JP4649146B2 - Propeller fan - Google Patents

Propeller fan Download PDF

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JP4649146B2
JP4649146B2 JP2004247068A JP2004247068A JP4649146B2 JP 4649146 B2 JP4649146 B2 JP 4649146B2 JP 2004247068 A JP2004247068 A JP 2004247068A JP 2004247068 A JP2004247068 A JP 2004247068A JP 4649146 B2 JP4649146 B2 JP 4649146B2
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boss
propeller fan
blades
cylindrical portion
notch
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JP2006063879A (en
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輝夫 藤社
茂樹 富田
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Daikin Industries Ltd
Panasonic Corp
Panasonic Holdings Corp
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Daikin Industries Ltd
Panasonic Corp
Matsushita Electric Industrial Co Ltd
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/325—Rotors specially for elastic fluids for axial flow pumps for axial flow fans
    • F04D29/329—Details of the hub

Description

この発明は、空気調和機の送風機等に使用されるプロペラファンに関する。   The present invention relates to a propeller fan used for a blower of an air conditioner or the like.

従来、プロペラファンとしては、空気調和機に搭載可能な室外ファンに用いられ、構成部位としてファンモータに取り付けられるボス(軸流部分)と、送風回路を形成する羽根部分とを備えたものがある(例えば、特開２００２−５４５９７号公報(特許文献１)参照)。上記プロペラファンでは、主に羽根部分の形状を薄肉化して、軽量化によりコストダウンを図っている。このため、羽根部分を薄肉化するさらなる軽量化は、ボスと羽根部分の接合部の強度が低下し、回転時の破壊強度の低下や熱変形反りによる送風性能の低下を生じるという問題がある。
特開２００２−５４５９７号公報 Conventionally, as a propeller fan, there is one that is used for an outdoor fan that can be mounted on an air conditioner, and includes a boss (axial flow portion) that is attached to a fan motor as a component and a blade portion that forms a blower circuit. (For example, refer to JP 2002-54597 A (Patent Document 1)). In the propeller fan, the shape of the blade portion is mainly thinned to reduce the cost by reducing the weight. For this reason, the further weight reduction that makes the blade portion thinner has a problem that the strength of the joint portion between the boss and the blade portion is lowered, and the breaking performance is lowered during rotation and the blowing performance is lowered due to thermal deformation warpage.
JP 2002-54597 A

そこで、この発明の目的は、強度低下や熱変形などによる信頼性低下を防止しつつ軽量化でき、さらに送風性能も向上できるプロペラファンを提供することにある。   Accordingly, an object of the present invention is to provide a propeller fan that can be reduced in weight while preventing deterioration in reliability due to a decrease in strength, thermal deformation, or the like, and can further improve air blowing performance.

上記目的を達成するため、この発明のプロペラファンは、
円筒部を有するボスと、上記ボスの円筒部の外周側に放射状に配置された複数の羽根とを備え、上記ボスと上記複数の羽根とが一体に成形された合成樹脂製のプロペラファンであって、
上記ボスの円筒部の上記複数の羽根が連結された連結部分の軸方向風下側への投影領域のうちの上記複数の羽根が連結された上記連結部分側に、上記各羽根の前縁側から後縁側に沿って非切り欠き部を設けると共に、
上記ボスの円筒部の上記複数の羽根が連結された連結部分の軸方向風下側への投影領域のうちの上記非切り欠き部を除く領域の全てを切り欠いている切り欠き部を設けたことを特徴とする。 In order to achieve the above object, the propeller fan of the present invention is:
A propeller fan made of a synthetic resin, comprising a boss having a cylindrical portion and a plurality of blades radially arranged on the outer peripheral side of the cylindrical portion of the boss, wherein the boss and the plurality of blades are integrally formed. And
From the front edge side of each blade to the connection portion side where the plurality of blades are connected in the axially leeward projection area of the connection portion where the plurality of blades of the boss cylindrical portion are connected. While providing a notch along the edge side,
Provided with a cutout portion that cuts out all of the region excluding the non-notch portion of the projection area on the axially leeward side of the connecting portion to which the plurality of blades of the cylindrical portion of the boss are connected. It is characterized by.

