JP2006070808A - Impeller and blower fan provided with it - Google Patents

Impeller and blower fan provided with it Download PDF

Info

Publication number
JP2006070808A
JP2006070808A JP2004255240A JP2004255240A JP2006070808A JP 2006070808 A JP2006070808 A JP 2006070808A JP 2004255240 A JP2004255240 A JP 2004255240A JP 2004255240 A JP2004255240 A JP 2004255240A JP 2006070808 A JP2006070808 A JP 2006070808A
Authority
JP
Japan
Prior art keywords
impeller
air
outer peripheral
blade
wing portion
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.)
Granted
Application number
JP2004255240A
Other languages
Japanese (ja)
Other versions
JP4670285B2 (en
Inventor
Ryozo Sato
亮三 佐藤
Shinji Yoshida
伸二 吉田
Masahiko Hirata
雅彦 平田
Ichiro Takahara
一郎 高原
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 Holdings Corp
Original Assignee
Matsushita Electric Industrial 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 Matsushita Electric Industrial Co Ltd filed Critical Matsushita Electric Industrial Co Ltd
Priority to JP2004255240A priority Critical patent/JP4670285B2/en
Publication of JP2006070808A publication Critical patent/JP2006070808A/en
Application granted granted Critical
Publication of JP4670285B2 publication Critical patent/JP4670285B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

<P>PROBLEM TO BE SOLVED: To provide an impeller and a blower fan provided with it by which sucked air is efficiently sent in the centrifugal direction thereby to improve efficiency of suction, and obtain a high air-volume, a high static pressure is obtained by restraining effluent of the air, at least the same performance can be achieved at low speed of rotation as compared with conventional blower fans, further, noise which becomes higher with increase in the number of revolutions can be reduced. <P>SOLUTION: The impeller 1 of a centrifugal type comprises a boss part 2, and a plurality of blades 3 radially extending from the periphery of the boss part 2. Each blade 3 is constituted to have a retreating blade part 4 extended from the periphery of the boss part 2 and curved or bent in the direction reverse to the rotation direction of the impeller 1, and an advancing blade part 5 which is extended from the end on the periphery of the retreating blade part 4 through an inflection part 6, and curved or bent in the rotation direction of the impeller 1. The blower fan is provided with a flat casing, upper and lower suction ports, an exhaust port, and the impeller 1. <P>COPYRIGHT: (C)2006,JPO&NCIPI

Description

本発明は、遠心型の送風ファンに用いられるインペラ及びそれを備えた送風ファンに関する。   The present invention relates to an impeller used for a centrifugal blower fan and a blower fan including the impeller.

近年、種々の電子機器において小型化、薄型化が求められている。一方で、電子機器の多機能化が進み、筐体内部は高密度化し発熱量は増加する傾向にある。このため、筐体内部の駆動回路基板や電源部等の発熱素子や発熱部品を冷却し、発生した熱を外部に効率的に放熱することが強く求められている。   In recent years, various electronic devices have been required to be smaller and thinner. On the other hand, as electronic devices have become more multifunctional, the inside of a housing tends to have a higher density and the amount of heat generation tends to increase. For this reason, it is strongly required to cool the heat generating elements and heat generating components such as the drive circuit board and the power supply unit inside the housing and efficiently dissipate the generated heat to the outside.

発熱素子や発熱部品を冷却するために、筐体内部の空気を筐体外部に排気するものとしては送風ファンが広く用いられている。このような送風ファンは、電子機器の筐体内部には高密度に素子や部品が実装されていることから、小型或いは薄型であることが必要とされている。そこで、小型或いは薄型の送風ファンとして、近年、特許文献1や特許文献2に開示されたような遠心型の送風ファンが広く用いられている。遠心型の送風ファンは、インペラの回転軸方向の両側又は片側から吸気し、回転軸に直交する遠心方向に送出して発熱部や放熱部等の方向に排気するもので、遠心方向に排気するため、発熱素子や発熱部品、又は放熱部の側方に並べて配置して用いることができるので、特に筐体内部の空きスペースが少ない薄型の電子機器に好適に用いられる。   A blower fan is widely used as an element for exhausting air inside the casing to the outside of the casing in order to cool the heat generating elements and the heat generating components. Such a blower fan is required to be small or thin because elements and parts are mounted at a high density inside the housing of the electronic device. Therefore, as a small or thin blower fan, a centrifugal blower fan as disclosed in Patent Document 1 or Patent Document 2 has been widely used in recent years. Centrifugal blower fans draw air from both sides or one side of the impeller in the direction of the rotation axis, send it in the centrifugal direction orthogonal to the rotation axis, and exhaust it in the direction of the heat generating part and heat dissipation part. Therefore, since it can be used by arranging side by side on the side of the heat generating element, the heat generating component, or the heat radiating portion, it is preferably used particularly for a thin electronic device with a small empty space inside the housing.

特許文献1には、円筒状のボスと、ボスの外周面から径方向に延びる幅広の複数のリブと、ボスの外周面から離れた位置にリブに設けられた羽根と、を備えたインペラ、及び該インペラを備えたファンモータが開示されている。   Patent Document 1 includes an impeller including a cylindrical boss, a plurality of wide ribs extending in a radial direction from the outer peripheral surface of the boss, and a blade provided on the rib at a position away from the outer peripheral surface of the boss. And a fan motor provided with the impeller.

特許文献2には、円板状主板と該主板に対向する円環状側板間に長手方向が挟まれ周方向に一定間隔で略放射状に配置された羽根を有する羽根車と、該羽根車を軸支して内部に設置し側板側から空気を導入し円周方向に吹き出すケーシングとを備えた多翼前向ファンが開示されている。
特開2004−52735号公報 特開2000−145693号公報
In Patent Document 2, an impeller having blades disposed in a substantially radial manner at regular intervals in the circumferential direction with a longitudinal direction sandwiched between a disk-shaped main plate and an annular side plate facing the main plate, and the impeller A multi-blade forward fan is disclosed that includes a casing that is supported and installed inside and that introduces air from the side plate side and blows it out in the circumferential direction.
Japanese Patent Laid-Open No. 2004-52735 JP 2000-145893 A

しかしながら上記従来の技術では、特許文献1に記載されたインペラの羽根のように、一般的にインペラのブレード部は直線状である。ブレード部が直線状の場合、その長さや幅を大きくしブレードの面積を大きくすることで風量や静圧を高めることができるが、全体として大型化し、小型或いは薄型の電子機器に搭載でき難くなるという課題を有していた。   However, in the above conventional technique, like the impeller blades described in Patent Document 1, the blade portion of the impeller is generally linear. When the blade part is straight, the air flow and static pressure can be increased by increasing the length and width of the blade and increasing the area of the blade, but the overall size increases, making it difficult to mount on a small or thin electronic device. It had the problem that.

また、インペラの回転数を上げることによっても風量や静圧を高めることができるが、発生する騒音が大きくなり、静音性の要求される音響機器や情報処理機器等には搭載でき難くなるという課題を有していた。   The air volume and static pressure can also be increased by increasing the number of revolutions of the impeller, but the problem is that the generated noise increases, making it difficult to install in acoustic equipment and information processing equipment that require quietness. Had.

特許文献2の多翼前向ファンでは、羽根の出口角が150°以上と大きく形成されているので、圧力損失が増大し、風量及び静圧共に低下してしまうという課題を有していた。特に、ボス部より連結された遠心型送風ファンの羽根の先端部近傍にケーシングの内壁が配設される場合は、羽根の出口角が150°以上であると圧力損失が著しく増大し、風量
及び静圧が益々低下するという課題を有していた。
The multi-blade forward fan of Patent Document 2 has a problem in that since the exit angle of the blades is formed as large as 150 ° or more, the pressure loss increases and the air volume and static pressure both decrease. In particular, when the inner wall of the casing is disposed in the vicinity of the tip of the blade of the centrifugal blower fan connected from the boss, the pressure loss increases remarkably when the blade outlet angle is 150 ° or more, and the air volume and There was a problem that the static pressure gradually decreased.

本発明は上記従来の課題を解決するもので、ブレード部の内周側において吸気した空気を効率よく遠心方向へ送り出すことで吸気効率を高め高風量を得ることができると共に、ブレード部の外周側においてブレード部の表面から空気の流出を適切に抑制することで高静圧を得ることができるインペラを提供することを目的とする。   The present invention solves the above-described conventional problems, and efficiently sends out the air sucked in the inner peripheral side of the blade portion in the centrifugal direction, thereby increasing the intake efficiency and obtaining a high air volume, and also providing the outer peripheral side of the blade portion. An object of the present invention is to provide an impeller capable of obtaining a high static pressure by appropriately suppressing the outflow of air from the surface of the blade portion.

また、本発明は上記従来の課題を解決するもので、高風量及び高静圧を得ることで従来の送風ファンに比べ低回転数で同等或いはそれ以上の性能を実現でき、回転数と共に大きくなる騒音を低減できる送風ファンを提供することを目的とする。   In addition, the present invention solves the above-described conventional problems, and by obtaining a high air volume and high static pressure, it is possible to achieve the same or higher performance at a lower rotational speed than a conventional blower fan, and increases with the rotational speed. It aims at providing the ventilation fan which can reduce a noise.

上記課題を解決するために、本発明のインペラは、円筒状のボス部と、ボス部の外周面から放射状に延びる複数のブレード部と、を備えた遠心型の送風ファンのインペラであって、ブレード部が、ボス部の外周面から延びインペラの回転方向の反対方向に湾曲又は屈曲した後退翼部と、変曲部を介して後退翼部の外周側端部から延びインペラの回転方向に湾曲又は屈曲した前進翼部と、を備え、後退翼部が前進翼部よりインペラの回転軸中心側に位置する構成を有している。   In order to solve the above problems, an impeller according to the present invention is an impeller of a centrifugal air blower fan that includes a cylindrical boss portion and a plurality of blade portions extending radially from the outer peripheral surface of the boss portion, The blade part extends from the outer peripheral surface of the boss part and curves or bends in the direction opposite to the impeller rotation direction, and extends from the outer peripheral end of the reverse blade part via the inflection part and curves in the impeller rotation direction. Alternatively, the forward wing portion is bent, and the backward wing portion is positioned closer to the rotation shaft center side of the impeller than the forward wing portion.

