JPS5845495A - Heat transmitting fin - Google Patents

Heat transmitting fin

Info

Publication number
JPS5845495A
JPS5845495A JP14231181A JP14231181A JPS5845495A JP S5845495 A JPS5845495 A JP S5845495A JP 14231181 A JP14231181 A JP 14231181A JP 14231181 A JP14231181 A JP 14231181A JP S5845495 A JPS5845495 A JP S5845495A
Authority
JP
Japan
Prior art keywords
louvers
louver
heat transfer
fin
fins
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
JP14231181A
Other languages
Japanese (ja)
Inventor
Toshio Hatada
畑田 敏夫
Takao Chiaki
千秋 隆雄
Sadatoshi Minagawa
皆川 貞利
Naoji Ajiki
安食 直二
Masanobu Ueda
上田 雅信
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.)
Hitachi Ltd
Original Assignee
Hitachi 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 Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP14231181A priority Critical patent/JPS5845495A/en
Publication of JPS5845495A publication Critical patent/JPS5845495A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F1/00Tubular elements; Assemblies of tubular elements
    • F28F1/10Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
    • F28F1/12Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
    • F28F1/126Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element consisting of zig-zag shaped fins
    • F28F1/128Fins with openings, e.g. louvered fins

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Geometry (AREA)
  • Thermal Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cooling Or The Like Of Electrical Apparatus (AREA)

Abstract

PURPOSE:To improve a heat transmitting performance and reduce a venting resistance by a method wherein louvers are cut to the bent parts of corrugate fins to form the longest louvers. CONSTITUTION:The configuration of whole U-turn parts are formed so that an unit fin is formed into a configuration wherein each louvers 9 are arranged in a wave form and the cut parts 10 are arriving at positions same as the U-turn parts or very near to the U-turn parts. Accordingly, inflow air A flows between the fins as shown by arrow signs 11, airflow colliding against each louvers becomes well mixed flow, it will not be affected easily by a temperature boundary layer formed by the front louver, and the airflow will never be bent extremely, therefore, a big separation and the generation of an eddy will never be caused. According to said functions, the heat transmitting performance of the fin may be improved and the venting resistance may be reduced remarkably.

Description

【発明の詳細な説明】 本発明は、空調機、冷凍機などく用いられる、熱交換器
用フィンに係り、特に扁平伝熱管を用い九ヨルゲート形
熱交換器の、フィン形状に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to fins for heat exchangers used in air conditioners, refrigerators, etc., and particularly relates to the fin shape of a nine-Yorgate type heat exchanger using flat heat transfer tubes.

コルゲート形熱交換器の形状は、第1図に示すような形
状が一般的であり、そのフィンは第2図のような形状に
なっている。またその■−■断面断面筒3図のような形
である。従来技術の第1の問題点は、第3図でわかるよ
うに、流入空気入が、図示のように渦6をともないなが
ら矢印7のように蛇行して流れるため、伝熱性能が部分
的に低下し、さらに通風抵抗が増加する欠点があった。
A corrugated heat exchanger generally has a shape as shown in FIG. 1, and its fins have a shape as shown in FIG. 2. In addition, the cross-sectional shape of the tube is as shown in Figure 3. The first problem with the prior art is that, as can be seen in Figure 3, the incoming air flows in a meandering manner as shown by the arrow 7 while creating a vortex 6 as shown in the figure, resulting in a partial loss of heat transfer performance. There was a drawback that the ventilation resistance was further increased.

第2の問題点は、第2図かられかるようにルーバの切り
込みに限界がある(Uターン部近傍まで切ることが困難
)ため、ルーバの性能が十分生かされない欠点があっ九
The second problem is that, as shown in Figure 2, there is a limit to how deep the louver can cut (it is difficult to cut to the vicinity of the U-turn), so the performance of the louver cannot be fully utilized.

