JP2011185166A - Blower fan - Google Patents

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JP2011185166A
JP2011185166A JP2010051772A JP2010051772A JP2011185166A JP 2011185166 A JP2011185166 A JP 2011185166A JP 2010051772 A JP2010051772 A JP 2010051772A JP 2010051772 A JP2010051772 A JP 2010051772A JP 2011185166 A JP2011185166 A JP 2011185166A
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connecting portion
blower fan
blades
blade
moving
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JP5095770B2 (en
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Katsunobu Hanetani
勝伸 羽谷
Osamu Sekiguchi
治 関口
Taro Tanno
太郎 旦野
Akira Higo
旭 比護
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Nidec Advanced Motor Corp
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Nidec Servo Corp
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Abstract

<P>PROBLEM TO BE SOLVED: To provide a blower fan with an impeller suppressing deterioration of impeller characteristics due to interference of an air flow generated by rotation of rotor blades with a connection part. <P>SOLUTION: The blower fan 2 includes a cylindrical cup part 10. the plurality of rotor blades 11, a motor rotating the plurality of rotor blades 11, and a housing 30. The plurality of rotor blades 11 are connected with each other by the annular connection part 12. The connection part 12 is formed at a position in 70% to 90% of the blade length from the roots of the rotor blades 11 at the outer peripheral face of the cup part 10 with respect to the blade length of the rotor blades 11 along the radial direction. Further, the housing 30 and a base part 24 are connected through a plurality of stator blades 31. The plurality of stator blades 31 are connected by a second annular connection part 32 and the second connection part 32 are arranged radially inward of the first connection part 12. <P>COPYRIGHT: (C)2011,JPO&INPIT

Description

本発明は、中心軸に沿った空気流を発生させるインペラを備えた送風ファンに関する。   The present invention relates to a blower fan provided with an impeller that generates an air flow along a central axis.

従来のいわゆる軸流ファン(送風ファン)に用いられるインペラは、円筒状のインペラカップの外周面に固定された複数の動翼が中心軸を中心に回転することによって、中心軸の方向に沿った空気流を発生させる。   An impeller used for a conventional so-called axial fan (blower fan) is arranged along the direction of the central axis by rotating a plurality of moving blades fixed to the outer peripheral surface of a cylindrical impeller cup around the central axis. Generate air flow.

ここで、インペラが回転する際、動翼には径方向の遠心力が働く。この遠心力による影響は、インペラを高速で回転させるほど顕著になる。また、前進度合が大きい動翼の場合、動翼の径方向外端が、動翼の付け根よりも回転方向前方に位置するため、動翼の各部位において発生する遠心力によって、動翼の付け根に大きなモーメントが発生する。従って、インペラは、このような遠心力による影響を考慮した強度設計が要求される。   Here, when the impeller rotates, a radial centrifugal force acts on the rotor blade. The effect of this centrifugal force becomes more pronounced as the impeller rotates at a higher speed. In addition, in the case of a moving blade with a high degree of advancement, since the radially outer end of the moving blade is positioned forward in the rotational direction from the root of the moving blade, the root of the moving blade is caused by the centrifugal force generated in each part of the moving blade. A large moment is generated. Therefore, the impeller is required to have a strength design that considers the influence of such centrifugal force.

この遠心力の影響を低減するために、複数の動翼を環状の連結部で互いに連結することによって、遠心力に対する動翼の強度を高める技術が、米国特許出願公開第2008/0056899号明細書、米国特許第6554574号明細書、米国特許第6241474号明細書等に記載されている。   In order to reduce the influence of the centrifugal force, a technique for increasing the strength of the moving blade against the centrifugal force by connecting a plurality of moving blades to each other through an annular connecting portion is disclosed in US Patent Application Publication No. 2008/0056899. U.S. Pat. No. 6,554,574 and U.S. Pat. No. 6,241,474.

