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JP2008157113A - Blower - Google Patents

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Publication number
JP2008157113A
JP2008157113A JP2006346975A JP2006346975A JP2008157113A JP 2008157113 A JP2008157113 A JP 2008157113A JP 2006346975 A JP2006346975 A JP 2006346975A JP 2006346975 A JP2006346975 A JP 2006346975A JP 2008157113 A JP2008157113 A JP 2008157113A
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Prior art keywords
blower
blade
shaped
blade surface
grooves
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JP2006346975A
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Japanese (ja)
Inventor
Toru Iwata
透 岩田
Akira Komatsu
彰 小松
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Daikin Industries Ltd
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Daikin Industries Ltd
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Priority to JP2006346975A priority Critical patent/JP2008157113A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/68Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
    • F04D29/681Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/38Blades
    • F04D29/384Blades characterised by form
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/20Rotors
    • F05D2240/30Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/306Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the suction side of a rotor blade

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

【課題】送風機の送風翼の低圧側翼面に送風音低減用の溝又は突起を形成するにあたり、その騒音低減効果を増進させること。
【解決手段】複数の送風翼をそなえた送風機において、前記送風翼の低圧側翼面に同低圧側翼面に沿って流れる空気流の流線に対して傾斜した直線状のエッジをもつ多数の溝又は突起を設ける。
各送風翼に形成した溝又は突起は、空気流の流線に対して傾斜した直線状のエッジをもつようにされているので、空気流が傾斜エッジと接触する長さが長くなり、上記の境界層剥離防止効果が大きくなる。
溝又は突起はその傾斜方向が同一方向とされていてもよく、その傾斜方向が相互に交叉する方向とされていてもよい。
溝又は突起はその形状がV字型又は略V字型であり、そのV字屈曲部が送風翼の低圧側翼面に沿って流れる空気流の上流側又は下流側に向いているようにすることができる。
【選択図】 図9
An object of the present invention is to enhance the noise reduction effect in forming a groove or protrusion for reducing blowing noise on a low pressure side blade surface of a blower blade of a blower.
In a blower having a plurality of blower blades, a plurality of grooves having linear edges inclined with respect to streamlines of airflow flowing along the low pressure side blade surface on the low pressure side blade surface of the blower blade, or Protrusions are provided.
The grooves or protrusions formed on each blower blade have a linear edge that is inclined with respect to the streamline of the airflow, so that the length of contact of the airflow with the inclined edge increases, The boundary layer peeling prevention effect is increased.
The grooves or protrusions may have the same inclination direction, or the inclination directions may cross each other.
The shape of the groove or protrusion is V-shaped or substantially V-shaped, and the V-shaped bent portion is directed to the upstream side or the downstream side of the air flow flowing along the low-pressure side blade surface of the blower blade. Can do.
[Selection] Figure 9

Description

本願発明は、空気調和機用プロペラファンなどの送風機に関するものである。   The present invention relates to a blower such as a propeller fan for an air conditioner.

一般に空気調和機用のプロペラファンなどの送風機では、たとえば図17に示すように、モータ等の回転駆動手段に連結されるボス部1に固定して設けられたハブ3の外周に所定のピッチと翼角をもって複数枚の翼2,2・・・を植設して構成されており、その翼列は上記翼2,2・・・の根元部断面から先端断面に向かうにつれて周速および翼ピッチが大きくなるようになっている。   In general, in a blower such as a propeller fan for an air conditioner, as shown in FIG. 17, for example, a predetermined pitch is set on the outer periphery of a hub 3 fixed to a boss portion 1 connected to a rotation driving means such as a motor. Is configured by implanting a plurality of blades 2, 2... With a blade angle, and the blade row has a circumferential speed and a blade pitch from the root cross section toward the tip cross section of the blades 2, 2,. Is getting bigger.

ところで、該プロペラファンが回転すると、所定レベルの騒音を発生するが、その原因として例えば次のような現象が考えられている。   By the way, when the propeller fan rotates, noise of a predetermined level is generated. As the cause, for example, the following phenomenon is considered.

