JPH04132898A - Diagonal flow impeller - Google Patents

Diagonal flow impeller

Info

Publication number
JPH04132898A
JPH04132898A JP24993490A JP24993490A JPH04132898A JP H04132898 A JPH04132898 A JP H04132898A JP 24993490 A JP24993490 A JP 24993490A JP 24993490 A JP24993490 A JP 24993490A JP H04132898 A JPH04132898 A JP H04132898A
Authority
JP
Japan
Prior art keywords
blade
core plate
impeller
rotor
outer diameter
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
JP24993490A
Other languages
Japanese (ja)
Inventor
Haruo Miura
治雄 三浦
Yasuo Fukushima
康雄 福島
Hideo Nishida
秀夫 西田
Hiromi Kobayashi
博美 小林
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 JP24993490A priority Critical patent/JPH04132898A/en
Publication of JPH04132898A publication Critical patent/JPH04132898A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To reduce the occurrence of a trouble owing to contact of the blade of an impeller with other member, such as a casing, during assembly and disassembly in a state to mount an impeller to a rotor by increasing the outside diameter of the core plate of the impeller to a value higher than the maximum outside diameter of the tip part on the outlet side of the impeller. CONSTITUTION:An outside diameter Da of a core plate 1a of an impeller 1 is increased to a value higher than a maximum outside diameter Db of the end part on the outlet side of a blade 1b. As a result, even in the case of a diagonal flow impeller wherein the impellers 1 are mounted in a multistage on a single rotor 2, a gap (g) is ensured between the blade 1b having low rigidity and other member 8, such as a casing, during assembly and disassembly, and contact is decreased. This constitution reduces the occurrence of a trouble, such as deformation, breakage, and the damage of the blade 1b, owing to contact between the blade 1b and the other member.

Description

【発明の詳細な説明】 [産業上の利用分野] 本発明は、羽根車入口で軸方向に流入した流体を1羽根
卓出口で軸方向に傾斜させて流出させる斜流羽根車に係
り、特にケーシングへの羽根車の組み付け時や分解時等
に際して1羽根の変形、破損や損傷等のトラブルを少な
くするために好適な斜流羽根車に関する。
[Detailed Description of the Invention] [Industrial Application Field] The present invention relates to a mixed-flow impeller in which fluid that has flowed in in the axial direction at the impeller inlet is inclined in the axial direction at the single blade outlet and flows out, and in particular, The present invention relates to a mixed flow impeller suitable for reducing troubles such as deformation, breakage, and damage to one blade when assembling or disassembling the impeller to a casing.

[従来の技術] この種斜流羽根車の従来技術としては、実開昭60−3
4593号公報、「産業機械(昭和38年4月号の第2
9頁、同52年8月号の第13頁)」、「神戸製鋼技報
(第38巻 第2号(昭和63年発行)第61頁)」に
記載されている技術がある。
[Prior art] As a conventional technology for this type of mixed flow impeller, there is a
Publication No. 4593, “Industrial Machinery (April 1963 Issue No. 2)
9, page 13 of the August 1952 issue) and "Kobe Steel Technical Report (Volume 38, No. 2 (published in 1988), page 61)".

前記実開昭60−34593号公報に記載されている従
来技術では、羽根の出口側先端部の外径が心板の外径と
同一に形成されている。
In the prior art described in the above-mentioned Japanese Utility Model Application Publication No. 60-34593, the outer diameter of the outlet end of the blade is formed to be the same as the outer diameter of the core plate.

一方、前掲産業機械および神戸製鋼技報に記載されてい
る従来技術では、そのいずれも羽根の出口側先端部が、
心板側はこの心板の外径と同じ外径に形成され、心板の
反対側は心板の外径よりも大きい外径に形成されている
On the other hand, in the industrial machinery mentioned above and the conventional technology described in the Kobe Steel Technical Report, the tip of the blade on the exit side is
The core plate side is formed to have the same outer diameter as the core plate, and the opposite side of the core plate is formed to have a larger outer diameter than the core plate.

[発明が解決しようとする課題] ところで、前記実開昭60−34593号公報に記載さ
れている技術のように、羽根の出口側端部の外径を、心
板の外径と同一に形成すると、次のような問題がある。
[Problems to be Solved by the Invention] By the way, as in the technique described in the above-mentioned Japanese Utility Model Publication No. 60-34593, the outer diameter of the outlet end of the blade is formed to be the same as the outer diameter of the core plate. Then, the following problem arises.

