JP4918650B2 - Multi-wing fan - Google Patents

Multi-wing fan Download PDF

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JP4918650B2
JP4918650B2 JP2006173398A JP2006173398A JP4918650B2 JP 4918650 B2 JP4918650 B2 JP 4918650B2 JP 2006173398 A JP2006173398 A JP 2006173398A JP 2006173398 A JP2006173398 A JP 2006173398A JP 4918650 B2 JP4918650 B2 JP 4918650B2
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blade
surface side
notches
fan
pressure
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JP2008002378A (en
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彰 小松
弘宣 寺岡
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Daikin Industries Ltd
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Description

本願発明は、多翼ファンの羽根車の羽根部の構造に関するものである。   The present invention relates to a structure of a blade portion of an impeller of a multiblade fan.

例えば、クロスフローファン、シロッコファン、ターボファン等の多翼ファンは、空気調和機用の送風機として一般に用いられている。   For example, multi-blade fans such as crossflow fans, sirocco fans, and turbo fans are generally used as blowers for air conditioners.

今例えば図9には、同多翼ファン3を送風機として用いて構成された壁掛型の空気調和機Aが示されている。   Now, for example, FIG. 9 shows a wall-mounted air conditioner A configured using the multiblade fan 3 as a blower.

この空気調和機Aは、上面に空気吸込口4を、下面前部に空気吹出口5を備えた本体ケーシング1と、該本体ケーシング1内に配設されたラムダ形状の熱交換器2と、該熱交換器2の二次側に配設された多翼ファン3とを備えて構成されている。   The air conditioner A includes a main body casing 1 having an air suction port 4 on the upper surface and an air outlet 5 on the lower surface front portion, a lambda-shaped heat exchanger 2 disposed in the main body casing 1, And a multi-blade fan 3 disposed on the secondary side of the heat exchanger 2.

熱交換器2は、空気吸込口4から本体ケーシング1の前面側および上面側に形成された空気通路6を介して供給される空気流が通過する前面側熱交換部2aと、該前面側熱交換部2aの上端に連設されて背面側に位置する背面側熱交換部2bとからなっている。   The heat exchanger 2 includes a front-side heat exchange part 2a through which an air flow supplied from an air suction port 4 through an air passage 6 formed on the front side and the upper side of the main casing 1 passes, and the front-side heat It consists of a back surface side heat exchanging portion 2b that is connected to the upper end of the exchanging portion 2a and is located on the back side.

一方、符号8は、上記前面側熱交換部2aからのドレンを受け止める第1のドレンパン、9は背面側熱交換部2bからのドレンを受け止める第2のドレンパン、10は上記多翼ファン3の羽根車7から吹き出される空気流を案内するガイド部、11は羽根車7から吹き出される空気流の逆流を防止するための逆流防止用舌部、12は空気吹出口5の上流部に配設された垂直羽根、13は空気吹出口5の下流部に配設された水平羽根である。   On the other hand, reference numeral 8 denotes a first drain pan that receives the drain from the front side heat exchange unit 2a, 9 denotes a second drain pan that receives the drain from the back side heat exchange unit 2b, and 10 denotes a blade of the multiblade fan 3 A guide portion for guiding the air flow blown out from the car 7, 11 is a backflow preventing tongue for preventing the backflow of the air flow blown out from the impeller 7, and 12 is provided in the upstream portion of the air outlet 5. The vertical blades 13 are horizontal blades arranged in the downstream portion of the air outlet 5.

そして、上記空気吸込口4から吸い込まれた空気流は、上記熱交換器2を通過する際に冷却あるいは加熱されて調和空気となり、例えば図11に示すように、多翼ファン3の羽根車7を回転軸16に対して直交するように貫流した後、空気吹出口5から室内へ吹き出される(矢線部参照)。   The air flow sucked from the air suction port 4 is cooled or heated when passing through the heat exchanger 2 to become conditioned air. For example, as shown in FIG. 11, the impeller 7 of the multiblade fan 3 is used. Is blown into the room from the air outlet 5 (see the arrow).

この多翼ファン3の羽根車7は、例えば図10に示すように、回転軸16方向に所定の間隔で平行に配設された複数の円形支持プレートの外周縁部に、回転軸16と平行となるように多数枚の羽根(ブレード)15,15・・・を所定の翼角をもって前進翼構造で配設して構成されている。   For example, as shown in FIG. 10, the impeller 7 of the multiblade fan 3 is parallel to the rotary shaft 16 at the outer peripheral edge portions of a plurality of circular support plates arranged in parallel at predetermined intervals in the direction of the rotary shaft 16. Are arranged in a forward blade structure with a predetermined blade angle so that a plurality of blades (blades) 15, 15.

このような多翼ファン3の羽根車7においては、羽根車7を構成する羽根15,15・・・を通過する空気流により生ずる空力騒音が問題となる。この空力騒音の主たる発生原因としては、羽根15,15・・・の負圧面側の空気の流れの剥離と翼後縁側で発生する後流渦とが挙げられる。   In such an impeller 7 of the multiblade fan 3, aerodynamic noise generated by the air flow passing through the blades 15, 15. The main causes of this aerodynamic noise include separation of the air flow on the suction surface side of the blades 15, 15... And wake vortex generated on the blade trailing edge side.