上記構成のプロペラファンによれば、ボスの円筒部において各羽根が連結された連結部分の軸方向風下側への投影領域のうちの上記連結部分側に、各羽根の前縁側から後縁側に沿って非切り欠き部を設けると共に、ボスの円筒部の上記連結部分の軸方向風下側への投影領域のうちの上記非切り欠き部を除く領域の全てを切り欠いている切り欠き部を設けることによって、強度低下や熱変形などによる信頼性低下を防止しつつ、軽量化によるコストダウンが図れると共に、送風回路形成上の流路損失であった軸流部分の送風抵抗を排除することにより、送風性能も向上できる。 According to the propeller fan having the above-described configuration, from the front edge side of each blade to the rear edge side of the projection portion on the axially leeward side of the connection portion where each blade is connected in the cylindrical portion of the boss. In addition to providing a non-notched portion, a notched portion is formed by notching the entire region excluding the non-notched portion of the projected area of the cylindrical portion of the boss toward the leeward side in the axial direction. As a result, it is possible to reduce costs by reducing weight while preventing deterioration in reliability due to strength reduction and thermal deformation, etc., and by removing the blowing resistance of the axial flow part that was a flow path loss in the blowing circuit formation, Performance can also be improved.

また、上記切り欠き部が、ボスの円筒部の複数の羽根が連結された連結部分の軸方向風下側への投影領域のうちの上記非切り欠き部を除く領域の全てを切り欠いていることによって、軸流部分の送風抵抗を大幅に排除でき、ボスの円筒部による流路損失を低減できる。
また、上記切り欠き部と複数の羽根が連結された連結部分との間に非切り欠き部を設けることによって、円筒部と複数の羽根との連結部分の強度を高めることができる。 Further , the cutout portion cuts out all of the region excluding the non-cutout portion of the projection region on the axial leeward side of the connecting portion where the plurality of blades of the cylindrical portion of the boss are connected. As a result, the blowing resistance in the axial flow portion can be largely eliminated, and the flow path loss due to the cylindrical portion of the boss can be reduced.
Moreover, the intensity | strength of the connection part of a cylindrical part and a some blade | wing can be raised by providing a non-notch part between the said notch part and the connection part to which the some blade | wing was connected.

また、一実施形態のプロペラファンは、上記ボスの円筒部の周方向に、上記複数の羽根が連結された連結部分と上記複数の羽根が連結されていない領域とが交互に配置され、上記切り欠き部は、上記ボスの円筒部の上記複数の羽根が連結されていない領域の少なくとも一部を切り欠いていることを特徴とする。   Further, in the propeller fan according to an embodiment, in the circumferential direction of the cylindrical portion of the boss, a connection portion where the plurality of blades are connected and a region where the plurality of blades are not connected are alternately arranged, The notch portion is characterized by notching at least a part of a region where the plurality of blades of the cylindrical portion of the boss are not connected.

上記実施形態のプロペラファンによれば、上記ボスの円筒部の周方向に、複数の羽根が連結された連結部分と複数の羽根が連結されていない領域とが交互に配置された構造のプロペラファンにおいて、切り欠き部が、ボスの円筒部の複数の羽根が連結されていない領域の少なくとも一部を切り欠いていることによって、羽根が連結された連結部分の軸方向風下側への投影領域のみを切り欠いた場合よりも、軸流部分の送風抵抗をより多く排除でき、ボスの円筒部による流路損失を低減できる。   According to the propeller fan of the above-described embodiment, a propeller fan having a structure in which a connection portion where a plurality of blades are connected and a region where the plurality of blades are not connected are alternately arranged in the circumferential direction of the cylindrical portion of the boss. In this case, the cutout portion cuts at least a part of the area where the plurality of blades of the cylindrical portion of the boss are not connected, so that only the projection area on the leeward side in the axial direction of the connection portion where the blades are connected. As compared with the case where the notch is notched, more airflow resistance in the axial flow portion can be eliminated, and the flow path loss due to the cylindrical portion of the boss can be reduced.