すなわち、回転時における各翼2,2・・・の低圧側翼面の空気圧は翼の前部側で高く、後部側で低くなり、それが翼自体の下流側への傾斜度合に応じて更に顕著となる。その結果、例えば図18に示すように翼の下流側低圧面側で空気流の剥離を生じ、該剥離部で圧力の変動を生じて空力性能の悪化や騒音の原因となっていた。   That is, the air pressure of the low pressure side blade surface of each blade 2, 2... During rotation is high on the front side of the blade and low on the rear side, which is more remarkable depending on the degree of inclination of the blade itself toward the downstream side. It becomes. As a result, for example, as shown in FIG. 18, separation of the air flow occurs on the downstream low pressure surface side of the blade, and pressure variation occurs in the separation portion, resulting in deterioration of aerodynamic performance and noise.

そこで、該問題に対する対策として例えば特開平3−294699号公報(第1図)に示されるように、従来上記翼の低圧面側に複数個の円形状ディンプルを形成し、該ディンプルの剥離低減作用によって騒音の発生量を低くするようにしたもの(本願の図19)や、特開2003−278696号公報(図3)に示すように、送風翼の低圧側翼面に該翼面に沿って流動する空気流にほぼ平行な溝又は突起を形成したもの(本願の図20)が知られている。   Therefore, as a countermeasure against this problem, for example, as shown in Japanese Patent Laid-Open No. 3-294699 (FIG. 1), a plurality of circular dimples are conventionally formed on the low-pressure surface side of the blade, and the dimple peeling-reducing action is achieved. As shown in Japanese Patent Application Laid-Open No. 2003-278696 (FIG. 3), the noise generation amount is reduced along the blade surface. There is known one having grooves or protrusions formed substantially parallel to the air flow (FIG. 20 of the present application).

特開平3−294699号公報(第1図)JP-A-3-294699 (FIG. 1) 特開2003−278696号公報(図3)Japanese Patent Laying-Open No. 2003-278696 (FIG. 3)

確かに、上記特許文献1のように翼(本願の図19中の符号102)の低圧面側に多数個のディンプル(本願の図19中の符号111)を設けると、ディンプル内に二次流れが生じ、それによって局所的に壁面での流速が回復し、境界層の発達を抑えることができるので、流れの剥離度合が低下することが予想され、同剥離部の圧力変動も低下し、騒音低減に寄与し得ると考えられる。   Certainly, when a large number of dimples (reference numeral 111 in FIG. 19 of the present application) are provided on the low pressure surface side of the blade (reference numeral 102 in FIG. 19 of the present application) as in the above-mentioned Patent Document 1, a secondary flow is generated in the dimple. As a result, the flow velocity at the wall surface is recovered locally and the development of the boundary layer can be suppressed, so that the degree of flow separation is expected to decrease, the pressure fluctuation at the separation portion also decreases, and noise It is thought that it can contribute to reduction.

一方、上記特許文献2に示すように、送風翼の低圧側翼面に溝又は突起(本願の図20中の符号120)を形成したものにあっては、当該溝又は突起120の形成方向が空気流の流線に対して平行であるため、空気流に影響を与える溝又は突起のエッジ部分の長さが十分に得られないという問題がある。   On the other hand, as shown in Patent Document 2, in the case where grooves or protrusions (reference numeral 120 in FIG. 20 of the present application) are formed on the low-pressure blade surface of the blower blade, the formation direction of the grooves or protrusions 120 is air. Since it is parallel to the streamline of the flow, there is a problem that the length of the edge portion of the groove or the projection that affects the airflow cannot be obtained sufficiently.

上記のように、送風翼の低圧側翼面にディンプルや空気流の流線に対して平行な溝又は突起を形成する従来の構成では、騒音低減効果にも限界があると考えられる。   As described above, it is considered that the noise reduction effect is limited in the conventional configuration in which grooves or protrusions parallel to dimples and air flow streamlines are formed on the low pressure side blade surface of the blower blade.

