JPH0545837Y2 - - Google Patents

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Publication number
JPH0545837Y2
JPH0545837Y2 JP901389U JP901389U JPH0545837Y2 JP H0545837 Y2 JPH0545837 Y2 JP H0545837Y2 JP 901389 U JP901389 U JP 901389U JP 901389 U JP901389 U JP 901389U JP H0545837 Y2 JPH0545837 Y2 JP H0545837Y2
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JP
Japan
Prior art keywords
wing
fan
boss
section
edge
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.)
Expired - Lifetime
Application number
JP901389U
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Japanese (ja)
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JPH0299296U (en
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Priority to JP901389U priority Critical patent/JPH0545837Y2/ja
Publication of JPH0299296U publication Critical patent/JPH0299296U/ja
Application granted granted Critical
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Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Description

【考案の詳細な説明】 〔産業上の利用分野〕 本考案は特に自動車用ラジエータのフアンであ
つて、ラジエータの通風抵抗が大なるものに適用
されるものである。
[Detailed Description of the Invention] [Industrial Field of Application] The present invention is particularly applicable to radiator fans for automobiles, where the ventilation resistance of the radiator is large.

〔従来技術〕[Prior art]

自動車のエンジンルーム内は各種機器が内装さ
れるため、ラジエータの通風性が悪くなつてい
る。しかも、ラジエータはエンジン冷却用のもの
と、インタークーラ用のものと、室内空調用のも
のとが夫々互いに重ね合わされるように設置され
る場合が多い。すると、それら全体の通風抵抗が
ますます悪くなる傾向にある。そのため従来の軸
流フアンでは十分ラジエータを冷却できない場合
がある。
Since various devices are housed in the engine room of an automobile, the ventilation of the radiator is poor. Furthermore, radiators are often installed such that one for engine cooling, one for intercooler, and one for indoor air conditioning are stacked on top of each other. As a result, the overall ventilation resistance tends to become worse. Therefore, conventional axial fans may not be able to sufficiently cool the radiator.

〔課題を解決するための手段〕[Means to solve the problem]

そこで本考案者は各種実験の結果、上記問題点
を解決するフアンを案出した。その構成は次のと
おりである。
As a result of various experiments, the present inventor devised a fan that solves the above problems. Its composition is as follows.

即ち、圧力係数Ψ=0.25〜0.35で且つ、ボス部
1が円錐台形状をなし、該ボス部1外周に複数の
翼部2が等間隔に配置され、該翼部の半径方向先
端縁が前記ボス部1の軸線に平行に形成されたフ
アンにおいて、前記ボス部1の外周面と前記軸線
とのなす角θをθ=27.5°〜35.5°とし、前記翼部
2の後縁における先端の半径Rpとその根元の半
径R2との関係をR2/Rb=0.45〜0.55とし、前記翼
部2の後縁の根元で前記ボス部1外面に直交する
仮想線lが該翼部2に投影されたとき、該仮想線
lと該翼部2の前記先端縁との交点と、該翼部2
の前記後端縁との距離Dが翼幅Tに対してD/T
=0.65〜1.0の関係にあり且つ、前記翼部2の前
記先端縁に近接して該先端縁の後端部が露出する
ようにシユラウドの筒状部3が軸方向長さSだけ
被嵌され、その被嵌割合がS/T=0.5〜0.7であ
ることを特徴とするラジエータのフアンである。
That is, the pressure coefficient Ψ=0.25 to 0.35, the boss part 1 has a truncated cone shape, a plurality of wing parts 2 are arranged at equal intervals on the outer periphery of the boss part 1, and the radial tip edge of the wing part is In a fan formed parallel to the axis of the boss part 1, the angle θ between the outer peripheral surface of the boss part 1 and the axis is θ=27.5° to 35.5°, and the radius of the tip at the trailing edge of the wing part 2 is The relationship between R p and the radius R 2 of its root is set as R 2 /R b =0.45 to 0.55, and the imaginary line l perpendicular to the outer surface of the boss 1 at the root of the trailing edge of the wing 2 , the intersection of the imaginary line l and the tip edge of the wing section 2
The distance D to the trailing edge of the wing is D/T with respect to the wingspan T
= 0.65 to 1.0, and the cylindrical portion 3 of the shroud is fitted by an axial length S so that the rear end portion of the tip edge of the wing portion 2 is exposed close to the tip edge. This is a radiator fan characterized in that the fitting ratio thereof is S/T=0.5 to 0.7.

