[go: up one dir, main page]

JP2017115769A - Blade for blower, and blower - Google Patents

Blade for blower, and blower Download PDF

Info

Publication number
JP2017115769A
JP2017115769A JP2015253678A JP2015253678A JP2017115769A JP 2017115769 A JP2017115769 A JP 2017115769A JP 2015253678 A JP2015253678 A JP 2015253678A JP 2015253678 A JP2015253678 A JP 2015253678A JP 2017115769 A JP2017115769 A JP 2017115769A
Authority
JP
Japan
Prior art keywords
blade
blower
upright
wing
fan
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP2015253678A
Other languages
Japanese (ja)
Inventor
一彦 三宮
Kazuhiko Sannomiya
一彦 三宮
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.)
Mitsubishi Chemical Infratec Co Ltd
Original Assignee
Mitsubishi Chemical Infratec 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 Mitsubishi Chemical Infratec Co Ltd filed Critical Mitsubishi Chemical Infratec Co Ltd
Priority to JP2015253678A priority Critical patent/JP2017115769A/en
Publication of JP2017115769A publication Critical patent/JP2017115769A/en
Pending legal-status Critical Current

Links

Images

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Other Air-Conditioning Systems (AREA)

Abstract

PROBLEM TO BE SOLVED: To reduce noise of a blower, the blower including a blade for a blower having a blade body and a standing blade erected on an outer peripheral edge of the blade body.SOLUTION: A blade 1 for a blower includes a blade body 2 and a standing blade 3 erected on an outer peripheral edge of the blade body 2. A height of the standing blade 3 is substantially constant in the rear of an intermediate point M. A height of the standing blade 3 is gradually reduced forward from the intermediate point M. The standing blade 3 is inclined in a radiation direction with respect to upright. An intersection angle δ between the standing blade 3 and the blade body 2 falls within a range of 90.1-91°.SELECTED DRAWING: Figure 5

Description

本発明は、軸流型送風機に用いられる送風機用翼に係り、特に翼本体の外周縁に沿って起立翼が設けられた送風機用翼に関する。また、本発明は、この送風機用翼を備えた送風機、そしてこの送風機を備えた冷却塔に関する。   The present invention relates to a blower blade used in an axial flow blower, and more particularly to a blower blade provided with standing blades along the outer peripheral edge of a blade body. The present invention also relates to a blower provided with the fan blades and a cooling tower provided with the blower.

冷却塔の送風機等として、ハブに取り付けられた翼をシュラウドが取り囲んでいる軸流型送風機が広く用いられている。この軸流型送風機においては、翼が回転することにより、ハブの軸心線方向に流体(多くの場合、空気)が流れる。この際、翼の両面側に圧力差が生じ、この圧力差によって翼の外周縁とシュラウド内周面との隙間を空気が逆流する。この空気の逆流に伴って翼の先端に渦が生じ、騒音が発生する。   As a cooling tower blower or the like, an axial flow blower in which a shroud surrounds a blade attached to a hub is widely used. In this axial flow type blower, fluid (in many cases, air) flows in the axial direction of the hub by rotating the blades. At this time, a pressure difference is generated on both sides of the blade, and the air flows backward through the gap between the outer peripheral edge of the blade and the inner surface of the shroud. As the air flows backward, a vortex is generated at the tip of the blade and noise is generated.

この騒音を小さくするために、特許文献1,2には、翼本体の外周縁に沿って送風方向下流側に向って起立する起立翼を設けることが記載されている。なお、特許文献1では、翼本体をブレードと称し、起立翼を補助翼と称している。特許文献2では、起立翼は翼端板と称されている。   In order to reduce this noise, Patent Documents 1 and 2 describe providing standing blades that stand along the outer peripheral edge of the blade body toward the downstream side in the blowing direction. In Patent Document 1, the blade body is referred to as a blade, and the upright blade is referred to as an auxiliary blade. In Patent Document 2, the upright blade is referred to as a blade end plate.

特開2000−314394号公報JP 2000-314394 A 特開2013−96307号公報JP 2013-96307 A

送風機の翼を回転させると、起立翼には遠心力によって放射方向に傾ける遠心力が作用する。この遠心力に抗するために、起立翼を翼本体側に傾ける(内倒させる)形状としたり、併せて翼本体と起立翼との交差部付近の厚みを大きくして補強することが考えられる。   When the blade of the blower is rotated, a centrifugal force that is inclined in the radial direction by the centrifugal force acts on the standing blade. In order to resist this centrifugal force, it is conceivable that the upright blade is inclined (inwardly tilted) toward the blade body side, and at the same time, the thickness near the intersection of the blade body and the upright blade is increased to reinforce. .

しかし起立翼が内倒した形状の場合は、たとえ補強部分の形状を曲面としても、起立翼と翼本体とのなす角度が鋭角となるために、翼後縁部に於いて気流が翼本体から離れる際の圧力変動が急激になる傾向があるので、気流の乱れを生ずる恐れがあり、翼本体の外周縁に沿って設けた起立翼による騒音低減効果を損なう恐れがある。   However, in the case where the standing blade has an inward shape, the angle between the standing blade and the blade body is an acute angle even if the shape of the reinforcing part is curved. Since the pressure fluctuation at the time of leaving tends to be abrupt, there is a risk that the air current is disturbed, and the noise reduction effect by the standing wing provided along the outer peripheral edge of the wing body may be impaired.

