JPS6189998A - Hydraulic machine - Google Patents

Hydraulic machine

Info

Publication number
JPS6189998A
JPS6189998A JP21126584A JP21126584A JPS6189998A JP S6189998 A JPS6189998 A JP S6189998A JP 21126584 A JP21126584 A JP 21126584A JP 21126584 A JP21126584 A JP 21126584A JP S6189998 A JPS6189998 A JP S6189998A
Authority
JP
Japan
Prior art keywords
blade
diffuser
shape
top end
heating
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
JP21126584A
Other languages
Japanese (ja)
Inventor
Kazumi Katayama
片山 一三
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 JP21126584A priority Critical patent/JPS6189998A/en
Publication of JPS6189998A publication Critical patent/JPS6189998A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To establish high efficiency over a wide flow rate varying range by forming a part of the blade on the diffuser of a shape memory alloy, controllably constituting optimum the shape of the blade with a temperature control means for it and removing the separation phenomenon. CONSTITUTION:A blade 12 of diffuser is made of a conventional metal and is constituted by coupling the top end portion 40 consisting of a shape memory alloy with the top end of the blade 12. A heating and cooling unit 14 and temperature detector 15 are buried in the blade 12 as shown in the figure and the heating and cooling are provided for the blade 12 from the exterior. According to the foregoing constitution, the shape of the top end 40 of the blade can be properly changed as shown in the solid line and broken line of the figure, therefore the shape of the blade can be controlled in optimum state, and fitted in the flowing direction toward the fluid diffuser. Thereby, high efficiency can be obtained over a wide flow rate varying range by removing the separation phenomenon, therefore the stability of the work can be improved with materization of a low cost.

Description

【発明の詳細な説明】 産業上の利用分野 本発明は、回転羽根車と、その外周に羽根を設置せるデ
ィフューザとを具備する流体機械の改良に関する。
DETAILED DESCRIPTION OF THE INVENTION Field of the Invention The present invention relates to an improvement in a fluid machine equipped with a rotary impeller and a diffuser having blades installed around its outer periphery.

従来の技術 羽根車1の外周に、これにより増速された流体の速度を
効率よ(減速させて圧力に変換するために、ディフュー
ザ3を設けている。そして、このディフューザ3の通路
内には、羽根3aを設けることにより、渦室4だけのも
のよりも数多効率を良くしている。なお、laは回転軸
、2は羽根である。
BACKGROUND ART A diffuser 3 is provided around the outer periphery of an impeller 1 in order to efficiently decelerate and convert the increased velocity of the fluid into pressure. By providing the blades 3a, the efficiency is improved compared to the case where only the vortex chamber 4 is provided.In addition, la is the rotation axis, and 2 is the blade.

発明が解決しようとする問題点 しかし、上述した羽根3a付きディフューザ3では、流
量が変化した時、効率のよい領域が狭い欠点がある。こ
れは、正規の流量よりずれると、第8図に矢印イで示す
ように、翼面には(離を生じ、高効率の範囲を狭める原
因となっている。これを防止するために、はく離を起し
難い羽根形状の研究や、羽根の取り付は角や形状を外部
より変化させる機構が考えられているが、いずれも構造
が複雑となり、信頼性が不足したり、高価な機械となっ
ている。
Problems to be Solved by the Invention However, the above-mentioned diffuser 3 with vanes 3a has a drawback that the efficient region is narrow when the flow rate changes. When the flow rate deviates from the normal flow rate, as shown by arrow A in Figure 8, separation occurs on the blade surface, which narrows the range of high efficiency. Research has been carried out on blade shapes that are less likely to cause this, and mechanisms have been considered to change the angles and shape from the outside to attach the blades, but these methods result in complicated structures, lack of reliability, and expensive machinery. ing.

そこで、本発明は、このような従来技術の問題点に鑑み
て、これを解決するためになされたもので、安価で、広
い流量範囲にわたって高効率が得られ、安定性のある新
規な遠心式の流体機械を提供することをn的とする。
Therefore, the present invention was made in view of the problems of the prior art and to solve the problems.The present invention is a novel centrifugal type that is inexpensive, has high efficiency over a wide flow range, and is stable. The objective is to provide a fluid machine of n.