また、一実施形態のプロペラファンは、上記ボスが、上記円筒部の内周側かつ軸方向風上側に設けられたリブを有し、上記切り欠き部は、上記円筒部の軸方向風下側の端から上記リブまで切り欠いていることを特徴とする。   In one embodiment of the propeller fan, the boss has a rib provided on the inner peripheral side of the cylindrical portion and on the axially windward side, and the notch portion is located on the axially leeward side of the cylindrical portion. It is characterized by notching from the end to the rib.

上記実施形態のプロペラファンによれば、上記切り欠き部は、円筒部の軸方向風下側の端から、円筒部の内周側かつ軸方向風上側に設けられたリブまで切り欠いているので、円筒部を補強するリブの働きを妨げることなく、流路損失を低減するのに有効な切り欠き部を形成できる。   According to the propeller fan of the above embodiment, the cutout portion is cut out from the axial leeward end of the cylindrical portion to the rib provided on the inner peripheral side and the axial leeward side of the cylindrical portion. A notch portion effective in reducing the flow path loss can be formed without hindering the function of the rib for reinforcing the cylindrical portion.

また、一実施形態のプロペラファンは、上記複数の羽根が、上記ボスの円筒部近傍の肉厚が前縁側から後縁側に向かって徐々に薄くなっており、上記非切り欠き部は、上記各羽根の前縁側から後縁側に向かって幅が狭くなっていることを特徴とする。   Further, in the propeller fan according to an embodiment, the plurality of blades are such that the thickness in the vicinity of the cylindrical portion of the boss gradually decreases from the front edge side toward the rear edge side, and the non-notched portion The width is narrowed from the front edge side of the blade toward the rear edge side.

上記実施形態のプロペラファンによれば、上記複数の羽根がボスの円筒部近傍の肉厚が前縁側から後縁側に向かって徐々に薄くなるのに従って、非切り欠き部が各羽根の前縁側から後縁側に向かって幅を狭くすることにより、ボスの円筒部の複数の羽根が連結された連結部分の羽根の肉厚が厚い領域に対応する非切り欠き部の幅を広くして、羽根を支える強度を適切に保つことにより羽根の変形を防止できる。   According to the propeller fan of the above-described embodiment, as the thickness of the plurality of blades in the vicinity of the cylindrical portion of the boss gradually decreases from the front edge side toward the rear edge side, the non-notched portions are formed from the front edge side of each blade. By narrowing the width toward the trailing edge, the width of the non-notched portion corresponding to the region where the blade thickness of the connecting portion where the plurality of blades of the cylindrical portion of the boss are connected is thickened. It is possible to prevent the blades from being deformed by appropriately maintaining the supporting strength.

以上より明らかなように、この発明のプロペラファンによれば、ボスの円筒部において各羽根との連結部分の投影領域のうちの少なくとも１部に切り欠き部を設けることによって、強度低下や熱変形などによる信頼性低下を防止しつつ軽量化できると共に、送風性能を向上できるプロペラファンを実現することができる。   As is clear from the above, according to the propeller fan of the present invention, the notch portion is provided in at least one of the projection areas of the connection portion with each blade in the cylindrical portion of the boss, thereby reducing the strength and thermal deformation. Thus, it is possible to realize a propeller fan that can be reduced in weight while preventing a decrease in reliability due to the above, and that can improve air blowing performance.

以下、この発明のプロペラファンを図示の実施の形態により詳細に説明する。   Hereinafter, the propeller fan of this invention is demonstrated in detail by embodiment of illustration.

図１(a)はこの発明の実施の一形態の空気調和機の送風機等に使用されるプロペラファンの正面図であり、図１(b)は上記プロペラファンの側面図であり、図１(c)は上記プロペラファンの他方から見た側面図である。   FIG. 1 (a) is a front view of a propeller fan used in an air conditioner blower or the like according to an embodiment of the present invention, and FIG. 1 (b) is a side view of the propeller fan. c) is a side view seen from the other side of the propeller fan.