本発明は、起立翼を有する送風機翼の騒音抑制効果を十分に発揮させつつ、起立翼の外倒を抑制することを目的とする。   An object of this invention is to suppress the falling of a standing blade, fully exhibiting the noise suppression effect of the fan blade which has a standing blade.

本発明の送風機用翼は、ハブと、該ハブに取り付けられる翼と、該翼の外周を取り囲む環状シュラウドとを有する送風機の該翼であって、該翼は、基端側が該ハブに取り付けられる翼本体と、該翼本体の外周縁から送風方向下流側に立設された起立翼とを有する送風機用翼において、該起立翼は、該翼本体から直立よりも放射方向に傾斜していることを特徴とするものである。   The blade for a blower of the present invention is a blade of a blower having a hub, a blade attached to the hub, and an annular shroud surrounding the outer periphery of the blade, and the proximal end side of the blade is attached to the hub. In a fan blade having a blade body and a standing blade standing on the downstream side in the blowing direction from the outer periphery of the blade body, the rising blade is inclined more radially than the upright blade from the blade body. It is characterized by.

本願発明の一態様では、前記翼本体と起立翼との交差隅角部は凹に湾曲した曲面となっている。   In one aspect of the present invention, the intersection corner between the blade body and the upright blade is a curved surface that is concavely curved.

本願発明の一態様では、前記翼本体と起立翼との交差隅角部は凹に湾曲した曲面となっており、この曲面の曲率半径は、該送風機用翼の後縁側ほど小さくなっている。   In one aspect of the present invention, the intersection corner between the blade body and the upright blade is a curved surface that is concavely curved, and the radius of curvature of the curved surface is smaller toward the trailing edge side of the fan blade.

本願発明の一態様では、この傾斜角度(起立翼と該翼本体との交差角度)は90.1°〜91°である。   In one aspect of the present invention, the inclination angle (intersection angle between the standing blade and the blade body) is 90.1 ° to 91 °.

本願発明の一態様では、前記起立翼の高さは、外周縁方向の中間部Mよりも後方側が前方側よりも大きい。   In one aspect of the present invention, the height of the upright blade is greater on the rear side than on the front side with respect to the intermediate portion M in the outer peripheral edge direction.

本願発明の送風機は、ハブと、該ハブに取り付けられた本発明の送風機用翼と、該送風機用翼を取り囲むシュラウドとを有する。   The blower of the present invention has a hub, the fan blades of the present invention attached to the hub, and a shroud surrounding the fan blades.

本願発明の送風機は、前記送風機用翼の外周縁の曲率半径は、前記シュラウド内周面の曲率半径よりも小さい。   In the blower of the present invention, the radius of curvature of the outer peripheral edge of the fan blade is smaller than the radius of curvature of the inner surface of the shroud.

本願発明の冷却塔は、その送風機として、前記送風機を有する。   The cooling tower of the present invention has the blower as the blower.

本発明の送風機用翼は、起立翼が翼本体から直立よりも放射方向に傾いている(外倒している)ことを特徴とする。この形状のために、翼を回転させたときに、翼全体が遠心力によって撓むことで翼本体長L(回転半径方向長さ)と翼本体幅B(回転周方向長さ)との比(アスペクト比L/B)が見かけ上増加し、送風機翼としての効率、即ち、翼回転後方に発生する騒音の発生原因の一つである気流の乱れ(気流の渦)の発生を抑制することが出来る。   The wing for a blower of the present invention is characterized in that the upright wing is inclined in the radial direction from the wing main body in the radial direction (outside down). Due to this shape, when the blade is rotated, the entire blade is bent by centrifugal force, so that the ratio between the blade body length L (rotation radial direction length) and the blade body width B (rotation circumferential direction length). (Aspect ratio L / B) apparently increases, suppressing the generation of airflow turbulence (airflow vortex), which is one of the causes of noise generated behind the blade rotation, that is, efficiency as a fan blade I can do it.

加えて、起立翼を外倒させたことで翼本体とのなす角度は鈍角となり、翼本体の前縁部に於いて、回転によって切り込んで行く際、起立翼と翼本体との間の渦の発生を低減する効果が期待出来る。   In addition, when the standing wing is turned over, the angle with the wing body becomes an obtuse angle, and the vortex between the standing wing and the wing body is broken when turning at the front edge of the wing body by rotation. The effect of reducing the generation can be expected.

更には、起立翼と翼本体との交差隅角部を凹に湾曲した曲面とすることで、外倒した起立翼を支える起立翼下部、即ち翼本体との取り合い部分に係る力に抗う為の補強肉盛り表面の曲率半径が、直立した起立翼と同等の補強を行った場合と比べて大きくなる。即ち、起立翼と翼本体とが、より緩やかな曲面で接続されるので、上述した渦の発生を低減する効果が、より一層期待出来る。   Furthermore, by making the intersecting corner of the standing wing and the wing body into a curved surface that is concavely curved, it is necessary to resist the force related to the lower part of the standing wing that supports the upside-down standing wing, that is, the portion that engages with the wing body. The radius of curvature of the reinforcement build-up surface is larger than when the reinforcement equivalent to that of the upright standing wing is performed. That is, since the standing blade and the blade body are connected with a more gently curved surface, the effect of reducing the above-described generation of vortices can be further expected.