一方、軸流ファンの動翼後方には旋回流が必ず生じるが、この旋回流を軸方向流に転向させる目的で、インペラを回転させるモータの支持部(ベース部)の外周面に、放射状に伸びる複数の静翼を設ける技術が知られている。しかし、この複数の静翼は、ベース部の外周面に固定されるため、ベース部の強度が低下する。そこで、複数の静翼を環状の連結部で互いに連結することによって、ベース部の強度を向上させる技術が、特開2008−261280号公報に記載されている。また、この連結部を特定の形状にすることによって、空気流の特性を変える技術が、特開2005−76590号公報に記載されている。
米国特許出願公開第2008/0056899号明細書 米国特許第6554574号明細書 米国特許第6241474号明細書 特開2008−261280号公報 特開2005−76590号公報
On the other hand, a swirl flow is always generated behind the rotor blades of the axial fan. For the purpose of turning this swirl flow into an axial flow, the swirl flow is radially formed on the outer peripheral surface of the motor support (base) that rotates the impeller. A technique for providing a plurality of stationary vanes is known. However, since the plurality of stationary blades are fixed to the outer peripheral surface of the base portion, the strength of the base portion is reduced. Therefore, Japanese Patent Application Laid-Open No. 2008-261280 discloses a technique for improving the strength of the base portion by connecting a plurality of stationary blades to each other with an annular connecting portion. Japanese Patent Laying-Open No. 2005-76590 discloses a technique for changing the characteristics of the air flow by making the connecting portion into a specific shape.
US Patent Application Publication No. 2008/0056899 US Pat. No. 6,554,574 US Pat. No. 6,241,474 JP 2008-261280 A JP 2005-76590 A

しかしながら、上記特許文献1〜3には、動翼の回転によって発生する空気流と、動翼を連結する連結部との干渉によるインペラ特性の影響は考慮されていない。   However, the above Patent Documents 1 to 3 do not consider the influence of the impeller characteristics due to the interference between the air flow generated by the rotation of the moving blade and the connecting portion connecting the moving blade.

また、上記特許文献4〜5には、動翼を連結する連結部と、静翼を連結する連結部との位置関係によるインペラ特性の影響は考慮されていない。   Further, in Patent Documents 4 to 5, the influence of the impeller characteristic due to the positional relationship between the connecting portion that connects the moving blades and the connecting portion that connects the stationary blades is not considered.

本発明は、動翼の回転によって発生する空気流と連結部との干渉によるインペラ特性の低下を抑制したインペラを備えた送風ファンを提供することにある。   An object of the present invention is to provide a blower fan including an impeller that suppresses deterioration of impeller characteristics due to interference between an air flow generated by rotation of a moving blade and a connecting portion.

上記課題を解決するために、本発明は、複数の動翼を互いに連結する環状の連結部を備えたインペラにおいて、連結部を、動翼の径方向に沿った翼長に対して、動翼の付け根から翼長の70%〜90%の位置に形成し、かつ、複数の静翼を連結する環状の連結部を、複数の動翼の連結部から径方向内方に配置する構成を採用する。   In order to solve the above-described problem, the present invention provides an impeller having an annular connecting portion that connects a plurality of moving blades to each other, and the connecting portion is connected to the blade length along the radial direction of the moving blade. Adopting a configuration in which an annular connecting part that connects a plurality of stationary blades is arranged radially inward from the connecting part of a plurality of moving blades at a position 70% to 90% of the blade length from the root of the blade To do.

すなわち、本発明の一側面における送風ファンは、中心軸を中心に回転する略円筒状のカップ部と、カップ部の外周面に固定され、カップ部と共に回転することにより、軸方向の一方から吸気し、軸方向の他方に排気する複数の動翼と、複数の動翼をカップ部と共に回転させるモータと、モータを支持するベース部と、複数の動翼の外周を囲うハウジングとを備え、複数の動翼は、略環状の第1の連結部によって互いに連結されており、第1の連結部は、動翼の径方向に沿った翼長に対して、動翼のカップ部外周面における付け根から、翼長の70%〜90%の位置に、略円筒形状に形成されており、ハウジングとベース部とは、複数の静翼で連結され、かつ、複数の静翼は、略環状の第2の連結部によって互いに連結されており、第2の連結部は、第1の連結部から径方向内方に配置されていることを特徴とする。   That is, the blower fan according to one aspect of the present invention is fixed to the substantially cylindrical cup portion that rotates about the central axis and the outer peripheral surface of the cup portion, and rotates together with the cup portion, thereby sucking air from one side in the axial direction. A plurality of moving blades that exhaust in the other axial direction, a motor that rotates the plurality of moving blades together with the cup portion, a base portion that supports the motor, and a housing that surrounds the outer periphery of the plurality of moving blades. Are connected to each other by a substantially ring-shaped first connecting portion, and the first connecting portion is connected to the blade length along the radial direction of the moving blade, at the root of the outer peripheral face of the cup portion of the moving blade. Are formed in a substantially cylindrical shape at a position of 70% to 90% of the blade length, the housing and the base portion are connected by a plurality of stationary blades, and the plurality of stationary blades are substantially annular first. Are connected to each other by two connecting portions, Parts is characterized by being arranged from the first connecting portion radially inward.