本願発明は、上記のような従来技術における課題を改善しようとしてなされたもので、複数の送風翼をそなえた送風機において、前記送風翼の低圧側翼面に同低圧側翼面に沿って流れる空気流の流線に対して傾斜した直線状のエッジをもつ多数の溝又は突起を設けたことを基本的構成とする。   The present invention has been made in order to improve the problems in the prior art as described above. In a blower having a plurality of blower blades, the flow of air flowing along the low pressure side blade surface on the low pressure side blade surface of the blower blade is described. A basic configuration is that a large number of grooves or protrusions having linear edges inclined with respect to the streamline are provided.

上記のように、送風翼の低圧側翼面に同低圧側翼面に沿って流れる空気流の流線に対して傾斜した直線状のエッジをもつ多数の溝又は突起を設けると、溝の場合は図1に例示するように、また突起の場合は図2に例示するように、送風翼の表面の近傍に局所的な渦Uを生成し、境界層に乱れを与えて乱流境界層Wcとすることにより大きな剥離を防ぐことができる。   As described above, when a large number of grooves or protrusions having straight edges inclined with respect to the streamline of the air flow flowing along the low pressure side blade surface are provided on the low pressure side blade surface of the blower blade, As illustrated in FIG. 1 and in the case of a protrusion, as illustrated in FIG. 2, a local vortex U is generated near the surface of the blower blade, and the boundary layer is turbulent to form a turbulent boundary layer Wc. In this way, large peeling can be prevented.

その場合、本願発明の送風機では各送風翼に形成した溝又は突起が空気流の流線に対して傾斜した直線状のエッジをもつようにされているので、空気流が傾斜エッジと接触する長さが長くなり、上記の境界層剥離防止効果が大きくなる。   In that case, in the blower of the present invention, the grooves or protrusions formed on each blower blade have a straight edge inclined with respect to the streamline of the airflow, so that the airflow is in contact with the inclined edge. The above-mentioned boundary layer peeling preventing effect is increased.

また、上記の場合において前記溝又は突起は図3に例示するように、その傾斜方向が同一方向とされていてもよく、また図4に例示するように、その傾斜方向が相互に交叉する方向とされていてもよい。   Further, in the above case, the grooves or protrusions may have the same inclination direction as illustrated in FIG. 3, and the inclination directions intersect with each other as illustrated in FIG. It may be said.

さらに前記溝又は突起はその形状がV字型又は略V字型であり、そのV字屈曲部が送風翼の低圧側翼面に沿って流れる空気流の上流側又は下流側に向いているようにすることができる(溝がV字型でそのV字屈曲部が空気流の上流側に向いている場合は図5に例示し、同じくV字屈曲部が空気流の下流側に向いている場合は図6に例示し、さらに突起がV字型でその屈曲部が空気流の上流側に向いている場合は図7に例示し、同じくV字屈曲部が空気流の下流側に向いている場合は図8に例示)。   Further, the groove or the projection is V-shaped or substantially V-shaped, and the V-shaped bent portion faces the upstream side or the downstream side of the airflow flowing along the low pressure side blade surface of the blower blade. (When the groove is V-shaped and the V-shaped bent portion faces the upstream side of the air flow, it is illustrated in FIG. 5, and when the V-shaped bent portion faces the downstream side of the air flow as well. Is illustrated in FIG. 6, and when the protrusion is V-shaped and its bent portion faces the upstream side of the airflow, it is exemplified in FIG. 7. Similarly, the V-shaped bent portion faces the downstream side of the airflow. The case is illustrated in FIG. 8).