また、翼本体と起立翼との交差隅角部の曲率半径を後方側程小さくすることにより、具体的には、翼本体幅Bの略中央部付近から翼後縁部にかけて、当該曲面の曲率半径が小さくなっていることで、翼後縁部から排出される気流による渦の発生を抑制することができ、騒音が小さくなることが期待される。   In addition, by reducing the radius of curvature of the intersection corner between the blade body and the upright blade toward the rear side, specifically, the curvature of the curved surface from approximately the center of the blade body width B to the trailing edge of the blade. Since the radius is small, generation of vortices due to the airflow discharged from the blade trailing edge can be suppressed, and noise is expected to be small.

翼本体と起立翼との交差隅角部の曲面における曲率半径が、翼後縁部にかけて急激に小さくなる場合、即ち曲率半径の変化量が大きいと、気流渦の発生が増加する恐れがある。また当該曲率半径の変化量を小さくする場合には、当該表面の曲率半径自体を出来るだけ小さくすることが好ましい。   If the radius of curvature of the curved surface at the intersection corner between the blade body and the upright blade decreases rapidly toward the trailing edge of the blade, that is, if the amount of change in the radius of curvature is large, the generation of airflow vortices may increase. In order to reduce the amount of change in the curvature radius, it is preferable to make the curvature radius of the surface itself as small as possible.

しかし曲率半径を小さくすると、当然に肉盛り量が減る為に起立翼下部の補強が不十分となる。これに対して本発明の送風機翼は、起立翼を外倒させることによって、翼本体に対して直立した起立翼の場合と比べて、同様の曲率半径の変化量で且つ同様の補強効果(肉盛り量)を得ようとした場合には、当該肉盛り量が増加することになるので、気流渦の発生抑制に加えて、起立翼の補強効果向上の双方が同時に期待出来る。   However, when the radius of curvature is reduced, the amount of build-up is naturally reduced, so that the reinforcement at the lower part of the standing wing becomes insufficient. On the other hand, the blower blade of the present invention has the same amount of change in the radius of curvature and the same reinforcing effect (meat) as compared with the case of the upright blade standing upright with respect to the blade body by turning the upright blade outward. In the case of trying to obtain the fill amount), the build-up amount increases, so that in addition to suppressing the generation of airflow vortices, it is possible to expect both the improvement effect of the upright blades at the same time.

実施の形態に係る送風機用翼の下流側からの斜視図である。It is a perspective view from the downstream of the blade for blowers concerning an embodiment. (a)は図1の一部拡大図、(b)は(a)に説明線を記載した斜視図である。(A) is the elements on larger scale of FIG. 1, (b) is the perspective view which described the explanatory line in (a). (a)は実施の形態に係る送風機用翼の外周縁側の平面図、(b)は(a)の一部(後縁側)の拡大図である。(A) is a top view of the outer peripheral edge side of the fan blade according to the embodiment, and (b) is an enlarged view of a part (rear edge side) of (a). 送風機用翼の起立翼の側面図(図2のIV矢視図)である。It is a side view (IV arrow line view of FIG. 2) of the standing wing | blade of the wing | blade for air blowers. 図4のV−V線に沿う断面図である。It is sectional drawing which follows the VV line of FIG. (a)は送風機用翼の平面図、(b)は(a)のB−B線及びB−B線に沿う断面図である。(A) is a plan view of a blade blower, (b) is a sectional view taken along the B 1 -B 1-wire and B 2 -B 2-wire (a). 送風機を上流側から見た平面図である。It is the top view which looked at the air blower from the upstream.

以下、図面を参照して実施の形態について説明する。   Hereinafter, embodiments will be described with reference to the drawings.

図1の通り、送風機用翼1は、翼本体2と、該翼本体2の外周縁2g(図3)側から下流側に立設された起立翼3とを有する。翼本体2の基端側のボス部4が送風機10のハブ11(図7)に取り付けられる。ハブ11に複数枚の送風機用翼1が取り付けられ、その外周を短い円筒状のシュラウド12が取り巻いている。   As shown in FIG. 1, the blower blade 1 includes a blade body 2 and upright blades 3 erected on the downstream side from the outer peripheral edge 2 g (FIG. 3) side of the blade body 2. The boss 4 on the base end side of the wing body 2 is attached to the hub 11 (FIG. 7) of the blower 10. A plurality of blower blades 1 are attached to the hub 11, and a short cylindrical shroud 12 surrounds the outer periphery thereof.

翼本体2は、図6(b)の通り、回転前後方向の断面が、B−B、B−B断面のように送風方向上流側に向って凸に湾曲している。 As shown in FIG. 6B, the blade main body 2 has a cross section in the front-rear direction of rotation that is convexly curved toward the upstream side in the air blowing direction like the B 1 -B 1 and B 2 -B 2 cross sections.

この翼本体2の前縁2aは、送風機用翼1の回転方向前方に向って凹となるように湾曲している。   The leading edge 2a of the blade body 2 is curved so as to be concave toward the front in the rotational direction of the fan blade 1.