ここで、第2の連結部は、第1の連結部から、カップ部外周と第1の連結部との距離に対して、この距離の50〜65%の範囲で径方向内方に配置されていることが好ましい。   Here, the second connecting portion is disposed radially inward within a range of 50 to 65% of the distance from the first connecting portion to the distance between the outer periphery of the cup portion and the first connecting portion. It is preferable.

本発明によれば、複数の動翼を連結する環状の第1の連結部を備えたインペラにおいて、第1の連結部を、動翼の径方向に沿った翼長に対して、動翼の付け根から翼長の70%〜90%の位置に形成することによって、空気流と連結部との干渉による騒音の増加が抑制できると共に、複数の静翼を連結する環状の第2の連結部を、第1の連結部から径方向内方に配置することによって、最大効率における静圧の低下を抑制できる。これにより、インペラ特性の低下を抑制しつつ、強度の高い送風ファンが実現できるため、自由度の高い送風ファンの設計が可能となる。   According to the present invention, in an impeller including an annular first connecting portion that connects a plurality of moving blades, the first connecting portion is connected to the blade length along the radial direction of the moving blade. By forming at a position of 70% to 90% of the blade length from the root, an increase in noise due to interference between the air flow and the connecting portion can be suppressed, and an annular second connecting portion that connects a plurality of stationary blades is provided. By disposing radially inward from the first connecting portion, it is possible to suppress a decrease in static pressure at maximum efficiency. Thereby, since a high intensity | strength ventilation fan is realizable, suppressing the fall of an impeller characteristic, design of a ventilation fan with a high freedom degree is attained.

本発明の一実施形態におけるインペラの軸方向吸気側から見た平面図である。It is the top view seen from the axial direction intake side of the impeller in one Embodiment of this invention. 図1のインペラの側面図である。It is a side view of the impeller of FIG. 図1のインペラを備えた送風ファンの構成を示した断面図である。It is sectional drawing which showed the structure of the ventilation fan provided with the impeller of FIG. 異なる位置に第1の連結部が形成されたインペラの複数のサンプルについて、各インペラの静圧特性及び騒音特性を示したグラフである。It is the graph which showed the static pressure characteristic and noise characteristic of each impeller about the some sample of the impeller in which the 1st connection part was formed in a different position. 本発明の一実施形態における送風ファンの構成を示した断面図である。It is sectional drawing which showed the structure of the ventilation fan in one Embodiment of this invention. 2種類の静翼X、Yを用いて作製した送風ファンにおけるボス部半径、第1の連結部の距離、第2の連結部の距離をそれぞれ示した表である。It is the table | surface which each showed the boss | hub part radius in the ventilation fan produced using two types of stationary blades X and Y, the distance of the 1st connection part, and the distance of the 2nd connection part. 図6の静翼X、Yを用いて作製した送風ファンの静圧特性を示したグラフである。It is the graph which showed the static pressure characteristic of the ventilation fan produced using the stationary blades X and Y of FIG. 本発明の一実施形態における送風ファンのハウジングを軸方向吸気側から見た平面図である。It is the top view which looked at the housing of the ventilation fan in one Embodiment of this invention from the axial direction intake side.

以下、本発明の実施形態を図面に基づいて詳細に説明する。なお、本実施形態における説明では、中心軸に平行な方向を「軸方向」とし、中心軸を中心とする半径方向を「径方向」としている。なお、本発明は、以下の実施形態に限定されるものではない。また、本発明の効果を奏する範囲を逸脱しない範囲で、適宜変更は可能である。   Hereinafter, embodiments of the present invention will be described in detail with reference to the drawings. In the description of the present embodiment, a direction parallel to the central axis is referred to as “axial direction”, and a radial direction centered on the central axis is referred to as “radial direction”. In addition, this invention is not limited to the following embodiment. Moreover, it can change suitably in the range which does not deviate from the range which has the effect of this invention.

図1は、本発明の一実施形態におけるインペラ1の軸方向吸気側から見た平面図で、図2は、図1のインペラ1の側面図である。また、図3は、図1のインペラ1を備えた送風ファン2の断面図である。   FIG. 1 is a plan view of an impeller 1 according to an embodiment of the present invention as viewed from the axial intake side, and FIG. 2 is a side view of the impeller 1 of FIG. FIG. 3 is a cross-sectional view of the blower fan 2 including the impeller 1 of FIG.