すなわち1羽根間の平均ピッチをW、羽根の長さをLと
するとき、心板の反対側における羽根の出口側先端部の
弦節比L/Wが、心板側における羽根の出口側先端部の
弦節比L/Wよりも小さくなる。このようになると、羽
根車内の速度ひずみが大きくなり、そのため羽根車の出
口流れのひずみも大きくなるので、羽根車効率やデイフ
ユーザ効率が低くなる。
In other words, when the average pitch between one blade is W and the length of the blade is L, the chord ratio L/W of the exit side tip of the blade on the opposite side of the core plate is the exit side tip of the blade on the core plate side. It becomes smaller than the chord ratio L/W of the section. In this case, the velocity distortion within the impeller increases, and therefore the distortion of the flow at the exit of the impeller also increases, resulting in a decrease in impeller efficiency and differential user efficiency.

そこで、前掲産業機械および神戸製鋼技報に記載されて
いる従来技術では、第6図に示すように、羽根車11の
羽根11bの出口側端部の形状を、心板11aの反対側
から各板11a側に向かって下り勾配に形成している。
Therefore, in the prior art described in the above-mentioned industrial machinery and Kobe Steel technical report, as shown in FIG. It is formed with a downward slope toward the plate 11a side.

なお、第6図中、12はロータ、13゜14はダイアフ
ラム、15はデイフユーザである。
In addition, in FIG. 6, 12 is a rotor, 13° and 14 are diaphragms, and 15 is a differential user.

しかし、第6図に示すように、羽根11bの出口側先端
部の最大外径を、心板11aの外径よりも大きくすると
、次のような問題がある。
However, as shown in FIG. 6, when the maximum outer diameter of the outlet end of the blade 11b is made larger than the outer diameter of the core plate 11a, the following problem occurs.

すなわち、ロータに羽根車を取り付けた斜流羽根車のケ
ーシングへの組み付け時、または保守の際の分解時等に
、突出している羽根の先端部がケーシング等の他の部材
に接触しやすい。羽根の先端部は、最も剛性が小さいた
め、羽根の先端部が他の部材に接触すると、羽根が変形
、破損や損傷する等のトラブルが生じやすい。
That is, when assembling a mixed flow impeller in which the impeller is attached to a rotor to a casing or disassembling it for maintenance, the protruding tips of the blades tend to come into contact with other members such as the casing. The tips of the blades have the lowest rigidity, so if the tips of the blades come into contact with other members, problems such as deformation, breakage, or damage to the blades are likely to occur.

また、従来技術では羽根の出口側先端部の最大外径を、
心板の外径と等しく、または心板の外径より大きくして
いるので、第7図に示すように、心板11aに対して羽
根11bの出口側先端部の付け根部分で円弧面で連接す
ることができない。したがって、羽根11bの付け根部
分、すなわち第7図に示す鋭角のA部分に応力が集中し
、疲労破壊を起こしやすい問題もある。
In addition, in the conventional technology, the maximum outer diameter of the tip of the blade on the exit side is
The outer diameter of the blade 11b is equal to or larger than the outer diameter of the core plate, so as shown in FIG. Can not do it. Therefore, there is a problem that stress is concentrated at the root portion of the blade 11b, that is, the acute angle A portion shown in FIG. 7, and fatigue failure is likely to occur.

本発明の第1の目的は、ロータに羽根車を取り付けた状
態で、ケーシングへの組み付け時、および分解時等に際
して、羽根車の羽根と、ケーシング等の他の部材との接
触によるトラブルを少なくし得る斜流羽根車を提供する
ことにある。
A first object of the present invention is to reduce troubles caused by contact between the blades of the impeller and other members such as the casing when assembling the impeller to the casing or disassembling the rotor. The object of the present invention is to provide a mixed flow impeller that can perform mixed flow.

本発明の第2の目的は、羽根車効率およびデイフユーザ
効率を高めることができ、かつ羽根車の羽根の強度を補
強し得る斜流羽根車を提供することにある。
A second object of the present invention is to provide a mixed flow impeller that can improve impeller efficiency and diff user efficiency, and can strengthen the strength of the impeller blades.

本発明の第3の目的は、羽根車間のピッチ、ロータのス
パンやロータの軸受間距離を短縮し得る斜流羽根車を提
供することにある。
A third object of the present invention is to provide a mixed flow impeller that can shorten the pitch between the impellers, the span of the rotor, and the distance between the bearings of the rotor.

