JP3164940U - Fan structure - Google Patents

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JP3164940U
JP3164940U JP2010006733U JP2010006733U JP3164940U JP 3164940 U JP3164940 U JP 3164940U JP 2010006733 U JP2010006733 U JP 2010006733U JP 2010006733 U JP2010006733 U JP 2010006733U JP 3164940 U JP3164940 U JP 3164940U
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blade
fan
fan structure
polygonal
recesses
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正鋼 陳
正鋼 陳
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南實企業有限公司
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Abstract

【課題】翼片の回転をより円滑、省力、省電にし、ファンのヒートシンク効率が向上する改良したファン構造を提供する。【解決手段】ファン構造は、ホイール20と、ホイール外縁から延伸する複数の翼片30と、を含み、ファン1が回転時に発生する気流は、翼片表面に境界層を形成し、各翼片に複数の多辺形凹部(溝)33を設け、気流が各凹部を流れる時、凹部中に停滞する乱流を発生し、複数の乱流を収集し、翼片表面と前記境界層との間に介する一層の気膜を形成する。これにより、境界層の分離点を延ばし、摩擦抵抗力及び翼片の騒音を低減する効果を達成する。【選択図】図1An improved fan structure in which rotation of a blade piece is made smoother, labor-saving and power-saving, and the heat sink efficiency of the fan is improved. The fan structure includes a wheel 20 and a plurality of blade pieces 30 extending from the outer edge of the wheel, and an air flow generated when the fan 1 rotates forms a boundary layer on the blade piece surface, and each blade piece is formed. Are provided with a plurality of polygonal recesses (grooves) 33, and when the airflow flows through the respective recesses, turbulent flow stagnating in the recesses is generated, and a plurality of turbulent flows are collected, and the blade surface and the boundary layer are A single air film is formed between them. Thereby, the separation point of the boundary layer is extended, and the effect of reducing frictional resistance and blade noise is achieved. [Selection] Figure 1

Description

本考案は、ファンに関し、特に、気流の抵抗力を低減することができる改良された翼片構造に関する。   The present invention relates to a fan, and more particularly, to an improved winglet structure capable of reducing airflow resistance.

従来のコンピュータホスト又はその他の電子設備に応用するヒートシンクシステムは、ヒートシンク風が発生する強制気流により熱気を外部に排除し、ファンは、通常長時間の運転のために設置されるので、ファンの運転効率は、ヒートシンク効果と深く関連し、また、該ファンの回転時の騒音が大きすぎる場合、使用者に不快感をもたらす。   A heat sink system applied to a conventional computer host or other electronic equipment removes hot air to the outside by the forced air flow generated by the heat sink air, and the fan is usually installed for a long time operation, so the fan operation Efficiency is closely related to the heat sink effect, and also causes discomfort to the user if the noise during the fan rotation is too loud.

一般的に、ファンは、運転度にすぐ気流を発生し、該気流が翼片表面を流れる時、一層の薄い層を形成し、これは、境界層(boundary layer)と称され、気流の境界層は、翼片と分離点を過ぎた後に乱流を発生し、該乱流は、翼片を震動させ、騒音を発生し、後方の翼片表面及び気流間に摩擦抵抗力を生じさせ、更に、ファンの運転効率に影響を及ぼす。但し、研究に基づき、流場の制御は、摩擦抵抗力を低減し、境界層の分離点を延ばす方法の1つであることが示されているが、物体表面付近の流場を変更することにより摩擦抵抗力の低減を達成することが、本考案者の考案の動機である。   In general, a fan generates an air current immediately during operation, and forms a thinner layer when the air current flows on the blade surface, which is referred to as a boundary layer, The layer generates turbulence after passing the separation point from the winglet, the turbulent flow vibrates the winglet, generates noise, and creates a frictional resistance between the rear winglet surface and the airflow, Furthermore, it affects the operating efficiency of the fan. However, based on research, flow field control has been shown to be one of the ways to reduce frictional drag and extend the boundary layer separation point, but changing the flow field near the object surface Achieving a reduction in frictional resistance by this is the motive behind the inventor's idea.

特開平5−340390JP-A-5-340390

本考案の目的は、摩擦抵抗力を減少し、翼片の騒音を低減する効果を達成する改良されたファン構造を提供することにある。   It is an object of the present invention to provide an improved fan structure that achieves the effect of reducing frictional resistance and reducing blade noise.