本実施形態におけるインペラ1は、図1及び図2に示すように、中心軸Jを中心に回転する略円筒状のカップ部10と、カップ部10の外周面10aに固定され、カップ部10と共に回転することにより、軸方向の一方から吸気し、軸方向の他方に排気する複数の動翼11と、複数の動翼11を互いに連結する略環状の連結部12とを備えている。ここで、連結部12は、中心軸Jを中心とした任意の円に沿って周方向に、略円筒形状に形成されている。   As shown in FIGS. 1 and 2, the impeller 1 in the present embodiment is fixed to a substantially cylindrical cup portion 10 that rotates about a central axis J and an outer peripheral surface 10 a of the cup portion 10. By rotating, a plurality of moving blades 11 that intake air from one side in the axial direction and exhaust air to the other side in the axial direction, and a substantially annular connecting portion 12 that connects the plurality of moving blades 11 to each other are provided. Here, the connection part 12 is formed in the substantially cylindrical shape in the circumferential direction along the arbitrary circle centering on the central axis J. As shown in FIG.

また、本実施形態における送風ファン2は、図3に示すように、インペラ1を駆動するモータと、モータを支持するベース部24と、インペラ1の外周を囲うハウジング30と、ハウジング30とベース部24とを連結する複数の静翼31とを備えている。   In addition, as shown in FIG. 3, the blower fan 2 in the present embodiment includes a motor that drives the impeller 1, a base portion 24 that supports the motor, a housing 30 that surrounds the outer periphery of the impeller 1, and a housing 30 and a base portion. 24 and a plurality of stationary blades 31 that are connected to each other.

モータは、インペラ1のカップ部10の内周面に取り付けられたロータホルダ22及びロータマグネット23と、ステータコアにコイルを巻装してなるステータ26と、軸受保持部25の内側に固定されたスリーブ軸受21とを備えている。カップ部10の中心部に固定されたシャフト20は、スリーブ軸受21に挿入されて回転可能に支持されている。   The motor includes a rotor holder 22 and a rotor magnet 23 attached to the inner peripheral surface of the cup portion 10 of the impeller 1, a stator 26 in which a coil is wound around a stator core, and a sleeve bearing fixed inside the bearing holding portion 25. 21. The shaft 20 fixed to the center portion of the cup portion 10 is inserted into a sleeve bearing 21 and is rotatably supported.

このように構成された送風ファン2は、ステータ26のコイルに駆動電流を供給することによって、ステータ26とロータマグネット23との間で回転トルクを発生させ、これにより、カップ部10の外周面10aに固定された複数の動翼11が中心軸Jを中心に回転する。   The blower fan 2 configured in this manner generates a rotational torque between the stator 26 and the rotor magnet 23 by supplying a drive current to the coil of the stator 26, and thereby the outer peripheral surface 10 a of the cup portion 10. A plurality of blades 11 fixed to the center of the rotor 11 rotate about the central axis J.

本願発明者等は、動翼11の回転によって発生する空気流と連結部12との干渉によるインペラ特性の影響を検討した結果、動翼11の径方向における連結部12の形成位置に関して重要な知見を得た。   The inventors of the present application have studied the influence of the impeller characteristics due to the interference between the air flow generated by the rotation of the moving blade 11 and the connecting portion 12, and as a result, important knowledge regarding the formation position of the connecting portion 12 in the radial direction of the moving blade 11. Got.

図4は、動翼11の径方向に対して異なる位置に連結部12が形成されたインペラ1の複数のサンプルA〜Eについて、インペラ1の静圧特性及び騒音特性をそれぞれ示したグラフである。ここで、サンプルA〜Eは、図1に示すように、連結部12を、動翼11の径方向に沿った翼長Laに対して、動翼11のカップ部外周面10aにおける付け根から連結部12までの距離Lbが、翼長Laの50%、70%、80%、90%、100%になる位置にそれぞれ形成したものである。図中の曲線G1b〜G5bは、サンプルA〜Eの風量と静圧との関係を、また、曲線G1a〜G5aは、サンプルA〜Eの風量と騒音との関係を、それぞれ測定した結果を示したものである。   FIG. 4 is a graph showing the static pressure characteristics and noise characteristics of the impeller 1 for a plurality of samples A to E of the impeller 1 in which the connecting portions 12 are formed at different positions with respect to the radial direction of the moving blade 11. . Here, in the samples A to E, as shown in FIG. 1, the connecting portion 12 is connected to the blade length La along the radial direction of the moving blade 11 from the root of the cup outer peripheral surface 10 a of the moving blade 11. The distance Lb to the portion 12 is formed at a position where the distance Lb is 50%, 70%, 80%, 90%, and 100% of the blade length La. Curves G1b to G5b in the figure show the results of measuring the relationship between the air volume and static pressure of samples A to E, and curves G1a to G5a show the results of measuring the relationship between the air volume and noise of samples A to E, respectively. It is a thing.