そこで、このような多翼ファン3の羽根車7の空力騒音を減少させる方法として、従来から例えば図12〜図16に示すように上記羽根車7の各羽根15,15・・・の外周側翼端15a,15a・・・に平滑部18,18・・・を介して断続的に切欠部17,17・・・を設けたり、翼端15a,15a・・・に連続的に切欠部17,17・・・を形成してのこぎり歯状にすることなどで、吹出し時の翼後縁側で発生する後流渦を低減して騒音を低減する方法が提案されている(例えば特許文献1、2等参照)。   Therefore, as a method of reducing the aerodynamic noise of the impeller 7 of the multiblade fan 3 as described above, the outer peripheral side blades of the blades 15, 15. .. Are provided intermittently at the ends 15 a, 15 a... Via the smooth portions 18, 18..., Or continuously at the blade tips 15 a, 15 a. A method of reducing noise by reducing the wake vortex generated on the trailing edge side of the blade at the time of blowing is proposed (for example, Patent Documents 1 and 2). Etc.).

特開平3−249400号公報JP-A-3-249400 特開平11−141494号公報JP-A-11-141494

しかし、これらの構成では、例えば図14および図15から理解できるように、例えば羽根15の外周側翼端15a,15a・・・の正圧面側および負圧面側両面に亘る同じ形状、同じ深さ、同じ角度の切欠部17,17・・・があるために(D1=D2で、左右の切り欠かれた面17a,17aが他面方向にストレートになっている)、吹出し時においては、図16の(a)に示す切欠部17がある部分は図16の(b)に示す無い部分(平坦な平滑部分18)と比べて羽根15の出口がファンの周方向に十分に向く前に広がっているために、ファン吹出し流れが周方向に十分に向かなくなって吹出気流の速度が低下し、圧力が低くなる。その結果、フィルタ等の圧力損失に対して弱くなり、有効な風量が出にくくなるという問題がある。   However, in these configurations, for example, as can be understood from FIGS. 14 and 15, for example, the same shape and the same depth over both the pressure surface side and the suction surface side of the outer peripheral side blade tips 15 a, 15 a. Since there are notches 17, 17... Of the same angle (D1 = D2, the left and right notched surfaces 17a, 17a are straight in the direction of the other surface), at the time of blowing, FIG. The portion with the notch portion 17 shown in (a) of FIG. 16 expands before the exit of the blade 15 is sufficiently oriented in the circumferential direction of the fan as compared with the portion (flat smooth portion 18) shown in FIG. 16 (b). For this reason, the fan blowout flow is not sufficiently directed in the circumferential direction, the speed of the blown airflow is reduced, and the pressure is lowered. As a result, there is a problem that it becomes weak against pressure loss of a filter or the like, and it becomes difficult to produce an effective air volume.

本願発明は、このような問題を解決するためになされたもので、羽根外周側翼端に断続的にまたは連続的に切欠を設けた多翼ファンにおいて、切欠部の形状を正圧面側と負圧面側とで異なるものとすることなどによって、可能な限り切欠部を通過する空気の速度を上昇させることによって、有効に吹出し流れの圧力を上昇させることができるようにした多翼ファンを提供することを目的とするものである。   The present invention has been made to solve such a problem, and in a multiblade fan in which notches are provided intermittently or continuously at the blade outer peripheral blade tip, the shape of the notch is changed to the pressure surface side and the suction surface. To provide a multiblade fan that can effectively increase the pressure of the blown flow by increasing the speed of air passing through the notch as much as possible by making it different from the side It is intended.

本願発明は、上記の問題を解決することを目的としてなされたものであって、次のような有効な課題解決手段を備えて構成されている。   The present invention has been made for the purpose of solving the above problems, and comprises the following effective problem solving means.

(1) 第1の課題解決手段
この発明の第1の課題解決手段は、羽根15の外周側翼端15aに断続的または連続的に切欠部27,27・・・を設け、上記切欠部27,27・・・の形状を羽根正圧面側と負圧面側とで異なるものとした多翼ファンにおいて、上記切欠部27,27・・・の形状は略三角形であり、羽根正圧面側の三角形の面積が負圧面側の三角形の面積よりも大きく形成されていることを特徴としている。
(1) first means for solving problems of the first means for solving problems The present invention, only setting the intermittent or continuous notched portions 27, 27 ... on the outer circumference side tip 15a of the blade 15, the cutout portion 27 In the multiblade fan in which the shapes of the blade pressure surface side and the suction surface side are different , the shape of the notches 27, 27... Is substantially triangular, and the triangle on the blade pressure surface side. The area is formed larger than the area of the triangle on the suction surface side .

このような構成によると、正圧面側切欠部27,27・・・の左右の面がテーパー面となり、それによって同切欠部27,27・・・を通過する空気流の速度を上昇させることができ、ファンより吹出される空気の流れを周方向に向けやすくなるので、より有効にファン圧力を上昇させることができる。   According to such a configuration, the left and right surfaces of the pressure surface side notches 27, 27... Become tapered surfaces, thereby increasing the speed of the air flow passing through the notches 27, 27. This makes it easier to direct the flow of air blown from the fan in the circumferential direction, so that the fan pressure can be increased more effectively.

(2) 第2の課題解決手段
この発明の第2の課題解決手段は、羽根15の外周側翼端15aに断続的または連続的に切欠部27,27・・・を設け、上記切欠部27,27・・・の形状を羽根正圧面側と負圧面側とで異なるものとした多翼ファンにおいて、上記切欠部27,27・・・の形状は略三角形であり、羽根正圧面側の三角形の面積が負圧面側の三角形の面積よりも小さく形成されていることを特徴としている。
(2) Second Problem Solving Means The second problem solving means of the present invention is provided with notches 27, 27... Intermittently or continuously on the outer wing tip 15a of the blade 15, and the notches 27, 27. In the multiblade fan in which the shape of 27... Is different between the blade pressure surface side and the suction surface side, the shape of the notches 27, 27. The area is smaller than the area of the triangle on the suction surface side .