〔実施例〕〔Example〕

次に図面に基づいて本考案の実施例につき説明
する。
Next, embodiments of the present invention will be described based on the drawings.

第1図は本ラジエータフアンの使用状態を示す
軸断面略図であり、第2図はその要部を示し、第
3図は同フアンの正面図である。
FIG. 1 is a schematic axial cross-sectional view showing the state in which the present radiator fan is used, FIG. 2 shows its main parts, and FIG. 3 is a front view of the same fan.

このラジエータのフアンはボス部1が円錐台形
状に形成されると共に、その外周面に等間隔に翼
部2が配設されている。そしてボス部1の中心部
は大きく開口し、その内周縁に環状の取付け面7
がボス部1に一体的に固定されている。このフア
ンは合成樹脂の成形体からなり、その成形が容易
なように各翼部2,2間は互いに僅かずつ〓間が
あけられている。又、翼部2の付け根部はボス部
1の軸線に対して所定角度傾斜して取付けられる
と共に、翼部2自体が付け根部からその先端縁に
行くに従つて、わずか捩じれた形状になつてい
る。これらの捩じれ角は従来の軸流フアンのそれ
に比べて小さい。なお、翼部2の前端縁12は第
1図及び第2図に示す如くボス部1の前端よりも
僅かに後方から立ち上げられ、それによりラジエ
ータ4を通過した空気流が円滑に後方へ導かれる
ようになつている。次に翼部2の先端縁11は軸
線に対して平行に形成されると共に、後端縁13
はボス部1後端と一致している。なお、ボス部1
の軸線に対する傾斜角度θは27.5°〜35.5°とする
のが好ましい。27.5°よりも小さいと、ラジエー
タ4の背面側に大きな負圧を生じさせることがで
きない。又、36°以上であるとフアンの抵抗が大
きくなりすぎ、動力に対する効率が悪くなり、結
果としてラジエータ4を通過する風量が小さくな
る欠点があることを実験により確認した。次に、
翼部2の後端縁13における先端半径Rpとその
前後縁の中央の根元における半径Rbとの比は0.45
〜0.55程度が好ましい。この値が0.55超えるとフ
アンの出口側における風抜けの断面積が小さくな
りすぎ、通風性を害し結果としてラジエータ4の
通過風量を減少させるものとなる。又、0.45以下
となると、ボス部が余りにも小さくなり、必要と
するフアンクラツチの装着が無理になる欠点があ
る。それと共に、ラジエータ4背面側の負圧を十
分に大きくすることができない。
In this radiator fan, a boss portion 1 is formed in a truncated conical shape, and blade portions 2 are arranged at equal intervals on the outer peripheral surface of the boss portion 1. The central part of the boss part 1 has a large opening, and an annular mounting surface 7 is formed on the inner peripheral edge of the central part.
is integrally fixed to the boss portion 1. This fan is made of a synthetic resin molded body, and the wings 2 are spaced slightly apart from each other to facilitate molding. In addition, the base of the wing section 2 is attached at a predetermined angle with respect to the axis of the boss section 1, and the wing section 2 itself has a slightly twisted shape as it goes from the base to its tip edge. There is. These torsional angles are small compared to those of conventional axial fans. The front edge 12 of the wing section 2 is raised slightly from the rear of the front end of the boss section 1, as shown in FIGS. 1 and 2, so that the airflow that has passed through the radiator 4 is smoothly guided rearward. It's starting to get worse. Next, the leading edge 11 of the wing portion 2 is formed parallel to the axis, and the trailing edge 13
coincides with the rear end of the boss portion 1. In addition, boss part 1
The inclination angle θ with respect to the axis is preferably 27.5° to 35.5°. If it is smaller than 27.5°, it is not possible to generate a large negative pressure on the back side of the radiator 4. Furthermore, it has been confirmed through experiments that if the angle is 36 degrees or more, the resistance of the fan becomes too large, resulting in poor efficiency with respect to the power, and as a result, the amount of air passing through the radiator 4 becomes small. next,
The ratio of the tip radius R p at the trailing edge 13 of the wing section 2 to the radius R b at the center root of its front and rear edges is 0.45
~0.55 is preferable. If this value exceeds 0.55, the cross-sectional area of the air outlet on the exit side of the fan becomes too small, which impairs ventilation and results in a decrease in the amount of air passing through the radiator 4. Moreover, if it is less than 0.45, the boss portion will become too small, making it difficult to attach the required fan clutch. At the same time, the negative pressure on the back side of the radiator 4 cannot be made sufficiently large.

