JP2017129069A - Centrifugal fan - Google Patents

Centrifugal fan Download PDF

Info

Publication number
JP2017129069A
JP2017129069A JP2016009419A JP2016009419A JP2017129069A JP 2017129069 A JP2017129069 A JP 2017129069A JP 2016009419 A JP2016009419 A JP 2016009419A JP 2016009419 A JP2016009419 A JP 2016009419A JP 2017129069 A JP2017129069 A JP 2017129069A
Authority
JP
Japan
Prior art keywords
blade
centrifugal fan
fluid
main flow
shroud
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
JP2016009419A
Other languages
Japanese (ja)
Inventor
遼 黒田
Ryo Kuroda
遼 黒田
欣公 田積
Yoshitaka Tazumi
欣公 田積
小川 修
Osamu Ogawa
修 小川
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.)
Panasonic Intellectual Property Management Co Ltd
Original Assignee
Panasonic Intellectual Property Management Co 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 Panasonic Intellectual Property Management Co Ltd filed Critical Panasonic Intellectual Property Management Co Ltd
Priority to JP2016009419A priority Critical patent/JP2017129069A/en
Publication of JP2017129069A publication Critical patent/JP2017129069A/en
Pending legal-status Critical Current

Links

Images

Abstract

PROBLEM TO BE SOLVED: To reduce turbulence noise because a main flow passing between blades is not disturbed.SOLUTION: A centrifugal fan 100 is provided, which is composed of a main plate 101, a shroud 102, and a blade 103. The blade 103 forms a negative pressure surface 143 which has a small distance between a blade surface composed of a front edge 113 and a rear edge 123 of the blade 103 and a rotary shaft, and a hole 110 is provided on the negative pressure surface 143. Therefore, although a part of a fluid blown off from the centrifugal fan 100 is blown off from the hole 110, by speed difference between a main flow 900 and a discharge flow 910, the main flow 900 is sucked to the blade surface side, and the main flow 900 is blown off along the blade 103 in the blade rear edge 123 direction, so that a turbulence noise can be reduced.SELECTED DRAWING: Figure 1

Description

本発明は、空気調和機の室内機などに幅広く用いられる遠心ファンを備えた送風装置に関するものである。   The present invention relates to an air blower including a centrifugal fan that is widely used in indoor units of air conditioners.

従来、この種の遠心ファンは、主板と、シュラウドと、翼と、で構成されており、前記翼の前縁に段差面を備えた不連続な形状とするとともに、前記段差面を回転軸線に垂直な面に対して所定の傾斜角をもつ傾斜面を有している。(例えば、特許文献1参照)
図6は前記公報に記載された従来遠心ファンの回転軸方向の断面図を示すものである。図6に示すように、主板101と、主板101に対向配置され略中空円錐台形状のシュラウド102と、主板101とシュラウド102との間に配置される翼103と、を有する遠心ファン100で構成され、翼前縁113に段差面210を備えた不連続な形状とするとともに、段差面210を回転軸150に垂直な面に対して所定の傾斜角をもつ傾斜面220を有している。
Conventionally, this type of centrifugal fan is composed of a main plate, a shroud, and a blade. The centrifugal fan has a discontinuous shape with a step surface at the leading edge of the blade, and the step surface is a rotation axis. An inclined surface having a predetermined inclination angle with respect to a vertical surface is provided. (For example, see Patent Document 1)
FIG. 6 shows a sectional view of the conventional centrifugal fan described in the publication in the direction of the rotation axis. As shown in FIG. 6, the centrifugal fan 100 includes a main plate 101, a substantially hollow frustoconical shroud 102 disposed opposite to the main plate 101, and a blade 103 disposed between the main plate 101 and the shroud 102. In addition, the blade leading edge 113 has a discontinuous shape having a step surface 210, and the step surface 210 has an inclined surface 220 having a predetermined inclination angle with respect to a surface perpendicular to the rotation shaft 150.