本考案の他の目的は、翼片の回転をより円滑、省力、省電にし、ファンのヒートシンク効率を向上する改良されたファン構造を提供することにある。   Another object of the present invention is to provide an improved fan structure that makes the rotation of the blades smoother, labor-saving, and power-saving, and improves the heat sink efficiency of the fan.

上記の目的を達成する為、本考案が提供するファン構造は、ホイールと、該ホイール外縁から延伸する複数の翼片と、を含み、前記ファンが回転時に発生する気流は、該翼片表面に境界層を形成し、各該翼片に複数の多辺形凹部を設け、前記気流が各該凹部を流れる時、該凹部中に停滞する乱流を発生し、複数の乱流を収集し、該翼片表面と前記境界層との間に介する一層の気膜を形成することを特徴とする。   In order to achieve the above object, a fan structure provided by the present invention includes a wheel and a plurality of blades extending from an outer edge of the wheel, and the air flow generated when the fan rotates rotates on the surface of the blades. Forming a boundary layer, providing each of the blades with a plurality of polygonal recesses, generating a turbulent flow stagnating in the recesses when the airflow flows through the recesses, collecting a plurality of turbulences; One layer of air film is formed between the blade surface and the boundary layer.

本考案のもう1つの目的は、基台の外縁に凹向きの収容空間を有する首部を成型し、より多くの外部の空気が吸気側に進入することに有利であり、且つ排気側の排気時の抵抗力を低減することに有利であるファン構造を提供することにある。   Another object of the present invention is to form a neck portion having a concave accommodation space on the outer edge of the base, which is advantageous for allowing more external air to enter the intake side, and during exhaust on the exhaust side. It is an object of the present invention to provide a fan structure that is advantageous in reducing the resistance force of the fan.

本考案のもう1つの目的は、翼片の多辺形凹溝が三辺形、四辺形・・・八辺形等の多辺形の混合により構成され、翼片が異なる回転速度で各多辺形の凹溝中に乱流を発生することに有利であるファン構造を提供することにある。   Another object of the present invention is that the multi-sided concave groove of the wing piece is composed of a mixture of polygons such as a triangle, a quadrilateral, an octagon, etc. It is an object of the present invention to provide a fan structure that is advantageous for generating turbulent flow in a side groove.

従来のファン構造に比較し、本考案の改良されたファン構造は、翼片に複数の多辺形の凹溝を敷設し、該翼片表面を流れる気流が該多辺形凹溝の側辺に接触する時、乱流を発生し、該乱流は、該凹溝中に停滞し、該翼片表面及び境界層を隔絶できる一層の気膜を集中形成し、該気膜の形成により境界層の分離点を延ばすことができ、該翼片付近に乱流が発生することを回避し、乱流により発生する翼片の騒音及び摩擦抵抗力を低減し、翼片の回転をより円滑、省力、省電にし、ファンのヒートシンク効率を向上することができる。   Compared with the conventional fan structure, the improved fan structure of the present invention has a plurality of multi-sided concave grooves laid on the wing piece, and the airflow flowing on the surface of the wing piece is on the side of the multi-sided groove. Turbulent flow is generated when it comes into contact with the turbulent flow, and the turbulent flow stagnates in the concave groove to concentrate and form a layer of air film that can isolate the blade surface and the boundary layer. The separation point of the layers can be extended, avoiding the generation of turbulent flow near the blade, reducing the noise and frictional resistance of the blade generated by the turbulent flow, smoothing the rotation of the blade It is possible to save power and power, and to improve the heat sink efficiency of the fan.

本考案の第1実施例のファン組み立て立体外観説明図である。1 is an explanatory diagram of a three-dimensional fan assembly according to a first embodiment of the present invention. 本考案のホイール及び翼片の立体外観説明図である。It is a three-dimensional external view explanatory drawing of the wheel of this invention, and a wing piece. 本考案のホイール及び翼片の組み合わせ断面図である。It is combination sectional drawing of the wheel of this invention, and a blade piece. 本考案のファン使用時の気流説明図である。It is airflow explanatory drawing at the time of fan use of this invention. 本考案の翼片及び気流の間の状態説明図である。It is state explanatory drawing between the blade piece and airflow of this invention. 本考案の翼片の第2実施例である。It is 2nd Example of the wing piece of this invention.