次に、翼部2の奥行き比を表すD/T即ち、翼
部2の後縁の根元でボス部1外面に直交する仮想
線lが翼部2に投影されたとき、その仮想線lと
翼部2の先端縁との交点(第2図)と、翼部2の
後端縁との距離Dが翼幅Tに対しての比D/Tは
0.65〜1.0が最も好ましい。これは、その値が1.0
以上であると翼部2の幅が狭すぎ翼部2背面側の
負圧が十分得られないからである。それと共に、
その値が0.65以下であると、翼部2の翼幅が大き
すぎ、効率が極端に悪くなると共に、フアン全体
の厚みが大きくなりその小型化を阻害することに
なるからである。
Next, D/T representing the depth ratio of the wing section 2, that is, when an imaginary line l perpendicular to the outer surface of the boss section 1 at the root of the trailing edge of the wing section 2 is projected onto the wing section 2, the imaginary line l and The ratio D/T of the distance D between the intersection with the leading edge of the wing section 2 (Fig. 2) and the trailing edge of the wing section 2 to the wing span T is
0.65-1.0 is most preferred. This means that its value is 1.0
This is because the width of the wing portion 2 is too narrow and sufficient negative pressure on the back side of the wing portion 2 cannot be obtained. Along with that,
If the value is less than 0.65, the blade span of the wing section 2 will be too large, resulting in extremely low efficiency, and the thickness of the fan as a whole will become large, impeding its miniaturization.

次に、翼部2の先端縁11に対向して筒状の筒
状部3が被嵌される。なお、この筒状部3は環状
ゴム板6を介してシユラウド本体14に連結さ
れ、シユラウド本体14の開口端はタンク5に固
定される。又、筒状部3はステー10を介してエ
ンジン9に固定される。なお、ボス部1はその取
付け面7にクラツチ8のフランジ部が固定され
る。そしてクラツチ8の駆動側軸部がエンジン9
のクランクシヤフトに歯車等を介して連結され
る。
Next, the cylindrical portion 3 is fitted opposite the tip edge 11 of the wing portion 2 . The cylindrical portion 3 is connected to a shroud body 14 via an annular rubber plate 6, and the open end of the shroud body 14 is fixed to the tank 5. Further, the cylindrical portion 3 is fixed to the engine 9 via a stay 10. Incidentally, the flange portion of the clutch 8 is fixed to the mounting surface 7 of the boss portion 1. The drive side shaft of the clutch 8 is connected to the engine 9.
It is connected to the crankshaft of the motor through gears, etc.