上記プロペラファンは、円筒部１aを有するボス１と、上記ボス１の円筒部１aの外周側に放射状に形成された複数の羽根２とを有する。上記ボス１の円筒部１aには、複数の羽根２が連結された連結部分の軸方向風下側への投影領域の一部を含む領域を切り欠く切り欠き部３を設けている。上記ボス１の円筒部１aに、ファンモータ(図示せず)の回転軸が軸中心に固定される。   The propeller fan includes a boss 1 having a cylindrical portion 1 a and a plurality of blades 2 formed radially on the outer peripheral side of the cylindrical portion 1 a of the boss 1. The cylindrical portion 1a of the boss 1 is provided with a cutout portion 3 that cuts out a region including a part of a projection region on the axially leeward side of a connecting portion where a plurality of blades 2 are connected. A rotating shaft of a fan motor (not shown) is fixed to the cylindrical portion 1a of the boss 1 at the shaft center.

図２は上記プロペラファンのボス１の要部の拡大斜視図を示しており、切り欠き部３は、ボス１の円筒部１aの複数の羽根２が連結された連結部分の軸方向風下側への投影領域３Ａの一部と、ボス１の円筒部１aの複数の羽根２が連結されていない領域３Ｂの一部を切り欠いている。また、上記切り欠き部３と複数の羽根２が連結された連結部分との間に非切り欠き部４を設けている。このプロペラファンは、ボス１と複数の羽根２とを合成樹脂を用いて一体に成形されている。また、上記ボス１の円筒部１aの内周側かつ軸方向風上側に、円筒部１aの軸を中心に複数のリブ１０を放射状に設けている。   FIG. 2 is an enlarged perspective view of the main part of the boss 1 of the propeller fan. The notch 3 is directed to the leeward side in the axial direction of the connecting portion where the plurality of blades 2 of the cylindrical part 1a of the boss 1 are connected. A part of the projection area 3A and a part of the area 3B where the plurality of blades 2 of the cylindrical portion 1a of the boss 1 are not connected are cut out. Moreover, the non-notch part 4 is provided between the said notch part 3 and the connection part to which the some blade | wing 2 was connected. In this propeller fan, a boss 1 and a plurality of blades 2 are integrally formed using a synthetic resin. In addition, a plurality of ribs 10 are provided radially around the axis of the cylindrical portion 1a on the inner peripheral side of the cylindrical portion 1a of the boss 1 and on the upstream side in the axial direction.

図２において、各羽根２のボス１の円筒部１a近傍の肉厚が前縁側２aから後縁側２bに向かって徐々に薄くなっている。上記非切り欠き部４は、羽根２の前縁側２aから後縁側２bに向かって幅が狭くなっている。   In FIG. 2, the thickness in the vicinity of the cylindrical portion 1a of the boss 1 of each blade 2 gradually decreases from the front edge side 2a toward the rear edge side 2b. The non-notched portion 4 has a width that decreases from the front edge side 2a of the blade 2 toward the rear edge side 2b.

また、図３,図４は上記プロペラファンの斜め前方(風上側)および斜め後方(風下側)から見た斜視図を示している。なお、図４において、１１は切り欠き部がないときの円筒部の風下側の端部の縁を示している。また、図４では、ボス１の円筒部１aの内周側のリブ１０等を省略している。   3 and 4 are perspective views of the propeller fan as viewed obliquely from the front (windward side) and obliquely from the rear (leeward side). In addition, in FIG. 4, 11 has shown the edge of the edge part of the leeward side of a cylindrical part when there is no notch part. In FIG. 4, the rib 10 on the inner peripheral side of the cylindrical portion 1a of the boss 1 is omitted.