これにより、ブレード部の内周側において吸気した空気を効率よく遠心方向へ送り出すことで吸気効率を高め高風量を得ることができると共に、ブレード部の外周側においてブレード部の表面から空気の流出を適切に抑制することで高静圧を得ることができるインペラを提供することができる。   As a result, the intake air can be efficiently sent out in the centrifugal direction to increase the intake efficiency to obtain a high air volume, and the air can be discharged from the surface of the blade part on the outer periphery side of the blade part. An impeller capable of obtaining a high static pressure by being appropriately suppressed can be provided.

上記課題を解決するために、本発明の送風ファンは、扁平状のケーシングと、ケーシングの上壁及び底壁に形成された上部吸気口及び下部吸気口と、ケーシングの側壁に形成された排気口と、ケーシングの内部に配設されたインペラと、を備え、インペラが、円筒状のボス部と、ボス部の外周面から放射状に延びる複数のブレード部と、を備えた遠心型の送風ファンのインペラであって、ブレード部が、ボス部の外周面から延びインペラの回転方向の反対方向に湾曲又は屈曲した後退翼部と、変曲部を介して後退翼部の外周側端部から延びインペラの回転方向に湾曲又は屈曲した前進翼部と、を備え、後退翼部が前進翼部よりインペラの回転軸中心側に位置する構成を有している。   In order to solve the above problems, a blower fan according to the present invention includes a flat casing, upper and lower intake ports formed on the upper and bottom walls of the casing, and an exhaust port formed on the side wall of the casing. And an impeller disposed inside the casing, wherein the impeller includes a cylindrical boss portion and a plurality of blade portions extending radially from the outer peripheral surface of the boss portion. An impeller, wherein a blade portion extends from the outer peripheral surface of the boss portion and is bent or bent in a direction opposite to the rotation direction of the impeller, and the impeller extends from the outer peripheral side end portion of the reverse wing portion via the inflection portion. And a forward wing portion curved or bent in the rotational direction of the forward wing portion, and the backward wing portion is positioned closer to the center of the impeller rotation axis than the forward wing portion.

これにより、高風量及び高静圧を得ることで従来の送風ファンに比べ低回転数で同等或いはそれ以上の性能を実現でき、回転数と共に大きくなる騒音を低減できる送風ファンを提供することができる。   Thereby, by obtaining a high air volume and a high static pressure, it is possible to provide a blower fan that can achieve performance equal to or higher than a conventional blower fan at a low rotational speed and can reduce noise that increases with the rotational speed. .

以上説明したように本発明のインペラ及びそれを備えた送風ファンによれば、以下のような有利な効果が得られる。   As described above, according to the impeller of the present invention and the blower fan including the impeller, the following advantageous effects can be obtained.

請求項1に記載の発明によれば、後退翼部がインペラの回転方向の反対方向に湾曲又は屈曲し、その前面が外周側に傾斜しているので、吸気した空気を効率よく外周側へ向かって送り出すことができると共に、前進翼部がインペラの回転方向に湾曲又は屈曲し、その前面が内周側に傾斜しているので、空気が前進翼部の前面から流出し難くなり、空気を外側へ強く押し出すことができ、風量及び静圧を共に高めることができファン性能を高めることができるインペラを提供することができる。   According to the first aspect of the present invention, the swept wing portion is bent or bent in the direction opposite to the rotation direction of the impeller, and the front surface thereof is inclined toward the outer peripheral side, so that the intake air is efficiently directed toward the outer peripheral side. Since the forward wing is curved or bent in the direction of rotation of the impeller and the front surface thereof is inclined toward the inner peripheral side, it is difficult for air to flow out from the front surface of the forward wing, It is possible to provide an impeller that can be pushed out strongly, can increase both air volume and static pressure, and can improve fan performance.

また、後退翼部と前進翼部とが滑らかな変曲部で接続されているので、空気がブレード部の内周側から外周側へ送り出される際の圧力損失が小さくでき、その結果ブレード部で
の渦流が抑制され、騒音を低減できるばかりでなく風量及び静圧の低下をも防止できるインペラを提供することができる。
In addition, since the backward wing and the forward wing are connected by a smooth inflection, the pressure loss when air is sent from the inner periphery to the outer periphery of the blade can be reduced. Thus, it is possible to provide an impeller that can suppress the vortex flow and reduce noise and also prevent a decrease in air volume and static pressure.

請求項2に記載の発明によれば、請求項1の効果に加え、後退翼部と前進翼部が対称に形成されているので、吸気と排気のバランスがよく、吸気した空気を効率よく外周側へ送り出し、且つ送り込まれた空気を効率よく強く押し出し排気ができ、その結果低回転で高風量且つ高静圧を得ることができ、低騒音のインペラを提供することができる。   According to the second aspect of the present invention, in addition to the effect of the first aspect, since the backward wing portion and the forward wing portion are formed symmetrically, the balance between the intake air and the exhaust air is good, and the intake air is efficiently discharged to the outer periphery. As a result, the exhausted air can be efficiently and strongly pushed out and exhausted. As a result, a high air volume and a high static pressure can be obtained at a low rotation, and a low noise impeller can be provided.

請求項3に記載の発明によれば、請求項1又は2の効果に加え、請求項1又は2の効果に加え、吸気の開口径及びインペラの外径に応じて、後退翼部と前進翼部との長さの比を1:0.5〜1.5の範囲とすることで、吸気と排気のバランスを適切に調整することができ、吸気した空気を効率良く外周部へ送り出し、効率良く強く押出し排気することができ、高風量且つ高静圧を得ることができるファン性能に優れた送風ファンで、低騒音の送風ファンを提供することができる。   According to the third aspect of the present invention, in addition to the effect of the first or second aspect, in addition to the effect of the first or second aspect, the reverse wing portion and the forward wing blade are provided in accordance with the opening diameter of the intake air and the outer diameter of the impeller. By making the ratio of the length with the part in the range of 1: 0.5 to 1.5, the balance between the intake and exhaust can be adjusted appropriately, and the intake air is efficiently sent to the outer peripheral part, the efficiency It is possible to provide a low-noise blower fan that is capable of extruding and exhausting well and is excellent in fan performance capable of obtaining a high air volume and high static pressure.

請求項4に記載の発明によれば、請求項1乃至3の内いずれか1項の効果に加え、後退翼部の出口角が10°〜50°であるので、吸気した空気を効率よくブレード部の外周側へ向かって送り出すことができ、吸気効率を高めることができるインペラを提供することができる。   According to the fourth aspect of the invention, in addition to the effect of any one of the first to third aspects, the exit angle of the swept wing portion is 10 ° to 50 °. It is possible to provide an impeller that can be sent out toward the outer peripheral side of the section and can increase the intake efficiency.

また効率よく吸気することができることで、吸気する際の渦流が抑制され、吸気による乱流騒音が低減できることで、低騒音の送風ファンを提供することができる。   In addition, since the air can be efficiently sucked in, the vortex flow during the air sucking is suppressed, and the turbulent noise caused by the air intake can be reduced, so that a low noise blower fan can be provided.

請求項5に記載の発明によれば、請求項1乃至4の内いずれか1項の効果に加え、前進翼部の出口角が55°〜110°であるので、空気が前進翼部の前面から流出し難くなると共に、空気を外側へ強く押し出す力を損なうことがなく、静圧を高めることができるインペラを提供することができる。   According to the fifth aspect of the invention, in addition to the effect of any one of the first to fourth aspects, since the exit angle of the forward wing portion is 55 ° to 110 °, the air is in front of the forward wing portion. Thus, it is possible to provide an impeller that can increase the static pressure without impairing the force of strongly pushing air outward.

請求項6に記載の発明によれば、インペラが後退翼部と前進翼部を有しているので吸気された空気を効率よく且つ強く送り出して排気でき、高風量且つ高静圧を得ることができるファン性能に優れた送風ファンを提供することができる。   According to the sixth aspect of the invention, since the impeller has the backward wing portion and the forward wing portion, the sucked air can be efficiently and strongly sent out and exhausted, and a high air volume and high static pressure can be obtained. It is possible to provide a blower fan having excellent fan performance.

また、従来の送風ファンに比べ低回転数で同等或いはそれ以上の性能を実現でき、回転数と共に大きくなる騒音を低減できる低騒音の送風ファンを提供することができる。   In addition, it is possible to provide a low-noise blower fan that can achieve the same or higher performance at a lower rotational speed than conventional blower fans and can reduce noise that increases with the rotational speed.

請求項7に記載の発明によれば、請求項6の効果に加え、略円形状の上部吸気口及び/又は下部吸気口の周縁部がインペラの変曲部の近傍に位置するので、ケーシング内に導入された空気を後退翼部により効率よく送り出すことができる吸気効率の高い送風ファンを提供することができる。   According to the seventh aspect of the invention, in addition to the effect of the sixth aspect, the peripheral portion of the substantially circular upper air inlet and / or lower air inlet is located in the vicinity of the inflection portion of the impeller. Thus, it is possible to provide a blower fan with high intake efficiency that can efficiently send out the air introduced into the retreat wing part.