翼本体2の後縁2bは、外周縁側を除き、回転方向後方に向って凸となるように湾曲して主後縁2cとなっており、該主後縁2cよりも外周縁側が、回転方向後方に向って凹に湾曲した翼端側後縁2dとなっている。主後縁2cと翼端側後縁2dとは点Qにおいて連続している。   The trailing edge 2b of the wing body 2 is curved so as to be convex rearward in the rotational direction except for the outer peripheral edge side, and becomes a main trailing edge 2c. The outer peripheral edge side of the main trailing edge 2c is in the rotational direction. The blade end side trailing edge 2d is curved concavely toward the rear. The main trailing edge 2c and the blade tip side trailing edge 2d are continuous at the point Q.

即ち、送風機用翼1を平面視した図6(a)の状態において、翼本体2の後縁の最ハブ側の点Uと該点Qとを結ぶ直線UQよりも主後縁2cは回転方向後方に弓形に張り出している。翼本体2の後縁の最外周縁側の点Eと該点Qとを結ぶ直線QEよりも翼端側後縁2dは回転方向前方に弓形に後退している。なお、図2(b)の通り、点Qにおける主後縁2dの接線mの延長線が翼本体2の外周縁2gと交わる点が点Pである。   That is, in the state of FIG. 6A in which the fan blade 1 is viewed in plan, the main trailing edge 2c is in the rotational direction with respect to the straight line UQ connecting the point U on the most hub side of the trailing edge of the blade body 2 and the point Q. Projected back in a bow shape. The blade end side rear edge 2d recedes in an arc shape forward in the rotational direction from a straight line QE connecting the point E on the outermost peripheral edge side of the rear edge of the blade body 2 and the point Q. 2B, the point P is the point where the extended line of the tangent m of the main trailing edge 2d at the point Q intersects the outer peripheral edge 2g of the blade body 2.

翼本体2の前縁2aは、その最ハブ側の点Tと最外周縁側の前端点Fとを結ぶ直線TFよりも回転方向後方に弓形に後退している。   The front edge 2a of the wing body 2 recedes in an arcuate shape behind the straight line TF connecting the point T on the outermost hub side and the front end point F on the outermost peripheral edge side.

尚、本発明の送風機用翼における主後縁2cは直線(図示せず)であってもよい。そしてその際の前縁2aは、直線であっても、又は送風機用翼1の回転方向前方に向って凹となるように湾曲していて(図示せず)もよい。好ましくは主後縁2cは、例えば図6の様に、回転方向後方に向って凸となるように湾曲していることが、気流の渦発生抑制の観点から好ましい。   The main trailing edge 2c in the fan blade of the present invention may be a straight line (not shown). And the front edge 2a in that case may be a straight line, or may be curving so that it may become concave toward the rotation direction front of the fan blade 1 (not shown). Preferably, the main trailing edge 2c is curved, for example, as shown in FIG. 6, so as to protrude rearward in the rotational direction, from the viewpoint of suppressing the vortex generation of the airflow.

起立翼3は、翼本体2から直立よりもわずかに放射方向に傾斜している。図5の通り、翼本体2の外周縁近傍と起立翼3との交差角度δは90.1°〜91°特に90.3°〜90.7°であることが好ましい。   The upright wing 3 is slightly inclined in the radial direction from the wing body 2 rather than upright. As shown in FIG. 5, the crossing angle δ between the vicinity of the outer peripheral edge of the blade body 2 and the upright blade 3 is preferably 90.1 ° to 91 °, particularly 90.3 ° to 90.7 °.

起立翼3は、翼本体2の前端点Fから若干離隔した点3fから起立開始することで、翼が回転することにより生ずる抵抗値を下げ、加えて気流の乱れを抑えることが期待できるので好ましい。そして起立翼は、後方に向って徐々に起立高さが大きくなる。送風機用翼1の外周縁の前後方向中間点Mにおいて起立翼3の高さh(図2(b))はほぼ最高となり、中間点Mよりも後方において起立翼3の高さは略一定である。この中間点Mにおける起立翼3の高さhは、ハブ中心(回転中心)Cからの翼1の全長L(図6参照)の4%超であり、その上限は好ましくはLの9%未満、より好ましくは5〜8%未満、特に好ましくは6〜8%未満である。   The upright blade 3 is preferable because it can be expected to start rising from a point 3f slightly separated from the front end point F of the blade body 2 to reduce the resistance value caused by the rotation of the blade and to suppress the turbulence of the airflow. . The rising height of the standing wing gradually increases toward the rear. The height h (FIG. 2 (b)) of the upright blade 3 is substantially the highest at the front-rear direction intermediate point M of the outer peripheral edge of the blower blade 1, and the height of the upright blade 3 is substantially constant behind the intermediate point M. is there. The height h of the upright blade 3 at the intermediate point M is more than 4% of the total length L (see FIG. 6) of the blade 1 from the hub center (rotation center) C, and the upper limit is preferably less than 9% of L. , More preferably less than 5-8%, particularly preferably less than 6-8%.

起立翼3の最前端の点3f(図3)と翼1の前端点Fとの離隔距離は、送風機用翼1の外周縁の全長(点EF間の距離)の8%以下、特に3〜6%が好ましい。ただし、起立翼3の最前端は、点Fであってもよい。   The separation distance between the front end point 3f (FIG. 3) of the upright blade 3 and the front end point F of the blade 1 is 8% or less of the total length (distance between points EF) of the outer peripheral edge of the fan blade 1, particularly 3 to 3. 6% is preferred. However, the front end of the upright wing 3 may be a point F.