本考案の実施例の詳細な説明及び技術的内容について、図面に併せて、以下に説明を行なうが、図面は、参考及び説明用に提供するだけであり、本考案に対して制限を加える為に用いるのではない。   The detailed description and technical contents of the embodiments of the present invention will be described below with reference to the drawings. However, the drawings are provided for reference and explanation only, and are intended to limit the present invention. It is not used for.

図1〜図3は、本考案の第1実施例のファンの組み合わせ立体外観説明図、ホイール及び翼片の立体外観説明図、及び他の角度の立体外観説明図である。本実施例のファン1は、基台10と、ホイール20と、該ホイール20外縁から突出する複数の翼片30と、を含む。   1 to 3 are a combined three-dimensional appearance explanatory view of a fan according to a first embodiment of the present invention, a three-dimensional appearance explanatory view of a wheel and a blade piece, and a three-dimensional appearance explanatory view of another angle. The fan 1 of the present embodiment includes a base 10, a wheel 20, and a plurality of blade pieces 30 protruding from the outer edge of the wheel 20.

前記基台10は、四角形筐体であり、且つ収容空間100を有し、該ホイール20及び複数の翼片30は、該収容空間100中に結合し、且つ該基台10は、吸気側11及び該吸気側11に相対する排気側12を含み、該吸気側11及び該排気側12の外縁は、凹向きの該収容空間100を有する首部13を成型する。本実施例中、該首部13は、該基台10の4つの側辺の中央に設けられる。   The base 10 is a rectangular housing and has a housing space 100, the wheel 20 and the plurality of blade pieces 30 are coupled into the housing space 100, and the base 10 has an intake side 11. And an exhaust side 12 opposite to the intake side 11, and the outer edges of the intake side 11 and the exhaust side 12 form a neck portion 13 having the accommodating space 100 in the concave direction. In the present embodiment, the neck 13 is provided at the center of the four sides of the base 10.

前記ホイール20及び該ホイール20外縁に突出する複数の翼片30は、該収容空間100中に結合し、該ホイール20の内部に回転軸21及びモータ(図示せず)を有し、該モータの運転後、該ホイール20の回転軸21の回転を連動することができ、該ホイール20外縁に設置される複数の翼片30も伴って回転し、気流を発生する。   The wheel 20 and a plurality of blades 30 projecting to the outer edge of the wheel 20 are coupled into the housing space 100 and have a rotating shaft 21 and a motor (not shown) inside the wheel 20. After operation, the rotation of the rotating shaft 21 of the wheel 20 can be interlocked, and the blades 30 installed on the outer edge of the wheel 20 also rotate to generate an air current.

前記翼片30は、第1表面31と、該第1表面31に相対する第2表面32を含み、各該翼片30は、複数の多辺形(多角形)の凹部(溝)33を敷設し、該多辺形凹部(溝)33は、三辺形、四辺形・・・八辺形等の多辺形中の任意の形状を呈することができ、即ち、該多辺形の凹部(溝)33の相互に隣接する2つの側辺は、挟み角を呈する。本実施例中、該翼片30の第1表面31及び第2表面32は、何れも該多辺形の凹部(溝)33を敷設し、実際の実施時、該多辺形の凹部(溝)33は、そのうちの1つの(片側)表面上にのみ設けてもよい。なお、両面に設けてもよいことは勿論である。   The blade piece 30 includes a first surface 31 and a second surface 32 opposite to the first surface 31, and each blade piece 30 has a plurality of polygonal (concave) recesses (grooves) 33. The polygonal recess (groove) 33 is laid and can exhibit any shape in a polygon such as a triangle, a quadrilateral ... an octagon, that is, the recess of the polygon The two adjacent sides of the (groove) 33 exhibit a sandwich angle. In the present embodiment, the first surface 31 and the second surface 32 of the blade piece 30 are both provided with the polygonal recesses (grooves) 33, and in the actual implementation, the polygonal recesses (grooves) are provided. ) 33 may be provided only on one (one side) surface. Of course, it may be provided on both sides.

図4及び図5は、それぞれ本考案の第1実施例のファンの使用時の気流説明図及び翼片と気流の間の状態説明図であり、該ファン1の運転時、該吸気側11において、該首部13の設置は、外部の空気が該吸気側11に進入することに有利であり、該排気側12から気流が排出する時、該首部13の設置は、排気時の抵抗力を低減することに有利である。   FIGS. 4 and 5 are an explanatory view of the airflow when the fan of the first embodiment of the present invention is used and an explanatory view of the state between the blade piece and the airflow, respectively. The installation of the neck 13 is advantageous for the outside air to enter the intake side 11, and when the airflow is discharged from the exhaust side 12, the installation of the neck 13 reduces the resistance during exhaust. It is advantageous to do.