この実施例で、シユラウドの筒状部3は翼部2
の中間部及び前端部のみを被嵌し、その後端部が
露出するように形成した。これは、フアンの出口
面積を十分確保し、通風量を増大させるためであ
り、S/Tを0.7以下とした。なお、S/Tは0.5
〜0.7の範囲に設定した。ここで、その値を0.5以
下としたのは筒状部3が余りにも短いと翼端部に
おける逆流が生じ結果として通風量が減少すると
共に、ラジエータ4背面側に大きな負圧を生じさ
せることができないからである。次に、このフア
ンは圧力係数Ψが0.25〜0.35の範囲で働く高静圧
フアンである。そして、このような高静圧フアン
であつて、なお且つ前記各フアンの諸元を有する
ことにより風量を多くし、熱交換性能を向上させ
るように形成している。この圧力係数Ψと流量係
数Φとの関係を示したのが第4図である。ここに
おいて各曲線A,B,Cは夫々本考案のフアンの
各実施例であり、そのボス部の軸線に対する角θ
は30°であり、Rb/Rpが夫々0.50,0.47,0.51であ
ると共に、D/Tが夫々0.87,0.76,1.07で且つ
S/Tが夫々0.5,0.5,0.5であつて夫々の外半径
Rpは335mm、240mm、212.5mmである。又、夫々の
翼部2の数は夫々10枚、10枚、12枚である。第4
図において曲線A,B,CはΦを横軸とした夫々
のフアンの圧力係数曲線であり、A′,B′,C′は
夫々の各フアンに適用されるラジエータの圧力係
数曲線である。従つて、夫々の曲線の交点が各実
施例の作動点となる。又曲線Dは従来の軸流フア
ンの圧力係数特性を示す。次に第4図において横
軸にΦを取り、縦軸にη(効率)を取つた夫々の
フアンの曲線がA1,B1,C1である。そして前記
の各作動点は夫々効率曲線のほぼ最大値付近に位
置する。このことから夫々の実施例はいずれも効
率が良く、高静圧で風量の大きなフアンであるこ
とが判る。第4図はボス部の角θを30°に固定し
て実験を行つたが、それ以外の数値の角度でもほ
ぼ同様の結果が得られた。又、本考案の範囲で他
の諸元においても同様であつた。なお、圧力係数
Ψ及び流量係数Φは次の式で表されるものであ
る。
In this embodiment, the cylindrical part 3 of the shroud is connected to the wing part 2.
It was formed so that only the middle part and the front end of the holder were fitted, and the rear end was exposed. This is to ensure a sufficient exit area of the fan and increase the amount of ventilation, and the S/T was set to 0.7 or less. In addition, S/T is 0.5
It was set in the range of ~0.7. Here, the value was set to 0.5 or less because if the cylindrical part 3 is too short, backflow will occur at the blade tip, resulting in a decrease in ventilation volume and a large negative pressure on the back side of the radiator 4. Because you can't. Next, this fan is a high static pressure fan that operates with a pressure coefficient Ψ in the range of 0.25 to 0.35. This high static pressure fan is designed to have the specifications of each of the fans described above, thereby increasing the air volume and improving the heat exchange performance. FIG. 4 shows the relationship between the pressure coefficient Ψ and the flow rate coefficient Φ. Here, the curves A, B, and C represent respective embodiments of the fan of the present invention, and the angle θ with respect to the axis of the boss portion thereof is
is 30°, R b /R p are 0.50, 0.47, and 0.51, respectively, D/T is 0.87, 0.76, and 1.07, and S/T is 0.5, 0.5, and 0.5, respectively. radius
R p is 335mm, 240mm, 212.5mm. Further, the numbers of the respective wing portions 2 are 10, 10, and 12, respectively. Fourth
In the figure, curves A, B, and C are the pressure coefficient curves of the respective fans with Φ as the horizontal axis, and A', B', and C' are the pressure coefficient curves of the radiators applied to the respective fans. Therefore, the intersection of the respective curves becomes the operating point of each embodiment. Curve D shows the pressure coefficient characteristics of a conventional axial flow fan. Next, in FIG. 4, the curves of the respective fans with Φ on the horizontal axis and η (efficiency) on the vertical axis are A 1 , B 1 , and C 1 . Each of the above-mentioned operating points is located near the maximum value of the efficiency curve. From this, it can be seen that each of the Examples is a fan with good efficiency, high static pressure, and large air volume. In Fig. 4, the experiment was conducted with the angle θ of the boss portion fixed at 30°, but almost the same results were obtained with other numerical angles. Moreover, the same applies to other specifications within the scope of the present invention. Note that the pressure coefficient Ψ and the flow rate coefficient Φ are expressed by the following equations.

流量係数Φ=Q/A・u 圧力係数Ψ=Ps/γ/2g 動力係数λ=L/γ/2g 効 率η=Φ・Ψ/λ Q:流量m3/s A:流路面積πRp 2(1−v2) v:ボス比Rb/Rp u:周速2πRpN N:回転数γPs Ps:静圧mmAg(Kg/m2) γ:比重Kg/m3 〔考案の効果〕 本考案のラジエータのフアンは、ラジエータの
通風抵抗が大きな場合に、高静圧冷却フアンとし
て風量が大でなお且つ効率の良いものを提供でき
る。即ち、θの値及びRb/Rp、D/T、S/T
の値を夫々特定の範囲に設定したから、ラジエー
タを通過する風量が大でなお且つフアン効率の大
きなものを提供できる。
Flow coefficient Φ=Q/A・u Pressure coefficient Ψ=P s /γ/2g Power coefficient λ=L/γ/2g Efficiency η=Φ・Ψ/λ Q: Flow rate m 3 /s A: Flow path area πR p 2 (1-v 2 ) v: Boss ratio R b /R p u: Peripheral speed 2πR p N N: Rotation speed γP s P s : Static pressure mmAg (Kg/m 2 ) γ: Specific gravity Kg/m 3 [ Effects of the Invention] The radiator fan of the present invention can provide a high static pressure cooling fan with a large air volume and high efficiency when the radiator has a large ventilation resistance. That is, the value of θ and R b /R p , D/T, S/T
Since the values of are set within specific ranges, it is possible to provide a large amount of air passing through the radiator and a high fan efficiency.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本ラジエータフアンの使用状態を示す
軸断面略図であり、第2図はその要部を示し、第
3図は同フアンの正面図、第4図は本考案のフア
ンの夫々の実施例における流量係数と圧力係数並
びに効率との関係を示す。 1……ボス部、2……翼部、l……仮想線、3
……筒状部、4……ラジエータ、5……タンク、
6……環状ゴム板、7……取付け面、8……クラ
ツチ、9……エンジン、10……ステー、11…
…先端縁、12……前端縁、13……後端縁、1
4……シユラウド本体。
Fig. 1 is a schematic axial cross-sectional view showing how the present radiator fan is used, Fig. 2 shows its main parts, Fig. 3 is a front view of the same fan, and Fig. 4 shows respective implementations of the fan of the present invention. The relationship between flow coefficient, pressure coefficient and efficiency in an example is shown. 1...Boss part, 2...Wing part, l...Virtual line, 3
... Cylindrical part, 4 ... Radiator, 5 ... Tank,
6... Annular rubber plate, 7... Mounting surface, 8... Clutch, 9... Engine, 10... Stay, 11...
...Tip edge, 12... Front end edge, 13... Rear end edge, 1
4... Shroud body.

