JP3075071B2 - Impeller for centrifugal compressor - Google Patents

Impeller for centrifugal compressor

Info

Publication number
JP3075071B2
JP3075071B2 JP06080659A JP8065994A JP3075071B2 JP 3075071 B2 JP3075071 B2 JP 3075071B2 JP 06080659 A JP06080659 A JP 06080659A JP 8065994 A JP8065994 A JP 8065994A JP 3075071 B2 JP3075071 B2 JP 3075071B2
Authority
JP
Japan
Prior art keywords
blade
impeller
thin plate
hub
mounting portion
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
JP06080659A
Other languages
Japanese (ja)
Other versions
JPH07286597A (en
Inventor
英雅 生越
和夫 相沢
謙年 林
俊明 大塚
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.)
JFE Engineering Corp
Original Assignee
JFE Engineering Corp
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 JFE Engineering Corp filed Critical JFE Engineering Corp
Priority to JP06080659A priority Critical patent/JP3075071B2/en
Publication of JPH07286597A publication Critical patent/JPH07286597A/en
Application granted granted Critical
Publication of JP3075071B2 publication Critical patent/JP3075071B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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、遠心式圧縮機等の高
速回転用のインペラ(羽根車)に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a high-speed rotating impeller such as a centrifugal compressor.

【0002】[0002]

【従来の技術】海水の淡水化プラント等では、減圧下で
水蒸気等の蒸気を蒸発させて圧縮することにより、塩分
等の不純物を除去する蒸気圧縮方式の設備が設置される
ことがある。この場合、蒸気の圧縮には遠心式圧縮機が
用いられる。例えば、特開昭60−62539号公報記
載の技術は、真空容器から水蒸気を取り出すのに遠心式
圧縮機を用いている。また、雑誌「化学工場」25巻第
1号p.86〜92記載の技術は、「ステンレス性可撓
性刃翼からなる特殊な圧縮機」を用いている。
2. Description of the Related Art In a seawater desalination plant or the like, a steam compression system for removing impurities such as salts by vaporizing steam such as steam under reduced pressure may be installed. In this case, a centrifugal compressor is used for compressing the steam. For example, the technique described in Japanese Patent Application Laid-Open No. Sho 60-62539 uses a centrifugal compressor to extract water vapor from a vacuum vessel. Also, the magazine “Chemical Factory”, Vol. 25, No. 1, p. The technique described in 86 to 92 uses a "special compressor made of stainless steel flexible blades".

【0003】減圧下での水蒸気の比容積は、例えば4.
6Torrで206.3m3 /kgであり、大気圧での
比容積1.673m3 /kgの約123倍もの容積を占
めることになる。そのため、質量流量が少なくても風量
としてはかなり大きくなる。その結果、遠心式圧縮機の
インペラの径は大きくなり、かつ、回転速度も大きい。
例えば、質量流量1000kg/h、入口圧力4.2t
orr、出口圧力7.5torrの場合、インペラの仕
様は、風量3730m3 /min、インペラの径148
7mm、回転数4817rpmとなる。この時、インペ
ラの周速は375m/sとなる。
The specific volume of water vapor under reduced pressure is, for example, 4.
Was 206.3m 3 / kg at 6 Torr, will account for about 123 times the volume of the specific volume 1.673m 3 / kg at atmospheric pressure. Therefore, even if the mass flow rate is small, the air volume becomes considerably large. As a result, the diameter of the impeller of the centrifugal compressor increases, and the rotation speed also increases.
For example, mass flow rate 1000 kg / h, inlet pressure 4.2 t
orr, outlet pressure 7.5 torr, impeller specifications: air volume 3730 m 3 / min, impeller diameter 148
7 mm and the number of rotations is 4817 rpm. At this time, the peripheral speed of the impeller is 375 m / s.

【0004】このような高速回転するインペラには、何
よりもまず高い比強度と靱性が要求される。比強度は、
高速回転に伴う遠心力による羽根の自重による破断を防
ぐため高いことが要求される。比強度が十分高くても、
靱性が低いと衝撃に弱くなり羽根が破壊し易くなる。羽
根の一部でも破壊すると、高速回転するインペラにおい
ては破片の衝突が一瞬の内に連鎖的に起こり、全部の羽
根の破壊に到る事故となる。
[0004] Such a high-speed rotating impeller is required first and foremost to have high specific strength and toughness. The specific strength is
It is required to be high in order to prevent the blade from being broken by its own weight due to the centrifugal force caused by the high-speed rotation. Even if the specific strength is high enough,
If the toughness is low, the blade is susceptible to impact and the blade is easily broken. If a part of the blade is destroyed, the impeller rotating at a high speed will cause a collision of fragments in a moment, resulting in an accident that destroys all the blades.