起立翼3と翼本体2との交差隅角部の内周面5aは、図5の通り凹に湾曲している。この内周面5aの曲率半径Rは、外周面5bの曲率半径よりも大きいものとなっている。この様な構成とすることによって、翼端部の強度が向上するので好ましい。また、この実施の形態では、この内周面5aの曲率半径Rは、翼本体2の後方側ほど小さくなるように構成されている。従って、交差隅角部の肉厚tは、翼本体2の後方側ほど小さくなっている。なお、この曲率半径Rは、中間点M付近では20mm以上、例えば20〜40mm特に25〜35mmであることが好ましい。中間点Mよりも前縁側では、曲率半径はほぼ同じであるが、先端部近傍において徐々に先端に向かって曲率半径は小さくなっている。尚、この曲率半径の暫減の程度は、後縁側におけるそれと比較して穏やかである。中間点Mよりも後縁側では、曲率半径はこれよりも次第に小さくなっている。最後縁の点E付近では、この曲率半径Rは10mm以下、例えば1〜10mm特に5〜8mm程度であることが好ましい。   The inner peripheral surface 5a at the crossing corner of the upright blade 3 and the blade body 2 is concavely curved as shown in FIG. The curvature radius R of the inner peripheral surface 5a is larger than the curvature radius of the outer peripheral surface 5b. Such a configuration is preferable because the strength of the blade tip is improved. Further, in this embodiment, the radius of curvature R of the inner peripheral surface 5a is configured to become smaller toward the rear side of the blade body 2. Therefore, the wall thickness t of the intersection corner is smaller toward the rear side of the blade body 2. In addition, it is preferable that this curvature radius R is 20 mm or more in the vicinity of the intermediate point M, for example, 20-40 mm, especially 25-35 mm. The curvature radius is substantially the same on the leading edge side from the intermediate point M, but the curvature radius gradually decreases toward the tip in the vicinity of the tip. Note that the degree of temporary decrease in the radius of curvature is gentle compared to that on the trailing edge side. On the trailing edge side from the intermediate point M, the radius of curvature gradually becomes smaller. In the vicinity of the point E at the last edge, the radius of curvature R is preferably 10 mm or less, for example, about 1 to 10 mm, particularly about 5 to 8 mm.

起立翼3は、前記点Qにおける接線mと翼本体2の外周縁2gとの交点Pよりも後方に延在している。この実施の形態では、起立翼3は、翼本体2の外周縁2gと、後縁2b(翼端側後縁2d)との交点Eにまで達している。この様な構成とすることによって、起立翼の後方延在部の補強を行い、且つ気流の乱れを抑制することが期待できるので好ましい。   The upright blade 3 extends rearward from the intersection P between the tangent m at the point Q and the outer peripheral edge 2 g of the blade body 2. In this embodiment, the upright blade 3 reaches the intersection E between the outer peripheral edge 2g of the blade body 2 and the trailing edge 2b (wing tip side trailing edge 2d). Such a configuration is preferable because it can be expected to reinforce the rearward extending portion of the upright blade and suppress the turbulence of the airflow.

起立翼3の最後部における上辺3aと後辺3bとの交差角度θは、略直角(具体的にはθ=85°〜95°特に88°〜92°)となっている。   The crossing angle θ between the upper side 3a and the rear side 3b at the rearmost part of the upright blade 3 is substantially a right angle (specifically, θ = 85 ° to 95 °, particularly 88 ° to 92 °).

以下の説明では、点Pよりも後方側における起立翼3の側面の面積をエンド面積Sと称し、点Pよりも後側の起立翼3の長さを出代長さDと称することがある。また、翼本体2のうち前記接線mよりも後方側、すなわち翼端側後縁2d側を張出部Wと称することがある。この張出部Wを含む翼本体2は、翼端部においてその厚みが、翼本体外周縁に向かって増している。具体的には接続点Qを通る、翼回転前後方向の線(図6(b)におけるB1−B1又はB2−B2の線分と平行な線分)から翼外周縁に向かって、張出部Wを含む翼本体2の厚みは徐々に大きくなっている。   In the following description, the area of the side surface of the upright wing 3 on the rear side of the point P may be referred to as an end area S, and the length of the upright wing 3 on the rear side of the point P may be referred to as an allowance length D. . Further, the rear side of the blade body 2 from the tangent line m, that is, the blade end side rear edge 2d side, may be referred to as a protruding portion W. The blade body 2 including the overhang portion W has a thickness increasing toward the outer peripheral edge of the blade body at the blade tip. Specifically, the projecting portion extends from the line in the front-rear direction of the blade rotation passing through the connection point Q (a line segment parallel to the line segment B1-B1 or B2-B2 in FIG. 6B) toward the outer periphery of the blade. The thickness of the wing body 2 including W is gradually increased.

なお、本発明では、接線mと翼端側後縁2dとが合致してもよい。即ち、張出部Wの面積=0(ゼロ)であってもよい。この場合、起立翼3は点Pよりも後側に延在している。   In the present invention, the tangent m and the wing tip side trailing edge 2d may coincide. That is, the area of the overhanging portion W may be 0 (zero). In this case, the upright blade 3 extends rearward from the point P.

