JP2007239675A - Centrifugal blower reducing stress concentration at joint part of blade plate - Google Patents

Centrifugal blower reducing stress concentration at joint part of blade plate Download PDF

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JP2007239675A
JP2007239675A JP2006065156A JP2006065156A JP2007239675A JP 2007239675 A JP2007239675 A JP 2007239675A JP 2006065156 A JP2006065156 A JP 2006065156A JP 2006065156 A JP2006065156 A JP 2006065156A JP 2007239675 A JP2007239675 A JP 2007239675A
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stress concentration
blade plate
impeller
centrifugal blower
notch
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JP4834430B2 (en
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Hidemitsu Nagai
秀満 永井
Shigemitsu Fujii
繁満 藤井
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Teral Kyokuto Inc
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Abstract

<P>PROBLEM TO BE SOLVED: To reduce stress concentration at a joint part of a blade plate in a centrifugal blower having a backward facing impeller. <P>SOLUTION: A cut-out part having a predetermined shape is provided in an end fringe part of the blade plate in the vicinity of a connection part with a shroud to reduce stress concentration at the joint part of the blade plate. A shape of the cut-out part is composed of side wall parts being parallel for each other and a curved bottom part connecting both of side wall parts mutually. <P>COPYRIGHT: (C)2007,JPO&INPIT

Description

この発明は、各種送排気、塗装設備、集塵装置、工場等の換気設備として使用される後向き羽根車を有する遠心送風機に関する。   The present invention relates to a centrifugal blower having a rear-facing impeller that is used as a ventilation facility in various air supply / exhaust, painting facilities, dust collectors, factories, and the like.

遠心送風機の後向き羽根車は、羽根板の出口部が半径方向に向いており、羽根板の出口角度は後向き(30°〜60°)であり、入口部から出口部に向けて曲線状に成型された羽根板が、等厚の主板、側板に溶接又はリベット締めされている。さらに、主板は羽根車入口の流路を形作るように形成されたハブに溶接又はリベット締めされる。また、羽根車入口には、シュラウドと呼ばれる円環部が、羽根板の外縁部に溶接等により接続され、羽根車への空気の導入を円滑にしている。
特開2001−82383号公報 特開2000−310197号公報
The rear impeller of the centrifugal blower has the exit portion of the blade plate facing in the radial direction, the exit angle of the blade plate is facing backward (30 ° to 60 °), and is molded in a curved shape from the inlet portion to the outlet portion. The slats are welded or riveted to equal thickness main and side plates. Further, the main plate is welded or riveted to a hub formed to form a flow path at the impeller inlet. In addition, an annular portion called a shroud is connected to the outer edge of the impeller by welding or the like at the inlet of the impeller to facilitate the introduction of air into the impeller.
JP 2001-82383 A JP 2000-310197 A

前記羽根板とシュラウドとの接続部には、羽根車の回転に伴う応力集中が生じやすく、しばしば羽根板とシュラウドとの隔離又は破損が生じる。これを防止し、且つ羽根車の小型化、高性能化を図るため、各羽根板を屈曲させたり(特許文献1)、羽根板の肉厚を上げたり(特許文献2)、夫々の羽根板の中間に補強リブを追加する構成としている。しかしこの場合、羽根車の重量や材料費の増加をもたらす。また、羽根車の重量の増加は、羽根車の慣性重量の増加につながり、送風機運転時の起動時間が長くなり、汎用の電動機トルクでは起動できないという問題や、汎用の電動機過負荷保護装置では、誤作動による起動不良が発生するという問題がある。さらに、送風機を起動可能にするために、特殊な電動機や電動機過負荷保護装置を使用することで、省資源、省エネルギーの面で不経済になるという問題があった。   Stress concentration accompanying the rotation of the impeller tends to occur at the connecting portion between the blade plate and the shroud, and the blade plate and the shroud are often separated or broken. In order to prevent this and to reduce the size and performance of the impeller, each blade is bent (Patent Document 1) or the thickness of the blade is increased (Patent Document 2). It is set as the structure which adds a reinforcement rib in the middle. In this case, however, the weight and material cost of the impeller are increased. In addition, the increase in the weight of the impeller leads to an increase in the inertia weight of the impeller, the startup time during fan operation becomes longer, and the problem that it cannot be started with a general-purpose motor torque, and in the general-purpose motor overload protection device, There is a problem that starting failure occurs due to malfunction. Furthermore, there is a problem that it becomes uneconomical in terms of resource saving and energy saving by using a special motor or a motor overload protection device in order to make the blower startable.