[課題を解決するための手段] 前記第1の目的は、少なくとも心板と羽根とを有する羽
根車の、前記心板の外径を羽根の出口側先端部の最大外
径よりも大きく形成したことにより、達成される。
[Means for Solving the Problems] The first object is to provide an impeller having at least a core plate and a blade, the outer diameter of the core plate being larger than the maximum outer diameter of the outlet side tip of the blade. This is achieved by:

前記第2の目的は、前記羽根の出口側先端部を、心板の
反対側から心板側に向かって下り勾配に傾斜させて形成
するとともに、前記羽根の出口側先端部における付け根
部分を、該付け根部分の厚さよりも曲率の大きい円弧面
で心板に連接したことにより、達成される。
The second object is to form the outlet end of the blade so as to be inclined downwardly from the opposite side of the core plate toward the core plate, and to form a root portion of the outlet end of the blade, This is achieved by connecting to the core plate with an arcuate surface having a larger curvature than the thickness of the root portion.

前記第3の目的は、前記心板におけるロータの軸方向と
子午面とにそれぞれ直角な面に対する傾き角を、ロータ
側から羽根の付け根付近までの傾き角よりも、羽根の付
け根付近から心板の出口側端部までの傾き角を小さく形
成したことにより、達成される。
The third purpose is to increase the inclination angle of the core plate with respect to a plane perpendicular to the axial direction of the rotor and the meridian plane, respectively, from the vicinity of the blade root to the core plate, rather than the inclination angle from the rotor side to the vicinity of the blade root. This is achieved by forming a small inclination angle to the outlet side end.

[作用] 本発明の請求項1記載の発明では、心板の外径を羽根の
出口側先端部の最大外径よりも大きく形成している。そ
の結果、単一のロータに羽根車を多段に取り付けた斜流
羽根車であっても、組み立て時や分解時等に際して、剛
性が小さい羽根と、ケーシング等の他の部材との接触を
少なくすることができる。したがって、羽根と他の部材
との接触による羽根の変形、破損や損傷等のトラブルを
少なくすることができる。
[Function] In the invention as set forth in claim 1 of the present invention, the outer diameter of the core plate is formed to be larger than the maximum outer diameter of the tip end on the exit side of the blade. As a result, even with mixed flow impellers in which impellers are mounted in multiple stages on a single rotor, contact between the less rigid blades and other components such as the casing is reduced during assembly or disassembly. be able to. Therefore, troubles such as deformation, breakage, and damage of the blade due to contact between the blade and other members can be reduced.

本発明の請求項2記載の発明では、羽根の出口側先端部
を、心板の反対側から心板側に向かって下り勾配に形成
している。その結果、羽根における心板の反対側の弦節
比L/Wを、羽根における心板側の弦節比L/Wに近づ
けることができる。
In the invention according to claim 2 of the present invention, the outlet side tip portion of the blade is formed in a downward slope from the side opposite to the core plate toward the core plate side. As a result, the chord ratio L/W on the side of the blade opposite to the core plate can be made closer to the chord ratio L/W on the core plate side of the blade.

したがって、羽根車内の速度ひずみが小さくなり、羽根
車の出口流れのひずみも小さくなるため、羽根車効率や
デイフユーザ効率を向上させることができる。また、こ
の請求項2記載の発明では、羽根の出口側先端部におけ
る付け根部分を、該付け根部分の厚さよりも曲率の大き
い円弧面で心板に連接している。これにより、羽根の付
け根部分の断面積を広くすることができ、この付け根部
分への応力の集中を緩和し、疲労破壊を防ぐことが可能
となる。
Therefore, the velocity distortion within the impeller is reduced, and the distortion of the flow at the outlet of the impeller is also reduced, so that impeller efficiency and differential user efficiency can be improved. Further, in the invention as set forth in claim 2, the root portion at the tip end on the outlet side of the blade is connected to the core plate by an arcuate surface having a larger curvature than the thickness of the root portion. As a result, the cross-sectional area of the root portion of the blade can be increased, and stress concentration on the root portion can be alleviated, thereby making it possible to prevent fatigue failure.

本発明の請求項3記載の発明では、心板におけるロータ
の軸方向と子牛面とに直角な面に対する傾き角を、ロー
タ側から羽根の付け根付近までの傾き角よりも、羽根の
付け根付近から心板の出口側端部までの傾き角を小さく
している。これにより、デイフユーザにおけるロータの
軸方向の寸法を短くでき、羽根車間のピッチを小さくで
き、ロータのスパンを短くでき、ロータの軸受間距離を
短くすることができる。したがって、ロータ自体の剛性
を大きくでき、軸受による回転ロータの支持安定性を大
きくすることが可能となる。
In the invention according to claim 3 of the present invention, the inclination angle of the core plate with respect to a plane perpendicular to the axial direction of the rotor and the calf surface is set closer to the root of the blade than the inclination angle from the rotor side to the vicinity of the root of the blade. The angle of inclination from the center to the outlet end of the core plate is made small. As a result, the axial dimension of the rotor in the differential user can be shortened, the pitch between the impellers can be shortened, the span of the rotor can be shortened, and the distance between the bearings of the rotor can be shortened. Therefore, the rigidity of the rotor itself can be increased, and the support stability of the rotating rotor by the bearing can be increased.

