JPH0512692U - Turbo Juan - Google Patents

Turbo Juan

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Publication number
JPH0512692U
JPH0512692U JP2738291U JP2738291U JPH0512692U JP H0512692 U JPH0512692 U JP H0512692U JP 2738291 U JP2738291 U JP 2738291U JP 2738291 U JP2738291 U JP 2738291U JP H0512692 U JPH0512692 U JP H0512692U
Authority
JP
Japan
Prior art keywords
blade
blades
turbofan
air
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
JP2738291U
Other languages
Japanese (ja)
Inventor
隆行 菱田
啓一 石川
靖 菱田
Original Assignee
太平洋工業株式会社
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 太平洋工業株式会社 filed Critical 太平洋工業株式会社
Priority to JP2738291U priority Critical patent/JPH0512692U/en
Publication of JPH0512692U publication Critical patent/JPH0512692U/en
Pending legal-status Critical Current

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Abstract

(57)【要約】 【目的】 ターボファンの羽根表面を流れる空気の剥離
現象を緩和して風量、静圧を増加し、効率の向上を図る
ことを目的とする。 【構成】 主板1上に複数個の羽根6が配設されたター
ボファンにおいて、前記羽根6の前面側7表面の任意の
箇所に、複数個の円形状の凹み面8を形成したものであ
る。
(57) [Summary] [Purpose] The purpose is to improve the efficiency by relaxing the separation phenomenon of the air flowing on the blade surface of a turbofan to increase the air volume and static pressure. In a turbofan having a plurality of blades 6 arranged on a main plate 1, a plurality of circular concave surfaces 8 are formed at arbitrary positions on the front surface 7 of the blades 6. ..

Description

【考案の詳細な説明】[Detailed description of the device]

【0001】[0001]

【産業上の利用分野】[Industrial applications]

本考案は、ターボファンに関し、その目的とするところは、羽根表面を流れる 空気の剥離現象を緩和して風量、静圧を増加し、ファン効率の向上を図ることに ある。 The present invention relates to a turbofan, and its purpose is to alleviate the separation phenomenon of the air flowing on the blade surface to increase the air volume and static pressure and improve the fan efficiency.

【0002】[0002]

【従来の技術と問題点】[Prior art and problems]

従来の技術を図7〜図9により説明する。 従来のターボファンには、主板1に一定の円弧面をもって形成した羽根2が設け られている。なお、図中、eは羽根の内側、fは羽根の外側である。 このため、吸込口3より吸い込まれた空気は、羽根の間の通路5を流れるが、羽 根形状は円弧面なので、羽根2の前面側4表面では剥離を起こしている。従って 、図7に矢印Uで示す空気の流れの中で、羽根の表面側ではほとんど流れない状 態となるため、ファン効率が悪くなっていた。 A conventional technique will be described with reference to FIGS. A conventional turbofan is provided with blades 2 formed on a main plate 1 with a constant arc surface. In the figure, e is the inside of the blade and f is the outside of the blade. Therefore, the air sucked from the suction port 3 flows through the passage 5 between the blades, but since the blade shape is an arc surface, the front surface 4 of the blade 2 is peeled off. Therefore, in the air flow indicated by the arrow U in FIG. 7, almost no air flows on the surface side of the blades, resulting in poor fan efficiency.

【0003】[0003]

【課題を解決するための手段】[Means for Solving the Problems]

本考案のターボファンは、主板1上に複数個の羽根6が配設されたターボファ ンにおいて、前記羽根6の前面側7表面の任意の箇所に、複数個の円形状の凹み 面8を形成したことを特徴とするものである。 The turbofan of the present invention is a turbofan in which a plurality of blades 6 are arranged on a main plate 1, and a plurality of circular concave surfaces 8 are formed at arbitrary positions on the front side 7 surface of the blades 6. It is characterized by having done.