このような構成によると、正圧面側切欠部27,27・・・の溝部が小さくなり、それによって同切欠部27,27・・・を通過する空気流の速度を上昇させることができ、ファンより吹出される空気の流れを周方向に向けやすくなる。その結果、より有効にファン圧力を上昇させることができる。   According to such a configuration, the groove portions of the pressure surface side cutout portions 27, 27... Can be reduced, thereby increasing the speed of the air flow passing through the cutout portions 27, 27. It becomes easier to direct the flow of air blown out in the circumferential direction. As a result, the fan pressure can be increased more effectively.

(3) 第3の課題解決手段
この発明の第3の課題解決手段は、羽根15の外周側翼端15aに断続的または連続的に切欠部27,27・・・を設け、上記切欠部27,27・・・の形状を羽根正圧面側と負圧面側とで異なるものとした多翼ファンにおいて、上記切欠部27,27・・・の形状は略台形であり、羽根正圧面側の台形の面積が負圧面側の台形の面積よりも大きく形成されていることを特徴としている。
(3) Third problem solving means The third problem solving means of the present invention is provided with notches 27, 27... Intermittently or continuously on the outer wing tip 15 a of the blade 15. In the multiblade fan in which the shape of 27... Is different between the blade pressure surface side and the suction surface side, the shape of the notches 27, 27. The area is larger than the area of the trapezoid on the suction surface side .

このような構成によっても、正圧面側切欠部27,27・・・の左右の面がテーパー面となり、それによって同切欠部27,27・・・を通過する空気流の速度を上昇させることができ、ファンより吹出される空気の流れを周方向に向けやすくなる。その結果、より有効にファン圧力を上昇させることができる。   Even in such a configuration, the left and right surfaces of the pressure surface side cutout portions 27, 27... Become tapered surfaces, thereby increasing the speed of the air flow passing through the cutout portions 27, 27. It is possible to easily direct the air flow blown from the fan in the circumferential direction. As a result, the fan pressure can be increased more effectively.

(4) 第4の課題解決手段
この発明の第4の課題解決手段は、羽根15の外周側翼端15aに断続的または連続的に切欠部27,27・・・を設け、上記切欠部27,27・・・の形状を羽根正圧面側と負圧面側とで異なるものとした多翼ファンにおいて、上記切欠部27,27・・・の形状は略台形であり、羽根正圧面側の台形の面積が負圧面側の台形の面積よりも小さく形成されていることを特徴としている。
(4) Fourth Problem Solving Means According to a fourth problem solving means of the present invention, the notch portions 27, 27... Are provided intermittently or continuously on the outer wing tip 15a of the blade 15, and the notch portions 27, 27,. In the multiblade fan in which the shape of 27... Is different between the blade pressure surface side and the suction surface side, the shape of the notches 27, 27. The area is smaller than the trapezoidal area on the suction surface side .

このような構成によると、正圧面側切欠部27,27・・・の溝部小さくなり、それによって同切欠部27,27・・・を通過する空気流の速度を上昇させることができ、ファンより吹出される空気の流れを周方向に向けやすくなる。その結果、より有効にファン圧力を上昇させることができる。   According to such a configuration, the groove portion of the pressure side cutout portions 27, 27... Can be reduced, thereby increasing the speed of the air flow passing through the cutout portions 27, 27. It becomes easy to direct the flow of the blown-out air in the circumferential direction. As a result, the fan pressure can be increased more effectively.

(5) 第5の課題解決手段
この発明の第5の課題解決手段は、羽根15の外周側翼端15aに断続的または連続的に切欠部27,27・・・を設け、上記切欠部27,27・・・の幅を羽根正圧面側と負圧面側とで異なるものとした多翼ファンにおいて、切欠部27,27・・・の深さ方向の幅の変化は、連続的であることを特徴としている。
(5) Fifth Problem Solving Means The fifth problem solving means of the present invention is provided with notches 27, 27... Intermittently or continuously on the outer wing tip 15a of the blade 15, and the notches 27, 27. In the multiblade fan in which the width of 27 ... differs between the blade pressure surface side and the suction surface side, the change in the width in the depth direction of the notches 27, 27 ... is continuous. It is a feature .

このような構成によると、特に上述した正圧面側切欠部27,27・・・の左右の切り欠き面が連続した一定傾斜角のテーパー面となり、それによって同切欠部27,27・・・を通過する空気流の速度を効率良く上昇させることができ、ファンより吹出される空気の流れを一層周方向に向けやすくなる。その結果、より有効にファン圧力を上昇させることができる。   According to such a configuration, the right and left notch surfaces of the pressure surface side notches 27, 27... Described above become continuous tapered surfaces having a constant inclination angle, and thereby the notches 27, 27. The speed of the passing air flow can be increased efficiently, and the air flow blown from the fan can be more easily directed in the circumferential direction. As a result, the fan pressure can be increased more effectively.

以上の構成では、羽根外周側端部に切欠部を設けた多翼ファンにおいて、切欠部を通過する空気の速度を上昇させ、有効に圧力を上昇させることにより、フィルタ等の抵抗がある場合でも、所定量の風量を出すことができる。   In the above configuration, even in the case where there is a resistance such as a filter by increasing the speed of the air passing through the notch and effectively increasing the pressure in the multiblade fan provided with the notch at the blade outer peripheral side end. A predetermined amount of airflow can be produced.