[実施例] 以下、本発明の実施例を図面により、説明する。[Example] Embodiments of the present invention will be described below with reference to the drawings.

第1図〜第3図は本発明の第1の実施例を示すもので、
第1図は斜流羽根車を子午面で切断した一部分の断面図
、第2図は第1図の一部分の拡大断面図、第3図は羽根
車の心板および羽根の出口側端部の拡大斜視図、第4図
は羽根車の組立状態における子午面での断面図であって
、第1の実施例の効果説明図である。
1 to 3 show a first embodiment of the present invention,
Figure 1 is a cross-sectional view of a portion of the mixed flow impeller taken along the meridian plane, Figure 2 is an enlarged cross-sectional view of a portion of Figure 1, and Figure 3 is a view of the core plate of the impeller and the outlet end of the blade. The enlarged perspective view and FIG. 4 are cross-sectional views taken on a meridian plane in an assembled state of the impeller, and are explanatory views of the effects of the first embodiment.

これらの図に示す第1の実施例では、第4図に示すごと
く、単一のロータ2に、これの軸方向に羽根車1が多段
に取り付けられている。
In the first embodiment shown in these figures, as shown in FIG. 4, impellers 1 are attached to a single rotor 2 in multiple stages in the axial direction thereof.

各羽根車1は、この第1の実施例では心板1aに羽根1
bを設けて構成されており、側板のない羽根車である。
In this first embodiment, each impeller 1 has blades 1 on a core plate 1a.
b, and is an impeller without side plates.

また、この羽根車1は羽根車入口で軸方向に流入した流
体を、羽根車出口で軸方向に傾斜させて流出させる斜流
羽根車である。前記羽根車1の出口には、第1図に示す
ように、ロータ2の軸方向に対向させて配置されたダイ
アフラム3゜4間にデイフユーザ5が設けられている。
Further, this impeller 1 is a mixed flow impeller in which the fluid that has flowed in in the axial direction at the impeller inlet is inclined in the axial direction and flows out at the impeller outlet. At the outlet of the impeller 1, as shown in FIG. 1, a differential user 5 is provided between diaphragms 3 and 4 arranged to face each other in the axial direction of the rotor 2.

また、ダイアフラム4と、羽根車1のボス部分またはス
ペーサとの間には、第2図に示すようにラビリンス構造
のシール部材6が配置されており、このシール部材6は
ダイアフラム4に組み付けられている。
Furthermore, a seal member 6 having a labyrinth structure is disposed between the diaphragm 4 and the boss portion or spacer of the impeller 1, as shown in FIG. There is.

前記羽根車1の心板1aの外径り、は、第2図に示すよ
うに1羽根1bの出口側先端部の最大外径Dbよりも大
きく形成されている。
As shown in FIG. 2, the outer diameter of the core plate 1a of the impeller 1 is larger than the maximum outer diameter Db of the outlet end of one blade 1b.

前記羽根1bの出口側先端部は、第2図および第3図に
示すように、心板1aの反対側から心板la側に向かっ
て下り勾配に形成され、しかも羽根1bの付け根部分が
心板1aに半径Rの比較的大きい円弧面で連接されてい
る。
As shown in FIGS. 2 and 3, the tip of the blade 1b on the outlet side is formed with a downward slope from the opposite side of the core plate 1a toward the core plate la side, and the root portion of the blade 1b is formed with a downward slope toward the core plate la side, as shown in FIGS. It is connected to the plate 1a by a relatively large circular arc surface with a radius R.

前記心板1aは、第2図に示すように、ロータ2の軸方
向と子午面とにそれぞれ直角な面に対して、ロータ2側
から羽根1bの付け根付近までの傾き角αよりも、羽根
1bの付け根付近から心板1aの出口側先端部までの傾
き角α′が小さく形成されている。
As shown in FIG. 2, the core plate 1a is larger than the inclination angle α from the rotor 2 side to the vicinity of the root of the blade 1b with respect to a plane perpendicular to the axial direction and the meridional plane of the rotor 2. The inclination angle α' from the vicinity of the base of the core plate 1b to the outlet side tip of the core plate 1a is formed small.