【0005】インペラには種々の構造のものがあり、通
常、知られているものは、羽根とハブとが一体削り出
し加工されたインペラ、羽根がハブに溶接されたイン
ペラ、羽根をハブの取付け部に嵌合させたインペラ等
である。
[0005] There are various types of impellers, and generally known ones are an impeller in which a blade and a hub are integrally machined, an impeller in which the blade is welded to the hub, and a blade attached to the hub. And the like.

【0006】図4は、従来技術の羽根をハブの取付け部
に嵌合させたインペラについて、羽根とハブの構造を示
す詳細図である。図中、1は羽根、2はハブ、8は孔、
9はスリット、10は取付け部、12は嵌合部をそれぞ
れ示す。羽根1は、厚板から削り出されており、羽根1
の嵌合部12が、ハブ2の取付け部10に嵌合させて、
インペラを構成するようになっている。
FIG . 4 is a detailed view showing the structure of a blade and a hub of an impeller in which a blade of the prior art is fitted to a mounting portion of a hub. In the figure, 1 is a blade, 2 is a hub, 8 is a hole,
Reference numeral 9 denotes a slit, 10 denotes a mounting portion, and 12 denotes a fitting portion. The blade 1 is cut out of a thick plate, and the blade 1
Is fitted to the mounting portion 10 of the hub 2,
It constitutes an impeller.

【0007】[0007]

【発明が解決しようとする課題】まず、羽根とハブと
が一体削り出し加工されたインペラは、羽根の部分の軽
量化が困難である。これは、インペラを削り出す前の素
材の加工度が低いため、羽根の靱性が低いことを補う必
要があり、羽根が厚くなったり、リブをつけたりするこ
とによる。この場合、素材は一般に鍛造されているが、
寸法が大きいので、圧延材等に比べて加工度が低くなる
ことは避けられない。
First, it is difficult to reduce the weight of the blade of an impeller in which the blade and the hub are integrally machined. This is because it is necessary to compensate for the low toughness of the blade because the workability of the raw material before the impeller is cut is low, and the blade is thickened or ribbed. In this case, the material is generally forged,
Since the dimensions are large, it is inevitable that the working ratio is lower than that of a rolled material or the like.

【0008】このように、一体削り出し加工されたイン
ペラは、羽根が厚くなるのでハブの部分が大型化し、軽
量化が困難となる。その結果、圧縮機の軸受けが大型化
し、運転時の機械的損失が大きくなり、モータの容量も
大きくなるなど、効率の悪い圧縮機となる。また、一体
削り出し加工するためには、大型の素材の鍛造や熱処理
が必要であり、更に大型の工作機械も必要であるから、
加工・製作が困難である。更に、当然のことながら、材
料の歩留りは最も悪い。
[0008] As described above, the impeller which has been integrally machined has thicker blades, so that the hub portion becomes larger and it is difficult to reduce the weight. As a result, the compressor becomes inefficient because the bearing of the compressor becomes large, the mechanical loss during operation increases, and the capacity of the motor also increases. In addition, in order to perform integrated machining, forging and heat treatment of a large material are required, and a large machine tool is also required.
Processing and manufacturing are difficult. In addition, of course, the material yield is the worst.

【0009】次に、羽根がハブに溶接されたインペラ
では、溶接部の靱性が低い。従って、特に靱性の高い溶
接金属を用いたり、特別な溶接方法や条件で製作する必
要があり、製造コストが増加する。しかし、溶接作業に
そのような注意を払っても、溶接部の熱影響部は一般に
組織が粗大化するので、特に羽根の付け根の部分の靱性
が低下することが多い。
Next, in the impeller in which the blades are welded to the hub, the toughness of the weld is low. Therefore, it is necessary to use a particularly high toughness weld metal or to manufacture with a special welding method and condition, and the manufacturing cost increases. However, even if such attention is paid to the welding operation, the structure of the heat-affected zone of the weld generally becomes coarse, so that the toughness particularly at the root of the blade often decreases.