また、羽根外周側端部の2次元性を無くすことができるので、吹出し時の翼後縁側で発生する後流渦を低減し、騒音を低下させることもできる。   Further, since the two-dimensionality of the blade outer peripheral end can be eliminated, the wake vortex generated on the blade trailing edge side at the time of blowing can be reduced, and the noise can be reduced.

したがって、空気調和機用の送風機、例えば空気調和機用クロスフローファン等として最適なものとなり、安定した一定量の送風量で、しかも静音性の高い高性能の空気調和機を提供することができる。   Therefore, the air conditioner is optimal as a blower for an air conditioner, for example, a cross flow fan for an air conditioner, and a high-performance air conditioner having a stable and constant air flow rate and high quietness can be provided. .

以下、添付の図面を参照して、本願発明の幾つかの最良の実施の形態について説明する。   Hereinafter, some preferred embodiments of the present invention will be described with reference to the accompanying drawings.

(最良の実施の形態1)
先ず図1〜図4には、本願発明の実施の形態1に係る多翼ファンの羽根車の羽根部の構成が示されている。
(Best Embodiment 1)
First, FIGS. 1 to 4 show a configuration of a blade portion of an impeller of a multiblade fan according to Embodiment 1 of the present invention.

この実施の形態の多翼ファンの羽根車も、前述の従来例のもの(図10参照)と同様に回転軸16方向に所定の間隔で平行に配設された複数枚の円形支持プレート14,14・・・の外周縁部に、回転軸16と平行となるように多数枚の断面円弧状の羽根(ブレード)15,15・・・を所定の翼角をもって前進翼構造で配設して構成されている。   The multi-blade fan impeller of this embodiment also has a plurality of circular support plates 14 arranged in parallel at a predetermined interval in the direction of the rotation axis 16 as in the conventional example (see FIG. 10). .. Are arranged in a forward blade structure with a predetermined blade angle so as to be parallel to the rotating shaft 16 at the outer peripheral edge of. It is configured.

そして、各羽根15,15・・・の外周側翼端15aには、例えば図1〜図4に示すように、その長手方向に所定の間隔をもって略三角形状の多数の切欠部27,27・・・が形成され、かつ該切欠部27,27・・・の間には、翼端の一部を構成する所定の幅の平滑部(非切欠部)18,18・・・がそれぞれ設けられている。   The outer wing tips 15a of the blades 15, 15... Have a number of substantially triangular notches 27, 27,. Are formed, and smooth portions (non-notched portions) 18, 18... Having a predetermined width constituting part of the blade tip are provided between the notched portions 27, 27. Yes.

このように、羽根15の外周側翼端15aに、所定の間隔をもって略三角形状の多数の切欠部27,27・・・を形成し、かつ該切欠部27,27・・・の間に所定の幅の平滑部18,18・・・を設けると、例えば前述の図11に示すようにクロスフローファンとして用いた場合に、吹出側領域では翼後縁側において翼端から放出されるスケールの大きな横渦が、上記切欠部27,27・・・により形成される縦渦によって、スケールが小さく組織化され、安定した横渦に細分化されるため、効果的に空力騒音の低減を図ることができるメリットがある。   In this way, a large number of substantially triangular notches 27, 27... Are formed at predetermined intervals on the outer wing tip 15a of the blade 15, and a predetermined interval is formed between the notches 27, 27. When the smooth portions 18, 18... Of the width are provided, for example, when used as a cross flow fan as shown in FIG. Since the vortex is formed by the vertical vortex formed by the notches 27, 27,..., The scale is organized small and subdivided into a stable lateral vortex, so that aerodynamic noise can be effectively reduced. There are benefits.

しかし、先にも述べたように単に切欠部27,27・・・を設けただけの構成では、羽根の外周側翼端15aに切欠部27,27・・・があるために、吹出し時においては、切欠部27,27・・・がある部分は無い部分と比べて羽根出口がファンの周方向に十分に向く前に広がっているために、ファン吹出し流れが周方向に十分に向かなくなって、速度が低下し、圧力が減少する。   However, as described above, in the configuration in which the notches 27, 27,... Are simply provided, the notches 27, 27,. The fan outlet flow is not sufficiently directed in the circumferential direction because the blade outlet is expanded before it is sufficiently oriented in the circumferential direction of the fan as compared with the portion without the cutout portions 27, 27. , The speed decreases and the pressure decreases.

その結果、フィルタ等の圧力損失に対して弱くなり、有効な風量が出にくくなるという問題が生じる。   As a result, there arises a problem that it becomes weak against pressure loss of a filter or the like, and it becomes difficult to produce an effective air volume.

この場合、羽根15に設けた切欠部27,27・・・の数が多いほど、また切欠部27,27・・・の大きさが大きいほど圧力の減少量が大きくなる。   In this case, the greater the number of notches 27, 27... Provided in the blade 15, and the greater the size of the notches 27, 27.

そこで、本実施の形態では、このような問題を解決するために、上記切欠部27,27・・・の形状を羽根正圧面側と負圧面側とで異ならせて構成している。   Therefore, in this embodiment, in order to solve such a problem, the shape of the notches 27, 27... Is different between the blade pressure surface side and the suction surface side.