この第1の実施例の斜流羽根車では、第2図に示すよう
に、羽根車1の心板1aの外径り、が羽根1bの出口側
端部の最大外径Dbよりも大きく形成されている。その
結果、第4図に示すように、単一のロータ2に羽根車1
を多段に取り付けた斜流羽根車であっても、組み立て時
や分解時等に際して、剛性が小さい羽根1bと、ケーシ
ング等の他の部材8との間にギャップgを確保し、接触
を少なくすることができる。したがって、羽根1bと他
の部材との接触による羽根1bの変形、破損や損傷等の
トラブルを少なくすることができる。
In the mixed flow impeller of the first embodiment, as shown in FIG. 2, the outer diameter of the core plate 1a of the impeller 1 is larger than the maximum outer diameter Db of the outlet end of the blade 1b. has been done. As a result, as shown in FIG.
Even in the case of a mixed flow impeller in which the blades are mounted in multiple stages, a gap g is ensured between the blades 1b with low rigidity and other members 8 such as the casing to reduce contact during assembly or disassembly. be able to. Therefore, troubles such as deformation, breakage, and damage of the blade 1b due to contact between the blade 1b and other members can be reduced.

また1羽根1bの出口側先端部を、心板1aの反対側か
ら心板la側に向かって下り勾配に形成しているので、
心板1aの反対側における羽根1bの出口側先端部弦節
比L/Wを、心板la側における羽根1bの出口側先端
部の弦節比L/Wに近づけることができる。その結果、
羽根車1内の速度ひずみが小さくなり、羽根車1の出口
流れのひずみも小さくなるので、羽根車効率やデイフユ
ーザ効率を高くすることができる。また、羽根1bの出
口側先端部を心板1aに向かって下り勾配に傾けたこと
により、羽根1bの出口側先端部の最大外径Dbよりも
心板1aの外径Daを大きくしたうえで、半径Rの比較
的大きい円弧面で羽根1bの付け根部分の断面積を広く
シ、この付け根部分への応力の集中を緩和することがで
き、疲労破壊を防止することが可能となる。
In addition, since the exit side tip of one blade 1b is formed with a downward slope from the opposite side of the core plate 1a toward the core plate la side,
The chord ratio L/W of the outlet-side tip of the blade 1b on the opposite side of the core plate 1a can be brought close to the chord ratio L/W of the outlet-side tip of the blade 1b on the side of the core plate la. the result,
Since the velocity distortion within the impeller 1 is reduced and the distortion of the flow at the outlet of the impeller 1 is also reduced, impeller efficiency and differential user efficiency can be increased. In addition, by tilting the outlet side tip of the blade 1b downward toward the core plate 1a, the outer diameter Da of the core plate 1a is made larger than the maximum outer diameter Db of the outlet side tip of the blade 1b. , the cross-sectional area of the root portion of the blade 1b is widened by a circular arc surface with a relatively large radius R, and the concentration of stress on this root portion can be alleviated, making it possible to prevent fatigue failure.

さらに、心板1aをロータ2の軸方向と子午面とにそれ
ぞれ直角な面に対して、ロータ2側から羽根1bの付け
根付近までの傾き角αよりも、前記羽根1bの付け根付
近から心板1aの出口側先端部までの傾き角α′を小さ
くしているので、デイフユーザ5におけるロータ2の軸
方向の寸法Qを短くすることができる結果、羽根車1を
多段に設ける斜流羽根車の羽根車間のピッチを小さくす
ることができ、ロータ2のスパンを短くでき、ロータ2
の軸受間距離を短くすることができる。したがって、ロ
ータ2自体の剛性を大きくすることができ、ロータ2の
回転時の安定性を高めることが可能となる。
Furthermore, with respect to the planes perpendicular to the axial direction and the meridional plane of the rotor 2, the core plate 1a is tilted from the vicinity of the base of the blade 1b to the base of the blade 1b, rather than the inclination angle α from the rotor 2 side to the vicinity of the base of the blade 1b. Since the inclination angle α' up to the tip of the outlet side of 1a is made small, the axial dimension Q of the rotor 2 in the differential user 5 can be shortened, and as a result, the impeller 1 is arranged in multiple stages. The pitch between the impellers can be reduced, the span of the rotor 2 can be shortened, and the pitch between the impellers can be reduced.
The distance between the bearings can be shortened. Therefore, the rigidity of the rotor 2 itself can be increased, and the stability of the rotor 2 during rotation can be increased.

