JP2008248739A - Side cut fan - Google Patents
Side cut fan Download PDFInfo
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- JP2008248739A JP2008248739A JP2007088806A JP2007088806A JP2008248739A JP 2008248739 A JP2008248739 A JP 2008248739A JP 2007088806 A JP2007088806 A JP 2007088806A JP 2007088806 A JP2007088806 A JP 2007088806A JP 2008248739 A JP2008248739 A JP 2008248739A
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- 230000002093 peripheral effect Effects 0.000 claims description 12
- 230000000694 effects Effects 0.000 description 5
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 230000001914 calming effect Effects 0.000 description 1
- 230000035772 mutation Effects 0.000 description 1
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Abstract
Description
本発明は、軸流ファン、特にサイドカットファンでの、ベンチュリの風洞部形状に関する。 The present invention relates to a venturi wind tunnel shape of an axial fan, particularly a side cut fan.
上述特許文献にも見られる通り送風性能の向上と静穏化という相反する要素に対応するため、ベンチュリの風洞部形状については種々の検討が試みられ実用化されており、本願発明に係る、実装スペース抑制を意図した所謂サイドカットファンも、その適用範囲であることに変わりはない。 As seen in the above-mentioned patent document, in order to cope with the conflicting elements of improvement in air blowing performance and quietness, various studies have been tried on the venturi shape of the venturi, and it has been put into practical use. The so-called side cut fan intended to be suppressed is still in the applicable range.
そして、サイドカットファン自体でも、切除部形成に伴うベンチュリの薄肉化対応として剛性を保持する目的もあって、風洞を形成するベンチュリ内周面には、当該切除部で、初期の風洞外側円弧面の円弧径とは異なる曲率径として、プロペラの転回外周円弧面との空隙の変化を少なくして連通するように形成されていることも周知の通りである。 The side cut fan itself also has the purpose of maintaining rigidity as a countermeasure for thinning the venturi accompanying the formation of the cut portion, and the venturi inner peripheral surface forming the wind tunnel has an initial wind tunnel outer arc surface at the cut portion. As is well known, it is formed so as to have a curvature diameter different from the arc diameter of the propeller so as to communicate with the rotating outer peripheral arc surface of the propeller with less change in the gap.
しかし、サイドカットファンでは、上述のように、従来技術に成る改善効果に加えて、サイドカット部に対応するベンチュリの内周面の円弧径が、当初の風洞外側円弧面を形成する初期円弧径とは異なる円弧径として形成されることによる、圧力変動の影響対策が求められて来ている。 However, in the side cut fan, as described above, in addition to the improvement effect of the prior art, the arc diameter of the inner peripheral surface of the venturi corresponding to the side cut portion is the initial arc diameter that forms the original wind tunnel outer arc surface. There is a demand for countermeasures against the influence of pressure fluctuations by forming the arc diameter different from that of the arc.
本発明に成るサイドカットファンは、ベンチュリ外周面の所定の切除部に対応する部位の内面に、初期円弧径とこれと異なる円弧径で連通する円弧径連通部が形成されると共に、周方向で変移した部位にも初期円弧径とこれと異なる円弧径で連通する別の追加円弧径連通部を備え、好ましくは、 In the side cut fan according to the present invention, an arc diameter communicating portion communicating with an initial arc diameter and a different arc diameter is formed on an inner surface of a portion corresponding to a predetermined cut portion on the outer peripheral surface of the venturi, and in the circumferential direction. The displaced part also includes another additional arc diameter communicating portion that communicates with the initial arc diameter and a different arc diameter,
前記追加円弧径連通部が、当初の2箇所の切除部形成部位に対し90度変移する部位の、別の2箇所に設けられ、また、 The additional arc diameter communicating portion is provided at another two locations of the portion shifted 90 degrees with respect to the initial two excised portion forming portions,
前記ベンチュリ内周面で初期円弧径に連通する異なる円弧径が、いずれも同一円弧径として形成されている。 Different arc diameters communicating with the initial arc diameter on the inner peripheral surface of the venturi are all formed as the same arc diameter.
本発明に成るサイドカットファンは、当該サイドカットファンでの特異な課題である、ベンチュリ外周面の切除による、風洞外側内周面の円弧径変化に伴うプロペラの転回外周円弧面との空隙変化での、プロペラと風洞外側内周面との圧力干渉の影響を抑制する効果を実現している。 The side-cut fan according to the present invention is a unique problem in the side-cut fan. The effect of suppressing the influence of pressure interference between the propeller and the outer peripheral surface of the wind tunnel is realized.
以下図面により本発明の実施例を説明する。 Embodiments of the present invention will be described below with reference to the drawings.