このように、羽根15の外周側翼端15aに断続的または連続的に切欠部27,27・・・を設けた多翼ファン3において、同切欠部27,27・・・の形状を羽根15の正圧面側と負圧面側で異なるものとすると、同切欠部27,27・・・がある位置における断面の羽根出口の角度を、翼端15aに切欠部27,27・・・がない場合(破線で示している)と同様に周方向に向けることができ、ファン圧力を上昇させることができる。   In this way, in the multiblade fan 3 in which the outer peripheral blade tip 15a of the blade 15 is provided with the notches 27, 27... Intermittently or continuously, the shape of the notches 27, 27. If the pressure surface side and the suction surface side are different, the blade outlet angle of the cross section at the position where the cutout portions 27, 27... Are present, and the blade tip 15a has no cutout portions 27, 27. It can be directed in the circumferential direction as in the case of the broken line), and the fan pressure can be increased.

これによりフィルタ等の抵抗がある場合でも、所定の風量を出すことができるようになり、従来の単に正圧、負圧両面側で同形状の切欠部17,17・・・を設けた羽根よりも低回転で同風量の送風機を実現できるので、ファンの回転による騒音を低減させることもできる。   As a result, even when there is a resistance such as a filter, it becomes possible to produce a predetermined air volume, which is more than a conventional blade provided with notches 17, 17... Having the same shape on both the positive and negative pressure sides. In addition, since a blower with the same air volume can be realized with low rotation, noise due to rotation of the fan can be reduced.

また、羽根15の外周側翼端部15aの2次元性を無くすことができるので、吹出し時の翼後縁側で発生する後流渦を低減し、効果的に騒音を低下させることもできる。   Further, since the two-dimensionality of the outer peripheral blade tip 15a of the blade 15 can be eliminated, the wake vortex generated on the blade trailing edge side during blowing can be reduced, and the noise can be effectively reduced.

(実施例)
以上のように、羽根15の外周側翼端部15a,15a・・・の切欠部27,27・・・の形状を正圧面側と負圧面側とで変える場合、その具体的な実施例として、例えば次のような各種の形状の採用が考えられる。
(Example)
As described above, when the shape of the cutout portions 27, 27... Of the outer peripheral side blade tips 15a, 15a... Of the blade 15 is changed between the pressure surface side and the suction surface side, as a specific example thereof, For example, the following various shapes can be considered.

(1) 実施例1
上記切欠部27,27・・・の溝部の形状は、全体として上述のように略三角形であるが、例えば図1および図2に示すように、羽根正圧面側の三角形(図2(b))の面積が負圧面側の三角形(図2(a))の面積よりも十分に大きくなるように形成する。
(1) Example 1
The shape of the groove portions of the notches 27, 27... Is generally a triangle as described above. For example, as shown in FIGS. 1 and 2, the blade pressure surface side triangle (FIG. 2B). ) Is sufficiently larger than the area of the triangle on the suction surface side (FIG. 2A).

この場合、図3に示すように、正圧面側と負圧面側各切欠部27の深さ(翼弦方向の深さ)は全く同一である(D1=D2)。   In this case, as shown in FIG. 3, the depth (the depth in the chord direction) of each notch 27 on the pressure side and the suction side is exactly the same (D1 = D2).

このような構成によると、正圧面側切欠部27,27・・・の左右の切り欠き面(溝面)が、図2(b)に示すように幅広のテーパー面となり、それによって図4に示すように同切欠部27,27・・・を通過する空気流の速度を上昇させることができ、ファンより吹出される空気の流れを周方向に向けやすくなる。その結果、より有効にファン圧力を上昇させることができる。   According to such a configuration, the left and right cut-out surfaces (groove surfaces) of the pressure-side cut-out portions 27, 27... Become wide tapered surfaces as shown in FIG. As shown, the speed of the air flow passing through the notches 27, 27... Can be increased, and the air flow blown from the fan can be easily directed in the circumferential direction. As a result, the fan pressure can be increased more effectively.

(2) 実施例2
上記実施例1の場合と同じく上記切欠部27,27・・・の形状は略三角形であるが、実施例1とは逆に羽根正圧面側の三角形の面積を負圧面側の三角形の面積よりも小さく形成する。
(2) Example 2
The shape of the notches 27, 27... Is substantially triangular as in the case of the first embodiment. However, in contrast to the first embodiment, the area of the triangle on the blade pressure side is smaller than the area of the triangle on the suction side. Also make it small.

このような構成によると、正圧面側切欠部27,27・・・の溝部の幅が小さくなる一方、負圧面側の切欠部27,27・・・の左右の面が、テーパー面となり、それによって同切欠部17,17・・・を通過する空気流の速度を上昇させることができ、やはりファンより吹出される空気の流れを周方向に向けやすくなる。その結果、より有効にファン圧力を上昇させることができる。   According to such a configuration, the width of the groove portion of the pressure side cutout portions 27, 27... Is reduced, while the left and right surfaces of the cutout portions 27, 27. Can increase the speed of the air flow passing through the notches 17, 17..., And the air flow blown from the fan can be easily directed in the circumferential direction. As a result, the fan pressure can be increased more effectively.

(3) 実施例3
上記切欠部17,17・・・の形状が略台形であり、羽根正圧面側の台形の面積の方を負圧面側の台形の面積よりも大きく形成する。
(3) Example 3
The shape of the notches 17, 17... Is substantially trapezoidal, and the area of the trapezoid on the blade pressure surface side is formed larger than the area of the trapezoid on the suction surface side.

このような構成によっても、上記実施例1の場合と同様に羽根正圧面側の切欠部17,17・・・の左右の切り欠き面が幅広のテーパー面となり、それによって切欠部17,17・・・を通過する空気流の速度を上昇させることができ、ファンより吹出される空気の流れを周方向に向けやすくなる。その結果、より有効にファン圧力を上昇させることができる。   Even with such a configuration, as in the case of the first embodiment, the left and right cutout surfaces of the blade pressure surface side cutout portions 17, 17... Become wide tapered surfaces, thereby forming the cutout portions 17, 17. .. The speed of the air flow passing through can be increased, and the air flow blown out from the fan can be easily directed in the circumferential direction. As a result, the fan pressure can be increased more effectively.