特開2001−153094号公報JP 2001-153094 A

しかしながら、前記従来の構成では、ファンモータの所定の回転に伴い、シュラウド102の小径側開口部から吸込まれた流体(以下、主流900と呼ぶ)が、傾斜面220への衝突によって、その流れが乱され、翼前縁113から翼後縁123に向かうに従って次第に成長する縦渦920が生成されることで、主流900の有効流路が低下し、縦渦920と主流900が混合した際に主流900が乱されるため、反って乱流騒音が増大する課題を有していた。   However, in the above-described conventional configuration, the fluid sucked from the small-diameter side opening of the shroud 102 (hereinafter referred to as the main flow 900) with the predetermined rotation of the fan motor flows due to the collision with the inclined surface 220. When the longitudinal vortex 920 that is disturbed and gradually grows from the blade leading edge 113 toward the blade trailing edge 123 is generated, the effective flow path of the main flow 900 is reduced, and the main flow when the vertical vortex 920 and the main flow 900 are mixed is reduced. Since 900 is disturbed, there is a problem that the turbulent noise increases due to warping.

本発明は、前記従来の課題を解決するもので、翼の負圧面に生ずる流体の乱れを低減し、乱流騒音が低下する送風装置を提供することを目的とする。   The present invention solves the above-described conventional problems, and an object thereof is to provide a blower that reduces fluid turbulence generated on the suction surface of a blade and reduces turbulent noise.

前記従来の課題を解決するために、本発明の遠心ファンは、主板と、シュラウドと、翼と、で構成されており、ある所定の肉厚を有する中空の翼と、前記翼は前記翼の前縁と後縁で構成される翼面と回転軸との距離が小さい側の負圧面を形成し、前記負圧面に孔が設けられている。   In order to solve the above-described conventional problems, a centrifugal fan of the present invention includes a main plate, a shroud, and a blade, a hollow blade having a predetermined thickness, and the blade is a member of the blade. A suction surface on the side where the distance between the blade surface constituted by the front edge and the rear edge and the rotating shaft is small is formed, and a hole is provided in the suction surface.

これによって、前記遠心ファンを所定の回転方向に回転させると、前記翼の昇圧作用によって、前記シュラウド小径側開口部から吸込まれた流体は、前記遠心ファンの回転軸方向の断面で見たときに、前記流体が前記シュラウドと前記主板で形成される略並行な2円弧の流体流路で曲げられ前記翼と前記翼の間を通過(以下、主流と呼ぶ)し、略遠心方向に吹出される。   As a result, when the centrifugal fan is rotated in a predetermined rotation direction, the fluid sucked from the shroud small-diameter side opening due to the pressure increasing action of the blades is seen when viewed in a cross section in the rotation axis direction of the centrifugal fan. The fluid is bent by a substantially parallel two-circular fluid flow path formed by the shroud and the main plate, passes between the wings and the wings (hereinafter referred to as main flow), and is blown out in a substantially centrifugal direction. .

前記遠心ファンから吹出された流体の一部は前記翼の前記中空部の流体流路を通過し、前記孔から吹出される(以下、吐出流と呼ぶ)。ここで、速度の異なる流体同士が合流する場合、速度の大きい流体が速度の小さい流体側へ吸引されるため、前記主流と前記吐出流の速度差によって、前記主流が前記吐出流側へ即ち前記翼面側に吸引され、前記主流が
前記翼後縁方向に前記翼面を沿うように吹出される。
Part of the fluid blown out from the centrifugal fan passes through the fluid flow path in the hollow portion of the blade and is blown out from the hole (hereinafter referred to as a discharge flow). Here, when fluids having different velocities merge, a fluid having a high speed is sucked to a fluid side having a low speed, and therefore, the main flow is moved to the discharge flow side, i.e. Suction is performed on the blade surface side, and the main flow is blown out along the blade surface in the blade trailing edge direction.

また、本発明の送風装置は、前記孔を覆う前記翼後縁側が開口されたガイダーを有している。   Moreover, the air blower of this invention has the guider by which the said blade trailing edge side which covers the said hole was opened.

前記遠心ファンの動作点が高静圧・低風量では、前記遠心ファンの回転軸に対して垂直方向の断面で見た場合に、遠心方向の速度成分が低下するため、前記翼に流入する流体の流入角が本来の動作点よりも小さくなり、前記負圧面側を通過する流体の剥離点が前記翼前縁側に移動するため、流体の乱れ成分が大きくなる。   When the operating point of the centrifugal fan is high static pressure and low airflow, the fluid flowing into the blades because the speed component in the centrifugal direction decreases when viewed in a cross section perpendicular to the rotational axis of the centrifugal fan. The inflow angle becomes smaller than the original operating point, and the separation point of the fluid passing through the suction surface moves to the blade leading edge side, so that the fluid turbulence component increases.