【0004】[0004]

【実施例】【Example】

以下、この考案の実施例を図面に基づいて詳細に説明する。 図1〜図4において、1は主板、6は主板1に配設された羽根で、吸込口3と 羽根間に通路5を形成している。また、前記羽根6の前面側7の表面の任意な箇 所には、図2〜図4に示すように、複数個の円形状の凹み面8が形成されている 。なお、図中、矢印で示した9はターボファンの回転方向を示している。 図6は、他の実施例を示すもので、図2〜図4に示した円形状の凹み面8に替え て縦長形状の凹み面10を形成したものである。 Hereinafter, embodiments of the present invention will be described in detail with reference to the drawings. 1 to 4, 1 is a main plate, 6 is a blade arranged on the main plate 1, and a passage 5 is formed between the suction port 3 and the blade. Further, as shown in FIGS. 2 to 4, a plurality of circular recessed surfaces 8 are formed at arbitrary points on the front surface 7 of the blade 6. In the figure, 9 indicated by an arrow indicates the rotation direction of the turbo fan. FIG. 6 shows another embodiment, in which a vertically long concave surface 10 is formed instead of the circular concave surface 8 shown in FIGS.

【0005】[0005]

【作用】[Action]

次に、本考案の作用について説明する。 本考案のターボファンを回転させると、吸込口3より吸い込まれた空気は、羽根 6によりターボファンの外周から吐き出され送風される。 この時、羽根前面側7表面の空気の流れは、前記の円形状の凹み面8によって乱 され通路5を流れる空気と入り交じりエネルギーの供給を受け、前面側7表面か ら剥離しようとする現象が緩和されて空気の流れが生じ、通路5の空気流域面積 が大きくなる。 Next, the operation of the present invention will be described. When the turbofan of the present invention is rotated, the air sucked from the suction port 3 is discharged from the outer periphery of the turbofan by the blades 6 and is blown. At this time, the flow of air on the front surface 7 side of the blade is disturbed by the circular concave surface 8 and mixed with the air flowing through the passage 5 to receive energy supplied to the front surface 7 surface of the front surface 7 to cause separation. Are alleviated to generate an air flow, and the air basin area of the passage 5 is increased.

【0006】 なお、図4に示したように、羽根6に形成する円形状の凹面8の範囲は、ファ ン形状によっても異なるため一概に定めることが出来ないが、考案者の実験によ れば、円形状の凹面8を形成させる範囲は、羽根6の内側e端部からl/L×1 00=60%の位置に配設するとその効果が表れ、図5に示すようなファン特性 が得られた。なお、この図において、特性Aは、本考案におけるファンの風量と 静圧の関係を示し、特性Bは、従来のファンの風量と静圧の関係を示している。 なお、上記ファン特性の比較に用いた羽根の凹面形状は、円形状のものであるが 、これを縦長形状のものにしても同様の結果を得ている。As shown in FIG. 4, the range of the circular concave surface 8 formed on the blade 6 cannot be unconditionally determined because it varies depending on the fan shape. For example, when the circular concave surface 8 is formed in the range of 1 / L × 100 = 60% from the inner end e of the blade 6, its effect is exhibited, and the fan characteristic as shown in FIG. Was obtained. In this figure, the characteristic A shows the relationship between the air volume and the static pressure of the fan in the present invention, and the characteristic B shows the relationship between the air volume and the static pressure of the conventional fan. Although the concave shape of the blade used for the comparison of the fan characteristics is circular, the same result is obtained even when the concave shape is elongated.

【0007】[0007]

【考案の効果】[Effect of the device]

以上のように、本考案によれば、羽根6の前面側7表面の任意の箇所に、複数 個の凹み面8または10を形成しているため、羽根前面側7表面の空気の流れは 乱され、その外側を流れる空気と入り交じって吐出側へ流れる。従って、従来の ものに比べて有効通路面積が増加して風量、静圧が増加し、ファン効率を向上さ せることができ、その実用的効果は大なるものである。 As described above, according to the present invention, since a plurality of concave surfaces 8 or 10 are formed at arbitrary positions on the front surface 7 surface of the blade 6, the air flow on the front surface 7 of the blade is disturbed. The air is mixed with the air flowing outside and flows to the discharge side. Therefore, compared with the conventional one, the effective passage area is increased, the air volume and the static pressure are increased, the fan efficiency can be improved, and the practical effect is great.