この送風機用翼1、ハブ11及びシュラウド12を有する送風機10は、モータ(図示略)によって送風機用翼1が図7の時計回り方向に回転駆動され、空気が送風される。翼1のピッチ角α(回転軸を鉛直とした場合、直線EFと水平面との交角)は5〜30°程度が好ましい。   In the blower 10 having the blower blade 1, the hub 11, and the shroud 12, the blower blade 1 is rotationally driven in a clockwise direction in FIG. 7 by a motor (not shown), and air is blown. The pitch angle α of the blade 1 (intersection angle between the straight line EF and the horizontal plane when the rotation axis is vertical) is preferably about 5 to 30 °.

この送風機用翼1及び送風機10の作用効果は次の通りである。この送風機10は、送風機用翼1に起立翼3が設けられており、起立翼を設けていない場合と比べて、送風時の騒音が小さい。特に、この実施の形態では、起立翼3の高さhが適切であると共に、起立翼3が後方に長く延在しており、騒音低減効果が良好である。また、起立翼3の前端点3fを点Fから所定距離後退させており、翼本体2の外周縁前縁付近における渦の抑制効果が得られ、これによっても騒音が減少する。   The effects of the fan blade 1 and the fan 10 are as follows. In the blower 10, the rising blade 3 is provided on the blower blade 1, and noise during blowing is small as compared with the case where the rising blade is not provided. In particular, in this embodiment, the height h of the upright blade 3 is appropriate, and the upright blade 3 extends long rearward, so that the noise reduction effect is good. Further, the front end point 3f of the upright blade 3 is retracted by a predetermined distance from the point F, and the effect of suppressing the vortex in the vicinity of the front edge of the outer peripheral edge of the blade body 2 is obtained, which also reduces the noise.

本発明では、起立翼3を放射方向に傾けているので、翼全体が遠心力によって撓むことで翼本体長L(回転半径方向長さ)と翼本体幅B(回転周方向長さ)との比(アスペクト比L/B)が見かけ上増加し、送風機翼としての効率、即ち、翼回転後方に発生する騒音の発生原因の一つである気流の乱れ(気流の渦)の発生を抑制することが出来る。   In the present invention, since the upright blade 3 is inclined in the radial direction, the blade main body length L (rotational radial length) and the blade main body width B (rotational circumferential length) are obtained by bending the entire blade by centrifugal force. Ratio (aspect ratio L / B) is apparently increased, suppressing the generation of airflow turbulence (airflow vortex), which is one of the causes of noise generated behind the blade rotation, that is, efficiency as a fan blade I can do it.

この実施の形態では、点E付近において翼本体2の厚みを大きくしている。具体的には接続点Qを通る、翼回転前後方向の線(図6(b)におけるB1−B1又はB2−B2の線分と平行な線分)から翼外周縁に向かって、張出部Wを含む翼本体2の厚みは徐々に大きくなっているので、該点E付近における送風機用翼1の強度及び剛性が高いが、これによる重量増加はきわめて少ない。また、この実施の形態では、翼本体2と起立翼3との交差内周面の曲率半径R(図5)を後縁2b側ほど小さくしている。これにより、起立翼3の後部側における渦の発生を抑制する効果が得られる。   In this embodiment, the thickness of the blade body 2 is increased in the vicinity of the point E. Specifically, the projecting portion extends from the line in the front-rear direction of the blade rotation passing through the connection point Q (a line segment parallel to the line segment B1-B1 or B2-B2 in FIG. 6B) toward the outer periphery of the blade. Since the thickness of the blade main body 2 including W is gradually increased, the strength and rigidity of the fan blade 1 near the point E is high, but the weight increase due to this is very small. In this embodiment, the radius of curvature R (FIG. 5) of the inner circumferential surface of the blade body 2 and the upright blade 3 is made smaller toward the trailing edge 2b side. Thereby, the effect which suppresses generation | occurrence | production of the vortex in the rear part side of the standing blade 3 is acquired.

なお、図6の通り、この実施の形態では、翼本体2の外周縁2gは、翼本体2の回転の直径方向外方に向って凸となるように湾曲している。外周縁2gの曲率半径は、シュラウド12の内周面の曲率半径よりも小さいものとなっている。   As shown in FIG. 6, in this embodiment, the outer peripheral edge 2 g of the wing body 2 is curved so as to protrude outward in the diameter direction of the rotation of the wing body 2. The radius of curvature of the outer peripheral edge 2g is smaller than the radius of curvature of the inner peripheral surface of the shroud 12.

上記の通り、起立翼3の高さhが大きい起立翼3の後縁は、送風機用翼1の回転時に遠心力によって外方(放射方向)に倒れるように変形する。翼本体2の外周縁2gの曲率半径をシュラウド12の内周面の曲率半径よりも小さく設定しておくことにより、この実施の形態による起立翼3の傾倒が抑制される効果と相俟って、起立翼3とシュラウド12の内周面との接触が防止効果が向上する。   As described above, the trailing edge of the upright blade 3 having the large height h of the upright blade 3 is deformed so as to fall outward (radially) by centrifugal force when the fan blade 1 rotates. Combined with the effect of suppressing the tilt of the upright blade 3 according to this embodiment by setting the radius of curvature of the outer peripheral edge 2g of the blade body 2 smaller than the radius of curvature of the inner peripheral surface of the shroud 12. Further, the effect of preventing contact between the upright blade 3 and the inner peripheral surface of the shroud 12 is improved.