本発明は、ブレード部の内周側において吸気した空気を効率よく遠心方向へ送り出すことで吸気効率を高め高風量を得ることができると共に、ブレード部の外周側においてブレード部の表面から空気を流出し難くすることで高静圧を得ることができるインペラを提供するという目的を、インペラのブレード部が、ボス部の外周面から延びインペラの回転方向の反対方向に湾曲又は屈曲した後退翼部と、変曲部を介して後退翼部の外周側端部から延びインペラの回転方向に湾曲又は屈曲した前進翼部と、を備え、後退翼部が前進翼部よりインペラの回転軸中心側に位置することにより実現した。   In the present invention, the intake air is efficiently sent out in the centrifugal direction on the inner peripheral side of the blade part to increase the intake efficiency and obtain a high air volume, and the air flows out from the surface of the blade part on the outer peripheral side of the blade part. For the purpose of providing an impeller capable of obtaining a high static pressure by making it difficult to do so, a blade portion of the impeller extends from the outer peripheral surface of the boss portion, and a retracted wing portion curved or bent in a direction opposite to the rotation direction of the impeller, A forward wing portion that extends from the outer peripheral side end of the backward wing portion via the inflection portion, and is curved or bent in the rotation direction of the impeller, and the backward wing portion is positioned closer to the center of the impeller rotation axis than the forward wing portion. It was realized by doing.

本発明は、高風量及び高静圧を得ることで従来の送風ファンに比べ低回転数で同等或い
はそれ以上の性能を実現でき、回転数と共に大きくなる騒音を低減できる送風ファンを提供するという目的を、扁平状のケーシングと、ケーシングの上壁及び底壁に形成された上部吸気口及び下部吸気口と、ケーシングの側壁に形成された排気口と、ケーシングの内部に配設されたインペラと、を備え、インペラのブレード部が、ボス部の外周面から延びインペラの回転方向の反対方向に湾曲又は屈曲した後退翼部と、変曲部を介して後退翼部の外周側端部から延びインペラの回転方向に湾曲又は屈曲した前進翼部と、を備え、後退翼部が前進翼部よりもインペラの回転軸中心側に位置することにより実現した。
An object of the present invention is to provide a blower fan that can achieve a performance equal to or higher than a conventional blower fan at a low rotational speed by obtaining a high air volume and a high static pressure, and can reduce noise that increases with the rotational speed. A flat casing, an upper inlet and a lower inlet formed in the upper wall and the bottom wall of the casing, an exhaust outlet formed in the side wall of the casing, an impeller disposed inside the casing, The impeller blade portion extends from the outer peripheral surface of the boss portion and is bent or bent in the direction opposite to the rotation direction of the impeller, and the impeller extends from the outer peripheral side end portion of the reverse wing portion via the inflection portion. And a forward wing portion that is curved or bent in the rotational direction, and the backward wing portion is located closer to the center of the rotation axis of the impeller than the forward wing portion.

上記課題を解決するためになされた第1の発明は、円筒状のボス部と、ボス部の外周面から放射状に延びる複数のブレード部と、を備えた遠心型の送風ファンのインペラであって、ブレード部が、ボス部の外周面から延びインペラの回転方向の反対方向に湾曲又は屈曲した後退翼部と、変曲部を介して後退翼部の外周側端部から延びインペラの回転方向に湾曲又は屈曲した前進翼部と、を備え、後退翼部が前進翼部よりもインペラの回転軸中心側に位置する構成を有している。   A first invention made to solve the above-described problem is an impeller of a centrifugal blower fan including a cylindrical boss portion and a plurality of blade portions extending radially from the outer peripheral surface of the boss portion. The blade portion extends from the outer peripheral surface of the boss portion and is bent or bent in the direction opposite to the rotation direction of the impeller, and extends from the outer peripheral side end portion of the reverse rotation blade portion via the inflection portion in the rotation direction of the impeller. A forward wing portion that is curved or bent, and the backward wing portion is positioned closer to the center of the impeller rotation axis than the forward wing portion.

この構成により、以下の作用を有する。   This configuration has the following effects.

ブレード部の後退翼部により空気を外周側へ押し出す際に、後退翼部がインペラの回転方向の反対方向に湾曲又は屈曲し、空気を押し出す後退翼部の前面が外周側に傾斜しているので、吸気した空気を効率よく外周側へ向かって送り出すことができ、風量を高めることができる。   When pushing out the air to the outer peripheral side by the retreating wing part of the blade part, the retreating wing part curves or bends in the direction opposite to the rotation direction of the impeller, and the front surface of the retreating wing part pushing out the air is inclined to the outer peripheral side. The intake air can be efficiently sent toward the outer peripheral side, and the air volume can be increased.

また、前進翼部がインペラの回転方向に湾曲又は屈曲し、空気を押し出す前進翼部の前面が内周側に傾斜しているので、空気が前進翼部の前面から流出し難くなり、空気を外側へ強く押し出すことができ、静圧を高めることができる。   In addition, the forward wing is curved or bent in the direction of rotation of the impeller, and the front surface of the forward wing that pushes out the air is inclined toward the inner peripheral side. It can be pushed out strongly and the static pressure can be increased.

後退翼部と前進翼部とが滑らかな変曲部で接続されているので、空気がブレード部の内周側から外周側へ送り出される際の圧力損失が小さく、風量及び静圧の低下を防止できる。   Since the reverse wing and the forward wing are connected by a smooth inflection, the pressure loss when air is sent from the inner periphery to the outer periphery of the blade is small, and the reduction of air volume and static pressure is prevented. it can.

また、吸気した空気をブレード部の内周側から外周側へ送り出す際の圧力損失が小さくなることで、ブレード部での渦流が抑制され、インペラの回転に伴い発生する騒音を低減することができる。   Further, since the pressure loss when the sucked air is sent from the inner peripheral side to the outer peripheral side of the blade part is reduced, the vortex flow in the blade part is suppressed, and the noise generated with the rotation of the impeller can be reduced. .

上記課題を解決するためになされた第2の発明は、第1の発明に記載のインペラであって、後退翼部と前進翼部が、変曲部を対称中心として対称に形成された構成を有している。   A second invention made to solve the above problems is the impeller according to the first invention, wherein the backward wing portion and the forward wing portion are formed symmetrically with the inflection portion as the symmetry center. Have.

この構成により、第1の発明の作用に加え、以下の作用を有する。   With this configuration, in addition to the operation of the first invention, the following operation is provided.

後退翼部と前進翼部が対称に形成されているので、吸気と排気のバランスがよく、吸気した空気を効率よく外周側へ送り出し、且つ送り込まれた空気を効率よく強く押し出すことができる。   Since the backward wing portion and the forward wing portion are formed symmetrically, the balance between intake and exhaust is good, the intake air can be efficiently sent to the outer peripheral side, and the supplied air can be efficiently and strongly pushed out.

上記課題を解決するためになされた第3の発明は、第1又は第2の発明に記載のインペラであって、後退翼部と前進翼部の長さの比が1:0.5〜1.5である構成を有している。   3rd invention made | formed in order to solve the said subject is an impeller as described in 1st or 2nd invention, Comprising: The ratio of the length of a backward wing | blade part and an advance wing | blade part is 1: 0.5-1. .5.

この構成により、第1又は第2の発明の作用に加え、以下の作用を有する。   With this configuration, in addition to the functions of the first or second invention, the following functions are provided.

吸気口の開口径及びインペラの外径に応じて、後退翼部と前進翼部との長さを1:0.5〜1.5の範囲で可変する事で、ファン及びインペラのサイズと吸気径及び排気口のサイズに応じて吸気と排気とのバランスの調整を適切に設定し、ファンの吸気の際の渦流を抑制することが可能となり、吸気による乱流騒音の低減ができ、低騒音化が実現できる。   Depending on the opening diameter of the intake port and the outer diameter of the impeller, the size of the fan and impeller and the intake air can be changed by changing the length of the backward blade portion and the forward blade portion within a range of 1: 0.5 to 1.5. The balance between intake and exhaust can be adjusted appropriately according to the diameter and the size of the exhaust port, and the vortex flow during fan intake can be suppressed, turbulence noise due to intake can be reduced, and low noise Can be realized.

特に、(前進翼部の長さ)/(後退翼部の長さ)を0.5以上とすることで、送り込まれた空気を効率よく強く押し出すことができる。また、(前進翼部の長さ)/(後退翼部の長さ)を1.5以下とすることで、吸気した空気を効率よく外周へ送り出すことができ、吸気口での渦流を抑制し、送風ファンの低騒音ができ、かつ高風量を得る事ができる。   In particular, by setting (the length of the forward wing portion) / (the length of the backward wing portion) to be 0.5 or more, the fed air can be pushed out efficiently and strongly. In addition, by setting (the length of the forward wing portion) / (the length of the backward wing portion) to 1.5 or less, the intake air can be efficiently sent to the outer periphery, and the vortex flow at the intake port is suppressed. The noise of the blower fan can be reduced, and a high air volume can be obtained.

(前進翼部の長さ)/(後退翼部の長さ)が0.5より小さくなるにつれて、ブレード部の外周側に向かって送り出された空気を適切に流出しない状態でインペラの回転方向に対し外側へ強く押出す力が損なわれる傾向があり、静圧を高めることができ難くなり好ましくない。   As (the length of the forward wing portion) / (the length of the backward wing portion) becomes smaller than 0.5, the air sent toward the outer peripheral side of the blade portion does not flow out properly in the direction of rotation of the impeller. On the other hand, there is a tendency that the force of strongly extruding to the outside tends to be impaired, and it becomes difficult to increase the static pressure, which is not preferable.

また、(前進翼部の長さ)/(後退翼部の長さ)が1.5より大きくなるにつれて、吸気した空気を効率よくブレード部の外周側へ向かって送り出す範囲が短くなり、ブレード部の内径に近い範囲でインペラの回転方向に直交するように立ち上がるため、羽根の外周部へ吸気した空気を円滑に外周側へ押し出すことができ難くなり、好ましくない。   Further, as (the length of the forward wing portion) / (the length of the backward wing portion) becomes larger than 1.5, the range in which the intake air is efficiently sent toward the outer peripheral side of the blade portion becomes shorter. Since it rises so as to be orthogonal to the rotation direction of the impeller within a range close to the inner diameter of the impeller, it is difficult to smoothly push out the air sucked into the outer peripheral portion of the blades to the outer peripheral side, which is not preferable.