【0010】最後に、羽根をハブの取付け部に嵌合さ
せたインペラは、羽根を削り出す材料に厚板を用いるこ
とができる。従って、一体削り出し加工の材料である鍛
造材に比べて材料の加工度は高いので、羽根の薄肉化即
ち軽量化が可能となる。しかし、削り出しにより羽根を
形成する必要があるので、加工のコストはやはり高く、
材料の歩留りも悪い。
Finally, in the impeller in which the blades are fitted to the mounting portion of the hub, a thick plate can be used as a material for shaving the blades. Therefore, since the degree of processing of the material is higher than that of a forged material, which is a material of the integrated machining, the blade can be made thinner, that is, lighter in weight. However, since the blades must be formed by shaving, the processing cost is still high,
The material yield is also poor.

【0011】また、一般に板厚の中央部は結晶粒度が粗
く靱性が低いが、削り出しにより羽根に形成されるのは
板厚の中央部付近の材料であり、羽根の靱性が低くなる
ことが避けられない。これについては、羽根の部分に別
途鍛造等の加工を施して対処することはできるが、羽根
を個々に鍛造加工するのはコストがかかり、現実的では
ない。
In general, the central part of the plate thickness has a coarse grain size and low toughness, but the material formed on the blade by cutting is the material near the central part of the plate thickness, and the toughness of the blade may be reduced. Unavoidable. This can be dealt with by separately performing processing such as forging on the blade portion, but it is not realistic to forge the blade individually, which is costly.

【0012】更に、羽根の嵌合部(図5の12)とハブ
の取付け部(同10)については、嵌合が緩いと運転中
の羽根のズレやガタツキが生じ、逆に嵌合がきついと取
付け部の部分手直し等が必要となる。従って、これらの
加工においては、高い加工精度(例えば許容誤差:−
0,+数10μm)が要求されることになり、これも加
工コストを押し上げる要因となっている。
Further, if the fitting of the blade (12 in FIG. 5) and the mounting portion of the hub (10) are loose, if the fitting is loose, the blade may shift or rattle during operation, and conversely, the fitting is tight. In addition, it is necessary to partially modify the mounting portion. Therefore, in these processings, high processing accuracy (for example, tolerance:-
0, + several tens of μm), which is also a factor that increases the processing cost.

【0013】この発明は、これらの問題を解決するた
め、軽量化が可能でかつ製作が容易なインペラを提供す
る。
The present invention solves these problems and provides an impeller that can be reduced in weight and that is easy to manufacture.

【0014】[0014]

【課題を解決するための手段】この発明は、外周に開口
したスリットとそれに連接して設けられた孔とからなる
取付け部を有するハブと、この取付け部に嵌合される羽
根とを備えたインペラにおいて、(イ)前記羽根は、実
質的に、棒とこの棒を内側に挟みそこを折り返し部とし
て、互いに全面が折り重ねられた薄板とからなり、
(ロ)羽根の折り返し部が前記孔に、折り重ねられた薄
板の一部が前記スリットに、それぞれ嵌合されているこ
とを特徴とする遠心式圧縮機用インペラである。
SUMMARY OF THE INVENTION The present invention comprises a hub having a mounting portion consisting of a slit opened on the outer periphery and a hole provided in connection with the slit, and a blade fitted to the mounting portion. In the impeller, (a) the blades are substantially composed of a rod and a thin plate that is sandwiched between the rods and that is a folded portion, and the entire surface of which is folded over,
(B) An impeller for a centrifugal compressor, wherein a folded portion of the blade is fitted in the hole and a part of the folded thin plate is fitted in the slit.

【0015】[0015]

【作用】一般に、薄板は、鍛造品や厚板に比べて加工度
が高いので組織が微細となっており、靱性が高い。従っ
て、羽根を薄板で製作することにより、羽根の薄肉化が
可能となる。羽根の製作については、基本的に薄板を羽
根の幅と長さに応じて切断すれば、後は曲げ加工とプレ
ス成形により製作できる。
In general, a thin plate has a higher degree of processing than a forged product or a thick plate, and therefore has a fine structure and high toughness. Therefore, the blade can be made thinner by manufacturing the blade with a thin plate. The blades can be manufactured basically by cutting a thin plate according to the width and length of the blades, and then by bending and press forming.

【0016】この羽根の折り返し部を、ハブの孔に嵌合
させると、折り返し部に挟まれた棒が変形する。これに
より、ハブの孔と羽根の折り返し部の形状の違いが吸収
される。また、ハブのスリットの寸法を、薄板の折り重
ねられた部分の厚さに合わせて加工すれば、羽根とスリ
ットとの嵌合により羽根がハブに固定される。
When the folded portion of the blade is fitted into the hole of the hub, the rod sandwiched by the folded portion is deformed. Thereby, the difference in shape between the hole of the hub and the folded portion of the blade is absorbed. Further, if the dimensions of the slit of the hub are processed in accordance with the thickness of the folded portion of the thin plate, the blade is fixed to the hub by fitting the blade with the slit.