該ファン1の運転時に発生する気流Aは、該翼片30表面に境界層Bを形成し、一方で、該気流Aが多辺形の凹部(溝)33の側辺を流れる時、該気流Aは、該多辺形の凹部(溝)33に停滞する乱流Tを発生し、複数の乱流Tが集中し、一層の気膜を形成し、該気膜は、該翼片30表面及び該境界層Bの間に介在し、該気膜の形成が該境界層Bの分離点Sを延ばし、該分離点Sを該翼片30の外側に形成させ、該翼片30付近に乱流Tが発生し、該翼片30に騒音を発生させることを回避し、乱流Tが増加する摩擦抵抗力を低減する。   The airflow A generated during operation of the fan 1 forms a boundary layer B on the surface of the blade piece 30. On the other hand, when the airflow A flows through the side of the polygonal recess (groove) 33, A generates a turbulent flow T stagnating in the polygonal concave portion (groove) 33, and a plurality of turbulent flows T are concentrated to form a single air film, which is the surface of the blade piece 30. And the formation of the gas film extends the separation point S of the boundary layer B, the separation point S is formed outside the blade piece 30, and turbulence occurs in the vicinity of the blade piece 30. The generation of the flow T and the generation of noise in the blade piece 30 are avoided, and the frictional resistance force that increases the turbulent flow T is reduced.

上記の構造において、乱流Tを発生しやすい箇所は、該多辺形凹部(溝)33の側辺に沿って発生し、且つ気流Aの速度が速い時、該乱流Tは、容易に発生するので、気流Aの速度が速い時、該多辺形凹溝33は、複数の比較的少ない三辺形又は四辺形等に設けることができ、一方で、気流Aの速度が遅い時、該多辺形凹部(溝)33は、比較的大きな六辺形又は七辺形等に設けることが好ましい。   In the above structure, the portion where the turbulent flow T is likely to occur is generated along the side of the polygonal recess (groove) 33, and when the velocity of the airflow A is high, the turbulent flow T is easily generated. Therefore, when the velocity of the airflow A is high, the polygonal concave groove 33 can be provided in a plurality of relatively few triangles or quadrilaterals, while the velocity of the airflow A is slow, The polygonal recess (groove) 33 is preferably provided in a relatively large hexagon or heptagon.

図6は、本考案のファンの翼片の第2実施例であり、本実施例は、第1実施例とほぼ同一であり、その異なる箇所は、翼片30aの該多辺形凹部(溝)33aが三辺形、四辺形・・・八辺形中のいずれか2種以上の多辺形凹部(溝)から構成されることにより、該翼片30aが異なる回転速度において、各多辺形凹部(溝)33a中に乱流及び気膜が発生することを円滑にすることができる。   FIG. 6 shows a second embodiment of the blade of the fan of the present invention. This embodiment is substantially the same as the first embodiment, and the different points are the polygonal recesses (grooves) of the blade 30a. ) 33a is formed of any two or more polygonal concave portions (grooves) in the shape of a triangle, a quadrilateral, an octagon, etc. It is possible to smoothly generate a turbulent flow and a gas film in the concave portion (groove) 33a.

以上のように、本考案の各実施例によれば、ファンが回転時に発生する気流は、翼片表面に境界層を形成し、各翼片に複数の多辺形凹部(溝)を設け、気流が各凹部(溝)を流れる時、凹部(溝)中に停滞する乱流を発生し、複数の乱流を収集し、翼片表面と前記境界層との間に介する一層の気膜を形成することにより、境界層の分離点を延ばし、摩擦抵抗力及び翼片の騒音を低減し、結果として、翼片の回転をより円滑、省力、省電にし、ファンのヒートシンク効率も向上する。
なお、本考案では好ましい実施例を前述の通り開示したが、これらは決して本考案に限定するものではなく、当該技術を熟知する者なら誰でも、本考案の精神と領域を脱しない均等の範囲内で各種の変動や潤色を加えることができることは勿論である。
As described above, according to each embodiment of the present invention, the airflow generated when the fan rotates forms a boundary layer on the blade piece surface, and a plurality of polygonal recesses (grooves) are provided on each blade piece. When the airflow flows through each recess (groove), a turbulent flow stagnating in the recess (groove) is generated, and a plurality of turbulent flows are collected to form a single air film between the blade surface and the boundary layer. By forming the boundary layer, the separation point of the boundary layer is extended, the frictional resistance and the noise of the blade piece are reduced, and as a result, the rotation of the blade piece becomes smoother, power saving, and power saving, and the heat sink efficiency of the fan is improved.
In the present invention, preferred embodiments have been disclosed as described above, but these are not intended to limit the present invention in any way, and anyone who is familiar with the technology has an equivalent scope that does not depart from the spirit and scope of the present invention. Of course, various fluctuations and moist colors can be added.

