150449

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6072283A Pending JPS59185896A (en) 1983-04-08 1983-04-08 Centrifugal impeller

Country Status (1)

Country Link
JP (1) JPS59185896A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107580647A (en) * 2015-05-15 2018-01-12 诺沃皮尼奥内技术股份有限公司 Centrufugal compressor impeller and the compressor for including the impeller

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107580647A (en) * 2015-05-15 2018-01-12 诺沃皮尼奥内技术股份有限公司 Centrufugal compressor impeller and the compressor for including the impeller
CN107580647B (en) * 2015-05-15 2020-11-27 诺沃皮尼奥内技术股份有限公司 Centrifugal compressor impeller and compressor comprising said impeller
US11053951B2 (en) 2015-05-15 2021-07-06 Nuovo Pignone Srl Centrifugal compressor impeller and compressor comprising said impeller

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