【0017】[0017]

【実施例】図1は、発明の実施例の1つとしてインペラ
の構造を示す構造図である。図中、1は羽根、2はハ
ブ、3は回転軸、10は取付け部をそれぞれ示す。図2
は、羽根1および取付け部10の詳細図である。図中、
5は薄板、6は棒、7は接合部分、11は折り返し部、
8は孔、9はスリットをそれぞれ示す。その他の符号
は、図1と同じである。
FIG. 1 is a structural view showing the structure of an impeller as one embodiment of the present invention. In the figure, 1 is a blade, 2 is a hub, 3 is a rotating shaft, and 10 is a mounting portion. FIG.
FIG. 3 is a detailed view of the blade 1 and the mounting portion 10. In the figure,
5 is a thin plate, 6 is a bar, 7 is a joint portion, 11 is a folded portion,
Reference numeral 8 denotes a hole, and 9 denotes a slit. Other symbols are the same as those in FIG.

【0018】ここでは、棒6に丸棒を用いている。薄板
5は、折り返し部11で、丸棒6に巻き付くような形で
折り重ねられている。薄板5の合わせ面は、接合部分7
により接合されている。羽根の製作の一例を説明する。
まず、薄板をU字型に折り曲げて丸棒6を挟む。次い
で、プレス加工により薄板を折り重ね、折り返し部11
が丸棒6を挟みこむようプレス成形する。最後に、薄板
5の合わせ面を溶接等により接合する。
Here, a round bar is used as the bar 6. The thin plate 5 is folded at the folded portion 11 so as to be wound around the round bar 6. The mating surface of the thin plate 5 is
It is joined by. An example of manufacturing a blade will be described.
First, the thin plate is bent into a U-shape and the round bar 6 is sandwiched. Next, the thin plate is folded by press working,
Is press-formed so as to sandwich the round bar 6. Finally, the mating surfaces of the thin plates 5 are joined by welding or the like.

【0019】接合部分7は、この実施例では、薄板5の
合わせ面の周囲に溶接(スポット溶接)により設けられ
ているが、シーム溶接でもよい。また、接合部分は、周
囲のみに限らず全面に設けてもよい。また、接合には接
着材等を用いてもよい。
In this embodiment, the joining portion 7 is provided by welding (spot welding) around the mating surface of the thin plate 5, but may be seam welding. Further, the joining portion may be provided not only on the periphery but also on the entire surface. Further, an adhesive or the like may be used for bonding.

【0020】羽根の大半の部分(折り返し部11を除い
た部分)については、薄板を加工せずそのまま用いてい
るので靱性が高い。また、薄板を長手方向に板取りして
おけば、靱性が高くなる。
The most part of the blade (excluding the folded portion 11) has high toughness because it is used as it is without processing a thin plate. If the thin plate is cut in the longitudinal direction, the toughness is increased.

【0021】ハブの取付け部のスリット9は、切削加工
により製作する。この寸法は薄板の厚さの2倍にしてお
けば、折り重ねられた薄板を嵌合させることで、羽根を
ハブに確実に固定することができる。
The slit 9 in the mounting portion of the hub is manufactured by cutting. If this dimension is set to be twice the thickness of the thin plate, the blade can be securely fixed to the hub by fitting the folded thin plate.

【0022】ハブの取付け部の孔8の加工精度は、多少
低くてもよい。特に、折り返し部11の内側に挟まれた
棒6の強度より羽根の薄板5の強度が高ければ、羽根の
嵌合の際は棒6の断面が多少変形するので、折り返し部
11との馴染みがよくなる。これと同時に、羽根の折り
返し部の薄板がハブの取付け部の側面に均一に押しつけ
られ、嵌合部における残留応力が均一化されるので、羽
根の嵌合部が破壊しにくくなる。
The machining accuracy of the hole 8 in the mounting portion of the hub may be somewhat lower. In particular, if the strength of the thin plate 5 of the blade is higher than the strength of the rod 6 sandwiched inside the folded portion 11, the cross section of the rod 6 is slightly deformed when the blade is fitted, so that the familiarity with the folded portion 11 is improved. Get better. At the same time, the thin plate at the folded portion of the blade is pressed uniformly against the side surface of the mounting portion of the hub, and the residual stress at the fitting portion is made uniform, so that the fitting portion of the blade is less likely to break.