このような動作点の場合、前記ガイダーが前記吐出流の吐出方向を前記翼後縁方向にガイドすることで、前記吐出流の吐出角度が前記翼後縁方向となり、更に前記吐出流の速度を小さくするため、前記主流と前記吐出流の速度差が一層大きくなり前記主流が前記翼面に吸引され前記翼面を前記翼後縁方向に沿うように送風される。   In the case of such an operating point, the guider guides the discharge direction of the discharge flow toward the blade trailing edge, so that the discharge angle of the discharge flow becomes the blade trailing edge direction, and further the speed of the discharge flow is increased. In order to make it smaller, the speed difference between the main flow and the discharge flow becomes larger, and the main flow is sucked into the blade surface and blown along the blade trailing edge direction.

本発明の送風装置は、前記翼面上を前記翼後縁方向に沿うように送風されるため、乱流騒音が低減できる。   Since the blower of the present invention is blown on the blade surface along the blade trailing edge direction, turbulent noise can be reduced.

本発明の実施の形態1に係る遠心ファンの一例を示すシュラウド小径開口部側斜視図The shroud small diameter opening side perspective view which shows an example of the centrifugal fan which concerns on Embodiment 1 of this invention 本発明の実施の形態1に係る遠心ファンの一例を示す回転軸に対し垂直方向翼断面図Cross-sectional view of a blade in a direction perpendicular to a rotation shaft showing an example of a centrifugal fan according to Embodiment 1 of the present invention 本発明の実施の形態1に係る遠心ファンの一例を示す回転軸方向翼断面図Rotational axis direction blade sectional view showing an example of a centrifugal fan according to Embodiment 1 of the present invention 本発明の実施の形態1に係る遠心ファンの一例を示す斜視図The perspective view which shows an example of the centrifugal fan which concerns on Embodiment 1 of this invention. 本発明の実施の形態2に係る遠心ファンの一例を示す回転軸に対し垂直方向翼断面図Cross-sectional view of a blade in a direction perpendicular to a rotation shaft showing an example of a centrifugal fan according to Embodiment 2 of the present invention 従来技術1記載の遠心ファンの一例を示す回転軸方向翼断面図Rotating axial direction blade sectional view showing an example of the centrifugal fan described in the prior art 1

第1の発明は、ファンモータの回転シャフト軸と連結されており前記ファンモータを格納するための一端が開口した略中空円錐台形状を有する主板と、前記主板に対向配置される略中空円錐台形状のシュラウドと、前記主板と前記シュラウドとの間に配置され、ある所定の肉厚を有する中空の翼と、前記翼は前記翼の前縁と後縁で構成される翼面と回転軸との距離が小さい側の負圧面を形成し前記負圧面に孔が設けられている。   A first aspect of the invention is a main plate having a substantially hollow truncated cone shape that is connected to a rotating shaft of a fan motor and has one end opened to store the fan motor, and a substantially hollow truncated cone disposed opposite to the main plate. A shroud having a shape, a hollow wing disposed between the main plate and the shroud and having a predetermined thickness, the wing includes a wing surface and a rotation shaft configured by a leading edge and a trailing edge of the wing. The suction surface having a smaller distance is formed, and a hole is provided in the suction surface.

前記遠心ファンを所定の回転方向に回転させると、前記翼の昇圧作用によって、前記シュラウド小径側開口部から吸込まれた流体は、前記遠心ファンの回転軸方向の断面で見たときに、前記流体が前記シュラウドと前記主板で形成される略並行な2円弧の流体流路で曲げられ前記翼と前記翼の間を通過(以下、主流と呼ぶ)し、略遠心方向に吹出される。   When the centrifugal fan is rotated in a predetermined rotation direction, the fluid sucked from the shroud small-diameter side opening due to the pressure-increasing action of the blades shows the fluid when viewed in a section in the rotation axis direction of the centrifugal fan. Is bent by a substantially parallel two-circular fluid flow path formed by the shroud and the main plate, passes between the blades and the blades (hereinafter referred to as main flow), and is blown out in a substantially centrifugal direction.