図1は、本発明の第1の実施例を示す正面図であり、図2は、従来技術の実施例を示す正面図である。図2に示す2面を切除した従来周知のサイドカットファン1に対し、図1では、サイドカット部2−1の風洞外側円弧面に形成された円弧径連通部3−1と共に、90度変移した部位の風洞外側円弧面に追加円弧径連通部3−4を設け、初期の真円状風洞外側円弧面3−2に対し大きな曲率径とした円弧径連通部を追加形成することで、プロペラ転回での空隙の変化を極力抑制するようにして、静穏化効果を高めている。
FIG. 1 is a front view showing a first embodiment of the present invention, and FIG. 2 is a front view showing an embodiment of the prior art. In contrast to the conventionally known side-
上述図1は、ベンチュリー2の外周面での形状は、図2のものと類似しているが、上述の通り、サイドカット部2−1と90度変移した部位のベンチュリ2の内周面に、追加円弧径連通部3−4を追加形成する例として示している。
1 is similar to that of FIG. 2 on the outer peripheral surface of the
なお、通常、サイドカットファン1としての2面のサイドカット部2−1は、180度の変移で対向する部位に設けられる例が多く、対応する、追加される異なる曲率径の円弧径連通部を前記2面のサイドカット部2−1と90度変異させることが一般的と言える。
In general, the two side cut portions 2-1 as the
図3と図4は、上述図1、図2に例示するサイドカット部2−1が180度偏移したサイドカットファン1の構成に係る、図2に示す従来構造と図1に示す2個の追加円弧径連通部3−4を付加した構成での、風量性能と騒音のオーバーオール値での比較データ、及び、両者の騒音を周波数分析として示す比較データである。
FIGS. 3 and 4 show the conventional structure shown in FIG. 2 and the two shown in FIG. 1 according to the configuration of the
上述図1に示す本願発明構成の実施例では、図3に見る騒音のオーバーオール値で高風量領域での騒音レベルの顕著な低減効果を確認でき、図4の周波数分析のデータからは、ほぼ400Hzのサイクルで発生する騒音ピーク値のうち、特に最大値を示す800Hzでの低減効果が確認され、上記オーバーオール値での低減に寄与している。 In the embodiment of the present invention configuration shown in FIG. 1 described above, a significant reduction effect of the noise level in the high air volume region can be confirmed by the overall noise value shown in FIG. 3, and the frequency analysis data of FIG. Among the noise peak values generated in this cycle, a reduction effect at 800 Hz, which indicates the maximum value, has been confirmed, which contributes to the reduction in the overall value.
本発明に成るサイドカットファンは、実装スペースの拡大を派生することなしに、プロペラ転回時の外周円弧面と、風洞外側円弧面との空隙の変化での、圧力干渉の影響による騒音を抑制することができるので、省スペース用軸流ファンとしてのサイドカットファンの用途を拡大することを可能とする。 The side cut fan according to the present invention suppresses noise due to the influence of pressure interference caused by the change in the gap between the outer peripheral arc surface and the wind tunnel outer arc surface during propeller rotation without deriving an increase in mounting space. Therefore, it is possible to expand the application of the side cut fan as a space-saving axial fan.
1 サイドカットファン
2 ベンチュリ
2−1 サイドカット部
3 風洞
3−1 サイドカット部内面の円弧径連通部
3−2 初期風洞外側円弧面
3−3 風洞内側円弧面
DESCRIPTION OF
Claims (3)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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JP2007088806A JP4611333B2 (en) | 2007-03-29 | 2007-03-29 | Side cut fan |
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JP2007088806A JP4611333B2 (en) | 2007-03-29 | 2007-03-29 | Side cut fan |
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JP2008248739A true JP2008248739A (en) | 2008-10-16 |
JP4611333B2 JP4611333B2 (en) | 2011-01-12 |
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JP2007088806A Active JP4611333B2 (en) | 2007-03-29 | 2007-03-29 | Side cut fan |
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Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS60107391U (en) * | 1983-12-22 | 1985-07-22 | 日本サ−ボ株式会社 | fan motor |
JPH0389997U (en) * | 1989-12-28 | 1991-09-12 | ||
JPH0630499U (en) * | 1992-09-22 | 1994-04-22 | 日本サーボ株式会社 | Axial fan |
JPH11223196A (en) * | 1998-02-05 | 1999-08-17 | Japan Servo Co Ltd | Rotor of axial fan |
JP2001349299A (en) * | 2000-06-06 | 2001-12-21 | Hisashi Akaishi | Axial blower |
JP2005076473A (en) * | 2003-08-28 | 2005-03-24 | Japan Servo Co Ltd | Fan motor |
-
2007
- 2007-03-29 JP JP2007088806A patent/JP4611333B2/en active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS60107391U (en) * | 1983-12-22 | 1985-07-22 | 日本サ−ボ株式会社 | fan motor |
JPH0389997U (en) * | 1989-12-28 | 1991-09-12 | ||
JPH0630499U (en) * | 1992-09-22 | 1994-04-22 | 日本サーボ株式会社 | Axial fan |
JPH11223196A (en) * | 1998-02-05 | 1999-08-17 | Japan Servo Co Ltd | Rotor of axial fan |
JP2001349299A (en) * | 2000-06-06 | 2001-12-21 | Hisashi Akaishi | Axial blower |
JP2005076473A (en) * | 2003-08-28 | 2005-03-24 | Japan Servo Co Ltd | Fan motor |
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