上記構成のプロペラファンにおいて、図３,図４に示すように、矢印Ｒ１の方向にボス１を中心に回転すると、図３中の上方の風上側から下方の風下側に向かって空気が流れる。このとき、羽根２の正圧側(風下側)の翼面に沿って前縁２a側から流れ込んだ空気流の一部は、矢印Ｒ２に示す方向に流れて、ボス１側の切り欠き部３を通過する。   In the propeller fan configured as described above, as shown in FIGS. 3 and 4, when the boss 1 is rotated in the direction of the arrow R1, air flows from the upper windward side toward the lower windward side in FIG. At this time, a part of the airflow flowing from the front edge 2a side along the blade surface on the positive pressure side (leeward side) of the blade 2 flows in the direction indicated by the arrow R2, and passes through the notch 3 on the boss 1 side. pass.

次に、図１〜図４に示すボス１に切り欠き部３が設けられたプロペラファンと、ボスに切り欠き部を設けていない比較例のプロペラファンとの性能比較を行った結果を説明する。   Next, the results of performance comparison between the propeller fan in which the boss 1 shown in FIGS. 1 to 4 is provided with the notch 3 and the propeller fan of the comparative example in which the boss is not provided with the notch will be described. .

図５は上記プロペラファンの回転数と風量との関係を示しており、図５において、横軸はプロペラファンの回転数[ｒｐｍ]を表し、縦軸は風量[ｍ3／min]を表している。図５に示すように、この実施形態のプロペラファンは、比較例のプロペラファンに比べて全ての回転数領域において風量が増大している。 FIG. 5 shows the relationship between the rotation speed of the propeller fan and the air volume. In FIG. 5, the horizontal axis represents the rotation speed [rpm] of the propeller fan, and the vertical axis represents the air volume [m 3 / min]. Yes. As shown in FIG. 5, the propeller fan of this embodiment has an increased air volume in all rotation speed regions as compared with the propeller fan of the comparative example.

また、図６は上記プロペラファンの送風音と風量との関係を示しており、図６において、横軸はプロペラファンの送風音[dＢ]を表し、縦軸は風量[ｍ3／min]を表している。図６に示すように、この実施形態のプロペラファンは、比較例のプロペラファンに比べて同一送風音において風量が増大している。 FIG. 6 shows the relationship between the blowing sound of the propeller fan and the air volume. In FIG. 6, the horizontal axis represents the blowing sound [dB] of the propeller fan, and the vertical axis represents the air volume [m 3 / min]. Represents. As shown in FIG. 6, the propeller fan of this embodiment has an increased air volume in the same blowing sound as compared to the propeller fan of the comparative example.

また、図７は上記プロペラファンの風量と静圧との関係を示しており、図７において、横軸はプロペラファンの風量[ｍ3／min]を表し、縦軸は静圧[ｍｍＡｑ]を表している。図７に示すように、この実施形態のプロペラファンは、比較例のプロペラファンに比べて全体に静圧が増大しており、風量が少ないほど静圧の増大量が大きい。 FIG. 7 shows the relationship between the air flow and the static pressure of the propeller fan. In FIG. 7, the horizontal axis represents the air flow [m 3 / min] of the propeller fan, and the vertical axis represents the static pressure [mmAq]. Represents. As shown in FIG. 7, the propeller fan of this embodiment has an increased static pressure as a whole as compared with the propeller fan of the comparative example, and the amount of increase in static pressure is larger as the air volume is smaller.

このように、この発明の実施形態のプロペラファンによれば、ボス１の円筒部１aにおいて各羽根２が連結された連結部分の投影領域のうちの少なくとも１部に切り欠き部３を設けることによって、強度低下や熱変形などによる信頼性低下を防止しつつ、軽量化によるコストダウンが図れる。また、送風回路形成上の流路損失であった軸流部分の送風抵抗を排除することにより、送風性能も向上できる。   Thus, according to the propeller fan of the embodiment of the present invention, by providing the notch portion 3 in at least one portion of the projection area of the connecting portion where the blades 2 are connected in the cylindrical portion 1a of the boss 1. Further, it is possible to reduce the cost by reducing the weight while preventing the decrease in reliability due to the decrease in strength or thermal deformation. In addition, the air blowing performance can be improved by eliminating the air flow resistance in the axial flow portion, which is the flow path loss in the air blowing circuit formation.