問題点を解決するための手段 この目的を達成するために、本発明の流体機械では、回
転羽根車と、その外周に羽根を設置するティフユーザと
を具備する流体機械において、上記ディフューザの羽根
の全部又は一部を熱膨脹率の異なる複数の材料又は形状
記憶合金で形成すると共に、上記羽根の温度制御手段を
設けて羽根形状を最適に制御し得るよう構成したことを
特徴とする。
Means for Solving the Problems In order to achieve this object, the fluid machine of the present invention includes a rotary impeller and a tiff user that installs the blades on the outer periphery of the rotary impeller. The blade is characterized in that the blade is formed entirely or partially from a plurality of materials or shape memory alloys having different coefficients of thermal expansion, and is provided with temperature control means for the blade to optimally control the blade shape.

実施例 以下、本発明の詳細を図示する実施例を参照しながら説
明する。
EXAMPLES The present invention will now be described in detail with reference to illustrative examples.

第7図に本発明に係る流体機械の部位の構造を示す。同
図において、1は回転軸1aに取付けられた羽根車であ
り、該羽根車lの回転により、該羽根車1に取付けられ
た羽根20作用で流体に回転速度が付与される。該羽根
車1を出た流体は高速で押し出され、これを静圧に変換
するために取付けられている羽根付ディフューザ3に流
入する。
FIG. 7 shows the structure of the parts of the fluid machine according to the present invention. In the figure, reference numeral 1 denotes an impeller attached to a rotating shaft 1a, and as the impeller 1 rotates, rotational speed is imparted to the fluid by the action of the blades 20 attached to the impeller 1. The fluid exiting the impeller 1 is pushed out at high speed and flows into a vaned diffuser 3 installed to convert it into static pressure.

勿論、設計点においては、第8図に示す従来の羽根付デ
ィフューザ3においても、その羽[JJ3aの形状は流
体の流れ方向に合致するようになってし・ろ。
Of course, at the design point, even in the conventional vaned diffuser 3 shown in FIG. 8, the shape of the vanes [JJ3a] should match the flow direction of the fluid.

ところが、流量が設計点より減少した場合には、第8図
に示すように流入角が羽根方向と合致しないため、はく
離を起し所期の目的が達成できなくなることは上述した
辿りである。
However, when the flow rate decreases from the design point, as shown in FIG. 8, the inflow angle does not match the direction of the blades, so separation occurs and the intended purpose cannot be achieved, as described above.

そのため、本発明では、以下に述べる実施例に示すよう
に、上記ディ2ユーザ31を改良した。
Therefore, in the present invention, the D2 user 31 is improved as shown in the embodiment described below.

菓1図乃至第3図はその第一実施例である。Figures 1 to 3 show the first embodiment.

第1図及び第2図において、11はディフューザを構成
する側壁を示し、12は熱膨張係数の異る2種以上の金
属12a1.12a2を貼り合せて製造したディフュー
ザの羽根である。該羽根12は上記側壁11に固定され
たビン13により位置が決められている。該ビン13は
上記羽根12の肉厚内に開設せる断面長円形状の空隙部
12bを貫通しイ ており、従って、該羽根12は側壁11に対して滑動可
能となるよう隙間10が設けられている。
In FIGS. 1 and 2, reference numeral 11 indicates a side wall constituting the diffuser, and reference numeral 12 indicates a diffuser blade manufactured by bonding two or more metals 12a1 and 12a2 having different coefficients of thermal expansion. The vane 12 is positioned by a pin 13 fixed to the side wall 11. The bottle 13 passes through a gap 12b having an oval cross section and formed within the thickness of the blade 12, and therefore, a gap 10 is provided so that the blade 12 can slide against the side wall 11. ing.

そして、該羽根12の中には、第2図に示すように、加
熱冷却装置14及び羽根の温度を検出し外部に導く温度
検出装置15等が埋込まれている。
As shown in FIG. 2, embedded in the blade 12 are a heating and cooling device 14, a temperature detection device 15 that detects the temperature of the blade, and guides the temperature to the outside.

この羽根12は、前もってその温度と形状との関係を検
定してお(。今、流体の流量が変化したとすると、前述
したようなディフューザ3内の流れに乱れが発生しない
ように、前もって検定されたデーターに基づいて、該羽
根12を適当な形状にすべ(外部から加熱又は冷却する
ことにより、該羽根12の温度を制御してその形状を、
第3図の破線で示すように変形させる。
The relationship between the temperature and the shape of the blade 12 has been verified in advance. Based on the obtained data, the blade 12 is shaped into an appropriate shape (by heating or cooling from the outside, the temperature of the blade 12 is controlled to change its shape,
It is deformed as shown by the broken line in FIG.