Claims (1)

【実用新案登録請求の範囲】 圧力係数Ψ=0.25〜0.35で且つ、ボス部1が円
錐台形状をなし、該ボス部1外周に複数の翼部2
が等間隔に配置され、該翼部の半径方向先端縁が
前記ボス部1の軸線に平行に形成されたフアンに
おいて、前記ボス部1の外周面と前記軸線とのな
す角θをθ=27.5°〜35.5°とし、前記翼部2の後
縁における先端の半径Rpとその前後縁の中央の
根元の半径Rbとの関係をRb/Rp=0.45〜0.55と
し、前記翼部2の後縁の根元で前記ボス部1外面
に直交する仮想線lが該翼部2に投影されたと
き、該仮想線lと該翼部2の前記先端縁との交点
と、該翼部2の前記後端縁との距離Dが翼幅Tに
対してD/T=0.65〜1.0の関係にあり且つ、前
記翼部2の前記先端縁に近接して該先端縁の後端
部が露出するようにシユラウドの筒状部3が軸方
向長さSだけ被嵌され、その被嵌割合がS/T=
0.5〜0.7であることを特徴とするラジエータのフ
アン。 但し、前記圧力係数Ψはフアンの動作点を示
し、流量係数Φを横軸としたフアンおよびラジエ
ータの圧力係数曲線の交点を示す。
[Claims for Utility Model Registration] Pressure coefficient Ψ = 0.25 to 0.35, the boss portion 1 has a truncated conical shape, and a plurality of wing portions 2 are provided on the outer periphery of the boss portion 1.
are arranged at equal intervals, and the radial tip edge of the wing section is formed parallel to the axis of the boss section 1, and the angle θ between the outer circumferential surface of the boss section 1 and the axis line is θ=27.5. ° to 35.5°, and the relationship between the radius R p of the tip at the trailing edge of the wing section 2 and the radius R b of the center root of the front and rear edges is R b /R p = 0.45 to 0.55, and the wing section 2 When an imaginary line l perpendicular to the outer surface of the boss portion 1 at the root of the trailing edge is projected onto the wing portion 2, the intersection of the imaginary line l and the tip edge of the wing portion 2 and the wing portion 2 The distance D from the trailing edge of the blade has a relationship of D/T=0.65 to 1.0 with respect to the wing width T, and the rear end of the leading edge is exposed close to the leading edge of the wing section 2. The cylindrical part 3 of the shroud is fitted by the axial length S, and the fitting ratio is S/T=
Radiator fan characterized by 0.5~0.7. However, the pressure coefficient Ψ indicates the operating point of the fan, and indicates the intersection of the pressure coefficient curves of the fan and the radiator with the flow coefficient Φ as the horizontal axis.
JP901389U 1989-01-26 1989-01-26 Expired - Lifetime JPH0545837Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP901389U JPH0545837Y2 (en) 1989-01-26 1989-01-26

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP901389U JPH0545837Y2 (en) 1989-01-26 1989-01-26

Publications (2)

Publication Number Publication Date
JPH0299296U JPH0299296U (en) 1990-08-07
JPH0545837Y2 true JPH0545837Y2 (en) 1993-11-26

Family

ID=31215390

Family Applications (1)

Application Number Title Priority Date Filing Date
JP901389U Expired - Lifetime JPH0545837Y2 (en) 1989-01-26 1989-01-26

Country Status (1)

Country Link
JP (1) JPH0545837Y2 (en)

Also Published As

Publication number Publication date
JPH0299296U (en) 1990-08-07

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