次に、第5図は第2の実施例を示すもので、子午面で切
断した要部の断面図である。
Next, FIG. 5 shows a second embodiment, and is a sectional view of the main part taken along a meridian plane.

この第2の実施例では、羽根車1が心板1aと、羽根1
bと、側板1cとで構成されている。
In this second embodiment, an impeller 1 has a core plate 1a and a blade 1.
b, and a side plate 1c.

そして、ダイアフラム3と側板1cの外周側間には、ラ
ビリンス構造のシール部材7が配置されており、このシ
ール部材7はダイアフラム3に組み付けられている。
A seal member 7 having a labyrinth structure is disposed between the diaphragm 3 and the outer peripheral side of the side plate 1c, and this seal member 7 is assembled to the diaphragm 3.

この第2の実施例では、羽根1bが側板1cにより補強
されており、側板1c側もシール部材7によりシールさ
れている。その他の構成9作用については、前記第1の
実施例と同様である。
In this second embodiment, the blade 1b is reinforced by a side plate 1c, and the side plate 1c is also sealed by a sealing member 7. The other functions of the configuration 9 are the same as those of the first embodiment.

[発明の効果] 以上説明した本発明の請求項1記載の発明によれば、少
なくとも心板と羽根とを有する羽根車の前記心板の外径
を羽根の出口側先端部の最大外径よりも大きく形成して
いる結果、単一のロータに羽根車を多段に取り付けた斜
流羽根車であっても、組み立て時や分解時等に際して、
剛性が小さい羽根と、ケーシング等の他の部材との接触
を少なくすることができ、したがって羽根と他の部材と
の接触による羽根の変形、破損や損傷等のトラブルを少
なくし得る効果がある。
[Effects of the Invention] According to the invention described in claim 1 of the present invention described above, the outer diameter of the core plate of an impeller having at least a core plate and a blade is set to be smaller than the maximum outer diameter of the outlet side tip of the blade. As a result, even with mixed flow impellers in which impellers are mounted in multiple stages on a single rotor, during assembly and disassembly, etc.
It is possible to reduce the contact between the blades having low rigidity and other members such as the casing, and therefore it is possible to reduce troubles such as deformation, breakage, and damage of the blades due to contact between the blades and other members.

また、本発明の請求項2記載の発明によれば、前記羽根
の出口側先端部を、心板の反対側から心板側に向かって
下り勾配に傾斜させて形成しており、羽根における心板
の反対側の弦節比L/Wを、羽根における心板側の弦節
比L/Wにできるだけ近づけることができるので、羽根
車内の速度ひずみが小さくなり、羽根車の出口流れのひ
ずみも小さくなるため1羽根車効率やデイフユーザ効率
を向上させ得る効果があり、しかも羽根の出口側先端部
における付け根部分を、半径Rの比較的大きい円弧面で
心板に連接しているので、羽根の付け根部分の断面積を
広くすることができ、この付け根部分への応力の集中を
緩和し、疲労破壊を防止し得る効果がある。
Further, according to the second aspect of the present invention, the outlet side tip portion of the blade is formed to be inclined downwardly from the opposite side of the core plate toward the core plate side, so that the blade has a Since the chord ratio L/W on the opposite side of the plate can be made as close as possible to the chord ratio L/W on the core plate side of the blade, velocity distortion in the impeller is reduced, and distortion in the flow at the exit of the impeller is also reduced. Because it is smaller, it has the effect of improving single impeller efficiency and differential user efficiency.Moreover, since the root part at the tip of the outlet side of the blade is connected to the core plate by a relatively large arcuate surface with a radius R, the blade The cross-sectional area of the root portion can be increased, which has the effect of alleviating the concentration of stress on the root portion and preventing fatigue failure.

さらに、本発明の請求項3記載の発明によれば、前記心
板におけるロータの軸方向と子午面とにそれぞれ直角な
面に対する傾き角を、ロータ側から羽根の付け根付近ま
での傾き角よりも、羽根の付け根付近から心板の出口側
端部までの傾き角を小さく形成しており、デイフユーザ
におけるロータの軸方向の寸法を短くでき、羽根車間の
ピッチを小さくでき、ロータのスパンを短くでき、ロー
タの軸受間距離を短くすることができるので、ロータ自
体の剛性を大きくでき、軸受による回転時ロータの支持
安定性を大きくなし得る効果がある。
Furthermore, according to the third aspect of the present invention, the inclination angle of the core plate with respect to a plane perpendicular to the axial direction of the rotor and the meridional plane, respectively, is set to be smaller than the inclination angle from the rotor side to the vicinity of the root of the blade. , the angle of inclination from near the root of the blade to the outlet end of the core plate is formed small, allowing the axial dimension of the rotor in a differential user to be shortened, the pitch between the impellers to be small, and the span of the rotor to be shortened. Since the distance between the rotor bearings can be shortened, the rigidity of the rotor itself can be increased, and the rotor can be supported with greater stability during rotation by the bearings.