図4に示すように、連結部12の位置が50%、100%に対応するサンプルA、E(曲線G1a、G5a)では、連結部12の位置が70%、80%、90%に対応するサンプルB、C、D(曲線G2a、G3a、G4a)に比べて騒音が増大しているのが分かる。サンプルAで騒音が増大するのは、動翼11の径方向の中央部は、空気流生成の寄与度が大きいため、空気流と連結部12との干渉が大きくなるためと考えられる。また、サンプルEで騒音が増大するのは、連結部12を動翼11の径方向外端11bに設けると、連結部12とハウジングの側壁との隙間に、逆方向の空気流が発生するためと考えられる。   As shown in FIG. 4, in the samples A and E (curves G1a and G5a) where the position of the connecting portion 12 corresponds to 50% and 100%, the positions of the connecting portion 12 correspond to 70%, 80% and 90%. It can be seen that the noise increases compared to samples B, C, and D (curves G2a, G3a, and G4a). The reason for the increase in noise in the sample A is considered to be that the interference between the air flow and the connecting portion 12 becomes large in the radial center portion of the rotor blade 11 because the contribution of air flow generation is large. Moreover, the noise increases in the sample E because the air flow in the reverse direction is generated in the gap between the connecting portion 12 and the side wall of the housing when the connecting portion 12 is provided at the radially outer end 11b of the moving blade 11. it is conceivable that.

従って、連結部12を、動翼11の径方向に沿った翼長Laに対して、動翼11の付け根から、翼長Laの70%〜90%の位置に形成することによって、連結部12の付与に起因した騒音の増加を抑制することができる。   Therefore, the connecting portion 12 is formed at a position 70% to 90% of the blade length La from the root of the moving blade 11 with respect to the blade length La along the radial direction of the moving blade 11. The increase in noise due to the application of can be suppressed.

また、連結部12は、動翼11の径方向外端11bよりも径方向内方側に配置されるため、連結部12よりも径方向内方に位置する動翼11の領域11Aにおいては、連結部12の内側面がハウジングの内側面の役目を担うことになる。すなわち、仮想的なハウジングの内側面(連結部12の内側面)と連結部12よりも径方向内方に位置する動翼11の領域11Aとの間にはギャップがない。そのため、連結部12よりも径方向内方に位置する動翼11の領域11Aにおいて、空気流の逆流が発生しにくくなり、逆流する空気流の大半は、連結部12よりも径方向外方に位置する動翼11の領域11Bを通過することになる。その結果、連結部12よりも径方向外方に位置する動翼11の領域11Bは、専ら空気流の逆流防止のために機能させることができる。これにより、連結部12よりも径方向内方に位置する動翼11の領域11Aにおいてインペラ1の風量特性を確保しつつ、低風量側での静圧特性の改善を図ることができる。   In addition, since the connecting portion 12 is disposed radially inward from the radially outer end 11b of the rotor blade 11, in the region 11A of the rotor blade 11 positioned radially inward from the connecting portion 12, The inner surface of the connecting portion 12 serves as the inner surface of the housing. That is, there is no gap between the inner surface of the virtual housing (the inner surface of the connecting portion 12) and the region 11 </ b> A of the moving blade 11 located radially inward of the connecting portion 12. Therefore, in the region 11A of the rotor blade 11 that is located radially inward of the connecting portion 12, it is difficult for the backflow of airflow to occur, and most of the backflowing airflow is radially outward from the connecting portion 12. It passes through the region 11B of the moving blade 11 located. As a result, the region 11B of the moving blade 11 positioned radially outward from the connecting portion 12 can function exclusively for preventing the backflow of airflow. Thereby, it is possible to improve the static pressure characteristics on the low air volume side while securing the air volume characteristics of the impeller 1 in the region 11A of the rotor blade 11 located radially inward of the connecting portion 12.