ここで、前記遠心ファンから吹出された流体の一部は前記翼の前記中空部の流体流路を通過し、前記孔から吹出される(以下、吐出流と呼ぶ)。速度の異なる流体同士が合流する場合、速度の大きい流体が速度の小さい流体側へ吸引されるため、前記主流と前記吐出流の速度差によって、前記主流が前記吐出流側へ即ち前記翼面側に吸引され、前記主流が前記翼後縁方向に前記翼面を沿うように吹出される。   Here, a part of the fluid blown out from the centrifugal fan passes through the fluid flow path in the hollow portion of the blade and is blown out from the hole (hereinafter referred to as a discharge flow). When fluids having different velocities merge, a fluid having a high speed is sucked to a fluid side having a low speed, and therefore, the main flow is moved to the discharge flow side, that is, the blade surface side due to the speed difference between the main flow and the discharge flow. The main stream is blown out along the blade surface in the direction of the trailing edge of the blade.

これによって、前記翼面上を前記翼後縁方向に沿うように送風されるため、乱流騒音が低減できる。   As a result, since the air is blown along the blade trailing edge direction on the blade surface, turbulent noise can be reduced.

第2の発明は、特に第1の発明の前記孔を、前記孔を覆う前記翼後縁側が開口されたガイダーを有している。   The second invention has a guider in which the wing trailing edge side covering the hole is opened, particularly the hole of the first invention.

前記遠心ファンの動作点が高静圧・低風量では、前記遠心ファンの回転軸に対して垂直方向の断面で見た場合に、遠心方向の速度成分が低下するため、前記翼に流入する流体の流入角が本来の動作点よりも小さくなり、前記負圧面側を通過する流体の剥離点が前記翼前縁側に移動するため、流体の乱れ成分が大きくなる。   When the operating point of the centrifugal fan is high static pressure and low airflow, the fluid flowing into the blades because the speed component in the centrifugal direction decreases when viewed in a cross section perpendicular to the rotational axis of the centrifugal fan. The inflow angle becomes smaller than the original operating point, and the separation point of the fluid passing through the suction surface moves to the blade leading edge side, so that the fluid turbulence component increases.

このような動作点の場合、前記ガイダーが前記吐出流の吐出方向を前記翼後縁方向にガイドすることで、前記吐出流の吐出角度が前記翼後縁方向となり、更に前記吐出流の速度を小さくするため、前記主流と前記吐出流の速度差が一層大きくなり前記主流が前記翼面に吸引され前記翼面を前記翼後縁方向に沿うように送風される。   In the case of such an operating point, the guider guides the discharge direction of the discharge flow toward the blade trailing edge, so that the discharge angle of the discharge flow becomes the blade trailing edge direction, and further the speed of the discharge flow is increased. In order to make it smaller, the speed difference between the main flow and the discharge flow becomes larger, and the main flow is sucked into the blade surface and blown along the blade trailing edge direction.

前記遠心ファンの動作点が、高静圧・低風量の場合、前記遠心ファンの回転軸に対して垂直方向の断面で見た場合に、遠心方向の速度成分が低下するため、流入角が本来の動作点よりも小さくなり前記翼と前記翼の間の乱れのスケールが増加傾向となるが、本発明において、前記主流が乱されることなく前記翼面に吸引されるため、乱流騒音が低減できる。   When the operating point of the centrifugal fan is high static pressure and low air volume, the speed component in the centrifugal direction decreases when viewed in a cross section perpendicular to the rotational axis of the centrifugal fan. However, in the present invention, since the main flow is attracted to the blade surface without being disturbed, turbulent noise is generated. Can be reduced.

乱流騒音の低減によって、遠心ファンのコンパクト化と遠心ファンの壁面上の圧力変動を低減できるため、遠心ファンの動バランスが良化され、空気調和機の室内機に搭載した場合に周辺部品との距離が小さくでき、結果、室内機がコンパクト化できる。   By reducing the turbulent noise, the centrifugal fan can be made more compact and the pressure fluctuation on the wall surface of the centrifugal fan can be reduced.This improves the dynamic balance of the centrifugal fan, and improves the balance of peripheral components when installed in an indoor unit of an air conditioner. Distance can be reduced, and as a result, the indoor unit can be made compact.

以下、本発明の各実施形態について、送風装置を図面に基づき説明する。なお、以下に説明する各実施形態は一例であり、本発明は各実施形態により限定されるものではない。   Hereinafter, a blower will be described with reference to the drawings for each embodiment of the present invention. Each embodiment described below is an example, and the present invention is not limited to each embodiment.