さらに、(前進翼部の長さ)/(後退翼部の長さ)が1.5を超えると、吸気され外周側へ押し出される空気量が前進翼部の前面で保持される空気量よりも減少する傾向があるため、前進翼部の前面から空気が流出し難くなる。これにより、空気を外側へ強く押し出す力を得る事ができるが、空気が前進翼部の前面から流出し難いことにより発生する渦流が一因となって生成される騒音の増大という副作用の影響が発生するため、ファンの低騒音という観点から好ましくない。   Further, if (the length of the forward wing portion) / (the length of the backward wing portion) exceeds 1.5, the amount of air that is sucked and pushed out to the outer peripheral side is larger than the air amount that is held on the front surface of the forward wing portion. Since it tends to decrease, it becomes difficult for air to flow out from the front surface of the forward wing portion. As a result, it is possible to obtain a force that strongly pushes the air outward, but there is an adverse effect of an increase in noise that is generated due to the eddy current generated when the air hardly flows out from the front surface of the forward wing part. This is not preferable from the viewpoint of low fan noise.

上記課題を解決するためになされた第4の発明は、第1乃至第3の発明の内いずれか1に記載のインペラであって、インペラの回転軸を中心とし前記変曲部を通る仮想円の接線と前記後退翼部の外周側端部の延長線とのなす角度が10°〜50°である構成を有している。   A fourth invention made to solve the above-described problem is the impeller according to any one of the first to third inventions, wherein the virtual circle passes through the inflection portion about the rotation axis of the impeller. The angle formed by the tangent to the extension line of the outer peripheral end of the swept wing is 10 ° to 50 °.

この構成により、第1乃至第3の発明の内いずれか1の作用に加え、以下の作用を有する。   With this configuration, in addition to the operation of any one of the first to third inventions, the following operation is provided.

変曲部を通る仮想円の接線と後退翼部の外周側端部の延長線とのなす角度、すなわち後退翼部の出口角が10°〜50°であるので、吸気した空気を効率よくブレード部の外周側へ向かって送り出すことができ、吸気効率を高めることができる。   The angle between the tangent line of the virtual circle passing through the inflection part and the extension line of the outer peripheral side end of the swept wing, that is, the exit angle of the swept wing is 10 ° to 50 °. It is possible to send out toward the outer peripheral side of the part, and it is possible to increase the intake efficiency.

ここで、後退翼部の出口角が10°より小さくなるにつれ後退翼部がインペラの回転方向に沿うように傾斜していくため、吸気した空気を外周側へ押し出す力が小さくなり、また、50°より大きくなるにつれ後退翼部がインペラの回転方向に直交するように立ち上がるため、吸気した空気を円滑に外周側へ押し出すことができ難くなり、いずれも好ましくない。   Here, as the exit angle of the receding wing part becomes smaller than 10 °, the receding wing part inclines so as to follow the rotation direction of the impeller, so that the force for pushing out the sucked air to the outer peripheral side becomes small. As the angle becomes larger than 0 °, the retracted blade portion rises so as to be orthogonal to the direction of rotation of the impeller, so that it becomes difficult to push out the sucked air smoothly to the outer peripheral side.

上記課題を解決するためになされた第5の発明は、第1乃至第4の発明の内いずれか1に記載のインペラであって、インペラの回転軸を中心とし前記前進翼部の外周側端部を通る仮想円の接線と前記前進翼部の外周側端部の延長線とのなす角度が55°〜110°である構成を有している。   A fifth invention made to solve the above-described problem is the impeller according to any one of the first to fourth inventions, wherein the outer peripheral side end of the forward wing portion is centered on the rotation axis of the impeller. The angle formed by the tangent line of the virtual circle passing through the part and the extension line of the outer peripheral side end portion of the forward wing portion is 55 ° to 110 °.

この構成により、第1乃至第4の発明の内いずれか1の作用に加え、以下の作用を有する。   With this configuration, in addition to the operation of any one of the first to fourth inventions, the following operation is provided.

前進翼部の外周側端部を通る仮想円の接線と前進翼部の外周側端部の延長線とのなす角度、すなわち前進翼部の出口角が55°〜110°であるので、空気が前進翼部の前面から流出し難くなると共に、空気を外側へ強く押し出す力を損なうことがなく、静圧を高めることができる。   Since the angle formed by the tangent line of the imaginary circle passing through the outer peripheral end of the forward wing and the extended line of the outer peripheral end of the forward wing, ie, the exit angle of the forward wing is 55 ° to 110 °, the air It becomes difficult to flow out from the front surface of the forward wing portion, and the static pressure can be increased without impairing the force of strongly pushing air outward.

ここで、前進翼部の出口角が55°より小さくなるにつれ空気が前進翼部の前面から流出し易くなり、前進翼部における空気の保持力が低下し、また、110°より大きくなるにつれ前進翼部の外周側端部が大きく湾曲又は屈曲するため圧力損失が増大し、風量及び静圧共に低下してしまうため、いずれも好ましくない。特に、ボス部より連結されたブレード部を有する遠心ファンにおいてブレード前進翼部の先端部近傍にケーシングの内壁が配設されている場合は、前進翼部の出口角が110°より大きくなるにつれ圧力損失が著しく増大し、風量及び静圧が益々低下するため好ましくない。   Here, as the exit angle of the forward wing portion becomes smaller than 55 °, the air easily flows out from the front surface of the forward wing portion, the holding force of the air in the forward wing portion decreases, and as the outlet angle becomes larger than 110 °, the air advances. Since the outer peripheral side end of the wing is greatly curved or bent, the pressure loss increases and both the air volume and the static pressure decrease. In particular, in a centrifugal fan having a blade portion connected from a boss portion, when the inner wall of the casing is disposed in the vicinity of the tip of the blade forward blade portion, the pressure increases as the outlet angle of the forward blade portion becomes larger than 110 °. This is not preferable because the loss is remarkably increased and the air volume and static pressure are further reduced.

上記課題を解決するためになされた第6の発明は、送風ファンであって、扁平状のケーシングと、ケーシングの上壁又は底壁の内少なくともいずれか一方に形成された吸気口と、ケーシングの側壁に形成された排気口と、ケーシングの内部に配設された第1乃至第5の発明の内いずれか1に記載のインペラと、を備えた構成を有している。   A sixth invention made to solve the above-described problem is a blower fan, which is a flat casing, an intake port formed in at least one of the upper wall or the bottom wall of the casing, It has the structure provided with the exhaust port formed in the side wall, and the impeller as described in any one of the 1st thru | or 5th invention arrange | positioned inside the casing.

この構成により、以下の作用を有する。   This configuration has the following effects.

インペラが後退翼部と前進翼部を有しているので上部吸気口及び下部吸気口で吸気された空気を排気口から効率よく且つ強く送り出すことができ、高風量及び高静圧を得ることができ、従来の送風ファンに比べ低回転数で同等或いはそれ以上の性能を実現でき、回転数と共に大きくなる騒音を低減できる。   Since the impeller has a reverse wing part and a forward wing part, the air sucked at the upper and lower intake ports can be efficiently and strongly sent out from the exhaust port, and high air volume and high static pressure can be obtained. It is possible to achieve the same or higher performance at a lower rotational speed than the conventional blower fan, and to reduce noise that increases with the rotational speed.

ここで、ケーシングとしては、アルミニウム等の金属や合成樹脂等により底壁、上壁、及び側壁を有する扁平状の箱形に形成されたものが用いられる。また、ケーシングの上壁又は底壁の内少なくともいずれか一方に吸気口がインペラの回転軸を中心とする略円形状や多角形状等に形成される。下部吸気口又は上部吸気口の中央部には、周縁部から延びるリブ等の支持部材で支持された保持板が配設され、該保持板上に回路基板やステータ、軸支部等の駆動部が搭載され、インペラは該軸支部に軸支される。   Here, as a casing, what was formed in the flat box shape which has a bottom wall, an upper wall, and a side wall with metals, such as aluminum, synthetic resins, etc. is used. In addition, an air inlet is formed in a substantially circular shape or a polygonal shape around the rotation axis of the impeller on at least one of the upper wall or the bottom wall of the casing. A holding plate supported by a support member such as a rib extending from the peripheral portion is disposed in the central portion of the lower intake port or the upper intake port, and a drive unit such as a circuit board, a stator, or a shaft support portion is provided on the holding plate. It is mounted and the impeller is pivotally supported by the pivotal support.

上記課題を解決するためになされた第7の発明は、第6の発明に記載の送風ファンであって、上部吸気口及び/又は下部吸気口が略円形状に形成され、その周縁部がインペラの変曲部の近傍に位置するように形成された構成を有している。   7th invention made | formed in order to solve the said subject is a ventilation fan as described in 6th invention, Comprising: An upper inlet and / or a lower inlet are formed in substantially circle shape, The peripheral part is an impeller It has the structure formed so that it might be located in the vicinity of the inflection part.

この構成により、第6の発明の作用に加え、以下の作用を有する。   With this configuration, in addition to the operation of the sixth invention, the following operation is provided.

略円形状の上部吸気口及び/又は下部吸気口の周縁部がインペラの変曲部の近傍に位置するので、上部吸気口及び/又は下部吸気口からケーシング内に導入された空気を後退翼部により効率よく送り出すことができる。   Since the peripheral part of the substantially circular upper air inlet and / or lower air inlet is located in the vicinity of the inflection part of the impeller, the air introduced into the casing from the upper air inlet and / or the lower air inlet is moved backward by the wing part. Can be sent out more efficiently.