本発明は上記に鑑みて発明されたもので、ル−バ付コル
ゲートフィンにおいて、性能の優れ九ルーバ形状を提供
すること、また、ルーバ切り込み長さを最大限にし、ル
ーバを最も有効に利用することを目的とする。
The present invention was invented in view of the above-mentioned problems, and aims to provide a nine-louver shape with excellent performance in a corrugated fin with louvers, and to maximize the length of the louver cut to make the most effective use of the louver. The purpose is to

フィンの伝熱性能を向上させるには、747間を流通す
る空気流の温度の均一化を促進できるルーパ形状、ルー
バの配置構造を考える必要がある。さらに1このような
ルーバを有効に生かすには、ルーバ切り込み長さを出来
る限り大きくシ、ルーパ部の占める面積割合を大きくす
る必要がある上記観点から本発明は、所期の目的を達成
するため、フィン板に、フィン間を流通する流体の流通
方向に直交する方向に多数個の切込みを入れ、°この切
込み端部を曲折して、ルーツ(が曲折部まで形成されて
いるコルゲートフィンを形成し、且つ隣り合うルーバの
縁部の高さ位置を互にずらしたζ1ことをIIIt黴と
する。
In order to improve the heat transfer performance of the fins, it is necessary to consider the shape and arrangement of the louvers that can promote uniformity of the temperature of the airflow flowing between the fins. Furthermore, 1. In order to make effective use of such a louver, it is necessary to make the louver cut length as large as possible and increase the area ratio occupied by the louver portion.From the above viewpoint, the present invention has been developed to achieve the intended purpose. , a large number of cuts are made in the fin plate in a direction perpendicular to the flow direction of the fluid flowing between the fins, and the ends of these cuts are bent to form a corrugated fin in which the roots are formed up to the bent part. In addition, ζ1 in which the height positions of the edges of adjacent louvers are shifted from each other is defined as IIIt mold.

以下本発明の一実施例を図面に基ずき説明する。第4゛
図は、本発明の一実施例を示すコルゲートフィンの部分
拡大図である。本フィンを構成する個々のルーバ9の断
面形状は、第5図に示すように、山形断面であるととも
に、各ルーバ9は全体が波形に配置されている。コルゲ
ートフィンのUターン部(曲折部)8は、従来技術と全
て異なり、第5図に示した個々のルーバの位置に従って
折り曲げられるように形成される。従っ゛て、Uターン
部全体の形状は第4図のように、単位フイ/は各ルーバ
9を波形に配置した形状になり、さらに、ルーバ切り込
み部10は、Uターン部と同一か、極めて近い位置まで
切込みが達している。
An embodiment of the present invention will be described below with reference to the drawings. FIG. 4 is a partially enlarged view of a corrugated fin showing an embodiment of the present invention. As shown in FIG. 5, the cross-sectional shape of each louver 9 constituting this fin is a chevron-shaped cross section, and each louver 9 is arranged in a wave-like shape as a whole. The U-turn portion (bending portion) 8 of the corrugated fin is completely different from the conventional technique and is formed so as to be bent according to the position of each louver shown in FIG. Therefore, as shown in FIG. 4, the overall shape of the U-turn section is such that the unit fins are each louver 9 arranged in a waveform, and the louver cut section 10 is either the same as the U-turn section or very similar to the U-turn section. The depth of cut has reached a close position.

次にこのコルゲートフィンの作用について説明する。本
実施例のコルゲートフィンの第4図、マーマ断面は第5
図のような形状である。すなわち、山形断面ルーバ9が
、波形に配置されている。
Next, the function of this corrugated fin will be explained. The corrugated fin of this example is shown in Fig. 4, and the marma cross section is shown in Fig. 5.
The shape is as shown in the figure. That is, the chevron-shaped cross-section louvers 9 are arranged in a wave shape.