また、上記ボス１の円筒部１aの複数の羽根２が連結された連結部分の軸方向風下側への投影領域のうちの連結部分近傍を除く領域の全てを切り欠き部３により切り欠いていることによって、軸流部分の送風抵抗を大幅に排除でき、ボス１の円筒部１aによる流路損失を低減することができる。   Further, all of the region except for the vicinity of the connected portion of the projection region on the axially leeward side of the connecting portion to which the plurality of blades 2 of the cylindrical portion 1a of the boss 1 are connected is cut out by the notch portion 3. As a result, the blowing resistance in the axial flow portion can be largely eliminated, and the flow path loss due to the cylindrical portion 1a of the boss 1 can be reduced.

また、上記切り欠き部３が、ボス１の円筒部１aの複数の羽根２が連結されていない領域の少なくとも一部を切り欠いていることによって、羽根２が連結された連結部分の軸方向風下側への投影領域のみを切り欠いた場合よりも、軸流部分の送風抵抗をより多く排除でき、ボス１の円筒部１aによる流路損失を低減することができる。   Further, the cutout portion 3 cuts out at least a part of a region where the plurality of blades 2 of the cylindrical portion 1a of the boss 1 are not connected, so that the axially leeward of the connection portion to which the blades 2 are connected. As compared with the case where only the projection area to the side is cut out, more airflow resistance in the axial flow portion can be eliminated, and the flow path loss due to the cylindrical portion 1a of the boss 1 can be reduced.

また、上記切り欠き部３は、円筒部１aの軸方向風下側の端から、円筒部１aの内周側かつ軸方向風上側に設けられたリブ１０まで切り欠いているので、円筒部１aを補強するリブ１０の働きを妨げることなく、流路損失を低減するのに有効な切り欠き部３を形成できる。   The notch 3 is notched from the axially leeward end of the cylindrical part 1a to the rib 10 provided on the inner peripheral side and the axially leeward side of the cylindrical part 1a. The notch 3 effective to reduce the flow path loss can be formed without hindering the function of the reinforcing rib 10.

また、上記切り欠き部３と複数の羽根２が連結された連結部分との間に非切り欠き部４を設けることによって、円筒部１aと複数の羽根２との連結部分の強度を高めることができる。   Further, by providing the non-notched portion 4 between the notched portion 3 and the connecting portion where the plurality of blades 2 are connected, the strength of the connecting portion between the cylindrical portion 1a and the plurality of blades 2 can be increased. it can.

さらに、上記複数の羽根２がボス１の円筒部１a近傍の肉厚が前縁２a側から後縁２b側に向かって徐々に薄くなるのに従って、非切り欠き部４が各羽根２の前縁２a側から後縁２b側に向かって幅を狭くすることにより、ボス１の円筒部１aの複数の羽根２が連結された連結部分の羽根２の肉厚が厚い領域に対応する非切り欠き部４の領域の幅を広くして、羽根２を支える強度を適切に保つことにより羽根２の変形を防止することができる。   Further, as the thickness of the plurality of blades 2 in the vicinity of the cylindrical portion 1a of the boss 1 gradually decreases from the front edge 2a side toward the rear edge 2b side, the non-notched portions 4 become the front edges of the blades 2. By reducing the width from the 2a side toward the rear edge 2b side, the notched portion corresponding to the region where the thickness of the blade 2 of the connecting portion to which the plurality of blades 2 of the cylindrical portion 1a of the boss 1 are connected is thick. The deformation of the blade 2 can be prevented by widening the width of the region 4 and maintaining the strength for supporting the blade 2 appropriately.

上記実施の形態では、空気調和機の送風機等に使用されるプロペラファンについて説明したが、空気調和機に限らず、他の装置の送風機にこの発明のプロペラファンを適用してもよい。   Although the propeller fan used for the air conditioner blower or the like has been described in the above embodiment, the propeller fan of the present invention may be applied not only to the air conditioner but also to a blower of another device.