なお、複数の動翼11を連結部12で互いに連結することによって、遠心力に対する動翼11の強度が高められるが、動翼11が前進翼として構成されている場合、特にその効果が発揮される。ここで、前進翼とは、図1に示すように、動翼11の回転方向Rの最前方に位置する前縁11aと、動翼11の径方向外端に位置する動翼端11bとの交点P1が、前縁11aとカップ部10の外周面10aとの交点P2よりも回転方向Rの前方側に位置するものをいう。また、前進度合が極端に大きい場合、すなわち、図1に示すように、動翼11の回転方向Rの後方に位置する後縁11cと、動翼11の径方向外端に位置する動翼端11bとの交点P3が、動翼11の回転方向Rの前方に位置する前縁11aと、カップ部10の外周面10aとの交点P2よりも回転方向Rの前方側に位置している場合に、さらにその効果が発揮し得る。   In addition, although the intensity | strength of the moving blade 11 with respect to a centrifugal force is raised by mutually connecting the several moving blade 11 with the connection part 12, when the moving blade 11 is comprised as an advance blade, the effect is exhibited especially. The Here, as shown in FIG. 1, the forward blade is a front edge 11 a positioned at the forefront in the rotational direction R of the moving blade 11 and a moving blade end 11 b positioned at the radially outer end of the moving blade 11. The intersection point P1 is located on the front side in the rotational direction R with respect to the intersection point P2 between the front edge 11a and the outer peripheral surface 10a of the cup portion 10. Further, when the degree of forward movement is extremely large, that is, as shown in FIG. 1, the trailing edge 11 c located at the rear of the moving blade 11 in the rotation direction R and the moving blade tip located at the radially outer end of the moving blade 11. When the intersection P3 with 11b is located in the front side of the rotation direction R rather than the intersection P2 of the front edge 11a located in front of the rotation direction R of the moving blade 11 and the outer peripheral surface 10a of the cup part 10. Further, the effect can be exhibited.

ところで、本願発明者等は、図5に示すように、複数の静翼31を略環状の連結部32で互いに連結した送風ファンの静圧特性について検討していたところ、動翼11に設けた連結部(第1の連結部)12に対する静翼31に設けた連結部(第2の連結部)32の配置位置によっては、最大効率における静圧が十分に上昇しない場合があることが分かった。   Incidentally, as shown in FIG. 5, the inventors of the present application have examined the static pressure characteristics of the blower fan in which a plurality of stationary blades 31 are connected to each other by a substantially annular connecting portion 32. It has been found that the static pressure at the maximum efficiency may not be sufficiently increased depending on the arrangement position of the connecting portion (second connecting portion) 32 provided on the stationary blade 31 with respect to the connecting portion (first connecting portion) 12. .

図6は、2種類の静翼X、Yを用いて作製した送風ファンにおけるボス部半径、第1の連結部の距離、第2の連結部の距離をそれぞれ示した表で、図7は、静翼X、Yを用いて作製した送風ファンの静圧特性を示したグラフである。   FIG. 6 is a table showing the boss portion radius, the distance of the first connecting portion, and the distance of the second connecting portion in the blower fan manufactured using two types of stationary blades X and Y. FIG. It is the graph which showed the static pressure characteristic of the ventilation fan produced using the stationary blades X and Y.

ここで、作製した送風ファンは、図5に示すように、カップ部10の半径(A)を31.5mm、第1の連結部12のカップ部10の側面からの距離(B)を18.25mmとした。また、第2の連結部32の第1の連結部12からの距離(C)を、静翼Xでは10.45mm、静翼Yでは−2.25mmとした。なお、静翼Xでは、第2の連結部32を第1の連結部12から径方向内方に配置し、静翼Yでは、第2の連結部32を、第1の連結部12から径方向外方に配置している。   Here, as shown in FIG. 5, the produced blower fan has a radius (A) of the cup portion 10 of 31.5 mm and a distance (B) from the side surface of the cup portion 10 of the first connecting portion 12 of 18.7. It was 25 mm. Further, the distance (C) of the second connecting portion 32 from the first connecting portion 12 was set to 10.45 mm for the stationary blade X and −2.25 mm for the stationary blade Y. In the stationary blade X, the second coupling portion 32 is disposed radially inward from the first coupling portion 12, and in the stationary blade Y, the second coupling portion 32 is diameterd from the first coupling portion 12. It is arranged outside the direction.