そこでこの発明では、遠心送風機の後向き羽根車において、シュラウドとの接続部近傍の羽根板端縁部に、所定形状の切欠き部を設ける。この切欠き部の形状は、互いに平行する側壁部と、該両側壁部を互いに連結した湾曲底部とからなっており、それ自体が局部的な応力集中により、その部分から、破断が拡大したりしないような形状になっている。   Therefore, according to the present invention, in the rear impeller of the centrifugal blower, a notch portion having a predetermined shape is provided at the edge of the blade plate near the connection portion with the shroud. The shape of this notch part is composed of side wall parts parallel to each other and a curved bottom part connecting the both side wall parts to each other. It has a shape that does not.

切欠き部の深さは、羽根板とシュラウドとの接続部から切欠き部までの距離の2乃至3倍の範囲内とし、且つその湾曲底部の曲率半径は、切欠き部の応力集中係数が2.5乃至3.5の範囲内になるように決定される。また、羽根板とシュラウドとの接続部から切欠き部までの距離は、運動性能に影響を与えず、且つ羽根板とシュラウドとの接続部に作用する応力集中を軽減するように決定する。   The depth of the notch is in the range of 2 to 3 times the distance from the connecting portion between the blade and the shroud to the notch, and the curvature radius of the curved bottom is the stress concentration factor of the notch. It is determined to be within the range of 2.5 to 3.5. Further, the distance from the connection portion between the blade plate and the shroud to the cutout portion is determined so as not to affect the motion performance and to reduce the stress concentration acting on the connection portion between the blade plate and the shroud.

この発明の遠心送風機は以上のように構成したので、羽根車入口接続部分の応力の流れ込み分布が変わり、この部分への応力集中を軽減させることができる。そのために、応力集中に耐えるために羽根板の肉厚化等の検討を行う必要がなく、従来の羽根車の肉厚で十分強度を保つことができる。その結果、羽根車の軽量化により、慣性質量が低く保たれるので、起動トルクが不足したり、電動機過負荷保護装置の誤作動など、従来品に付随した問題点が解消されるほか、省エネルギーとなり、経済的効果を得ることができる。   Since the centrifugal blower of the present invention is configured as described above, the stress flow distribution at the impeller inlet connection portion is changed, and the stress concentration on this portion can be reduced. Therefore, it is not necessary to examine the thickness of the blades in order to withstand the stress concentration, and sufficient strength can be maintained with the wall thickness of the conventional impeller. As a result, the weight of the impeller keeps the inertial mass low, eliminating problems associated with conventional products such as insufficient starting torque and malfunctioning of the motor overload protection device, as well as energy savings. Thus, an economic effect can be obtained.

この発明の遠心送風機の羽根車の一実施例を図1に示す。後向き羽根車1は羽根板ブレード2、シュラウド3、インペラディスク4及びインペラハブ5とからなる。この羽根板2はシュラウド3との接合部近傍の外縁部に切欠き部6が設けられる。   One embodiment of the impeller of the centrifugal blower of the present invention is shown in FIG. The rear impeller 1 includes a blade blade 2, a shroud 3, an impeller disk 4, and an impeller hub 5. The blade 2 is provided with a notch 6 at the outer edge near the joint with the shroud 3.

切欠き部6の形状は、互いに平行する側壁部7と、該両側壁部を互いに連結した湾曲底部8とからなる。この切欠き部の基本形状、及び変形例を、図2A、B及びCに示す。切欠き深さd、及びブレードとシュラウドとの接続部から切欠き部までの距離

Figure 2007239675

については、次のような式1の関係が成り立つ。 The shape of the notch 6 includes a side wall 7 that is parallel to each other and a curved bottom 8 that connects both side walls to each other. 2A, 2B, and 2C show the basic shape of the notch and its modification. Notch depth d, and distance from blade to shroud connection to notch
Figure 2007239675

With respect to, the following equation 1 holds.

Figure 2007239675
Figure 2007239675

また、湾曲底部の曲率半径ρは、切欠き部の応力集中係数αが2.5乃至3.5の範囲内になるように決定される。ブレードとシュラウドとの入口接続部の作用応力σAと切欠き深さdとの関係を 式2に示す。但しσは、切欠きが無い場合のブレードとシュラウドとの入口接続部の作用応力を示す。 In addition, the curvature radius ρ of the curved bottom is determined so that the stress concentration coefficient α of the notch is in the range of 2.5 to 3.5. Equation 2 shows the relationship between the applied stress σA at the inlet connection between the blade and the shroud and the notch depth d. However, σ 0 indicates the acting stress at the inlet connection portion between the blade and the shroud when there is no notch.