また、上記実施の形態では、ボス１の円筒部１aの内周側かつ軸方向風上側に、円筒部１aの軸を中心に複数のリブ１０を放射状に設けたプロペラファンについて説明したが、リブの構造はこれに限らず、ボスの円筒部の内周側かつ軸方向風上側に設けられ、ボスの強度を高めるものであればよい。   Moreover, although the said embodiment demonstrated the propeller fan which provided the some rib 10 radially centering on the axis | shaft of the cylindrical part 1a on the inner peripheral side and the axial direction windward side of the cylindrical part 1a of the boss 1, The structure is not limited to this, and any structure may be used as long as it is provided on the inner peripheral side of the cylindrical portion of the boss and on the upwind side in the axial direction and increases the strength of the boss.

図１はこの発明の実施の一形態のプロペラファンの正面図と側面図である。FIG. 1 is a front view and a side view of a propeller fan according to an embodiment of the present invention. 図２は上記プロペラファンのボスの要部の拡大斜視図である。FIG. 2 is an enlarged perspective view of a main part of the boss of the propeller fan. 図３は上記プロペラファンの斜め前方(風上側)から見た斜視図である。FIG. 3 is a perspective view of the propeller fan as viewed obliquely from the front (windward side). 図４は上記プロペラファンの斜め後方(風下側)から見た斜視図である。FIG. 4 is a perspective view of the propeller fan as viewed obliquely from the rear (leeward side). 図５は上記プロペラファンの回転数と風量との関係を示す図である。FIG. 5 is a diagram showing the relationship between the rotation speed of the propeller fan and the air volume. 図６は上記プロペラファンの送風音と風量との関係を示す図である。FIG. 6 is a diagram showing the relationship between the blowing sound and the air volume of the propeller fan. 図７は上記プロペラファンの風量と静圧との関係を示す図である。FIG. 7 is a diagram showing the relationship between the air volume and static pressure of the propeller fan.

１…ボス
１a…円筒部
２…羽根
２a…前縁
２b…後縁
３…切り欠き部
４…非切り欠き部
１０…リブ DESCRIPTION OF SYMBOLS 1 ... Boss 1a ... Cylindrical part 2 ... Blade | wing 2a ... Front edge 2b ... Rear edge 3 ... Notch part 4 ... Non-notch part 10 ... Rib

Claims (4)