1 ファン
10 基台
100 収容空間
11 吸気側
12 排気側
13 首部
20 ホイール
21 回転軸
30 翼片
31 第1表面
32 第2表面
33 多辺形(多角形)凹部(溝)
A 気流
B 境界層
T 乱流
S 分離点
30a 翼片
33a 多辺形(多角形)凹部(溝)
DESCRIPTION OF SYMBOLS 1 Fan 10 Base 100 Accommodating space 11 Intake side 12 Exhaust side 13 Neck part 20 Wheel 21 Rotating shaft 30 Wing piece 31 First surface 32 Second surface 33 Polygonal (polygonal) recess (groove)
A Airflow B Boundary layer T Turbulence S Separation point 30a Wing piece 33a Polygonal (polygonal) recess (groove)

Claims (7)

ホイールと、該ホイール外縁から延伸する複数の翼片と、を含み、前記ファンが回転時に発生する気流は、該翼片表面に境界層を形成し、各該翼片に複数の多辺形凹部を設け、前記気流が各該凹部を流れる時、該凹部中に停滞する乱流を発生し、複数の乱流を収集し、該翼片表面と前記境界層との間に介する一層の気膜を形成することを特徴とするファン構造。   A plurality of blades extending from an outer edge of the wheel, and the airflow generated when the fan rotates forms a boundary layer on the surface of the blades, and a plurality of polygonal recesses on each blade When the airflow flows through each of the recesses, a turbulent flow stagnating in the recesses is generated, a plurality of turbulent flows are collected, and a single air film interposed between the blade surface and the boundary layer A fan structure characterized by forming. 前記ファン構造は基台とを更に含み、該基台は、四角形の筐体であり、且つ収容空間を有し、該ホイール及び複数の翼片は、該収容空間中に結合される請求項1に記載のファン構造。   The fan structure further includes a base, the base being a rectangular housing and having a receiving space, and the wheel and the plurality of blade pieces are coupled to the receiving space. The fan structure described in 1. 前記基台の外縁に凹向きの該収容空間を有する首部を成型する請求項2に記載のファン構造。   The fan structure according to claim 2, wherein a neck portion having the concave accommodating space is formed on an outer edge of the base. 前記凹部の相互隣接する二側辺は、挟み角を呈する請求項1に記載のファン構造。   The fan structure according to claim 1, wherein two adjacent sides of the concave portion exhibit a sandwich angle. 前記凹部は、三辺形から八辺形までの何れかの形状を呈する請求項1に記載のファン構造。   The fan structure according to claim 1, wherein the recess has any shape from a triangle to an octagon. 前記翼片の該多辺形凹部は、複数の三辺形から八辺形までの何れか2種以上の多辺形凹溝から構成される請求項1に記載のファン構造。   2. The fan structure according to claim 1, wherein the polygonal concave portion of the blade piece includes two or more types of polygonal concave grooves from a plurality of triangles to an octagon. 前記翼片は、第1表面及び該第1表面に相対する第2表面を含み、該多辺形の凹部は、該第1表面及び該第2表面に設けられる請求項1に記載のファン構造。   2. The fan structure according to claim 1, wherein the blade piece includes a first surface and a second surface opposite to the first surface, and the polygonal recess is provided in the first surface and the second surface. .
JP2010006733U 2010-10-12 2010-10-12 Fan structure Expired - Lifetime JP3164940U (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2024060878A1 (en) * 2022-09-22 2024-03-28 中兴通讯股份有限公司 Fan, and communication device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2024060878A1 (en) * 2022-09-22 2024-03-28 中兴通讯股份有限公司 Fan, and communication device

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