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

第1図〜第3図は本発明の第1の実施例を示すもので、
第1図は斜流羽根車を子午面で切断した一部分の断面図
、第2図は第1図の一部分の拡大断面図、第3図は羽根
車の心板および羽根の出口側端部の拡大斜視図、第4図
は羽根車の組立状態における子午面での断面図であって
、第1の実施例の効果説明図、第5図は本発明の第2の
実施例を示すもので、子午面で切断した要部の断面図で
ある。 第6図は従来技術を示すもので、子午面で切断した一部
分の断面図、第7図は従来技術の説明図であって1羽根
車の出口側先端部の斜視図である。 1・・・羽根車、1a・・・心板、■b・・・羽根、 
le・・・側板、Da・・・心板の外径、Db・・・羽
根の出口側先端部の最大外径、α・・・心板におけるロ
ータ側から羽根の付け根付近までの傾き角、α・・・心
板における羽根の付け根付近から出口側先端部の傾き角
、R・・・羽根の付け根部分の円弧面の半径、2・・・
ロータ、3゜4・・・ダイアフラム、5・・・デイフユ
ーザ、8・・・斜流羽根車の他の部材、g・・・斜流羽
根車の羽根と他の部材間のギャップ。 代理人 弁理士  秋 本 正 実 ら 第 図 第 図 第 図 1−−一羽狼車 la −−−、υ板 1b−m−羽根 2−−一ロータ 3.4−−一タイアフクム 5−−−デイ7エー亨゛ 第 図 第 図
1 to 3 show a first embodiment of the present invention,
Figure 1 is a cross-sectional view of a portion of the mixed flow impeller taken along the meridian plane, Figure 2 is an enlarged cross-sectional view of a portion of Figure 1, and Figure 3 is a view of the core plate of the impeller and the outlet end of the blade. The enlarged perspective view and FIG. 4 are cross-sectional views taken on the meridian plane in the assembled state of the impeller, and are explanatory views of the effects of the first embodiment, and FIG. 5 shows the second embodiment of the present invention. , is a sectional view of the main part taken along the meridian plane. FIG. 6 shows the prior art, and is a partial cross-sectional view taken along a meridian plane, and FIG. 7 is an explanatory diagram of the prior art, and is a perspective view of the tip end on the outlet side of one impeller. 1... Impeller, 1a... Core plate, ■b... Impeller,
le: side plate, Da: outer diameter of the core plate, Db: maximum outer diameter of the tip of the exit side of the blade, α: inclination angle from the rotor side to the vicinity of the root of the blade in the core plate, α...Inclination angle from near the root of the blade on the core plate to the tip on the outlet side, R...Radius of the circular arc surface at the root of the blade, 2...
Rotor, 3° 4...Diaphragm, 5...Diffusion user, 8...Other members of the mixed flow impeller, g...Gap between the blades of the mixed flow impeller and other members. Agent Patent Attorney Tadashi Akimoto Minora Figure 1--One Wolf Car la--, υ Plate 1b-m-Blade 2--One Rotor 3.4--One Tire Fukum 5--Day 7A diagram

Claims (1)