本願発明の送風機は、上記のように送風翼の低圧側翼面に形成した溝又は突起が空気流の流線に対して傾斜した直線状のエッジをもっているので、溝又は突起のエッジが空気流に対して作用する長さが長くなり、空気流が低圧側翼面から剥離するのを抑制する効果が大きくなる。また、溝又は突起をV字型又は略V字型形状とした場合は、V字型の頂点がクサビ型のボルテックス・ジェネレータ(渦発生器)の作用をするので、効果的に翼面境界層にエネルギーを与え、大きな剥離を抑制し、送風音を低減することができる効果がある。   In the blower of the present invention, since the groove or projection formed on the low pressure side blade surface of the blower blade has a linear edge inclined with respect to the streamline of the airflow as described above, the edge of the groove or projection is in the airflow. On the other hand, the acting length is increased, and the effect of suppressing separation of the air flow from the low-pressure blade surface is increased. Also, when the groove or protrusion is V-shaped or substantially V-shaped, the apex of the V-shape acts as a wedge-shaped vortex generator (vortex generator), so that the blade boundary layer is effectively Energy can be provided, large peeling can be suppressed, and blowing noise can be reduced.

続いて添付の図面を参照して本願発明の送風機の好適な実施例について説明する。   Next, preferred embodiments of the blower of the present invention will be described with reference to the accompanying drawings.

第1実施例(図9)
図9に示す第1実施例の送風機は、ボス部1の周囲に等角度間隔で3枚の同形の送風翼2,2,2をもち、各送風翼の低圧側翼面に図3に例示したような、深さ0.25〜0.3mmの相互に平行とされた多数の溝11,11・・・を形成している(なお、各溝のエッジと空気流Wの流線との接触角は同一とされている)。この第1実施例の送風機では、各送風翼2,2,2の低圧側翼面で図1に例示する作用説明図で述べたような空気流の乱流化がおこり、それによる乱流境界層Wcによって送風音の低減を図っている。
First embodiment (FIG. 9)
The blower of the first embodiment shown in FIG. 9 has three identical fan blades 2, 2, 2 at equiangular intervals around the boss portion 1, and is illustrated in FIG. 3 on the low pressure side blade surface of each fan blade. Are formed in parallel to each other at a depth of 0.25 to 0.3 mm (in addition, contact between the edge of each groove and the streamline of the air flow W) The corners are the same). In the blower of the first embodiment, the turbulence of the air flow as described in the action explanatory diagram illustrated in FIG. 1 occurs on the low pressure side blade surfaces of the blower blades 2, 2, and 2, and the turbulent boundary layer is thereby generated. The air blowing noise is reduced by Wc.

第2実施例(図10)
図10に示す第2実施例の送風機は、図9に示す送風機と同様にボス部1の周囲に等間隔で3枚の同形の送風翼2,2,2をもち、各送風翼の低圧側翼面に図4に例示したような相互に交差する方向に向いた、深さ0.25〜0.3mmの多数の溝11,11・・・、12,12・・・を形成したものである(なお、同一方向に傾斜している各溝11,11・・・と空気流Wの流線との接触角及び、溝11,11・・・と交叉して同一方向に傾斜する各溝12,12・・・と空気流Wの流線との接触角はそれぞれ同一とされている)。
Second embodiment (FIG. 10)
The blower of the second embodiment shown in FIG. 10 has three identically shaped blower blades 2, 2, and 2 at equal intervals around the boss portion 1 as in the blower shown in FIG. A large number of grooves 11, 11,..., 12, 12,... Having a depth of 0.25 to 0.3 mm are formed on the surface in directions intersecting with each other as illustrated in FIG. (Incidentally, the contact angle between each groove 11, 11... Inclined in the same direction and the stream line of the air flow W and each groove 12 inclined in the same direction crossing the grooves 11, 11. , 12... And the streamlines of the air flow W are the same).