(実施の形態1)
以下、本発明の実施の形態について、各図に基づいて説明する。
(Embodiment 1)
Hereinafter, embodiments of the present invention will be described with reference to the drawings.

図1(a)は本発明の実施の形態1におけるインペラの平面図であり、図1(b)は後退翼部と前進翼部の入口角及び出口角を説明するためのインペラの模式平面図である。   FIG. 1A is a plan view of an impeller according to Embodiment 1 of the present invention, and FIG. 1B is a schematic plan view of an impeller for explaining the entrance angle and the exit angle of the receding wing part and the advancing wing part. It is.

図1において、1は本発明の実施の形態1におけるインペラ、2は円筒状のボス部、2aはボス部2の天面部2bの下面中央部に固定された回転軸、3はボス部2の外周面から放射状に延びる複数のブレード部、4はボス部2の外周面から延びインペラ1の回転方向Xの反対方向に湾曲したブレード部3の後退翼部、5は後退翼部4の外周側端部から延びインペラ1の回転方向Xに湾曲した前進翼部、6はブレード部3において後退翼部4から前進翼部5へ変異する部分である変曲部、β1は後退翼部4の入口角、β2は前進翼部5の出口角、β3は後退翼部4の出口角であると共に前進翼部5の入口角である。   In FIG. 1, 1 is an impeller according to Embodiment 1 of the present invention, 2 is a cylindrical boss portion, 2 a is a rotating shaft fixed to the center of the lower surface of the top surface portion 2 b of the boss portion 2, and 3 is a boss portion 2. A plurality of blade portions extending radially from the outer peripheral surface, 4 extends from the outer peripheral surface of the boss portion 2, and the retreat wing portion of the blade portion 3 curved in the direction opposite to the rotation direction X of the impeller 1, 5 is the outer periphery side of the retreat wing portion 4 The forward wing portion extending from the end portion and curved in the rotation direction X of the impeller 1, 6 is a bending portion which is a portion of the blade portion 3 that changes from the backward wing portion 4 to the forward wing portion 5, and β 1 is the inlet of the backward wing portion 4. The angle β2 is the exit angle of the forward wing portion 5, and β3 is the exit angle of the backward wing portion 4 and the entrance angle of the forward wing portion 5.

ここで、各々のブレード部3の後退翼部4と前進翼部5は、同一の長さ及び同一の曲率半径を有する円弧上に形成され、変曲部6を対称中心として対称となるように形成されている。   Here, the retreat wing part 4 and the advance wing part 5 of each blade part 3 are formed on an arc having the same length and the same radius of curvature, and are symmetrical with respect to the inflection part 6 as a center of symmetry. Is formed.

また、後退翼部4の入口角β1とは、後退翼部4とボス部2の外周面との接続部6aにおけるボス部2の外周面の接線と後退翼部4の内周側端部とのなす角度のうち接線より外径側で接線から回転方向にとった角度である。前進翼部5の出口角β2とは、前進翼部5の外周側端部における回転軸2aを中心とする仮想円の接線と前進翼部5の外周側端部の延長線とのなす角度のうち接線より外径側で接線から回転方向にとった角度である。後退翼部4の出口角β3とは、変曲部6における回転軸2aを中心とする仮想円の接線と後退翼部4の外周側端部の延長線とのなす角度のうち接線より外径側で接線から回転方向にとった角度である。なお、後退翼部4と前進翼部5とはなめらか変曲部6で接続されている。すなわち、後退翼部4の出口角β3は前進翼部5の入口角と同一となっている。なお、前進翼部5の入口角β3とは、変曲部6における回転軸2aを中心とする仮想円の接線に対する前進翼部5の内周側端部とのなす角度である。   Further, the inlet angle β1 of the swept wing part 4 is the tangent to the outer peripheral surface of the boss part 2 at the connecting portion 6a between the swept wing part 4 and the outer peripheral surface of the boss part 2, and the inner peripheral side end of the swept wing part 4. Is an angle taken from the tangent to the rotational direction on the outer diameter side of the tangent. The exit angle β2 of the forward blade portion 5 is an angle formed by a tangent line of an imaginary circle centering on the rotation shaft 2a at the outer peripheral side end portion of the forward blade portion 5 and an extension line of the outer peripheral side end portion of the forward blade portion 5. It is an angle taken from the tangent in the rotational direction on the outer diameter side of the tangent. The exit angle β3 of the swept wing part 4 is the outer diameter of the angle formed by the tangent line of the imaginary circle centering on the rotation axis 2a in the inflection part 6 and the extension line of the outer peripheral side end part of the swept wing part 4. The angle taken from the tangent to the direction of rotation on the side. The backward wing portion 4 and the forward wing portion 5 are connected by a smooth inflection portion 6. That is, the exit angle β3 of the receding wing part 4 is the same as the entrance angle of the advancing wing part 5. The inlet angle β3 of the forward blade portion 5 is an angle formed with the inner peripheral side end portion of the forward blade portion 5 with respect to a tangent of a virtual circle centering on the rotation axis 2a in the inflection portion 6.

各々のブレード部3は、前進翼部5の出口角β2が55°〜110°、後退翼部4の出口角(前進翼部5の入口角)β3が10°〜50°となるように形成されている。   Each blade portion 3 is formed such that the outlet angle β2 of the forward blade portion 5 is 55 ° to 110 °, and the outlet angle (inlet angle of the forward blade portion 5) β3 of the backward blade portion 4 is 10 ° to 50 °. Has been.

また、後退翼部と前進翼部の長さの比は、1:0.5〜1.5となる様に形成されている。   Further, the ratio of the length of the backward wing portion and the forward wing portion is formed to be 1: 0.5 to 1.5.

以上のように構成された本発明の実施の形態1におけるインペラ1を備えた送風ファンについて、図2及び図3を用いて説明する。   A blower fan provided with impeller 1 according to Embodiment 1 of the present invention configured as described above will be described with reference to FIGS. 2 and 3.

図2(a)は本発明の実施の形態1における送風ファンの要部斜視図であり、図2(b)は本発明の実施の形態1における送風ファンの内部透視平面図であり、図2(c)は図2(b)の送風ファンの中央横断面図であり、図3はインペラ1の要部拡大平面図である。   FIG. 2A is a perspective view of a main part of the blower fan according to Embodiment 1 of the present invention, and FIG. 2B is an internal perspective plan view of the blower fan according to Embodiment 1 of the present invention. (C) is a central cross-sectional view of the blower fan of FIG. 2 (b), and FIG. 3 is an enlarged plan view of the main part of the impeller 1.

図中、10は本発明の実施の形態1における送風ファン、11は底壁11aと側壁11bとを有するケーシング、11cは側壁11bの内周面、12はケーシング11の上面に覆設されたケーシング11の上壁を形成するケーシングカバー、13はケーシング11の底壁11aの中央部に形成された円形の下部吸気口、14はケーシングカバー12の中央部に形成された円形の上部吸気口、15はケーシング11の側壁11bの所定部に形成された矩形の排気口、16は下部吸気口13の略中央部に支持部材(図示せず)により支持された保持板、17は保持板16の上面に立設固定されインペラ1の回転軸2aを回転自在に軸支する軸受部、18は軸受部17の周囲に固定されたコイルが巻着されたステータ、19はステータ18に対向してボス部2の内周面に嵌合固定された円筒状マグネット、20はステータ18の下部に配設された回路基板である。   In the figure, 10 is a blower fan according to the first embodiment of the present invention, 11 is a casing having a bottom wall 11a and a side wall 11b, 11c is an inner peripheral surface of the side wall 11b, and 12 is a casing covered on the upper surface of the casing 11. 11 is a casing cover forming the upper wall of the casing 11, 13 is a circular lower inlet formed at the center of the bottom wall 11a of the casing 11, 14 is a circular upper inlet formed at the center of the casing cover 12, Is a rectangular exhaust port formed in a predetermined portion of the side wall 11 b of the casing 11, 16 is a holding plate supported by a support member (not shown) at a substantially central portion of the lower intake port 13, and 17 is an upper surface of the holding plate 16. A bearing portion that is fixedly installed on the impeller 1 and rotatably supports the rotating shaft 2a of the impeller 1, 18 is a stator around which a coil fixed around the bearing portion 17 is wound, and 19 is opposed to the stator 18. The inner peripheral surface to the mating fixed cylindrical magnet boss portion 2, 20 is a circuit board which is arranged in a lower portion of the stator 18.

ここで、ケーシング11の内周面11cは排気口15を除いて略円形状に形成されている。排気口15は側壁11bの一つの辺を全て開口して形成してもよく、一つの辺の一部を開口して形成してもよい。   Here, the inner peripheral surface 11 c of the casing 11 is formed in a substantially circular shape except for the exhaust port 15. The exhaust port 15 may be formed by opening one side of the side wall 11b, or may be formed by opening a part of one side.

また、上部吸気口14及び下部吸気口13は、その周縁部がインペラ1の変曲部6の近傍に位置するような径で形成されている。   Further, the upper air inlet 14 and the lower air inlet 13 are formed with such diameters that their peripheral portions are located in the vicinity of the inflection portion 6 of the impeller 1.

以上のように構成された本発明の実施の形態1におけるインペラ1及び送風ファン10について、以下その動作を図面を用いて説明する。   Operation of the impeller 1 and the blower fan 10 according to Embodiment 1 of the present invention configured as described above will be described below with reference to the drawings.