【特許請求の範囲】 1、少なくとも心板と羽根とを有する羽根車において、
前記心板の外径を羽根の出口側先端部の最大外径よりも
大きく形成したことを特徴とする斜流羽根車。 2、前記羽根の出口側先端部を、心板の反対側から心板
側に向かって下り勾配に傾斜させて形成するとともに、
前記羽根の出口側先端部における付け根部分を、該付け
根部分の厚さよりも曲率の大きい円弧面で心板に連接し
たことを特徴とする請求項1記載の斜流羽根車。 3、前記心板におけるロータの軸方向と子午面とにそれ
ぞれ直角な面に対する傾き角を、ロータ側から羽根の付
け根付近までの傾き角よりも、羽根の付け根付近から心
板の出口側端部までの傾き角を小さく形成したことを特
徴とする請求項1または2記載の斜流羽根車。
[Claims] 1. An impeller having at least a core plate and blades,
A mixed flow impeller characterized in that the outer diameter of the core plate is larger than the maximum outer diameter of the outlet end of the blade. 2. The exit side tip portion of the blade is formed to be inclined downward from the side opposite to the core plate toward the core plate side, and
2. The mixed flow impeller according to claim 1, wherein a root portion at an outlet side tip of the blade is connected to the core plate by an arcuate surface having a larger curvature than the thickness of the root portion. 3. The inclination angle of the core plate with respect to a plane perpendicular to the axial direction of the rotor and the meridian plane, respectively, is set from the vicinity of the root of the blade to the outlet side end of the core plate, rather than the inclination angle from the rotor side to the vicinity of the root of the blade. 3. The mixed flow impeller according to claim 1, wherein the mixed flow impeller has a small inclination angle.
JP24993490A 1990-09-21 1990-09-21 Diagonal flow impeller Pending JPH04132898A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP24993490A JPH04132898A (en) 1990-09-21 1990-09-21 Diagonal flow impeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP24993490A JPH04132898A (en) 1990-09-21 1990-09-21 Diagonal flow impeller

Publications (1)

Publication Number Publication Date
JPH04132898A true JPH04132898A (en) 1992-05-07

Family

ID=17200349

Family Applications (1)

Application Number Title Priority Date Filing Date
JP24993490A Pending JPH04132898A (en) 1990-09-21 1990-09-21 Diagonal flow impeller

Country Status (1)

Country Link
JP (1) JPH04132898A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009078186A1 (en) * 2007-12-19 2009-06-25 Mitsubishi Heavy Industries, Ltd. Centrifugal compressor
WO2021117077A1 (en) * 2019-12-09 2021-06-17 三菱重工エンジン&ターボチャージャ株式会社 Impeller of centrifugal compressor, centrifugal compressor, and turbocharger

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5429722A (en) * 1977-08-09 1979-03-05 Nitto Chemical Industry Co Ltd Artificial culture soil
JPS6020598A (en) * 1983-07-13 1985-02-01 松下電器産業株式会社 High frequency multilayer conductor board

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5429722A (en) * 1977-08-09 1979-03-05 Nitto Chemical Industry Co Ltd Artificial culture soil
JPS6020598A (en) * 1983-07-13 1985-02-01 松下電器産業株式会社 High frequency multilayer conductor board

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009078186A1 (en) * 2007-12-19 2009-06-25 Mitsubishi Heavy Industries, Ltd. Centrifugal compressor
JP2009150245A (en) * 2007-12-19 2009-07-09 Mitsubishi Heavy Ind Ltd Centrifugal compressor
US8425186B2 (en) 2007-12-19 2013-04-23 Mitsubishi Heavy Industries, Ltd. Centrifugal compressor
WO2021117077A1 (en) * 2019-12-09 2021-06-17 三菱重工エンジン&ターボチャージャ株式会社 Impeller of centrifugal compressor, centrifugal compressor, and turbocharger
JPWO2021117077A1 (en) * 2019-12-09 2021-06-17
US11835057B2 (en) 2019-12-09 2023-12-05 Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. Impeller of centrifugal compressor, centrifugal compressor, and turbocharger

Similar Documents

Publication Publication Date Title
JP3462870B2 (en) Impeller for radial turbine
JPH0718436B2 (en) Steel plate intermediate casing and multi-stage pump using the intermediate casing
KR101226363B1 (en) Centrifugal compressor
JP7213141B2 (en) Double suction volute pump
US20050163610A1 (en) Diffuser for centrifugal compressor and method of producing the same
CN111412161B (en) Serial fan
JPH04132898A (en) Diagonal flow impeller
EP3828417B1 (en) Bridged stage piece
CN213981332U (en) Centrifugal fan impeller structure
JPH10131704A (en) Radial turbine impeller
JPH11125102A (en) Gas turbine stator blade
JPH0478803B2 (en)
US4676714A (en) Reversible centrifugal pump
EP3456937B1 (en) Turbocharger
JP2004353607A (en) Centrifugal compressor
CN216429989U (en) Fan of steady operation
US20230258197A1 (en) Impeller of centrifugal compressor and centrifugal compressor
JPS5853700A (en) Diffuser of pump, etc.
JP2019056344A (en) Centrifugal pump
JPS6179900A (en) Compressor housing
CN212079737U (en) Blade, impeller, fan and lampblack absorber
US11428240B2 (en) Centrifugal compressor and turbocharger including the same
US20230123100A1 (en) Impeller and centrifugal compressor
JPS6325355Y2 (en)
JPS63179101A (en) Axial flow turbine