(4) 実施例4
上記実施例3の場合と同様に上記切欠部27,27・・・の形状は略台形であるが、実施例3の場合とは逆に羽根正圧面側の台形の面積が負圧面側の台形の面積よりも小さく形成する。
(4) Example 4
The shape of the notches 27, 27... Is substantially trapezoidal as in the case of the third embodiment, but the trapezoid area on the blade pressure surface side is a trapezoid on the suction surface side, contrary to the case of the third embodiment. It is formed smaller than the area.

このような構成によると、上記羽根正圧面側の切欠部27,27・・・の溝部の幅が小さくなる一方、反対側負圧面の切欠部27,27・・・の左右の面がテーパー面となり、それによって正圧面側切欠部27,27・・・を通過する空気流の速度を上昇させることができ、ファンより吹出される空気の流れを周方向に向けやすくなる。その結果、より有効にファン圧力を上昇させることができる。   According to such a configuration, the width of the groove portions of the notches 27, 27... On the blade pressure surface side is reduced, while the left and right surfaces of the notches 27, 27. Thus, the speed of the air flow passing through the pressure side cutouts 27, 27... Can be increased, and the air flow blown from the fan can be easily directed in the circumferential direction. As a result, the fan pressure can be increased more effectively.

(最良の実施の形態2)
次に図5〜図8は、本願発明の最良の実施の形態2に係る多翼ファンの羽根車の羽根部の構成を示している。
(Best Mode 2)
Next, FIGS. 5 to 8 show the configuration of the blade portion of the impeller of the multiblade fan according to Embodiment 2 of the present invention.

この実施の形態は、上記最良の実施の形態1の構成と同様に羽根15の外周側翼端15aに平滑部18,18・・・を介して断続的に切欠部27,27・・・を設けた多翼ファンにおいて、上記切欠部27,27・・・の形状自体は正圧面側と負圧面側とで同じであるが、他方その溝部27bのを、例えば図5〜図7に示すように羽根正圧面側が大きく、羽根負圧面側で小さくなるものとしたことを特徴としている。 In this embodiment, the cutout portions 27, 27... Are intermittently provided on the outer peripheral blade tip 15a of the blade 15 via the smooth portions 18, 18,. In the multiblade fan, the shape of the notches 27, 27... Is the same on the pressure surface side and the suction surface side, but the width of the groove 27b is as shown in FIGS. The blade positive pressure surface side is large and the blade negative pressure surface side is small .

なお、この場合の切欠部27,27・・・の溝部27bの正圧面側から負圧面側への深さ方向のの変化は、例えば図6および図7に示すように連続的であることが好ましい。 In this case, the change in the width in the depth direction from the pressure surface side to the suction surface side of the groove portion 27b of the notches 27, 27... Is continuous as shown in FIGS. Is preferred.

このような構成によると、切欠部27,27・・・の左右の溝面が前述の図14の(a),(b)および図15に示す従来例のようなストレートな切断面ではなく、図6のように正圧面側切欠面が幅広のテーパー面となり(図6の(b)参照)、それによって正圧面側の切欠部27,27・・・を通過する空気流の速度を効果的に上昇させることができ、例えば図8の矢線に示すようにファンより吹出される空気の流れを周方向に向けることで、有効にファン圧力を上昇させることができる。   According to such a configuration, the left and right groove surfaces of the notches 27, 27... Are not straight cut surfaces as in the conventional example shown in FIGS. 14 (a), 14 (b) and FIG. As shown in FIG. 6, the notch surface on the pressure side becomes a wide tapered surface (see FIG. 6B), thereby effectively reducing the velocity of the air flow passing through the notches 27, 27. For example, the fan pressure can be effectively increased by directing the flow of air blown from the fan in the circumferential direction as indicated by the arrow in FIG.

その結果、フィルタ等の抵抗がある場合でも、所定の風量を出すことができるようになり、従来の単に切欠きを設けた羽根よりも低回転で実現できるので、ファンの回転による騒音を低減させることもできる。   As a result, even when there is resistance such as a filter, it becomes possible to output a predetermined air volume, which can be realized at a lower rotation than a conventional blade having a notch, so that noise due to fan rotation is reduced. You can also.

また、羽根15の外周側翼端部15aの2次元性を無くすことができるので、吹出し時の翼後縁側で発生する後流渦を低減し、効果的に騒音を低下させることもできる。   Further, since the two-dimensionality of the outer peripheral blade tip 15a of the blade 15 can be eliminated, the wake vortex generated on the blade trailing edge side during blowing can be reduced, and the noise can be effectively reduced.

なお、このように上記切欠部27,27・・・のを羽根16の正圧面側と負圧面側とで異なる構成にする場合において、上記とは逆に、そのを例えば羽根正圧面側が小さく、羽根負圧面側で大きくなるようにすることもできる。 In the case where the width of the notches 27, 27... Is different between the pressure surface side and the suction surface side of the blade 16, the width is, for example, the blade pressure surface side. It can be made smaller and larger on the blade suction surface side.