従って、流入空気入はフィン間を矢印11の如く流れ、
個々のルーバ、につき当たる空気流は、良く混合された
状態の流れ(温度分布が均一になっている)になシ、前
方のルーバで形成される温度境界層の影響を受けにくい
。さらに1空気流は極端に曲げられることがないので、
大きな剥離、渦の発生はない。これらの作用により、フ
イ、ンの伝熱性能が向上するとともに、通風抵抗が大幅
に減少する。さらに、前述し丸ように、本発明ではルー
バの切り込み部1Gを最大(折り返しのフラット部を除
くフィン全体がルーバになる)に取ることができるので
、ルーバの効果を最大限に生かすことができ、従来に比
較して、一層伝熱性能が向上する。一方、本発明によれ
ば、第5図に示したような性能の優れ九ルーバを有する
フィンを特別な゛製作方法を用いることなく実現できる
特徴がある。例えば、従来用いられている、歯車のかみ
合せ方式も導入でき、高速生産が可能である。
Therefore, the incoming air flows between the fins as shown by arrow 11,
If the air flow that impinges on each louver is well mixed (the temperature distribution is uniform), it will be less affected by the temperature boundary layer formed in the front louver. Furthermore, since the airflow is not extremely bent,
There were no major separations or vortices. These effects improve the heat transfer performance of the fins and significantly reduce ventilation resistance. Furthermore, as mentioned above, in the present invention, the notch 1G of the louver can be maximized (the entire fin except the folded flat part becomes the louver), so the effect of the louver can be maximized. , the heat transfer performance is further improved compared to the conventional method. On the other hand, according to the present invention, a fin having excellent performance and having nine louvers as shown in FIG. 5 can be realized without using any special manufacturing method. For example, the conventionally used gear meshing system can be introduced, allowing high-speed production.

第6−は他の実施例を示したものである。即ち、本実施
例は折り曲げ部8が曲面状に形成される場合である。こ
の場合は、流入空気方向から見た個々のルーバの位置関
係は第7図のようになっている。
No. 6 shows another embodiment. That is, in this embodiment, the bent portion 8 is formed into a curved shape. In this case, the positional relationship of the individual louvers viewed from the direction of the incoming air is as shown in FIG.

以上説明した様に、本発明によれば、コルゲートフィン
の折シ曲げ部までルーバが切り込まれ、最大長さのルー
バを備えたコルゲートフィンが得られ、大巾な伝熱性能
の向上と通風抵抗の低減がはかれる。を九生産スピード
の速いギヤ噛合せ方式による製作も容易である等の効果
を有する。
As explained above, according to the present invention, the louvers are cut up to the bent portion of the corrugated fin, and a corrugated fin with the maximum length of the louver can be obtained, which greatly improves heat transfer performance and ventilation. The resistance can be reduced. It also has the advantage of being easy to manufacture using the gear meshing method, which has a high production speed.

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

第1図は従来の熱交換器の概略形状図、第2図は従来の
コルゲートフィンの部分斜視図、第3図は第2図の1−
1位置の拡大断面図に空気流通状況を記入し丸断面図、
第4図は本発叫の一実施例を示すコルゲートフィンの部
分斜視図、第5図はs4図のv−v位置の拡大断面図に
空気流通状況を記入した断面図、第6図は他の実施例を
示すコルゲートフィンの部分斜視図、第1図は第6図の
コルゲートフィンを用いた熱交換器の部分正面図である
。 1・・・コルゲートフイ/ 2・・・扁平伝熱管 3・
・・ヘッダ  8・・・折り曲げフラット部  9・・
・山形L( 断面ルー−10・・・ルーバ切り込み部 11・・・フ
ィン間通過空気方向 12・・・曲面状切り込み部13
・・・扁平伝熱管 14.15.16・・・ルーパA・
・・流入空気方向 代通人 弁理士 薄 1)利 幸 隼11
Figure 1 is a schematic diagram of a conventional heat exchanger, Figure 2 is a partial perspective view of a conventional corrugated fin, and Figure 3 is 1-1 in Figure 2.
Fill in the air circulation situation on the enlarged cross-sectional view of position 1, and make a circular cross-sectional view.
Fig. 4 is a partial perspective view of a corrugated fin showing one embodiment of this ejection, Fig. 5 is a sectional view showing the air circulation situation in an enlarged sectional view taken along the v-v position in Fig. s4, and Fig. 6 is another example. FIG. 1 is a partial front view of a heat exchanger using the corrugated fins shown in FIG. 6. FIG. 1... Corrugated tube / 2... Flat heat exchanger tube 3.
...Header 8...Folded flat part 9...
・Chevron L (cross-sectional louver-10...louver cut portion 11...direction of air passing between fins 12...curved cut portion 13
...Flat heat exchanger tube 14.15.16...Looper A・
...Inflow air direction representative Patent attorney Susuki 1) Toshiyuki Hayabusa 11