第3実施例(図11)
図11に示す第3実施例の送風機は、第1実施例の送風機と同様に、ボス部1の周囲に等角度間隔で3枚の同形の送風翼2,2,2をもち、各送風翼の低圧側翼面に図5に例示するような、深さ0.25〜0.3mmのV字型の溝10,10・・・を、そのV字屈曲部17が空気流の上流側に向くようにして形成したものである。
Third embodiment (FIG. 11)
The blower of the third embodiment shown in FIG. 11 has three fan blades 2, 2, 2 having the same shape around the boss portion 1 at equal angular intervals, like the blower of the first embodiment. .. Of V-shaped grooves 10, 10... Having a depth of 0.25 to 0.3 mm as illustrated in FIG. 5 on the low-pressure side blade surface, and the V-shaped bent portion 17 faces the upstream side of the air flow. In this way, it is formed.

第4実施例(図12)
図12に示す第4実施例の送風機は、第1実施例の送風機と同様に、ボス部1の周囲に等角度間隔で3枚の同形の送風翼2,2,2をもち、各送風翼の低圧側翼面に図6に例示するような、深さ0.25〜0.3mmのV字型の溝10,10・・・を、そのV字屈曲部17が空気流の下流側に向くようにして形成したものである。
Fourth embodiment (FIG. 12)
The blower of the fourth embodiment shown in FIG. 12 has, in the same manner as the blower of the first embodiment, three identically shaped fan blades 2, 2, 2 around the boss portion 1 at equal angular intervals. .. Of V-shaped grooves 10, 10... Having a depth of 0.25 to 0.3 mm as illustrated in FIG. 6, and the V-shaped bent portion 17 faces the downstream side of the air flow. In this way, it is formed.

第5実施例(図13)
図13に示す第5実施例の送風機は、第1実施例の送風機と同様に、ボス部1の周囲に等角度間隔で3枚の同形の送風翼2,2,2をもち、各送風翼の低圧側翼面に図7に例示するような、高さ0.25〜0.3mmのV字型の突起20,20・・を、そのV字屈曲部27が空気流の上流側に向くようにして形成したものである。
Example 5 (FIG. 13)
The blower of the fifth embodiment shown in FIG. 13 has three fan blades 2, 2, 2 having the same shape around the boss portion 1 at equal angular intervals, like the blower of the first embodiment. The V-shaped protrusions 20, 20... Having a height of 0.25 to 0.3 mm as illustrated in FIG. 7 are arranged on the low-pressure side wing surface so that the V-shaped bent portion 27 faces the upstream side of the air flow. Is formed.

第6実施例(図14)
図14に示す第6実施例の送風機は、第1実施例の送風機と同様に、ボス部1の周囲に等角度間隔で3枚の同形の送風翼2,2,2をもち、各送風翼の低圧側翼面に図7に例示するような、高さ0.25〜0.3mmのV字型の突起20,20・・を、そのV字屈曲部27が空気流の下流側に向くようにして形成したものである。
Sixth embodiment (FIG. 14)
The blower of the sixth embodiment shown in FIG. 14 has three fan blades 2, 2, 2 having the same shape around the boss portion 1 at equal angular intervals, like the blower of the first embodiment. The V-shaped protrusions 20, 20... Having a height of 0.25 to 0.3 mm as illustrated in FIG. 7 are arranged on the low-pressure side blade surface of the blade so that the V-shaped bent portion 27 faces the downstream side of the air flow. Is formed.

なお、上記第3実施例ないし第6実施例においては、各溝10又は各突起20はそのV字型の中心線が空気流Wの流線と一致するような方向で形成されている。   In the third to sixth embodiments, each groove 10 or each projection 20 is formed in such a direction that its V-shaped center line coincides with the stream line of the air flow W.