【0008】[0008]

【図面の簡単な説明】[Brief description of drawings]

【図1】 本考案のターボファンの平面図。FIG. 1 is a plan view of a turbofan of the present invention.

【図2】 図1の羽根の斜視図。FIG. 2 is a perspective view of the blade shown in FIG.

【図3】 図2に示す羽根のC−C断面図。3 is a cross-sectional view taken along line CC of the blade shown in FIG.

【図4】 図2に示す羽根のC−C断面図。FIG. 4 is a cross-sectional view taken along line CC of the blade shown in FIG.

【図5】 ターボファンの風量と静圧の関係を示す特性
図。
FIG. 5 is a characteristic diagram showing a relationship between an air flow rate of a turbo fan and static pressure.

【図6】 本考案の他の実施例を示す羽根の斜視図。FIG. 6 is a perspective view of a blade according to another embodiment of the present invention.

【図7】 従来のターボファンの平面図。FIG. 7 is a plan view of a conventional turbo fan.

【図8】 図7のD−D断面図。8 is a cross-sectional view taken along the line DD of FIG.

【図9】 従来の羽根の斜視図。FIG. 9 is a perspective view of a conventional blade.

【符号の説明】[Explanation of symbols]

1 主板。 2 羽根。 3 吸込口。
4 羽根前面側。5 通路。 6 羽根。
7 羽根前面側。 8 円形状の凹面。9 回転方
向。 10 縦長形状の凹面。e 羽根の内側。
f 羽根の外側。
1 Main plate. 2 feathers. 3 Suction port.
4 Front side of the blade. 5 passages. 6 feathers.
7 Front side of the blade. 8 Circular concave surface. 9 Direction of rotation. 10 Vertically long concave surface. e Inside the blade.
f Outside of the blade.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 【請求項1】 主板1上に複数個の羽根6が配設された
ターボファンにおいて、前記羽根6の前面側7表面の任
意の箇所に、複数個の円形状の凹み面8を形成したこと
を特徴とするターボファン。
1. A turbofan having a plurality of blades 6 arranged on a main plate 1, wherein a plurality of circular concave surfaces 8 are formed at arbitrary positions on a front surface 7 of the blades 6. Is a turbo fan.
JP2738291U 1991-03-28 1991-03-28 Turbo Juan Pending JPH0512692U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2738291U JPH0512692U (en) 1991-03-28 1991-03-28 Turbo Juan

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2738291U JPH0512692U (en) 1991-03-28 1991-03-28 Turbo Juan

Publications (1)

Publication Number Publication Date
JPH0512692U true JPH0512692U (en) 1993-02-19

Family

ID=12219501

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2738291U Pending JPH0512692U (en) 1991-03-28 1991-03-28 Turbo Juan

Country Status (1)

Country Link
JP (1) JPH0512692U (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH074388A (en) * 1993-06-15 1995-01-10 Matsushita Refrig Co Ltd Impeller for centrifugal blower
JP2010229842A (en) * 2009-03-26 2010-10-14 Toyota Motor Corp Compressor
JP2011209403A (en) * 2010-03-29 2011-10-20 Seiko Epson Corp Projector device
US9709073B2 (en) 2012-10-03 2017-07-18 Minebea Co., Ltd. Centrifugal fan

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6035199A (en) * 1983-08-04 1985-02-22 Matsushita Electric Ind Co Ltd Impeller of blower

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6035199A (en) * 1983-08-04 1985-02-22 Matsushita Electric Ind Co Ltd Impeller of blower

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH074388A (en) * 1993-06-15 1995-01-10 Matsushita Refrig Co Ltd Impeller for centrifugal blower
JP2010229842A (en) * 2009-03-26 2010-10-14 Toyota Motor Corp Compressor
JP2011209403A (en) * 2010-03-29 2011-10-20 Seiko Epson Corp Projector device
US9709073B2 (en) 2012-10-03 2017-07-18 Minebea Co., Ltd. Centrifugal fan

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