(実施の形態1)
図1は本発明の実施の形態1に係る遠心ファンの一例を示すシュラウド小径開口部側斜視図を示し、図2は本発明の実施の形態1に係る遠心ファンの一例を示す回転軸に対し垂直方向翼断面図を示し、図3は本発明の実施の形態1に係る遠心ファンの一例を示す回転軸方向翼断面図を示し、図4は本発明の実施の形態1に係る遠心ファンの一例を示す斜視図を示すものである。
(Embodiment 1)
1 shows a perspective view of a shroud small-diameter opening side showing an example of a centrifugal fan according to Embodiment 1 of the present invention, and FIG. 2 shows a rotation shaft showing an example of a centrifugal fan according to Embodiment 1 of the present invention. FIG. 3 is a cross-sectional view of a vertical axis blade, FIG. 3 is a cross-sectional view of a rotary axis blade showing an example of a centrifugal fan according to Embodiment 1 of the present invention, and FIG. The perspective view which shows an example is shown.

第1の発明は、ファンモータの回転シャフト軸と連結されておりファンモータを格納するための一端が開口した略中空円錐台形状を有する主板101と、主板101に対向配置される略中空円錐台形状のシュラウド102と、主板101とシュラウド102との間に配置され、ある所定の肉厚を有する中空の翼103と、翼103は翼103の前縁113と後縁123で構成される翼面と回転軸との距離が小さい側の負圧面143を形成し負圧面143に孔110が設けられている。   1st invention is connected with the rotating shaft shaft of a fan motor, the main plate 101 which has the substantially hollow truncated cone shape which the end for storing a fan motor opened, and the substantially hollow truncated cone arrange | positioned facing the main plate 101 A blade having a shape, a hollow blade 103 disposed between the main plate 101 and the shroud 102 and having a certain predetermined thickness, and the blade 103 is constituted by a leading edge 113 and a trailing edge 123 of the blade 103. The negative pressure surface 143 on the side where the distance between the rotary shaft and the rotating shaft is small is formed, and a hole 110 is provided in the negative pressure surface 143.

遠心ファン100を所定の回転方向Rに回転させると、翼103の昇圧作用によって、シュラウド102の小径側開口部から吸込まれた流体は、遠心ファン100の回転軸方向の断面で見たときに、流体がシュラウド102と主板101で形成される略並行な2円弧の流体流路で曲げられ翼103と翼103の間を通過(以下、主流900と呼ぶ)し、略遠心方向に吹出される。   When the centrifugal fan 100 is rotated in a predetermined rotation direction R, the fluid sucked from the small-diameter side opening of the shroud 102 due to the pressure increasing action of the blades 103 is, when viewed in a section in the rotation axis direction of the centrifugal fan 100, The fluid is bent by a substantially parallel two-circular fluid flow path formed by the shroud 102 and the main plate 101, passes between the blades 103 and the blades 103 (hereinafter referred to as a main flow 900), and is blown out in a substantially centrifugal direction.

遠心ファン100から吹出された流体の一部は翼103の前記中空部の流体流路133を通過し、孔110から吹出される(以下、吐出流910と呼ぶ)。ここで、速度の異なる流体同士が合流する場合、速度の大きい流体が速度の小さい流体側へ吸引されるため、
主流900と吐出流910の速度差によって、主流900が吐出流910方向、すなわち翼面側に吸引され、主流900が翼後縁123方向に翼103を沿うように吹出される。
Part of the fluid blown out from the centrifugal fan 100 passes through the fluid flow path 133 in the hollow portion of the blade 103 and is blown out from the hole 110 (hereinafter referred to as a discharge flow 910). Here, when fluids with different velocities merge, a fluid with a high speed is sucked to a fluid side with a low speed,
Due to the speed difference between the main flow 900 and the discharge flow 910, the main flow 900 is sucked in the discharge flow 910 direction, that is, the blade surface side, and the main flow 900 is blown out along the blade 103 in the blade trailing edge 123 direction.

これによって、翼103面上を翼後縁123方向に沿うように送風されるため、乱流騒音が低減できる。   As a result, air is blown on the surface of the blade 103 along the direction of the blade trailing edge 123, so that turbulent noise can be reduced.

(実施の形態2)
図5は本発明の実施の形態2に係る遠心ファンの一例を示す回転軸に対し垂直方向翼断面図を示すものである。全体の構成は、図1および図2、図3に示すものと同様であり、同一構成要素には同一符号を付し、その説明を省略する。
(Embodiment 2)
FIG. 5 is a cross-sectional view of a blade in a direction perpendicular to the rotation axis showing an example of a centrifugal fan according to Embodiment 2 of the present invention. The entire configuration is the same as that shown in FIGS. 1, 2, and 3, and the same components are denoted by the same reference numerals and description thereof is omitted.