回路基板20に電力が供給されると、ステータ18に巻着された各コイルに電流が流れステータ18に磁力が発生する。円筒状マグネット19は周方向にN極とS極が交互に着磁されており、ステータ18に発生した磁力と引き合ってインペラ1が回転する。このとき、回路基板20に実装されたホール素子(図示せず)は円筒状マグネット19のN極とS極を検出し出力信号を発生する。各コイルに流れる電流をホール素子の出力信号により転流するように制御することで、ステータ18に発生する磁力の磁極は逐次変わって円筒状マグネット19のN極やS極と引き合い、インペラ1は所定の回転方向Xに連続的に回転する。インペラ1の回転により、下部吸気口13及び上部吸気口14から外気が吸気される。   When electric power is supplied to the circuit board 20, current flows through each coil wound around the stator 18, and magnetic force is generated in the stator 18. The cylindrical magnet 19 is alternately magnetized with N and S poles in the circumferential direction, and the impeller 1 rotates by attracting the magnetic force generated in the stator 18. At this time, a Hall element (not shown) mounted on the circuit board 20 detects the N pole and S pole of the cylindrical magnet 19 and generates an output signal. By controlling the current flowing through each coil to be commutated by the output signal of the Hall element, the magnetic poles of the magnetic force generated in the stator 18 are successively changed and attracted to the N pole and S pole of the cylindrical magnet 19. It rotates continuously in a predetermined rotation direction X. As the impeller 1 rotates, outside air is sucked from the lower air inlet 13 and the upper air inlet 14.

ケーシング11の内部に吸気された外気は、図3に示すように、ブレード部3の内周側の後退翼部4により外周側へ押し出される。このとき、後退翼部4はインペラ1の回転方向Xの反対方向に湾曲し、空気を押し出す後退翼部4の前面が外周側に向けて傾斜している。これにより、吸気した空気を効率よく外周側へ向かって遠心方向へ送り出すことができる。外周側へ送り出された空気は、ブレード部3の外周側の前進翼部5によりブレード部3の外側、すなわちブレード部3の外周側端部とケーシング11の内周面11cとの間に押し出される。このとき、前進翼部5はインペラ1の回転方向Xに湾曲し、空気を押し出す前進翼部5の前面が内周側に向けて傾斜している。これにより、空気が前進翼部5の前面から流出し難くなり、ブレード部3は空気を外側へ強く押し出すことができる。   As shown in FIG. 3, the outside air sucked into the casing 11 is pushed out to the outer peripheral side by the retreating wing part 4 on the inner peripheral side of the blade part 3. At this time, the retreat wing part 4 is curved in the direction opposite to the rotation direction X of the impeller 1, and the front surface of the retreat wing part 4 that pushes out air is inclined toward the outer peripheral side. Thereby, the inhaled air can be efficiently sent in the centrifugal direction toward the outer peripheral side. The air sent to the outer peripheral side is pushed out by the forward wing part 5 on the outer peripheral side of the blade part 3 to the outside of the blade part 3, that is, between the outer peripheral side end part of the blade part 3 and the inner peripheral surface 11c of the casing 11. . At this time, the forward blade portion 5 is curved in the rotation direction X of the impeller 1, and the front surface of the forward blade portion 5 that pushes out the air is inclined toward the inner peripheral side. Thereby, it becomes difficult for air to flow out from the front surface of the forward wing portion 5, and the blade portion 3 can strongly push the air outward.

次に、本発明の実施の形態1における送風ファンのファン性能について図4乃至図7を参照しながら説明する。   Next, the fan performance of the blower fan according to Embodiment 1 of the present invention will be described with reference to FIGS.

図4は本発明の実施の形態の送風ファンと従来の送風ファンの風量と静圧との関係を示す風量静圧特性曲線図であり、図5は本発明の実施の形態1の送風ファンの後退翼部の出口角β3を変化させた時の静圧の変化を示す相関図であり、図6は本発明の実施の形態1の送風ファンの前進翼部の出口角β2を変化させた時の静圧の変化を示す相関図であり、図7は本発明の実施の形態1の送風ファンの後退翼部の長さと前進翼部の長さの比率を変化させた時の静圧の変化を示す相関図である。   FIG. 4 is an air flow static pressure characteristic curve diagram showing the relationship between the air flow and static pressure of the blower fan according to the embodiment of the present invention and the conventional blower fan, and FIG. 5 is a diagram of the blower fan according to the first embodiment of the present invention. FIG. 6 is a correlation diagram showing a change in static pressure when the exit angle β3 of the swept wing part is changed, and FIG. 6 is a diagram when the exit angle β2 of the advancing wing part of the blower fan according to Embodiment 1 of the present invention is changed. FIG. 7 is a correlation diagram showing changes in the static pressure of the fan, and FIG. 7 shows changes in the static pressure when the ratio of the length of the backward blade portion and the length of the forward blade portion of the blower fan according to Embodiment 1 of the present invention is changed. FIG.

図4において、Aは本発明の実施の形態1の送風ファンの風量静圧特性曲線、Bは従来の送風ファンの風量静圧特性曲線である。ここで、従来の送風ファンとしては、インペラのブレード部として直線状のブレード部を用いた。この直線状のブレード部の入口角は実施の形態1のインペラの後退翼部4の入口角と同一とし、外径(インペラの回転軸からブレード部の外周側端部までの直線距離)も同一とした。従来の送風ファンのその他の構成は、実施の形態1の送風ファンと同じものを用い、インペラの回転数も略同一の約3500r/minとした。   In FIG. 4, A is the air volume static pressure characteristic curve of the blower fan according to Embodiment 1 of the present invention, and B is the air volume static pressure characteristic curve of the conventional fan. Here, as a conventional blower fan, a linear blade portion was used as the blade portion of the impeller. The inlet angle of the straight blade portion is the same as the inlet angle of the swept wing portion 4 of the impeller of the first embodiment, and the outer diameter (the linear distance from the impeller rotating shaft to the outer peripheral end of the blade portion) is also the same. It was. The other structure of the conventional blower fan is the same as that of the first embodiment, and the rotational speed of the impeller is about 3500 r / min, which is substantially the same.

図5において、A1は本発明の実施の形態1の送風ファン10の後進翼部4の出口角β3を変化させた時の静圧の変化を示す。なお、ブレード部3の前進翼部5の出口角β2は
100°に固定し、インペラ1の回転数は約3500r/minとし、風量は50L/minとした。
In FIG. 5, A1 shows the change of the static pressure when changing the exit angle β3 of the backward blade portion 4 of the blower fan 10 of Embodiment 1 of the present invention. The exit angle β2 of the forward blade portion 5 of the blade portion 3 was fixed at 100 °, the rotation speed of the impeller 1 was about 3500 r / min, and the air volume was 50 L / min.

図6において、A2は本発明の実施の形態1の送風ファン10の前進翼部5の出口角β2を変化させた時の静圧の変化を示す。なお、ブレード部3の後進翼部4の出口角β3は40°に固定した。インペラ1の回転数及び風量は図5の場合と同一とした。   In FIG. 6, A2 shows the change of the static pressure when the exit angle β2 of the forward blade portion 5 of the blower fan 10 according to the first embodiment of the present invention is changed. In addition, the exit angle β3 of the backward blade portion 4 of the blade portion 3 was fixed at 40 °. The rotation speed and air volume of the impeller 1 were the same as those in FIG.

図7において、A3は本発明の実施の形態1の送風ファン10の前進翼部5の長さと後進翼部4の長さの比率を変化させた時の静圧の変化を示す。なお、実施の形態1の前進翼部5の出口角β3は40°に固定し、後進翼部4の出口角β2は100°に固定した。インペラ1の回転数及び風量は図5の場合と同一とした。   In FIG. 7, A3 shows a change in static pressure when the ratio of the length of the forward blade portion 5 and the length of the backward blade portion 4 of the blower fan 10 according to the first embodiment of the present invention is changed. In addition, the exit angle β3 of the forward blade portion 5 of the first embodiment is fixed at 40 °, and the outlet angle β2 of the backward blade portion 4 is fixed at 100 °. The rotation speed and air volume of the impeller 1 were the same as those in FIG.

図4に示すように、実施の形態1の送風ファン10はブレード部3が後退翼部4と前進翼部5を有しているので、従来の送風ファンと比較して風量及び静圧が高く、インペラの回転数が同じであっても高風量及び高静圧を発生できることがわかった。この結果から、実施の形態1の送風ファン10はインペラの回転数を低くしても従来の送風ファンと同等のファン性能が得られることは明らかであり、通常、送風ファンの駆動時に発生する騒音はインペラの回転数が高くなると大きくなることから、実施の形態1によれば従来と同等のファン性能を得ながら騒音を低減できることがわかった。   As shown in FIG. 4, the air blowing fan 10 of the first embodiment has a higher air volume and static pressure than the conventional air blowing fan because the blade portion 3 has the backward blade portion 4 and the forward blade portion 5. It was found that a high air volume and a high static pressure can be generated even if the rotation speed of the impeller is the same. From this result, it is clear that the fan fan 10 of the first embodiment can obtain fan performance equivalent to that of the conventional fan even if the rotational speed of the impeller is lowered. Usually, noise generated when the fan is driven Therefore, according to the first embodiment, it has been found that noise can be reduced while obtaining fan performance equivalent to that of the prior art.

また、図5に示すように、後退翼部4の出口角β3が10°〜50°で形成されることで、吸気した空気を効率よくブレード部3の外周側へ向かって送り出すことができ、吸気効率を高めることができ、風量を一定にした場合の静圧を高めることができることがわかった。   Further, as shown in FIG. 5, by forming the exit angle β3 of the swept wing part 4 at 10 ° to 50 °, the intake air can be efficiently sent toward the outer peripheral side of the blade part 3, It was found that the intake efficiency can be increased and the static pressure can be increased when the airflow is constant.