【0023】インペラの運転時、折り返し部11には遠
心力による引抜き力が作用するが、この力は薄板5にお
いては張力として作用する。従って、薄板の強度が高け
れば折り返し部11で破壊することはない。なお、折り
返し部の曲げ加工は冷間加工で行われるが、曲げ加工の
際に亀裂が生じなければ問題はない。通常の金属薄板で
あれば、1t曲げ(曲げ半径が板厚に等しい曲げ加工)
程度は可能であり、特に延性の低い薄板でない限り、羽
根の材料として用いることが可能である。
During the operation of the impeller, a centrifugal pull-out force acts on the folded portion 11, and this force acts on the thin plate 5 as tension. Therefore, if the strength of the thin plate is high, the thin plate is not broken at the folded portion 11. Although the bending of the folded portion is performed by cold working, there is no problem as long as no crack occurs during the bending. If it is a normal metal sheet, it is bent by 1t (bending radius is equal to the sheet thickness)
The degree is possible, and it can be used as a material for the blade unless it is a thin plate having low ductility.

【0024】遠心力による引抜き力については、従来技
術では、例えば前述の図4で説明すると、嵌合部12と
孔9の接触面に抗力が作用し、その結果、羽根1の嵌合
部12の内部に剪断応力が発生する。従って、羽根1の
嵌合部12の強度自体が高いことが必要であり、これは
嵌合部の加工を困難にする。この発明では、引抜き力は
羽根1の薄板5に張力として作用し、折り返し部11の
内側に挟まれた棒6に対して、その断面積を収縮させる
力即ち圧縮力を及ぼす。
With respect to the pulling force due to the centrifugal force, in the prior art, for example, as described with reference to FIG. A shear stress is generated in the inside. Therefore, the strength of the fitting portion 12 of the blade 1 needs to be high, which makes processing of the fitting portion difficult. In the present invention, the pull-out force acts on the thin plate 5 of the blade 1 as tension, and exerts a force, ie, a compressive force, on the rod 6 sandwiched inside the folded portion 11 to reduce its cross-sectional area.

【0025】一般に、材料の応力が、圧縮応力の場合
は、剪断応力に比べ破壊応力が高いので、棒は破壊しに
くい。実際には、棒が脆性材料でなければ即ちある程度
の延性があれば、棒が破壊することはない。従って、棒
に通常の金属棒を用いれば特に問題ない。このように、
この発明では薄板5の強度が高ければ、遠心力による引
抜き力に十分対抗できることになる。なお、棒6は、丸
棒でなく多角形でもよく、中空の管でもよい。
In general, when the stress of the material is the compressive stress, the breaking stress is higher than the shearing stress. In practice, the bar will not break if the bar is not a brittle material, ie if it has some ductility. Therefore, there is no particular problem if a normal metal bar is used as the bar. in this way,
In the present invention, if the strength of the thin plate 5 is high, it is possible to sufficiently counter the pulling force due to the centrifugal force. The rod 6 may be not a round bar but a polygon, and may be a hollow tube.

【0026】このように、この発明では、強度の高い薄
板と延性のある棒を組み合わせることにより、嵌合部も
含めて高い強度でかつ取付け部によく嵌合する羽根を得
ることができる。なお、薄板5の材料は、アルミ、チタ
ン、又はこれらの合金等、軽量で強度の高いものが望ま
しい。また、これらは、耐蝕性等用途に応じて選択する
のは言うまでもない。
As described above, according to the present invention, by combining a thin plate having high strength and a ductile rod, it is possible to obtain a blade having high strength including the fitting portion and well fitting to the mounting portion. The material of the thin plate 5 is desirably a lightweight and strong material such as aluminum, titanium, or an alloy thereof. Needless to say, these are selected according to the use such as corrosion resistance.

【0027】図3は、別の実施例を示す図である。ここ
では、羽根1を構成する薄板5を折り曲げて、羽根の剛
性を高くしている。
FIG . 3 is a diagram showing another embodiment. Here, the thin plate 5 constituting the blade 1 is bent to increase the rigidity of the blade.

【0028】[0028]

【発明の効果】靱性が高い薄板を用いるので、羽根の薄
肉化が可能である。その結果、インペラ全体を軽量化で
きる。また、羽根の切削加工が不要なため、材料の歩留
りが飛躍的に向上するとともに、製作・加工が容易であ
る。
As described above, since a thin plate having high toughness is used, the blade can be made thinner. As a result, the weight of the entire impeller can be reduced. Further, since the cutting of the blade is not required, the yield of the material is remarkably improved, and the production and processing are easy.