Figure 2007239675
Figure 2007239675

切欠き深さdの影響による応力集中の軽減度合いは、応力集中軽減グラフとして図3に示す。さらに、この発明の、ブレードに所定の切り欠き部を設けた羽根車と、従来型の羽根車との応力集中の度合いを図4に示す。このように、ブレードの板厚を従来の切欠きが無い場合に比べて25〜30%程度薄くしても、ブレードとシュラウドの入口接続部分の作用応力σは、切欠きを設けることで、30〜40%軽減される。   The degree of stress concentration reduction due to the influence of the notch depth d is shown in FIG. 3 as a stress concentration reduction graph. Furthermore, FIG. 4 shows the degree of stress concentration between the impeller having a predetermined notch in the blade and the conventional impeller according to the present invention. Thus, even if the plate thickness of the blade is reduced by about 25 to 30% compared to the conventional case where there is no notch, the acting stress σ at the inlet connection portion of the blade and the shroud can be reduced to 30 by providing the notch. Reduced by ~ 40%.

この発明の送風機は以上のように構成したので、後向き羽根車を有する遠心送風機において、羽根板が、等厚の主板、側板に溶接又はリベット締めする場合、この接合部分にかかる応力集中を、比較的簡単な構成によって軽減させることができるので、比較的大型の各種送排気、塗装設備、集塵装置、工場等の換気設備として、広い用途に適用することができる。   Since the blower of the present invention is configured as described above, in the centrifugal blower having the rear impeller, when the blade plate is welded or riveted to the main plate and the side plate of equal thickness, the stress concentration applied to the joint portion is compared. Since it can be reduced by a simple configuration, it can be applied to a wide variety of uses as a relatively large variety of air supply / exhaust, painting equipment, dust collectors, factory ventilation equipment, and the like.

この発明の遠心送風機の羽根車の一実施例の見取り図である。It is a sketch of one Example of the impeller of the centrifugal blower of this invention. この発明の切欠き部の基本形状(A)、及び変形例(B),(C)を示す。The basic shape (A) of the notch part of this invention and modification (B), (C) are shown. 切欠き深さdの影響による応力集中の軽減度合いを示すグラフである。It is a graph which shows the reduction degree of the stress concentration by the influence of the notch depth d. ブレードに所定の切り欠き部を設けた羽根車と、従来型の羽根車との応力集中の度合いを比較して示すグラフである。It is a graph which compares and shows the degree of the stress concentration of the impeller which provided the predetermined notch part in the braid | blade, and the conventional impeller.

符号の説明Explanation of symbols

1 後向き羽根車
2 羽根板ブレード
3 シュラウド
4 インペラディスク
5 インペラハブ
6 切欠き部
DESCRIPTION OF SYMBOLS 1 Backward impeller 2 Blade blade 3 Shroud 4 Impeller disk 5 Impeller hub 6 Notch

Claims (2)

遠心送風機の後向き羽根車において、シュラウドとの接続部近傍の羽根板端縁部に所定形状の切欠き部を設けて、羽根板の接合部分への応力集中を低減した遠心送風機。 A centrifugal blower in which a notch having a predetermined shape is provided at a peripheral edge of a blade plate in the vicinity of a connection portion with a shroud to reduce stress concentration on a joint portion of the blade plate in a rear impeller of the centrifugal fan. 前記切欠き部の形状は、互いに平行する側壁部と、該両側壁部を互いに連結した湾曲底部とからなる、請求項1に記載の遠心送風機。 The shape of the said notch part is a centrifugal blower of Claim 1 which consists of a side wall part mutually parallel, and the curved bottom part which connected this both side wall part mutually.
JP2006065156A 2006-03-10 2006-03-10 Centrifugal blower with reduced stress concentration on the junction of the blades Active JP4834430B2 (en)

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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59211795A (en) * 1983-05-18 1984-11-30 Hitachi Ltd Impeller for centrifugal hydraulic machine
JPH0197062A (en) * 1987-10-09 1989-04-14 Canon Inc Picture processing device
JPH10306797A (en) * 1997-05-07 1998-11-17 Meidensha Corp Welding type moving blade
JP2003161107A (en) * 2001-11-22 2003-06-06 Mitsubishi Heavy Ind Ltd Partition plate structure in steam turbine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59211795A (en) * 1983-05-18 1984-11-30 Hitachi Ltd Impeller for centrifugal hydraulic machine
JPH0197062A (en) * 1987-10-09 1989-04-14 Canon Inc Picture processing device
JPH10306797A (en) * 1997-05-07 1998-11-17 Meidensha Corp Welding type moving blade
JP2003161107A (en) * 2001-11-22 2003-06-06 Mitsubishi Heavy Ind Ltd Partition plate structure in steam turbine

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