そのようにした場合、上述した図6の(a)と(b)の関係から理解されるように、正圧面側の切欠部27の溝部27bの大きさが小さくなり、その分正圧面側の切欠部27,27・・・を通過する空気流の速度を上昇させることができ、ファンより吹出される空気の流れを周方向に向けることで、有効にファン圧力を上昇させることができる。   In such a case, as can be understood from the relationship between FIGS. 6A and 6B described above, the size of the groove 27b of the notch 27 on the pressure surface side is reduced, and the pressure surface side is correspondingly reduced. The speed of the air flow passing through the notches 27, 27... Can be increased, and the fan pressure can be effectively increased by directing the air flow blown from the fan in the circumferential direction.

その結果、フィルタ等の抵抗がある場合でも、所定の風量を出すことができるようになり、従来の単に切欠きを設けた羽根よりも低回転で実現できるので、ファンの回転による騒音を低減させることもできる。   As a result, even when there is resistance such as a filter, it becomes possible to output a predetermined air volume, which can be realized at a lower rotation than a conventional blade having a notch, so that noise due to fan rotation is reduced. You can also.

(最良の実施の形態3)
なお、以上の最良の実施の形態1の構成、すなわち羽根15の外周側翼端15aに断続的(または連続的)に切欠部17,17・・・を設けるとともに、該切欠部17,17・・・の形状を羽根正圧面側と負圧面側とで異なるものとした多翼ファンにおいて、さらに上記最良の実施の形態2の構成である上記切欠部17,17・・・の深さを正圧面側と負圧面側とで異なるものとする構成を組み合わせることも可能である。
(Best Mode 3)
In addition, the above-described configuration of the first embodiment, that is, the notch portions 17, 17... Are provided intermittently (or continuously) on the outer peripheral blade tip 15a of the blade 15 and the notches 17, 17,. In the multiblade fan in which the shape of the blade pressure surface side and the suction surface side are different, the depth of the notches 17, 17.. It is also possible to combine configurations that are different on the side and the suction surface side.

そのようにすると、それら両者の作用が相乗して、より有効にファン圧力が上昇する。   If it does so, the effect | action of both will synergize and a fan pressure will rise more effectively.

本願発明の最良の実施の形態1に係る多翼ファンの羽根車の羽根部の全体的な構成を示す斜視図(圧力面側)である。It is a perspective view (pressure surface side) which shows the whole structure of the blade | wing part of the impeller of the multiblade fan which concerns on best Embodiment 1 of this invention. 同羽根の要部の構成を示す羽根外周端側から切欠部方向に見た羽根外周側翼端部(切欠部)の拡大図((a)負圧面側から見た図、(b)正圧面側から見た図)である。Enlarged view of blade outer edge (notch) viewed from blade outer edge side to notch direction showing configuration of main part of blade ((a) view from suction surface side, (b) pressure surface side Figure seen from). 同羽根の切欠部位置における羽根内外方向の切断部の断面図(横断面図)である。It is sectional drawing (cross-sectional view) of the cutting | disconnection part of the blade inside and outside direction in the notch part position of the blade. 同羽根の切欠部位置における羽根車構成時の作用を示す断面図である。It is sectional drawing which shows the effect | action at the time of the impeller structure in the notch part position of the blade. 本願発明の最良の実施の形態2に係る多翼ファンの羽根車の羽根の構成を示す斜視図(圧力面側)である。It is a perspective view (pressure surface side) which shows the structure of the blade | wing of the impeller of the multiblade fan which concerns on best Embodiment 2 of this invention. 同羽根の要部の構成を示す羽根外周端側から切欠部方向に見た羽根外周側翼端部(切欠部)の拡大図((a)負圧面側から見た図、(b)正圧面側から見た図)である。Enlarged view of blade outer edge (notch) viewed from blade outer edge side to notch direction showing configuration of main part of blade ((a) view from suction surface side, (b) pressure surface side Figure seen from). 同羽根の切欠部位置における羽根内外方向の切断部の断面図(横断面図)である。It is sectional drawing (cross-sectional view) of the cutting | disconnection part of the blade inside and outside direction in the notch part position of the blade. 同羽根の切欠部位置における羽根車構成時の作用を示す断面図である。It is sectional drawing which shows the effect | action at the time of the impeller structure in the notch part position of the blade. 多翼ファンよりなる羽根車の適用例である従来一般の壁掛け型空気調和機の構成を示す縦断面図である。It is a longitudinal cross-sectional view which shows the structure of the conventional general wall-hanging type air conditioner which is an application example of the impeller which consists of a multiblade fan. 同多翼ファンよりなる羽根車の全体的な構成を示す斜視図である。It is a perspective view which shows the whole structure of the impeller which consists of the multiblade fan. 同多翼ファンよりなる羽根車の羽根における吹出空気流の状態を示す図である。It is a figure which shows the state of the blowing air flow in the blade | wing of the impeller which consists of the multiblade fan. 同多翼ファンの羽根車における従来例の羽根の構成例を示す平面図である。It is a top view which shows the structural example of the blade | wing of the prior art example in the impeller of the multiblade fan. 同多翼ファンの羽根車の羽根外周端部の切欠部の配設状態を示す全体的な斜視図(圧力面側)である。It is a whole perspective view (pressure surface side) which shows the arrangement | positioning state of the notch part of the blade outer peripheral edge part of the impeller of the multiblade fan. 同多翼ファンの羽根の負圧面側から見た切欠部形状(a)と正圧面側から見た切欠部形状(b)を示す図である。It is a figure which shows the notch part shape (a) seen from the suction surface side of the blade | wing of the multiblade fan, and the notch part shape (b) seen from the pressure surface side. 同多翼ファンの羽根の切欠部の構成を示す羽根前後方向に切断した切断部の断面図(横断面図)である。It is sectional drawing (cross-sectional view) of the cut part cut | disconnected in the blade front-back direction which shows the structure of the notch part of the blade | wing of the multiblade fan. 同多翼ファンの羽根車の羽根翼間部分(図12のA−A線断面部(a)と図12のB−B線断面部(b))の吹出側の空気の流れの状態を示す説明図(切欠部がない場合とある場合)である。The state of the flow of air on the blowout side of the inter-blade part of the impeller of the multiblade fan (cross-section part A-A in FIG. 12 and cross-section part BB in FIG. 12) is shown. It is explanatory drawing (when there is a case where there is no notch part).