【0029】ハブの取付け部に羽根の折り返し部を嵌合
させると、折り返し部の内側に挟まれた棒が変形して形
状の違いを吸収するので、ハブの取付け部の加工精度を
特に高くしなくても容易に実施できる。
When the folded portion of the blade is fitted to the mounting portion of the hub, the rod sandwiched inside the folded portion is deformed to absorb the difference in shape, so that the machining accuracy of the mounting portion of the hub is particularly increased. It can be easily implemented without it.

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

【図1】実施例の1つのインペラの構造を示す構造図。FIG. 1 is a structural diagram showing the structure of one impeller of an embodiment.

【図2】羽根1および取付け部10の詳細図。FIG. 2 is a detailed view of a blade 1 and a mounting portion 10;

【図3】別の実施例を示す図。 FIG. 3 is a diagram showing another embodiment.

【図4】従来の技術における羽根1および取付け部10
の詳細図
FIG. 4 shows a blade 1 and a mounting portion 10 according to the prior art .
Detailed view of .

【符号の説明】[Explanation of symbols]

1 羽根 2 ハブ 5 薄板 6 棒 8 孔 9 スリット 10 取付け部 11 折り返し部 DESCRIPTION OF SYMBOLS 1 Blade 2 Hub 5 Thin plate 6 Rod 8 Hole 9 Slit 10 Mounting part 11 Folding part

───────────────────────────────────────────────────── フロントページの続き (72)発明者 大塚 俊明 東京都千代田区丸の内一丁目1番2号 日本鋼管株式会社内 (56)参考文献 特公 昭32−6801(JP,B1) 実公 昭49−1042(JP,Y1) (58)調査した分野(Int.Cl.7,DB名) F04D 29/30 F04D 17/10 ──────────────────────────────────────────────────続 き Continuing from the front page (72) Inventor Toshiaki Otsuka 1-2-1 Marunouchi, Chiyoda-ku, Tokyo Inside Nippon Kokan Co., Ltd. (56) References: Japanese Patent Publication No. 32-6801 (JP, B1) −1042 (JP, Y1) (58) Fields investigated (Int. Cl. 7 , DB name) F04D 29/30 F04D 17/10

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 外周に開口したスリットとそれに連接し
て設けられた孔とからなる取付け部を有するハブと、こ
の取付け部に嵌合される羽根とを備えたインペラにおい
て、 (イ)前記羽根は、実質的に、棒とこの棒を内側に挟み
そこを折り返し部として、互いに全面が折り重ねられた
薄板とからなり、 (ロ)羽根の折り返し部が前記孔に、折り重ねられた薄
板の一部が前記スリットに、それぞれ嵌合されているこ
とを特徴とする遠心式圧縮機用インペラ。
1. An impeller provided with a hub having a mounting portion comprising a slit opened on the outer periphery and a hole provided in connection with the slit, and a blade fitted into the mounting portion, wherein: is substantially as therein folded portion sandwiched the rod inside the rod consists of a thin plate entirely has been folded together, (b) the folded portion is the hole in the blade, folded sheet metal A part of the impeller for a centrifugal compressor is fitted in each of the slits.
JP06080659A 1994-04-19 1994-04-19 Impeller for centrifugal compressor Expired - Lifetime JP3075071B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP06080659A JP3075071B2 (en) 1994-04-19 1994-04-19 Impeller for centrifugal compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP06080659A JP3075071B2 (en) 1994-04-19 1994-04-19 Impeller for centrifugal compressor

Publications (2)

Publication Number Publication Date
JPH07286597A JPH07286597A (en) 1995-10-31
JP3075071B2 true JP3075071B2 (en) 2000-08-07

Family

ID=13724496

Family Applications (1)

Application Number Title Priority Date Filing Date
JP06080659A Expired - Lifetime JP3075071B2 (en) 1994-04-19 1994-04-19 Impeller for centrifugal compressor

Country Status (1)

Country Link
JP (1) JP3075071B2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2041398A2 (en) * 2006-06-19 2009-04-01 I.D.E. Technologies Ltd. Rotor for a compressor
CN104481929B (en) * 2014-11-20 2016-08-17 余姚天超通风设备有限公司 A kind of cross-flow fan impeller automatic inserting apparatus of assembling blade

Also Published As

Publication number Publication date
JPH07286597A (en) 1995-10-31

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