このような手段による制御操作で羽根12の形状を常に
最適とすることにより常時最高効率の運転が可能となる
By always optimizing the shape of the blades 12 through control operations using such means, it is possible to operate at the highest efficiency at all times.

第4図は第二実施例、即ち超音速ディフューザの場合の
事例を示す。
FIG. 4 shows a second embodiment, namely the case of a supersonic diffuser.

この場合、羽根12は薄板で中空状に形成されていて、
その中空81S12cに熱膨張係数の大きい小片20が
組み込まれている。この小片20には、外部より導入さ
れる加熱又は冷却装置及び温度検出装置(図示せず)が
第1図に示す第一実施例に準する方法で組込まれている
。この超音速ディンユーザでは、流量変化に対しては、
上記加熱又は冷却装置及び温度検出装置による制御操作
で第、1図に示す如(羽根12の形状を破線又は実線に
変えて、隣辺する羽根12.12間の間隔中dを調整し
て最適にすることがその性能に大きく作用するので有効
となる。
In this case, the blade 12 is formed into a hollow thin plate,
A small piece 20 having a large coefficient of thermal expansion is incorporated into the hollow 81S12c. A heating or cooling device and a temperature detection device (not shown) introduced from the outside are incorporated into this small piece 20 in a manner similar to the first embodiment shown in FIG. With this supersonic Din user, in response to flow rate changes,
Through control operations using the heating or cooling device and the temperature detection device, as shown in FIG. This is effective because it greatly affects its performance.

第5図、第6図は第三実施例を示す。FIGS. 5 and 6 show a third embodiment.

この場合は、第5図、第6図に示すように、羽根12は
通常の金属で作られ、該羽根12の先端に形状記憶合金
を材質とする先端部4oを接合して構成される。そして
、このような羽根12に、第6図に示すように、加熱・
冷却装置14及び温度検出装置15を埋め込み、外部か
ら加熱冷却することにより、羽根先端部40の形状を第
5図L・こ示す実線と破線の如く適当に変え、流体のデ
ィフューザへの流入方向に羽根形状を合せる。
In this case, as shown in FIGS. 5 and 6, the blade 12 is made of ordinary metal, and a tip 4o made of a shape memory alloy is bonded to the tip of the blade 12. Then, such a blade 12 is heated and heated as shown in FIG.
By embedding the cooling device 14 and the temperature detection device 15 and heating and cooling them from the outside, the shape of the blade tip 40 can be changed appropriately as shown in FIG. Match the blade shape.

発明の効果 以上述べたように、要するに、本発明の九体俄械では、
回転羽根車と、その外周に羽根を付設すろディフューザ
とを具備する流体機械において。
Effects of the Invention As stated above, in short, the nine-body machine of the present invention has the following effects:
In a fluid machine equipped with a rotary impeller and a diffuser with blades attached to the outer periphery of the impeller.

上記ディフューザの羽根の全部又は一部を熱j影脹率の
異なる複数の材料又は形状記憶合金で形成すると共に、
上記羽根の温度制御手段を設け、その羽根の形状を最適
に制御し得るよう構成したので、は(雅の現象を除去し
て広い流澄袈動範囲にわたって高効率が得られ、もって
、作業の安定性が向上し、しかも、安価に製造できるの
である。
All or part of the blades of the diffuser are formed of a plurality of materials or shape memory alloys having different thermal expansion coefficients, and
By providing temperature control means for the blades and arranging the configuration to optimally control the shape of the blades, high efficiency can be obtained over a wide flow range by eliminating the phenomenon of elegance, thereby improving work efficiency. It has improved stability and can be manufactured at low cost.