第7実施例(図15,16)
上記第1〜第6実施例の送風機は、いずれもボス部1の周囲に3枚の送風翼2,2,2をそなえたプロペラファンであったが、本願発明はこのようなプロペラファンだけでなく、たとえば図15に例示するようなターボファンの送風翼(図16)やクロスフローファンの送風翼(図示省略)に対しても適用することができるものであり、それらの送風翼についても図1〜図8に例示したような各種の溝又は突起を形成することが可能である。なお、図15,16において符号50はモータ、51はボス部、52,52は送風翼、60はV字型の溝又は突起である。
Seventh embodiment (FIGS. 15 and 16)
Each of the blowers of the first to sixth embodiments was a propeller fan having three blower blades 2, 2, 2 around the boss portion 1, but the present invention is only such a propeller fan. For example, the present invention can be applied to the blower blades of a turbo fan (FIG. 16) and the blower blades (not shown) of a cross flow fan as illustrated in FIG. It is possible to form various grooves or protrusions as illustrated in FIGS. 15 and 16, reference numeral 50 denotes a motor, 51 denotes a boss portion, 52 and 52 denote blower blades, and 60 denotes a V-shaped groove or protrusion.

本願発明の送風機の送風翼に溝を形成した場合の空気作用説明図である。It is explanatory drawing of an air action at the time of forming a groove | channel in the ventilation blade of the air blower of this invention. 本願発明の送風機の送風翼に突起を形成した場合の空気作用説明図である。It is explanatory drawing of an air action at the time of forming a protrusion in the ventilation blade of the air blower of this invention. 本願発明の送風機の送風翼上に形成する溝又は突起の配列例の説明図である。It is explanatory drawing of the example of arrangement | sequence of the groove | channel or protrusion formed on the ventilation blade of the air blower of this invention. 本願発明の送風機の送風翼上に形成する溝又は突起の他の配列例の説明図である。It is explanatory drawing of the other example of arrangement | sequence of the groove | channel or protrusion formed on the ventilation blade of the air blower of this invention. 本願発明の送風機の送風翼上に形成されるV字型溝の配列例の説明図である。It is explanatory drawing of the example of arrangement | sequence of the V-shaped groove | channel formed on the ventilation blade of the air blower of this invention. 本願発明の送風機の送風翼上に形成されるV字型溝の他の配列例の説明図である。It is explanatory drawing of the other example of arrangement | sequence of the V-shaped groove | channel formed on the ventilation blade of the air blower of this invention. 本願発明の送風機の送風翼上に形成されるV字型突起の配列例の説明図である。It is explanatory drawing of the example of arrangement | sequence of the V-shaped protrusion formed on the ventilation blade of the air blower of this invention. 本願発明の送風機の送風翼上に形成されるV字型突起の他の配列例の説明図である。It is explanatory drawing of the other example of arrangement | sequence of the V-shaped protrusion formed on the ventilation blade of the air blower of this invention. 本願発明の第1実施例にかかる送風機の形状説明図である。It is shape explanatory drawing of the air blower concerning 1st Example of this invention. 本願発明の第2実施例にかかる送風機の形状説明図である。It is shape explanatory drawing of the air blower concerning 2nd Example of this invention. 本願発明の第3実施例にかかる送風機の形状説明図である。It is shape explanatory drawing of the air blower concerning 3rd Example of this invention. 本願発明の第4実施例にかかる送風機の形状説明図である。It is shape explanatory drawing of the air blower concerning 4th Example of this invention. 本願発明の第5実施例にかかる送風機の形状説明図である。It is shape explanatory drawing of the air blower concerning 5th Example of this invention. 本願発明の第6実施例にかかる送風機の形状説明図である。It is shape explanatory drawing of the air blower concerning 6th Example of this invention. 本願発明をターボファンに実施した場合のファン形状説明図である。It is fan explanatory drawing at the time of implementing this invention for a turbofan. 図15に示すターボファンにおける送風翼の形状例説明図である。FIG. 16 is a diagram illustrating a shape example of a blower blade in the turbo fan illustrated in FIG. 15. 従来公知の送風機の形状例説明図である。It is explanatory drawing of the example of a shape of a conventionally well-known air blower. 図17に示す公知の送風機における送風翼上の空気流の説明図である。It is explanatory drawing of the airflow on the ventilation blade in the well-known air blower shown in FIG. 従来公知の送風機の一例における翼面の構成説明図である。It is composition explanatory drawing of the blade surface in an example of a conventionally well-known air blower. 従来公知の他の送風機の一例における翼面の構成説明図である。It is composition explanatory drawing of the blade surface in an example of another conventionally well-known air blower.