図7のグラフにおいて、曲線L1は、静翼Xを用いて作製した送風ファンの静圧特性、曲線L2は、静翼Yを用いて作製した送風ファンの静圧特性をそれぞれ示す。図7に示すように、第2の連結部32を第1の連結部12から径方向外方に配置した送風ファンでは、最高効率における静圧が低下しているのに対し、第2の連結部32を第1の連結部12から径方向内方に配置した送風ファンでは、最高効率における静圧の低下が抑制されているのが分かる。   In the graph of FIG. 7, the curve L1 indicates the static pressure characteristic of the blower fan manufactured using the stationary blade X, and the curve L2 indicates the static pressure characteristic of the blower fan manufactured using the stationary blade Y. As shown in FIG. 7, in the blower fan in which the second connecting portion 32 is arranged radially outward from the first connecting portion 12, the static pressure at the highest efficiency is reduced, whereas the second connecting portion 32 It can be seen that in the blower fan in which the portion 32 is disposed radially inward from the first connecting portion 12, the reduction in static pressure at the maximum efficiency is suppressed.

このように、第2の連結部32を第1の連結部12から径方向外方に配置した送風ファンで、最高効率における静圧が低下しているのは、カップ部10と第2の連結部32との間に安定した大きな空気渦が発生し、第2の連結部32と第1の連結部12との流路が狭くなるためと考えられる。一方、第2の連結部32を第1の連結部12から径方向内に配置した送風ファンで、最高効率における静圧の低下が抑制されているのは、カップ部10と第2の連結部32との間に発生する空気渦が大きくなるのが抑制されるので、第2の連結部32と第1の連結部12との流路が広くなるためと考えられる。   Thus, the static pressure at the highest efficiency is reduced in the blower fan in which the second connecting portion 32 is arranged radially outward from the first connecting portion 12, and the cup portion 10 and the second connecting portion are reduced. It is considered that a large stable air vortex is generated between the second connecting portion 32 and the flow path between the second connecting portion 32 and the first connecting portion 12 is narrowed. On the other hand, in the blower fan in which the second connecting portion 32 is arranged in the radial direction from the first connecting portion 12, the cup portion 10 and the second connecting portion are suppressed from decreasing in static pressure at the maximum efficiency. It is considered that the flow path between the second connecting portion 32 and the first connecting portion 12 is widened because an increase in the air vortex generated between the second connecting portion 32 and the first connecting portion 12 is suppressed.

なお、図6に示すように、静翼Xにおいて、第1の連結部12の距離(B)に対する第2の連結部32の距離(C)の比(C/B)は0.57となっており、第2の連結部32を配置する位置が、第1の連結部12よりも径方向内方に位置する動翼11の領域11Aに対して中央近傍にある。第2の連結部32を、動翼11の領域11Aの中央近傍に配置することによって、カップ部10と第2の連結部32との間で空気渦が大きくなることを抑制するため、最高効率における静圧の低下をより抑制することができる。このことから、第2の連結部32は、動翼11の領域11Aの中央近傍、すなわち、第1の連結部12から、カップ部10の外周と第1の連結部12との距離(B)に対して、距離(B)の50〜65%の範囲で径方向内方に配置されていることが好ましい。   As shown in FIG. 6, in the stationary blade X, the ratio (C / B) of the distance (C) of the second connecting portion 32 to the distance (B) of the first connecting portion 12 is 0.57. The position where the second connecting portion 32 is disposed is near the center with respect to the region 11A of the moving blade 11 located radially inward of the first connecting portion 12. By arranging the second connecting portion 32 in the vicinity of the center of the region 11A of the moving blade 11, the air vortex is prevented from becoming large between the cup portion 10 and the second connecting portion 32, so that the highest efficiency is achieved. The decrease in static pressure can be further suppressed. From this, the second connecting portion 32 is located near the center of the region 11A of the rotor blade 11, that is, from the first connecting portion 12, the distance (B) between the outer periphery of the cup portion 10 and the first connecting portion 12. On the other hand, it is preferable to arrange radially inward within a range of 50 to 65% of the distance (B).