3は多翼ファン(クロスフローファン)、7は羽根車、10はガイド部、11は舌部、14は円形支持プレート、15は羽根、15aは羽根外周側の翼端部、15bは羽根内周側の翼端部、16は回転軸、17,27は切欠部、18は平滑部、27aはテーパ面部、27bは溝部である。   3 is a multi-blade fan (cross flow fan), 7 is an impeller, 10 is a guide part, 11 is a tongue part, 14 is a circular support plate, 15 is a blade, 15a is a blade end part on the outer periphery of the blade, 15b is inside the blade A peripheral blade tip, 16 is a rotating shaft, 17 and 27 are notched portions, 18 is a smooth portion, 27a is a tapered surface portion, and 27b is a groove portion.

Claims (5)

羽根(15)の外周側翼端(15a)に断続的または連続的に切欠部(27),(27)・・・を設け、上記切欠部(27),(27)・・・の形状を羽根正圧面側と負圧面側とで異なるものとした多翼ファンにおいて、上記切欠部(27),(27)・・・の形状は略三角形であり、羽根正圧面側の三角形の面積が負圧面側の三角形の面積よりも大きく形成されていることを特徴とする多翼ファンIntermittently or continuously notch on the outer peripheral side tip of the blade (15) (15a) (27), only set (27) ..., the notch (27), the shape of the (27) ... In the multiblade fan that is different between the blade pressure surface side and the suction surface side, the shape of the notches (27), (27)... Is substantially triangular, and the area of the triangle on the blade pressure surface side is negative. A multiblade fan characterized in that it is formed larger than the area of a triangle on the pressure side . 羽根(15)の外周側翼端(15a)に断続的または連続的に切欠部(27),(27)・・・を設け、上記切欠部(27),(27)・・・の形状を羽根正圧面側と負圧面側とで異なるものとした多翼ファンにおいて、上記切欠部(27),(27)・・・の形状は略三角形であり、羽根正圧面側の三角形の面積が負圧面側の三角形の面積よりも小さく形成されていることを特徴とする多翼ファン。 The notches (27), (27), ... are provided intermittently or continuously on the outer wing tip (15a) of the blade (15), and the shape of the notches (27), (27),. In the multiblade fan that is different between the pressure surface side and the suction surface side, the shape of the notches (27), (27)... Is substantially triangular, and the area of the triangle on the blade pressure surface side is the suction surface. A multiblade fan characterized by being formed smaller than the area of the triangle on the side . 羽根(15)の外周側翼端(15a)に断続的または連続的に切欠部(27),(27)・・・を設け、上記切欠部(27),(27)・・・の形状を羽根正圧面側と負圧面側とで異なるものとした多翼ファンにおいて、上記切欠部(27),(27)・・・の形状は略台形であり、羽根正圧面側の台形の面積が負圧面側の台形の面積よりも大きく形成されていることを特徴とする多翼ファン。 The notches (27), (27), ... are provided intermittently or continuously on the outer wing tip (15a) of the blade (15), and the shape of the notches (27), (27),. In the multiblade fan that is different between the pressure surface side and the suction surface side, the shape of the notches (27), (27)... Is substantially trapezoidal, and the trapezoid area on the blade pressure surface side is the suction surface. A multiblade fan characterized in that it is formed larger than the area of the trapezoid on the side . 羽根(15)の外周側翼端(15a)に断続的または連続的に切欠部(27),(27)・・・を設け、上記切欠部(27),(27)・・・の形状を羽根正圧面側と負圧面側とで異なるものとした多翼ファンにおいて、上記切欠部(27),(27)・・・の形状は略台形であり、羽根正圧面側の台形の面積が負圧面側の台形の面積よりも小さく形成されていることを特徴とする多翼ファン。 The notches (27), (27), ... are provided intermittently or continuously on the outer wing tip (15a) of the blade (15), and the shape of the notches (27), (27),. In the multiblade fan that is different between the pressure surface side and the suction surface side, the shape of the notches (27), (27)... Is substantially trapezoidal, and the trapezoid area on the blade pressure surface side is the suction surface. A multiblade fan characterized by being formed smaller than the area of the trapezoid on the side . 羽根(15)の外周側翼端(15a)に断続的または連続的に切欠部(27),(27)・・・を設け、上記切欠部(27),(27)・・・の幅を羽根正圧面側と負圧面側とで異なるものとした多翼ファンにおいて、切欠部(27),(27)・・・の深さ方向の幅の変化は、連続的であることを特徴とする多翼ファン。The notches (27), (27)... Are provided intermittently or continuously on the outer wing tip (15a) of the blade (15), and the width of the notches (27), (27). In the multiblade fan that is different between the pressure surface side and the suction surface side, the change in the width in the depth direction of the notches (27), (27), ... is continuous. Wing fan.
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KR101883502B1 (en) 2011-11-22 2018-07-30 엘지전자 주식회사 Cross flow fan and air conditioner
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CN111963478B (en) * 2020-07-28 2021-10-01 宁波方太厨具有限公司 Blade for centrifugal fan, centrifugal fan and range hood

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