符号の説明Explanation of symbols

1はボス部、2は送風翼、10,11,12は溝又は突起、17はV字型屈曲部、20はV字型突起、27はV字型屈曲部である。   1 is a boss portion, 2 is a blower blade, 10, 11 and 12 are grooves or protrusions, 17 is a V-shaped bent portion, 20 is a V-shaped protrusion, and 27 is a V-shaped bent portion.

Claims (10)

複数の送風翼をそなえた送風機であって、前記送風翼の低圧側翼面に同低圧側翼面に沿って流れる空気流の流線に対して傾斜した直線状のエッジをもつ多数の溝を設けたことを特徴とする送風機。   A blower provided with a plurality of blower blades, wherein a plurality of grooves having linear edges inclined with respect to streamlines of airflow flowing along the low pressure side blade surface are provided on the low pressure side blade surface of the blower blade. A blower characterized by that. 溝の傾斜方向が同一方向とされていることを特徴とする請求項1記載の送風機。   The blower according to claim 1, wherein the grooves are inclined in the same direction. 溝の傾斜方向が相互に交叉する方向とされていることを特徴とする請求項1記載の送風機。   The blower according to claim 1, wherein the inclination directions of the grooves intersect with each other. 溝が略V字型であり、そのV字屈曲部が送風翼の低圧側翼面に沿って流れる空気流の上流側に向いていることを特徴とする請求項1記載の送風機。   The blower according to claim 1, wherein the groove is substantially V-shaped, and the V-shaped bent portion faces the upstream side of the air flow flowing along the low-pressure blade surface of the blower blade. 溝が略V字型であり、そのV字屈曲部が送風翼の低圧側翼面に沿って流れる空気流の下流側に向いていることを特徴とする請求項1記載の送風機。   The blower according to claim 1, wherein the groove is substantially V-shaped, and the V-shaped bent portion faces the downstream side of the air flow flowing along the low-pressure blade surface of the blower blade. 複数の送風翼をそなえた送風機であって、前記送風翼の低圧側翼面に同低圧側翼面に沿って流れる空気流の流線に対して傾斜した直線状のエッジをもつ多数の突起を設けたことを特徴とする送風機。   A blower provided with a plurality of blower blades, wherein a plurality of protrusions having a linear edge inclined with respect to a streamline of an air flow flowing along the low pressure side blade surface are provided on the low pressure side blade surface of the blower blade. A blower characterized by that. 突起の傾斜方向が同一方向とされていることを特徴とする請求項6記載の送風機。   The blower according to claim 6, wherein the inclination directions of the protrusions are the same. 突起の傾斜方向が相互に交叉する方向とされていることを特徴とする請求項6記載の送風機。   The blower according to claim 6, wherein the inclination directions of the protrusions intersect with each other. 突起が略V字型であり、そのV字屈曲部が送風翼の低圧側翼面に沿って流れる空気流の上流側に向いていることを特徴とする請求項6記載の送風機。   The blower according to claim 6, wherein the protrusion is substantially V-shaped, and the V-shaped bent portion faces the upstream side of the air flow flowing along the low-pressure blade surface of the blower blade. 突起が略V字型であり、そのV字屈曲部が送風翼の低圧側翼面に沿って流れる空気流の下流側に向いていることを特徴とする請求項6記載の送風機。   The blower according to claim 6, wherein the protrusion is substantially V-shaped, and the V-shaped bent portion faces the downstream side of the airflow flowing along the low-pressure blade surface of the blower blade.
JP2006346975A 2006-12-25 2006-12-25 Blower Pending JP2008157113A (en)

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Cited By (11)