図8は、本実施形態における送風ファン2を軸方向吸気側から見た平面図である。図8に示すように、ベース部24とハウジング30とは、複数の静翼31で連結され、複数の静翼31は、略環状の第2の連結部32によって互いに連結されている。そして、第2の連結部32は、第1の連結部(不図示)から径方向内方に配置されている。   FIG. 8 is a plan view of the blower fan 2 in the present embodiment as viewed from the axial suction side. As shown in FIG. 8, the base portion 24 and the housing 30 are coupled by a plurality of stationary blades 31, and the plurality of stationary blades 31 are coupled to each other by a substantially annular second coupling portion 32. And the 2nd connection part 32 is arrange | positioned radially inward from the 1st connection part (not shown).

ここで、ベース部24、ハウジング30、複数の静翼31、及び第2の連結部12は、射出成形により一体成形されていてもよい。また、第2の連結部12の形状は特に制限されないが、軸方向排気側に向かって、中心軸に近づくように傾斜した帯状にすることによって、第2の連結部12に集風効果を付与することができる。   Here, the base portion 24, the housing 30, the plurality of stationary blades 31, and the second connecting portion 12 may be integrally formed by injection molding. In addition, the shape of the second connecting portion 12 is not particularly limited, but a wind collecting effect is imparted to the second connecting portion 12 by forming a band shape inclined toward the central axis toward the axial exhaust side. can do.

Claims (5)

中心軸を中心に回転する略円筒状のカップ部と、
前記カップ部の外周面に固定され、該カップ部と共に回転することにより、軸方向の一方から吸気し、軸方向の他方に排気する複数の動翼と、
前記複数の動翼を前記カップ部と共に回転させるモータと、
前記モータを支持するベース部と、
前記複数の動翼の外周を囲うハウジングと、
を備え、
前記複数の動翼は、略環状の第1の連結部によって互いに連結されており、該第1の連結部は、前記動翼の径方向に沿った翼長に対して、前記動翼の前記カップ部外周面における付け根から、前記翼長の70%〜90%の位置に、略円筒形状に形成されており、
前記ハウジングと前記ベース部とは、複数の静翼で連結され、かつ、該複数の静翼は、略環状の第2の連結部によって互いに連結されており、
前記第2の連結部は、前記第1の連結部から径方向内方に配置されている、送風ファン。
A substantially cylindrical cup portion that rotates about a central axis;
A plurality of moving blades that are fixed to the outer peripheral surface of the cup portion and rotate together with the cup portion to suck air from one side in the axial direction and exhaust air to the other side in the axial direction;
A motor for rotating the plurality of moving blades together with the cup portion;
A base for supporting the motor;
A housing enclosing an outer periphery of the plurality of blades;
With
The plurality of moving blades are connected to each other by a substantially annular first connecting portion, and the first connecting portion is connected to the blade length along the radial direction of the moving blade with respect to the blade length. From the root of the cup outer peripheral surface, is formed in a substantially cylindrical shape at a position of 70% to 90% of the blade length,
The housing and the base portion are connected by a plurality of stationary blades, and the plurality of stationary blades are connected to each other by a substantially annular second connecting portion,
The said 2nd connection part is a ventilation fan arrange | positioned radially inward from the said 1st connection part.
請求項1に記載の送風ファンにおいて、
前記複数の動翼は、前進翼として構成されている、送風ファン。
The blower fan according to claim 1,
The plurality of rotor blades are blower fans configured as forward blades.
請求項1に記載の送風ファンにおいて、
前記第2の連結部は、前記第1の連結部から、前記カップ部外周と前記第1の連結部との距離に対して、該距離の50〜65%の範囲で径方向内方に配置されている、送風ファン。
The blower fan according to claim 1,
The second connecting portion is arranged radially inward within a range of 50 to 65% of the distance from the first connecting portion to the distance between the outer periphery of the cup portion and the first connecting portion. Being a blower fan.
請求項1に記載の送風ファンにおいて、
前記第2の連結部は、略円筒形状に形成されている、送風ファン。
The blower fan according to claim 1,
The second connecting part is a blower fan formed in a substantially cylindrical shape.
請求項1に記載の送風ファンにおいて、
前記動翼の回転方向後方に位置する後縁と、前記動翼の径方向外端に位置する動翼端との交点は、前記動翼の回転方向前方に位置する前縁と、前記カップ部外周面との交点よりも、回転方向前方側に位置している、送風ファン。
The blower fan according to claim 1,
The intersection of the trailing edge located at the rear in the rotational direction of the moving blade and the moving blade end located at the radially outer end of the moving blade is a front edge located at the front in the rotational direction of the moving blade, and the cup portion. A blower fan located on the front side in the rotational direction of the intersection with the outer peripheral surface.
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