Claims (1)

【特許請求の範囲】 1、 フィン板をヘアビン状に連続して曲折するコルゲ
ート形の伝熱フィンにおいて、フィン板に、フィン間を
流通する流体の流通方向に直交する方向に多数個の切込
みを入れ、切込み端部を曲折して、ルーバが曲折部まで
形成されるフィンを形成し、隣り合うルーバの縁部の高
さ位置を互いにずらしたことを**とする伝熱フィン。 2、ルーバが、ルーバの長手方向に株う中央部を稜線と
する鈍角に形成されている特許請求の範囲第1項記載の
伝熱フィン。 3、ルーバが、ルーバの長手方向Klう中央部を頂部と
するわん曲状に形成されている特許請求の範囲第1項記
載の伝熱フィン。 4、ルーバが、全体として波形に配置されている特許請
求の範囲第1項乃至第3項のいずれか一つに記載の伝熱
フィン。 5、ルーバが、交互に上下に配置されている特許請求の
範囲第1項乃至第3項のいずれか一つに記載の伝熱フィ
ン。
[Claims] 1. In a corrugated heat transfer fin in which the fin plate is continuously bent into a hairbin shape, the fin plate is provided with a large number of cuts in a direction perpendicular to the flow direction of fluid flowing between the fins. A heat transfer fin in which the louvers are formed up to the bent portion by bending the cut end, and the height positions of the edges of adjacent louvers are shifted from each other. 2. The heat transfer fin according to claim 1, wherein the louver is formed at an obtuse angle with a ridge line at the center extending in the longitudinal direction of the louver. 3. The heat transfer fin according to claim 1, wherein the louver is formed in a curved shape with the top at the center in the longitudinal direction K1 of the louver. 4. The heat transfer fin according to any one of claims 1 to 3, wherein the louvers are arranged in a wave shape as a whole. 5. The heat transfer fin according to any one of claims 1 to 3, wherein the louvers are alternately arranged one above the other.
JP14231181A 1981-09-11 1981-09-11 Heat transmitting fin Pending JPS5845495A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14231181A JPS5845495A (en) 1981-09-11 1981-09-11 Heat transmitting fin

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14231181A JPS5845495A (en) 1981-09-11 1981-09-11 Heat transmitting fin

Publications (1)

Publication Number Publication Date
JPS5845495A true JPS5845495A (en) 1983-03-16

Family

ID=15312401

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14231181A Pending JPS5845495A (en) 1981-09-11 1981-09-11 Heat transmitting fin

Country Status (1)