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US20120100001A1 (en) * 2010-10-20 2012-04-26 Zaward Corporation Fan structure
CN104544885A (en) * 2014-06-04 2015-04-29 新联电器厂有限公司 Wind blade and hair dryer with the same
US9771947B2 (en) 2011-03-02 2017-09-26 Sharp Kabushiki Kaisha Cross-flow fan, molding die, and fluid feeder
WO2021233483A1 (en) * 2020-08-31 2021-11-25 青岛海尔空调电子有限公司 Impeller, fan, and air conditioner outdoor unit
CN114046268A (en) * 2021-11-19 2022-02-15 杭州贝丰科技有限公司 Fan blade suitable for motor frame front axial flow fan
CN114909334A (en) * 2022-05-27 2022-08-16 珠海格力电器股份有限公司 Mixed flow fan and ducted air conditioner
CN114909322A (en) * 2022-05-27 2022-08-16 珠海格力电器股份有限公司 Impeller, mixed flow fan and ducted air conditioner
CN114962333A (en) * 2022-05-27 2022-08-30 珠海格力电器股份有限公司 Mixed flow fan and duct machine
EP4265914A4 (en) * 2020-12-18 2024-05-29 GD Midea Heating & Ventilating Equipment Co., Ltd. Wind wheel, fan, and air conditioner
EP4328456A4 (en) * 2021-08-07 2024-10-09 GD Midea Heating & Ventilating Equipment Co., Ltd. AXIAL FLOW WIND TURBINE, OUTDOOR UNIT OF AN AIR CONDITIONER AND AIR CONDITIONER
CN119878593A (en) * 2025-03-28 2025-04-25 广东美博制冷设备有限公司 Axial flow fan blade and axial flow fan

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20120100001A1 (en) * 2010-10-20 2012-04-26 Zaward Corporation Fan structure
US9771947B2 (en) 2011-03-02 2017-09-26 Sharp Kabushiki Kaisha Cross-flow fan, molding die, and fluid feeder
CN104544885A (en) * 2014-06-04 2015-04-29 新联电器厂有限公司 Wind blade and hair dryer with the same
WO2021233483A1 (en) * 2020-08-31 2021-11-25 青岛海尔空调电子有限公司 Impeller, fan, and air conditioner outdoor unit
EP4265914A4 (en) * 2020-12-18 2024-05-29 GD Midea Heating & Ventilating Equipment Co., Ltd. Wind wheel, fan, and air conditioner
EP4328456A4 (en) * 2021-08-07 2024-10-09 GD Midea Heating & Ventilating Equipment Co., Ltd. AXIAL FLOW WIND TURBINE, OUTDOOR UNIT OF AN AIR CONDITIONER AND AIR CONDITIONER
US20250084865A1 (en) * 2021-08-07 2025-03-13 Gd Midea Heating & Ventilating Equipment Co., Ltd. Axial flow wind wheel, air conditioner outdoor unit, and air conditioner
CN114046268A (en) * 2021-11-19 2022-02-15 杭州贝丰科技有限公司 Fan blade suitable for motor frame front axial flow fan
CN114909322A (en) * 2022-05-27 2022-08-16 珠海格力电器股份有限公司 Impeller, mixed flow fan and ducted air conditioner
CN114962333A (en) * 2022-05-27 2022-08-30 珠海格力电器股份有限公司 Mixed flow fan and duct machine
CN114909334A (en) * 2022-05-27 2022-08-16 珠海格力电器股份有限公司 Mixed flow fan and ducted air conditioner
CN114909322B (en) * 2022-05-27 2025-10-03 珠海格力电器股份有限公司 Mixed flow fans and duct fans
CN114909334B (en) * 2022-05-27 2025-11-04 珠海格力电器股份有限公司 Mixed flow fans and duct fans
CN114962333B (en) * 2022-05-27 2025-11-21 珠海格力电器股份有限公司 Mixed flow fan and air duct machine
CN119878593A (en) * 2025-03-28 2025-04-25 广东美博制冷设备有限公司 Axial flow fan blade and axial flow fan

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