円筒部(１a)を有するボス(１)と、上記ボス(１)の円筒部(１a)の外周側に放射状に配置された複数の羽根(２)とを備え、上記ボス(１)と上記複数の羽根(２)とが一体に成形された合成樹脂製のプロペラファンであって、
上記ボス(１)の円筒部(１a)の上記複数の羽根(２)が連結された連結部分の軸方向風下側への投影領域のうちの上記複数の羽根(２)が連結された上記連結部分側に、上記各羽根(２)の前縁側から後縁側に沿って非切り欠き部(４)を設けると共に、
上記ボス(１)の円筒部(１a)の上記複数の羽根(２)が連結された連結部分の軸方向風下側への投影領域のうちの上記非切り欠き部(４)を除く領域の全てを切り欠いている切り欠き部(３)を設けたことを特徴とするプロペラファン。 A boss (1) having a cylindrical portion (1a) and a plurality of blades (2) arranged radially on the outer peripheral side of the cylindrical portion (1a) of the boss (1), the boss (1) and the above-mentioned A propeller fan made of synthetic resin in which a plurality of blades (2) are integrally molded,
The connection in which the plurality of blades (2) in the projection area toward the leeward side in the axial direction of the connecting portion where the plurality of blades (2) of the cylindrical portion (1a) of the boss (1) are connected is connected. On the partial side, a notch (4) is provided from the front edge side to the rear edge side of each blade (2), and
All of the areas excluding the non-notched part (4) in the projected area toward the leeward side in the axial direction of the connecting part where the plurality of blades (2) of the cylindrical part (1a) of the boss (1) are connected. Propeller fan, characterized in that a notch (3) is provided . 請求項１に記載のプロペラファンにおいて、
上記ボス(１)の円筒部(１a)の周方向に、上記複数の羽根(２)が連結された連結部分と上記複数の羽根(２)が連結されていない領域とが交互に配置され、
上記切り欠き部(３)は、上記ボス(１)の円筒部(１a)の上記複数の羽根(２)が連結されていない領域の少なくとも一部を切り欠いていることを特徴とするプロペラファン。 The propeller fan according to claim 1 ,
In the circumferential direction of the cylindrical portion (1a) of the boss (1), a connection portion where the plurality of blades (2) are connected and a region where the plurality of blades (2) are not connected are alternately arranged,
The notch (3) is a propeller fan characterized by notching at least part of a region where the plurality of blades (2) of the cylindrical part (1a) of the boss (1) are not connected. . 請求項１または２に記載のプロペラファンにおいて、
上記ボス(１)は、上記円筒部(１a)の内周側かつ軸方向風上側に設けられたリブを有し、
上記切り欠き部(３)は、上記円筒部(１a)の軸方向風下側の端から上記リブ(１０)まで切り欠いていることを特徴とするプロペラファン。 The propeller fan according to claim 1 or 2 ,
The boss (1) has a rib provided on the inner peripheral side of the cylindrical part (1a) and on the axially upwind side,
The propeller fan, wherein the notch (3) is notched from the axially leeward end of the cylindrical part (1a) to the rib (10). 請求項１から３までのいずれか１つに記載のプロペラファンにおいて、
上記複数の羽根(２)は、上記ボス(１)の円筒部(１a)近傍の肉厚が前縁側から後縁側に向かって徐々に薄くなっており、
上記非切り欠き部(４)は、上記各羽根(２)の前縁側から後縁側に向かって幅が狭くなっていることを特徴とするプロペラファン。 The propeller fan according to any one of claims 1 to 3 ,
In the plurality of blades (2), the thickness in the vicinity of the cylindrical portion (1a) of the boss (1) is gradually reduced from the front edge side toward the rear edge side.
The propeller fan, wherein a width of the non-notched portion (4) is narrowed from a front edge side to a rear edge side of each blade (2).
JP2004247068A 2004-08-26 2004-08-26 Propeller fan Expired - Fee Related JP4649146B2 (en)

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JP4797776B2 (en) * 2006-04-24 2011-10-19 パナソニック株式会社 Mixed flow blower impeller and air conditioner
JP5120299B2 (en) * 2009-03-10 2013-01-16 パナソニック株式会社 Blower impeller
JP5980180B2 (en) * 2013-08-08 2016-08-31 三菱電機株式会社 Axial flow fan and air conditioner having the axial flow fan
CN112098834B (en) * 2020-06-06 2022-03-01 浙江永源机电制造有限公司 Heat dissipation mechanism for air compressor and control method of heat dissipation mechanism

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5114807U (en) * 1974-07-17 1976-02-03
JPS552240Y1 (en) * 1976-06-18 1980-01-21
JPS56135792A (en) * 1980-03-24 1981-10-23 Hitachi Ltd Blower
JPS62173595U (en) * 1986-04-24 1987-11-04
JPH0286998A (en) * 1988-09-22 1990-03-27 Mitsubishi Electric Corp Blower
JPH02188698A (en) * 1989-01-13 1990-07-24 Mitsubishi Electric Corp Blower
JPH11182493A (en) * 1997-12-19 1999-07-06 Fujitsu General Ltd Axial-flow fan

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5114807U (en) * 1974-07-17 1976-02-03
JPS552240Y1 (en) * 1976-06-18 1980-01-21
JPS56135792A (en) * 1980-03-24 1981-10-23 Hitachi Ltd Blower
JPS62173595U (en) * 1986-04-24 1987-11-04
JPH0286998A (en) * 1988-09-22 1990-03-27 Mitsubishi Electric Corp Blower
JPH02188698A (en) * 1989-01-13 1990-07-24 Mitsubishi Electric Corp Blower
JPH11182493A (en) * 1997-12-19 1999-07-06 Fujitsu General Ltd Axial-flow fan

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