特に第1の発明の孔110を、孔110を覆う翼後縁側が開口されたガイダー211を有している。   In particular, the hole 110 according to the first aspect of the invention has a guider 211 having an opening on the wing trailing edge side covering the hole 110.

遠心ファン100を所定の回転方向Rに回転させると、翼103の昇圧作用によって、シュラウド102の小径側開口部から吸込まれた流体は、遠心ファン100の回転軸方向の断面で見たときに、流体がシュラウド102と主板101で形成される略並行な2円弧の流体流路で曲げられ翼103と翼103の間を通過(以下、主流900と呼ぶ)し、略遠心方向に吹出される。   When the centrifugal fan 100 is rotated in a predetermined rotation direction R, the fluid sucked from the small-diameter side opening of the shroud 102 due to the pressure increasing action of the blades 103 is, when viewed in a section in the rotation axis direction of the centrifugal fan 100, The fluid is bent by a substantially parallel two-circular fluid flow path formed by the shroud 102 and the main plate 101, passes between the blades 103 and the blades 103 (hereinafter referred to as a main flow 900), and is blown out in a substantially centrifugal direction.

遠心ファン100から吹出された流体の一部は翼103の前記中空部の流体流路を通過し、孔110から吹出される(以下、吐出流910と呼ぶ)。遠心ファン100の動作点が高静圧・低風量では、遠心ファン100の回転軸150に対して垂直方向の断面で見た場合に、遠心方向の速度成分が低下するため、翼103に流入する流体の流入角が本来の動作点よりも小さくなり、負圧面143を通過する流体の剥離点が翼前縁113に移動するため、流体の乱れ成分が大きくなる。   Part of the fluid blown out from the centrifugal fan 100 passes through the fluid flow path in the hollow portion of the blade 103 and is blown out from the hole 110 (hereinafter referred to as a discharge flow 910). When the operating point of the centrifugal fan 100 is high static pressure and low airflow, when viewed in a cross section perpendicular to the rotating shaft 150 of the centrifugal fan 100, the centrifugal velocity component decreases, and therefore flows into the blades 103. The fluid inflow angle becomes smaller than the original operating point, and the separation point of the fluid passing through the suction surface 143 moves to the blade leading edge 113, so that the fluid turbulence component increases.

このような動作点の場合、ガイダー211が吐出流910の吐出方向を翼後縁123にガイドすることで、吐出流910の吐出角度が翼後縁123方向となり、更に吐出流910の速度を小さくするため、主流900と吐出流910の速度差が一層大きくなり主流900が翼103に吸引され翼103を翼後縁123方向に沿うように送風される。   In such an operating point, the guider 211 guides the discharge direction of the discharge flow 910 to the blade trailing edge 123, so that the discharge angle of the discharge flow 910 becomes the direction of the blade trailing edge 123, and the velocity of the discharge flow 910 is further reduced. Therefore, the speed difference between the main flow 900 and the discharge flow 910 is further increased, and the main flow 900 is sucked into the blade 103 and blown along the blade trailing edge 123 direction.

これによって、遠心ファン100の動作点が、高静圧・低風量の場合、主流900が乱されることなく翼103に吸引されるため、乱流騒音が低減できる。   Thereby, when the operating point of the centrifugal fan 100 is high static pressure and low air volume, the main flow 900 is sucked into the blades 103 without being disturbed, so that turbulent noise can be reduced.

乱流騒音の低減によって、遠心ファン100のコンパクト化と遠心ファン100の翼面上の圧力変動を低減できるため、遠心ファン100の動バランスが良化され、空気調和機の室内機に搭載した場合に周辺部品との距離が小さくでき、結果、空気調和機の室内機がコンパクト化できる。   When the centrifugal fan 100 is compact and the fluctuation in pressure on the blade surface of the centrifugal fan 100 can be reduced by reducing the turbulent noise, the dynamic balance of the centrifugal fan 100 is improved and the centrifugal fan 100 is installed in an indoor unit of an air conditioner. In addition, the distance from the peripheral parts can be reduced, and as a result, the indoor unit of the air conditioner can be made compact.