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

第1図乃至第3、図は本発明の流体機械の第一実施例を
示し、第1図はディフューザ羽根の断面図、第2図は第
1図の■−■線断面図、第3図は同上ディフューザ羽根
の作用の説明図である。第4図は本発明の流体機械の第
二実施例であるディフューザ羽根の断面図であり、第5
図及び第6図は本発明の流体機械の第三実施例を示し、
その第5図はディフューザ羽根の断面図、第6図は第5
図のVl−vt線断面図である。第7図及び第8図は従
来の流体機械の実施例を示し、その第7図はその一部縦
断面図、第8図は第7図の■−画線断面図である。 11・・ディフューザを構成する側壁、12・・ティフ
ユーザの羽根、13−・ビン、1・1・・加熱・冷却装
置、15・・温度検出装置、2o・・小片、40・・形
状記憶合金。 復代理人 木 村 正 巳 (ほか7名) 第1図 第3図 第4図 第5図 第6図 第7図
1 to 3 show a first embodiment of the fluid machine of the present invention, FIG. 1 is a sectional view of a diffuser blade, FIG. 2 is a sectional view taken along the line ■-■ in FIG. 1, and FIG. FIG. 2 is an explanatory diagram of the function of the diffuser blade as above. FIG. 4 is a sectional view of a diffuser blade which is a second embodiment of the fluid machine of the present invention, and
The figure and FIG. 6 show a third embodiment of the fluid machine of the present invention,
Figure 5 is a cross-sectional view of the diffuser blade, and Figure 6 is a cross-sectional view of the diffuser blade.
It is a sectional view taken along the line Vl-vt in the figure. 7 and 8 show an embodiment of a conventional fluid machine, of which FIG. 7 is a partial longitudinal cross-sectional view, and FIG. 8 is a cross-sectional view taken along the line --- in FIG. 7. 11... Side wall constituting the diffuser, 12... Blade of the tiff user, 13-... Bottle, 1.1... Heating/cooling device, 15... Temperature detection device, 2o... Small piece, 40... Shape memory alloy . Sub-agent Masami Kimura (and 7 others) Figure 1 Figure 3 Figure 4 Figure 5 Figure 6 Figure 7

Claims (1)

【特許請求の範囲】[Claims] 回転羽根車と、その外周に羽根を付設するディフューザ
とを具備する流体機械において、上記ディフューザの羽
根の全部又は一部を熱膨脹率の異なる複数の材料又は形
状記憶合金で形成すると共に、上記羽根の温度制御手段
を設け、羽根形状を最適に制御し得るよう構成した流体
機械。
In a fluid machine equipped with a rotary impeller and a diffuser having blades attached to its outer periphery, all or part of the blades of the diffuser are formed of a plurality of materials or shape memory alloys having different coefficients of thermal expansion, and A fluid machine equipped with temperature control means and configured to optimally control the blade shape.
JP21126584A 1984-10-11 1984-10-11 Hydraulic machine Pending JPS6189998A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP21126584A JPS6189998A (en) 1984-10-11 1984-10-11 Hydraulic machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP21126584A JPS6189998A (en) 1984-10-11 1984-10-11 Hydraulic machine

Publications (1)

Publication Number Publication Date
JPS6189998A true JPS6189998A (en) 1986-05-08

Family

ID=16603049

Family Applications (1)

Application Number Title Priority Date Filing Date
JP21126584A Pending JPS6189998A (en) 1984-10-11 1984-10-11 Hydraulic machine

Country Status (1)

Country Link
JP (1) JPS6189998A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7913928B2 (en) * 2005-11-04 2011-03-29 Alliant Techsystems Inc. Adaptive structures, systems incorporating same and related methods
CN110088481A (en) * 2016-12-21 2019-08-02 沙特阿拉伯石油公司 Centrifugal pump with adaptive pump stage
US11591899B2 (en) 2021-04-05 2023-02-28 Saudi Arabian Oil Company Wellbore density meter using a rotor and diffuser

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7913928B2 (en) * 2005-11-04 2011-03-29 Alliant Techsystems Inc. Adaptive structures, systems incorporating same and related methods
US8534570B2 (en) 2005-11-04 2013-09-17 Alliant Techsystems Inc. Adaptive structures, systems incorporating same and related methods
CN110088481A (en) * 2016-12-21 2019-08-02 沙特阿拉伯石油公司 Centrifugal pump with adaptive pump stage
US11268519B2 (en) 2016-12-21 2022-03-08 Saudi Arabian Oil Company Centrifugal pump with adaptive pump stages
US11268520B2 (en) 2016-12-21 2022-03-08 Saudi Arabian Oil Company Centrifugal pump with adaptive pump stages
US11591899B2 (en) 2021-04-05 2023-02-28 Saudi Arabian Oil Company Wellbore density meter using a rotor and diffuser

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