Country Link
JP (1) JPS5845495A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59212693A (en) * 1983-05-18 1984-12-01 Hitachi Ltd Heat conducting fin
JPH027489U (en) * 1988-06-17 1990-01-18
US6247527B1 (en) * 2000-04-18 2001-06-19 Peerless Of America, Inc. Fin array for heat transfer assemblies and method of making same
WO2002095315A1 (en) * 2001-05-18 2002-11-28 L'air Liquide Societe Anonyme A Directoire Et Conseil De Surveillance Pour L'etude Et L'exploitation Des Procedes Georges Claude Louvered fins for heat exchanger
US6598669B2 (en) 1999-04-19 2003-07-29 Peerless Of America Fin array for heat transfer assemblies and method of making same
US6932153B2 (en) * 2002-08-22 2005-08-23 Lg Electronics Inc. Heat exchanger
US7677057B2 (en) 2006-11-22 2010-03-16 Johnson Controls Technology Company Multichannel heat exchanger with dissimilar tube spacing
US7802439B2 (en) 2006-11-22 2010-09-28 Johnson Controls Technology Company Multichannel evaporator with flow mixing multichannel tubes
US8234881B2 (en) 2008-08-28 2012-08-07 Johnson Controls Technology Company Multichannel heat exchanger with dissimilar flow
WO2015118998A1 (en) * 2014-02-10 2015-08-13 三菱重工オートモーティブサーマルシステムズ株式会社 Heat-exchanger offset fin and coolant heat exchanger utilizing same
EP3255369A1 (en) * 2016-06-08 2017-12-13 Mahle International GmbH Fin element for a heat transferer

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59212693A (en) * 1983-05-18 1984-12-01 Hitachi Ltd Heat conducting fin
JPH027489U (en) * 1988-06-17 1990-01-18
JPH0539335Y2 (en) * 1988-06-17 1993-10-05
US6598669B2 (en) 1999-04-19 2003-07-29 Peerless Of America Fin array for heat transfer assemblies and method of making same
US6247527B1 (en) * 2000-04-18 2001-06-19 Peerless Of America, Inc. Fin array for heat transfer assemblies and method of making same
WO2002095315A1 (en) * 2001-05-18 2002-11-28 L'air Liquide Societe Anonyme A Directoire Et Conseil De Surveillance Pour L'etude Et L'exploitation Des Procedes Georges Claude Louvered fins for heat exchanger
CN100383485C (en) * 2001-05-18 2008-04-23 乔治洛德方法研究和开发液化空气有限公司 Louvered fins for heat exchanger
US6932153B2 (en) * 2002-08-22 2005-08-23 Lg Electronics Inc. Heat exchanger
US7802439B2 (en) 2006-11-22 2010-09-28 Johnson Controls Technology Company Multichannel evaporator with flow mixing multichannel tubes
US7757753B2 (en) 2006-11-22 2010-07-20 Johnson Controls Technology Company Multichannel heat exchanger with dissimilar multichannel tubes
US7677057B2 (en) 2006-11-22 2010-03-16 Johnson Controls Technology Company Multichannel heat exchanger with dissimilar tube spacing
US7832231B2 (en) 2006-11-22 2010-11-16 Johnson Controls Technology Company Multichannel evaporator with flow separating manifold
US7895860B2 (en) 2006-11-22 2011-03-01 Johnson Controls Technology Company Multichannel evaporator with flow mixing manifold
US7980094B2 (en) 2006-11-22 2011-07-19 Johnson Controls Technology Company Multichannel heat exchanger with dissimilar tube spacing
US8234881B2 (en) 2008-08-28 2012-08-07 Johnson Controls Technology Company Multichannel heat exchanger with dissimilar flow
US8938988B2 (en) 2008-08-28 2015-01-27 Johnson Controls Technology Company Multichannel heat exchanger with dissimilar flow
WO2015118998A1 (en) * 2014-02-10 2015-08-13 三菱重工オートモーティブサーマルシステムズ株式会社 Heat-exchanger offset fin and coolant heat exchanger utilizing same
JP2015152178A (en) * 2014-02-10 2015-08-24 三菱重工オートモーティブサーマルシステムズ株式会社 Off-set fin for heat exchanger and refrigerant heat exchanger using the same
US20160313070A1 (en) * 2014-02-10 2016-10-27 Mitsubishi Heavy Industries Automotive Thermal Systems Co., Ltd. Heat-exchanger offset fin and refrigerant heat-exchanger utilizing same
EP3255369A1 (en) * 2016-06-08 2017-12-13 Mahle International GmbH Fin element for a heat transferer

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