本発明の送風機翼の用途に制限は無く、冷却塔用送風機翼、CPU冷却ファンや自動車のラジエター冷却フィン、換気扇、扇風機(ケーシングが有るタイプ)等が挙げられる。中でも騒音低減効果が著しい冷却塔用送風機翼が好ましい。   There is no restriction | limiting in the use of the fan blade | wing of this invention, The fan blade | wing for cooling towers, a CPU cooling fan, the radiator cooling fin of a motor vehicle, a ventilation fan, a fan (type with a casing) etc. are mentioned. Among these, cooling tower fan blades that have a remarkable noise reduction effect are preferred.

送風機用翼の素材や成型方法に制限は無いが、大型・高強度・軽量等の要請から送風機用翼はFRP製が好ましい。   Although there is no restriction | limiting in the raw material and shaping | molding method of a wing | blade for air blowers, From the request | requirement of large sized, high intensity | strength, lightweight, etc., the wing | blade for air blowers is preferable from FRP.

送風機用翼の製造方法も任意であるが、一般的に冷却器塔の送風機などには大型であることから、CF(カーボンファイバー)やGF(ガラスファイバー)を含む繊維強化熱硬化性樹脂組成物シートを型内に設置し型押しするシートモールディング(SMC)が好ましい。   The method for manufacturing the blades for the blower is optional, but since the fan for the cooler tower is generally large, a fiber reinforced thermosetting resin composition containing CF (carbon fiber) or GF (glass fiber). Sheet molding (SMC) in which a sheet is placed in a mold and embossed is preferable.

SMC製法においては起立翼3端部にまで溶融した樹脂組成物が流れ込む様に、起立翼3端部が下方向となる様に成形金型を設置して製造することが好ましい。   In the SMC manufacturing method, it is preferable to manufacture by installing a molding die so that the end portion of the upright blade 3 is directed downward so that the molten resin composition flows to the end portion of the upright blade 3.

SMC成形時において、繊維強化熱硬化性樹脂組成物シートの組成比や設置方法を適宜選択し、起立翼3の端部へ流入する熱硬化性樹脂組成物において、CFやGF等の繊維状物質の含有量を調整し、起立翼3の端部の繊維量を調整し、強度や重量を調整してもよい。   At the time of SMC molding, the composition ratio and installation method of the fiber reinforced thermosetting resin composition sheet are appropriately selected, and in the thermosetting resin composition flowing into the end of the upright blade 3, a fibrous substance such as CF or GF May be adjusted, the fiber amount at the end of the upright blade 3 may be adjusted, and the strength and weight may be adjusted.

好ましくは、起立翼3における熱硬化性樹脂組成物中の繊維状物質含有量は、翼本体2のそれと比して少なくし、相対的に重量を減じる(即ち翼端部の重量増加を抑える)ことが好ましい。これは、翼回転時に於いて翼端部の重量が軽いほど、回転による翼本体の変形(撓み)を抑制でき、シュラウド12と起立翼3との間隙調整が容易となり、安全に回転させることができるためである。   Preferably, the fibrous substance content in the thermosetting resin composition in the upright blade 3 is less than that of the blade body 2 and relatively reduces the weight (ie, suppresses the increase in the weight of the blade tip). It is preferable. This is because, as the weight of the blade tip is lighter during blade rotation, the blade body can be prevented from being deformed (deflection) by rotation, the clearance between the shroud 12 and the upright blade 3 can be easily adjusted, and can be rotated safely. This is because it can.

なお、この送風機用翼1を成形金型から脱型する場合、起立翼3を翼本体2に対し放射方向に傾斜させてあるので、脱型が容易である。   Note that, when the blower blade 1 is removed from the molding die, the upright blade 3 is inclined in the radial direction with respect to the blade body 2, so that the removal is easy.

1 送風機用翼
2 翼本体
2c 主後縁
2d 翼端側後縁
3 起立翼
10 送風機
11 ハブ
12 シュラウド
DESCRIPTION OF SYMBOLS 1 Fan blade 2 Blade body 2c Main trailing edge 2d Blade tip side trailing edge 3 Standing blade 10 Blower 11 Hub 12 Shroud

Claims (8)