また、図6に示すように、前進翼部5の出口角β2が55°〜110°で形成されることで、送り込まれた空気が前進翼部5の前面から流出し難くなり、風量を一定にした場合は静圧を高めることができることがわかった。   Moreover, as shown in FIG. 6, since the exit angle β2 of the forward blade portion 5 is formed at 55 ° to 110 °, it is difficult for the fed air to flow out from the front surface of the forward blade portion 5, and the air volume is constant. It was found that the static pressure can be increased when

また、図7に示すように、後退翼部4と前進翼部5のブレードの長さの比が1:0.5〜1.5で形成されることで、吸気と排気のバランスがよく、吸気した空気を効率よく外周側へ向かって遠心方向へ送り出すことができ、且つ外周側へ送り込まれた空気を効率よく強く押し出すことができることで、風量を一定にした場合は静圧を高めることができることがわかった。   Further, as shown in FIG. 7, the ratio of the blade lengths of the backward blade portion 4 and the forward blade portion 5 is formed at 1: 0.5 to 1.5, so that the balance between intake and exhaust is good. The intake air can be efficiently sent in the centrifugal direction toward the outer peripheral side, and the air sent to the outer peripheral side can be pushed out efficiently and strongly, so that the static pressure can be increased when the air volume is constant. I knew it was possible.

また、上述したような直線状のブレード部を有する従来の送風ファンについて、図5乃至図7の場合と同一の条件(インペラ1の回転数:約3500r/min、風量:50L/min)でその静圧を測定したところ、15Paであった。この結果から、本発明の実施の形態1の送風ファン10では、後退翼部4の出口角β3を10°〜50°とすることで、又は、前進翼部5の出口角β2を55°〜110°とすることで、若しくは、後退翼部4と前進翼部5のブレードの長さの比が1:0.5〜1.5とすることで、いずれも約17Pa以上の静圧を発生することができ、従来より約10%以上静圧を高めることができ、ファン性能に著しく優れることがわかった。   Further, with respect to the conventional blower fan having the linear blade portion as described above, under the same conditions as in the case of FIGS. 5 to 7 (the rotation speed of the impeller 1: about 3500 r / min, the air volume: 50 L / min) When the static pressure was measured, it was 15 Pa. From this result, in the blower fan 10 according to Embodiment 1 of the present invention, the exit angle β3 of the receding wing portion 4 is set to 10 ° to 50 °, or the exit angle β2 of the forward wing portion 5 is set to 55 ° to By setting it to 110 °, or by setting the ratio of the blade lengths of the backward wing portion 4 and the forward wing portion 5 to 1: 0.5 to 1.5, all generate static pressure of about 17 Pa or more. It has been found that the static pressure can be increased by about 10% or more compared with the prior art, and the fan performance is remarkably excellent.

以上のように本発明の実施の形態1におけるインペラ1及びそれを備えた送風ファン10は構成されているので、以下のような作用を有する。   As described above, the impeller 1 and the blower fan 10 including the impeller 1 according to Embodiment 1 of the present invention are configured, and thus have the following operations.

後退翼部4がインペラ1の回転方向Xの反対方向に湾曲し、空気を押し出す後退翼部4の前面が外周側に向かって傾斜しているので、吸気した空気を効率よく外周側へ向かって送り出すことができ、風量を高めることができる。また、前進翼部5がインペラ1の回転
方向Xに湾曲し、空気を押し出す前進翼部5の前面が内周側に向かって傾斜しているので、空気が前進翼部5の前面から流出し難くなり、空気を外側へ強く押し出すことができ、静圧を高めることができる。
Since the retreating wing part 4 is curved in the direction opposite to the rotation direction X of the impeller 1 and the front surface of the retreating wing part 4 for pushing out air is inclined toward the outer peripheral side, the sucked air is efficiently directed toward the outer peripheral side. It can be sent out and the air volume can be increased. Further, since the forward blade portion 5 is curved in the rotation direction X of the impeller 1 and the front surface of the forward blade portion 5 that pushes out the air is inclined toward the inner peripheral side, the air flows out from the front surface of the forward blade portion 5. It becomes difficult, the air can be strongly pushed outward, and the static pressure can be increased.

後退翼部4と前進翼部5とが滑らかな変曲部6で接続されているので、空気がブレード部3の内周側から外周側へ送り出される際の圧力損失が小さく、風量及び静圧の低下を防止できる。   Since the backward wing portion 4 and the forward wing portion 5 are connected by the smooth inflection portion 6, the pressure loss when air is sent from the inner peripheral side to the outer peripheral side of the blade portion 3 is small, and the air volume and static pressure are reduced. Can be prevented.

後退翼部4と前進翼部5が変曲部6を対称中心として対称に形成されているので、吸気と排気のバランスがよく、吸気した空気を効率よく外周側へ送り出し、且つ送り込まれた空気を効率よく強く押し出すことができる。   Since the backward wing portion 4 and the forward wing portion 5 are formed symmetrically with the inflection portion 6 as the center of symmetry, the balance between the intake air and the exhaust air is good, and the intake air is efficiently sent to the outer peripheral side. Can be pushed out efficiently and strongly.

インペラ1が後退翼部4と前進翼部5を有しているので上部吸気口14及び下部吸気口13で吸気された空気を効率よく且つ強く送り出して排気口15から外部へ排気でき、高風量及び高静圧を得ることができ、従来の送風ファンに比べ低回転数で同様或いはそれ以上の性能を実現でき、回転数と共に大きくなる騒音を低減できる。   Since the impeller 1 has the retreating wing part 4 and the advancing wing part 5, the air sucked in the upper intake port 14 and the lower intake port 13 can be efficiently and strongly sent out and exhausted from the exhaust port 15 to the outside. In addition, a high static pressure can be obtained, the same or higher performance can be realized at a lower rotational speed than that of a conventional blower fan, and noise that increases with the rotational speed can be reduced.

略円形状の上部吸気口14及び下部吸気口13の周縁部がインペラ1の変曲部6の近傍に位置するので、ケーシング11内に導入された空気を後退翼部4により効率よく外周側へ送り出すことができ、吸気効率を高めることができる。   Since the peripheral portions of the substantially circular upper air inlet 14 and lower air inlet 13 are located in the vicinity of the inflection portion 6 of the impeller 1, the air introduced into the casing 11 is efficiently moved to the outer peripheral side by the receding blade portion 4. It can be sent out and the intake efficiency can be increased.

本発明は、遠心型の送風ファンに用いられるインペラに関し、特に本発明によれば、ブレード部の内周側において吸気した空気を効率よく遠心方向へ送り出すことで吸気効率を高め高風量を得ることができると共に、ブレード部の外周側においてブレード部の表面から空気の流出を適切に抑制することで高静圧を得ることができるインペラを提供することができる。   The present invention relates to an impeller used for a centrifugal blower fan. In particular, according to the present invention, the intake air is efficiently sent out in the centrifugal direction on the inner peripheral side of the blade portion to increase the intake efficiency and obtain a high air volume. In addition, it is possible to provide an impeller that can obtain a high static pressure by appropriately suppressing the outflow of air from the surface of the blade portion on the outer peripheral side of the blade portion.

本発明は、遠心型の送風ファンに関し、特に本発明によれば、高風量及び高静圧を得ることで従来の送風ファンに比べ低回転数で同様或いはそれ以上の性能を実現でき、回転数と共に大きくなる騒音を低減できる送風ファンを提供することができる。   The present invention relates to a centrifugal blower fan, and in particular, according to the present invention, by obtaining a high air volume and a high static pressure, the same or higher performance can be realized at a lower rotational speed than a conventional blower fan, and the rotational speed. Also, it is possible to provide a blower fan that can reduce noise that increases.

(a)本発明の実施の形態1におけるインペラの平面図、(b)後退翼部と前進翼部の入口角及び出口角を説明するためのインペラの模式平面図(A) The top view of the impeller in Embodiment 1 of this invention, (b) The schematic top view of the impeller for demonstrating the entrance angle and exit angle of a retreat wing | blade part and an advance wing | blade part (a)本発明の実施の形態1における送風ファンの要部斜視図、(b)本発明の実施の形態1における送風ファンの内部透視平面図、(c)図2(b)の送風ファンの中央横断面図(A) The principal part perspective view of the ventilation fan in Embodiment 1 of this invention, (b) The internal perspective top view of the ventilation fan in Embodiment 1 of this invention, (c) Of the ventilation fan of FIG.2 (b) Center cross section インペラの要部拡大平面図Main part enlarged plan view of impeller 本発明の実施の形態の送風ファンと従来の送風ファンの風量と静圧との関係を示す風量静圧特性曲線図Air flow static pressure characteristic curve diagram showing the relationship between air flow and static pressure of the blower fan of the embodiment of the present invention and the conventional blower fan 本発明の実施の形態1の送風ファンの後退翼部の出口角β3を変化させた時の静圧の変化を示す相関図Correlation diagram showing changes in static pressure when outlet angle β3 of the swept wing part of the blower fan according to the first embodiment of the present invention is changed. 本発明の実施の形態1の送風ファンの前進翼部の出口角β2を変化させた時の静圧の変化を示す相関図Correlation diagram showing changes in static pressure when outlet angle β2 of the forward blade portion of the blower fan according to Embodiment 1 of the present invention is changed. 本発明の実施の形態1の送風ファンの後退翼部の長さと前進翼部の長さの比率を変化させた時の静圧の変化を示す相関図The correlation diagram which shows the change of the static pressure when changing the ratio of the length of the backward wing | blade part of the ventilation fan of Embodiment 1 of this invention, and the length of an advance wing | blade part.