以上のように、本発明に係る送風装置の乱流騒音低減が可能となるので、家庭用及び業務用の各種形式の空気調和機の室内機に適用することができる。   As described above, since the turbulent flow noise of the blower according to the present invention can be reduced, it can be applied to indoor units of various types of air conditioners for home use and business use.

100 遠心ファン
101 主板
102 シュラウド
103 翼
110 孔
113 翼前縁
123 翼後縁
133 流体流路
143 負圧面
150 回転軸
210 段差面
211 ガイダー
900 主流
910 吐出流
920 縦渦
100 Centrifugal fan 101 Main plate 102 Shroud 103 Blade 110 Hole 113 Blade leading edge 123 Blade trailing edge 133 Fluid flow path 143 Negative pressure surface 150 Rotating shaft 210 Step surface 211 Guider 900 Main flow 910 Discharge flow 920 Vertical vortex

Claims (2)

一端が開口した略中空円錐台形状を有する主板と、
前記主板に対向配置される略中空円錐台形状のシュラウドと、
前記主板と前記シュラウドとの間に配置され、ある所定の肉厚を有する中空の翼と、
を有する遠心ファンにおいて、
前記翼は前記翼の前縁と後縁で構成される翼面と回転軸との距離が小さい側の負圧面を形成し、
前記負圧面に孔を設けたことを特徴とする、遠心ファン。
A main plate having a substantially hollow truncated conical shape with one end open;
A substantially hollow frustoconical shroud disposed opposite to the main plate;
A hollow wing disposed between the main plate and the shroud and having a predetermined thickness;
In a centrifugal fan having
The blade forms a suction surface on the side where the distance between the blade surface constituted by the leading edge and the trailing edge of the blade and the rotating shaft is small,
A centrifugal fan comprising a hole in the suction surface.
前記孔を覆う前記翼後縁側が開口されたガイダーを有する、
請求項1に記載の遠心ファン。
A guider having an opening on the wing trailing edge side covering the hole;
The centrifugal fan according to claim 1.
JP2016009419A 2016-01-21 2016-01-21 Centrifugal fan Pending JP2017129069A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2016009419A JP2017129069A (en) 2016-01-21 2016-01-21 Centrifugal fan

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2016009419A JP2017129069A (en) 2016-01-21 2016-01-21 Centrifugal fan

Publications (1)

Publication Number Publication Date
JP2017129069A true JP2017129069A (en) 2017-07-27

Family

ID=59394518

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2016009419A Pending JP2017129069A (en) 2016-01-21 2016-01-21 Centrifugal fan

Country Status (1)

Country Link
JP (1) JP2017129069A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108390500A (en) * 2018-02-08 2018-08-10 浙江希尔富电气有限公司 One kind being based on brushless motor and the special noise reduction combined mechanism of wind turbine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108390500A (en) * 2018-02-08 2018-08-10 浙江希尔富电气有限公司 One kind being based on brushless motor and the special noise reduction combined mechanism of wind turbine

Similar Documents

Publication Publication Date Title
JP4994421B2 (en) Centrifugal fan and air conditioner
JP5303877B2 (en) Centrifugal blower
JP4946396B2 (en) Centrifugal blower
JP6143596B2 (en) Centrifugal blower and vehicle air conditioner equipped with the centrifugal blower
WO2014061642A1 (en) Turbo fan and air conditioner
WO2014125710A1 (en) Outdoor cooling unit for air conditioning device for vehicle
JP6203294B2 (en) Centrifugal fan and air conditioner
JP2015063896A (en) Single suction type centrifugal blower
JP5682751B2 (en) Multi-blade blower
JP6739656B2 (en) Impeller, blower, and air conditioner
JP6250145B2 (en) Centrifugal blower and vacuum cleaner
JP5396965B2 (en) Axial blower, air conditioner and ventilator
JP2019113037A (en) Multiblade centrifugal fan
JP2017129069A (en) Centrifugal fan
JP6695509B1 (en) Centrifugal fan and air conditioner
JP2019127865A (en) Centrifugal fan
CN106609763B (en) Centrifugal fan
JP2010242597A (en) Axial blower and air conditioner
JP6191536B2 (en) Blower
EP3315786A1 (en) Turbofan and air conditioner in which same is used
JP6486459B2 (en) Centrifugal blower
US2211671A (en) Fan mounting
JP2016070075A (en) Centrifugal fan
JP2013217236A (en) Air-blowing device
WO2022085332A1 (en) Blower