ハブと、該ハブに取り付けられる翼と、該翼の外周を取り囲む環状シュラウドとを有する送風機の該翼であって、
該翼は、基端側が該ハブに取り付けられる翼本体と、該翼本体の外周縁から送風方向下流側に立設された起立翼とを有する送風機用翼において、
該起立翼は、該翼本体から直立よりも放射方向に傾斜していることを特徴とする送風機用翼。
The wing of a blower having a hub, a wing attached to the hub, and an annular shroud surrounding the outer periphery of the wing,
The blade is a blade for a blower having a blade body whose base end side is attached to the hub, and a standing blade erected on the downstream side in the blowing direction from the outer periphery of the blade body.
The fan blades characterized in that the upright blades are inclined in a radial direction from the blade main body in an upright direction.
請求項1において、前記翼本体と起立翼との交差隅角部は凹に湾曲した曲面となっていることを特徴とする送風機用翼。   2. The fan blade according to claim 1, wherein an intersection corner portion between the blade body and the upright blade is a curved surface that is concavely curved. 請求項2において、前記翼本体と起立翼との交差隅角部が凹に湾曲した曲面であり、この曲面の曲率半径は、該送風機用翼の後縁側ほど小さくなっていることを特徴とする送風機用翼。   In Claim 2, the intersection corner of the blade body and the upright blade is a curved surface that is concavely curved, and the curvature radius of the curved surface is smaller toward the trailing edge side of the fan blade. Blower for blower. 請求項1ないし3のいずれか1項において、前記起立翼と翼本体との交差角度が90.1°〜91°であることを特徴とする送風機用翼。   4. The fan blade according to claim 1, wherein an angle of intersection between the upright blade and the blade body is 90.1 ° to 91 °. 請求項1ないし4のいずれか1項において、前記起立翼の高さは、外周縁方向の中間部Mよりも後方側が前方側よりも大きいことを特徴とする送風機用翼。   5. The fan blade according to claim 1, wherein a height of the upright blade is greater on the rear side than the front side of the intermediate portion M in the outer peripheral edge direction. ハブと、該ハブに取り付けられた請求項1ないし5のいずれか1項に記載の送風機用翼と、該送風機用翼を取り囲むシュラウドとを有する送風機。   A blower comprising: a hub; the fan blade according to any one of claims 1 to 5 attached to the hub; and a shroud surrounding the fan blade. 請求項6において、前記送風機用翼の外周縁の曲率半径は、前記シュラウド内周面の曲率半径よりも小さいことを特徴とする送風機。   The blower according to claim 6, wherein a radius of curvature of an outer peripheral edge of the blade for a blower is smaller than a radius of curvature of an inner peripheral surface of the shroud. 請求項6又は7に記載の送風機を有する冷却塔。   A cooling tower having the blower according to claim 6.
JP2015253678A 2015-12-25 2015-12-25 Blade for blower, and blower Pending JP2017115769A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2015253678A JP2017115769A (en) 2015-12-25 2015-12-25 Blade for blower, and blower

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2015253678A JP2017115769A (en) 2015-12-25 2015-12-25 Blade for blower, and blower

Publications (1)

Publication Number Publication Date
JP2017115769A true JP2017115769A (en) 2017-06-29

Family

ID=59233564

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015253678A Pending JP2017115769A (en) 2015-12-25 2015-12-25 Blade for blower, and blower

Country Status (1)

Country Link
JP (1) JP2017115769A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2021513029A (en) * 2018-02-12 2021-05-20 エドワーズ リミテッド Enhanced vacuum system components

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5425509A (en) * 1977-07-28 1979-02-26 Sumitomo Precision Prod Co Lower noise fan
JPS5627398U (en) * 1979-08-10 1981-03-13
JPS5822497U (en) * 1981-08-07 1983-02-12 三菱重工業株式会社 Air conditioner propeller fan
JPS59185898A (en) * 1983-04-08 1984-10-22 Aisin Seiki Co Ltd Fan blade
JP2013096307A (en) * 2011-11-01 2013-05-20 Mitsubishi Plastics Inc Blower, blower unit, and cooling tower

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5425509A (en) * 1977-07-28 1979-02-26 Sumitomo Precision Prod Co Lower noise fan
JPS5627398U (en) * 1979-08-10 1981-03-13
JPS5822497U (en) * 1981-08-07 1983-02-12 三菱重工業株式会社 Air conditioner propeller fan
JPS59185898A (en) * 1983-04-08 1984-10-22 Aisin Seiki Co Ltd Fan blade
JP2013096307A (en) * 2011-11-01 2013-05-20 Mitsubishi Plastics Inc Blower, blower unit, and cooling tower

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2021513029A (en) * 2018-02-12 2021-05-20 エドワーズ リミテッド Enhanced vacuum system components
JP7618906B2 (en) 2018-02-12 2025-01-22 エドワーズ リミテッド Enhanced Vacuum System Components

Similar Documents

Publication Publication Date Title
JP7092433B2 (en) Forward / reverse rotation fan
JP7140911B2 (en) forward and reverse fan
AU2006270875B2 (en) Axial flow fan
JP6493682B2 (en) Centrifugal fan
US9394911B2 (en) Axial flow fan
CN106460868A (en) Axial fan and air conditioner having the same
JP4867950B2 (en) Blower
KR20090014308A (en) Axial fan assembly
JP6914371B2 (en) Axial blower
JP5425192B2 (en) Propeller fan
WO2010047242A1 (en) Molding machine for following-through fan, blower and blade wheel
JP6373439B1 (en) Axial fan
CA2572925C (en) Axial fan blade having a convex leading edge
JP6604981B2 (en) Axial blower impeller and axial blower
JP6066691B2 (en) Propeller fan and air conditioner using the propeller fan
CN104791301B (en) One kind is curved to plunder aluminium alloy axial blade
JP2017115769A (en) Blade for blower, and blower
JP5041446B2 (en) Cross-flow fan, blower and impeller molding machine
JP2008232049A (en) Centrifugal impeller and centrifugal blower
JP2017115768A (en) Blade for blower, and blower
CN108506246B (en) Axial flow wind wheel, air conditioner outdoor unit and air conditioner
JP4839901B2 (en) Jet fan
JP5114845B2 (en) Blower impeller
JP7217176B2 (en) Blade structure of centrifugal blower
CN108138787B (en) Impeller and axial flow fan including the impeller

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20181121

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20190816

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20190827

A02 Decision of refusal

Free format text: JAPANESE INTERMEDIATE CODE: A02

Effective date: 20200303