符号の説明Explanation of symbols

1 インペラ
2 ボス部
2a 回転軸
2b 天面部
3 ブレード部
4 後退翼部
5 前進翼部
6 変曲部
6a 接続部
10 送風ファン
11 ケーシング
11a 底壁
11b 側壁
11c 内周面
12 ケーシングカバー(ケーシング上壁)
13 下部吸気口
14 上部吸気口
15 排気口
16 保持板
17 軸受部
18 ステータ
19 円筒状マグネット
20 回路基板
X インペラの回転方向
β1 後退翼部の入口角
β2 前進翼部の出口角
β3 後退翼部の出口角(前進翼部の入口角)
DESCRIPTION OF SYMBOLS 1 Impeller 2 Boss part 2a Rotating shaft 2b Top surface part 3 Blade part 4 Backward wing part 5 Forward wing part 6 Inflection part 6a Connection part 10 Blower fan 11 Casing 11a Bottom wall 11b Side wall 11c Inner peripheral surface 12 Casing cover (casing upper wall) )
13 Lower intake port 14 Upper intake port 15 Exhaust port 16 Holding plate 17 Bearing portion 18 Stator 19 Cylindrical magnet 20 Circuit board X Rotating direction of impeller β1 Inlet angle of retracted blade portion β2 Outlet angle of forward blade portion β3 Inverted blade portion Exit angle (advance angle of forward wing)

Claims (7)

円筒状のボス部と、前記ボス部の外周面から放射状に延びる複数のブレード部と、を備えた遠心型の送風ファンのインペラであって、
前記ブレード部が、前記ボス部の外周面から延びインペラの回転方向の反対方向に湾曲又は屈曲した後退翼部と、変曲部を介して前記後退翼部の外周側端部から延びインペラの回転方向に湾曲又は屈曲した前進翼部と、を備え、前記後退翼部が前記前進翼部よりインペラの回転軸中心側に位置することを特徴とするインペラ。
A centrifugal blast fan impeller comprising a cylindrical boss portion and a plurality of blade portions extending radially from the outer peripheral surface of the boss portion,
The blade portion extends from the outer peripheral surface of the boss portion and is bent or bent in a direction opposite to the rotation direction of the impeller, and the impeller rotates from the outer peripheral side end portion of the reverse blade portion via the inflection portion. And an advancing wing portion curved or bent in a direction, wherein the advancing wing portion is located closer to a rotation shaft center side of the impeller than the advancing wing portion.
前記後退翼部と前記前進翼部が、前記変曲部を対称中心として対称に形成されていることを特徴とする請求項1に記載のインペラ。 2. The impeller according to claim 1, wherein the backward wing portion and the forward wing portion are formed symmetrically with the inflection portion as a center of symmetry. 前記後退翼部と前記前進翼部の長さの比が1:0.5〜1.5であることを特徴とする請求項1又は2に記載のインペラ。 The impeller according to claim 1 or 2, wherein a ratio of a length of the backward wing portion and the forward wing portion is 1: 0.5 to 1.5. インペラの回転軸を中心とし前記変曲部を通る仮想円の接線と前記後退翼部の外周側端部の延長線とのなす角度が10°〜50°であることを特徴とする請求項1乃至3の内いずれか1項に記載のインペラ。 2. An angle formed by a tangent line of an imaginary circle passing through the inflection portion with the rotation axis of the impeller as a center and an extension line of an outer peripheral side end portion of the swept wing portion is 10 ° to 50 °. 4. The impeller according to any one of items 3 to 3. インペラの回転軸を中心とし前記前進翼部の外周側端部を通る仮想円の接線と前記前進翼部の外周側端部の延長線とのなす角度が55°〜110°であることを特徴とする請求項1乃至4の内いずれか1項に記載のインペラ。 An angle formed by a tangent line of an imaginary circle passing through the outer peripheral side end of the forward wing portion and the extension line of the outer peripheral side end of the forward wing portion is 55 ° to 110 ° with the impeller rotating shaft as a center. The impeller according to any one of claims 1 to 4. 扁平状のケーシングと、前記ケーシングの上壁又は底壁の内少なくともいずれか一方に形成された吸気口と、前記ケーシングの側壁に形成された排気口と、前記ケーシングの内部に配設された請求項1乃至5の内いずれか1項に記載のインペラと、を備えていることを特徴とする送風ファン。 A flat casing, an intake port formed in at least one of an upper wall or a bottom wall of the casing, an exhaust port formed in a side wall of the casing, and an inside of the casing. An air blower comprising the impeller according to any one of Items 1 to 5. 前記ケーシングの上壁又は底壁の少なくともその一方に形成された吸気口が略円形状に形成され、その周縁部が前記インペラの前記変曲部の近傍に位置するように形成されていることを特徴とする請求項6に記載の送風ファン。 The intake port formed in at least one of the upper wall or the bottom wall of the casing is formed in a substantially circular shape, and the peripheral edge thereof is formed in the vicinity of the inflection portion of the impeller. The blower fan according to claim 6, wherein
JP2004255240A 2004-09-02 2004-09-02 Impeller and blower fan having the same Expired - Lifetime JP4670285B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2004255240A JP4670285B2 (en) 2004-09-02 2004-09-02 Impeller and blower fan having the same

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2004255240A JP4670285B2 (en) 2004-09-02 2004-09-02 Impeller and blower fan having the same

Publications (2)

Publication Number Publication Date
JP2006070808A true JP2006070808A (en) 2006-03-16
JP4670285B2 JP4670285B2 (en) 2011-04-13

Family

ID=36151687

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2004255240A Expired - Lifetime JP4670285B2 (en) 2004-09-02 2004-09-02 Impeller and blower fan having the same

Country Status (1)

Country Link
JP (1) JP4670285B2 (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2946399A1 (en) * 2009-06-05 2010-12-10 Turbomeca CENTRIFUGAL COMPRESSOR WHEEL.
US8152474B2 (en) 2008-04-11 2012-04-10 Furui Precise Component (Kunshan) Co., Ltd. Cooling fan impeller
JP2014088787A (en) * 2012-10-29 2014-05-15 Minebea Co Ltd Impeller for centrifugal fan, and centrifugal fan
CN107956740A (en) * 2017-05-27 2018-04-24 莱克电气股份有限公司 A kind of impeller assembly and air purifier for air purifier
US10076056B2 (en) 2016-11-04 2018-09-11 Champ Tech Optical (Foshan) Corporation Cooling fan and electronic device having the same
KR101913147B1 (en) * 2016-10-10 2018-10-30 소애련 Centrifugal impeller having backward blades using dual gradient sectional shape type
JP2019044647A (en) * 2017-08-31 2019-03-22 山本光学株式会社 Fan unit and breathing protector equipped with the fan unit
JP2019515637A (en) * 2016-05-13 2019-06-06 エルジー イノテック カンパニー リミテッド Rotor and motor including the same

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2711402B2 (en) * 1988-01-05 1998-02-10 小原 康範 Transfer device with rotating blades

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2711402B2 (en) * 1988-01-05 1998-02-10 小原 康範 Transfer device with rotating blades

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8152474B2 (en) 2008-04-11 2012-04-10 Furui Precise Component (Kunshan) Co., Ltd. Cooling fan impeller
FR2946399A1 (en) * 2009-06-05 2010-12-10 Turbomeca CENTRIFUGAL COMPRESSOR WHEEL.
JP2014088787A (en) * 2012-10-29 2014-05-15 Minebea Co Ltd Impeller for centrifugal fan, and centrifugal fan
JP2019515637A (en) * 2016-05-13 2019-06-06 エルジー イノテック カンパニー リミテッド Rotor and motor including the same
JP7175767B2 (en) 2016-05-13 2022-11-21 エルジー イノテック カンパニー リミテッド rotor and motor including this
KR101913147B1 (en) * 2016-10-10 2018-10-30 소애련 Centrifugal impeller having backward blades using dual gradient sectional shape type
US10076056B2 (en) 2016-11-04 2018-09-11 Champ Tech Optical (Foshan) Corporation Cooling fan and electronic device having the same
TWI642852B (en) * 2016-11-04 2018-12-01 鴻準精密工業股份有限公司 Fan and electronic having the same
CN107956740A (en) * 2017-05-27 2018-04-24 莱克电气股份有限公司 A kind of impeller assembly and air purifier for air purifier
CN107956742A (en) * 2017-05-27 2018-04-24 莱克电气股份有限公司 A kind of impeller assembly and air purifier
JP2019044647A (en) * 2017-08-31 2019-03-22 山本光学株式会社 Fan unit and breathing protector equipped with the fan unit

Also Published As

Publication number Publication date
JP4670285B2 (en) 2011-04-13

Similar Documents

Publication Publication Date Title
JP2007182880A (en) Heat dissipation fan
JP2006046317A (en) Structure of centrifugal radiation fan
JP2008261280A (en) Axial fan
JP6012034B2 (en) Axial fan
JP2011080427A (en) Electric blower and vacuum cleaner using the same
JP4621980B2 (en) Fan motor
JP2007009831A (en) Impeller and blower fan equipped with it
JP4995464B2 (en) Blower
JP6019391B2 (en) Centrifugal blower and clothes dryer having the same
JP4670285B2 (en) Impeller and blower fan having the same
JP2010124534A (en) Mixed flow fan for electric motors and motor equipped with this mixed flow fan
JP5353864B2 (en) Blower
JP2010209770A (en) Electric blower and electric vacuum cleaner
JP2009203837A (en) Centrifugal fan
JP6719670B2 (en) Electric blower, vacuum cleaner, and hand dryer
JP2006177235A (en) Impeller and blower fan provided with the same
JP5500050B2 (en) Blower
CN111089069A (en) Fan with cooling device
JP2005273593A (en) Centrifugal fan
JP2005171987A (en) Small-sized mixed flow fan motor
JP2018112190A (en) Serial axial flow fan
WO2006082876A1 (en) Axial flow blower
JP2006220021A (en) Blast fan and electronic apparatus
KR100532052B1 (en) Air Inhalation Structure of Blower
JP2016070075A (en) Centrifugal fan

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20070807

RD01 Notification of change of attorney

Free format text: JAPANESE INTERMEDIATE CODE: A7421

Effective date: 20070912

RD01 Notification of change of attorney

Free format text: JAPANESE INTERMEDIATE CODE: A7421

Effective date: 20091120

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20101005

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20101203

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20101221

A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20110103

R151 Written notification of patent or utility model registration

Ref document number: 4670285

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R151

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20140128

Year of fee payment: 3