JPS62112997A - Heat exchanger - Google Patents

Heat exchanger

Info

Publication number
JPS62112997A
JPS62112997A JP25147485A JP25147485A JPS62112997A JP S62112997 A JPS62112997 A JP S62112997A JP 25147485 A JP25147485 A JP 25147485A JP 25147485 A JP25147485 A JP 25147485A JP S62112997 A JPS62112997 A JP S62112997A
Authority
JP
Japan
Prior art keywords
slit
gas flow
piece
airflow
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
JP25147485A
Other languages
Japanese (ja)
Inventor
Osao Kido
長生 木戸
Hiroshi Yoneda
米田 浩
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.)
Panasonic Holdings Corp
Original Assignee
Matsushita Refrigeration Co
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 Matsushita Refrigeration Co filed Critical Matsushita Refrigeration Co
Priority to JP25147485A priority Critical patent/JPS62112997A/en
Publication of JPS62112997A publication Critical patent/JPS62112997A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To enable a high heat transfer rate on the average to be obtained even in the case of a heat exchanger elongate in the direction of a gas flow, by a construction wherein slit pieces having leading edge parts opposed to a gas flow are provided on the surfaces of fins, and base parts of each of the slit pieces are inclined to the inner side of the slit piece relative to the direction of the gas flow. CONSTITUTION:Heat is exchanged between a gas flow B passing between fins 5 and a heat-transmitting medium flowing in flat pipes 4, through the fins 5 and the pipes 4. A temperature boundary layer of the gas flow B formed on the surface of the fin 5 is split by slit pieces 6, so that the boundary layer is made to be thin. Since a slit part 6b of the slit piece 6 is parallel to the gas flow B, the draft resistance is not extremely increased by the slit pieces 6, and the gas flow B is not extremely biased while being led to the outside of both ends of the slit piece 6. In addition, since the gas flow B passing on the outside of both ends of the slit piece 6 is drawn to the inside of the slit piece 6 by base parts 6a provided at both ends of the slit piece 6, the gas flow passing through the interior of the slit piece 6 is accelerated, and a high heat transfer rate on the average can be obtained.

Description

【発明の詳細な説明】 産業上の利用分野 本発明は空調機器や冷凍機器等に用いられる熱交換器に
関するものである。
DETAILED DESCRIPTION OF THE INVENTION Field of Industrial Application The present invention relates to a heat exchanger used in air conditioning equipment, refrigeration equipment, etc.

従来の技術 近年、熱交換器の性能向上は目ざましいものがあり、空
気側伝熱面積が大きいことを特徴とする波形状フィンを
備えた熱交換器がすでに実用化されている。
BACKGROUND OF THE INVENTION In recent years, there has been a remarkable improvement in the performance of heat exchangers, and heat exchangers equipped with wave-shaped fins characterized by a large heat transfer area on the air side have already been put into practical use.

以下図面を参照しながら、上述した従来の熱交換器につ
いて説明を行なう。
The conventional heat exchanger mentioned above will be explained below with reference to the drawings.

第5図〜第9図は従来の熱交換器を示すものである。第
6図〜第9図において、1は蛇行状に屈曲した偏平管で
、鉛直方向で直管部1′を平行に備えている。2は偏平
管1の向い合う直管部1′相互間に水平に設けられたフ
ィンで、波形状に一定間隔で偏平管1に固定されている
。3はフィン2の表面に設けられたルーバー片で、その
前縁部3aが気流Aと対向し、かつルーバー面3bが気
流Aと傾斜を持って構成されている。
5 to 9 show conventional heat exchangers. In FIGS. 6 to 9, reference numeral 1 denotes a flat tube bent in a meandering manner, and is provided with straight tube portions 1' parallel to each other in the vertical direction. Fins 2 are provided horizontally between the opposing straight pipe portions 1' of the flat tube 1, and are fixed to the flat tube 1 at regular intervals in a wave shape. A louver piece 3 is provided on the surface of the fin 2, and its front edge 3a faces the airflow A, and the louver surface 3b is inclined with respect to the airflow A.

以上のように構成された熱交換器について、以下その動
作について説明する。
The operation of the heat exchanger configured as above will be described below.

フィン2のフィン間を流れる気流Aと偏平管1の管内を
流れる熱媒体の間で、フィン2及び偏平管1を介して熱
交換が行なわれる。その際、フィン2表面にルーバー片
3が多数施しであるために、フィン2の表面に生じる気
流Aの温度境界層の発達が分断されて境界層厚さは薄く
なると共に、傾斜したルーバー面3bにより気流Aが流
れ方向を変えられて流れを乱されることによっても、気
流3ベーゾ Aとフィン2の間で大きい熱伝達を得ている。
Heat exchange is performed between the airflow A flowing between the fins of the fins 2 and the heat medium flowing inside the flat tube 1 via the fins 2 and the flat tube 1. At this time, since a large number of louver pieces 3 are provided on the surface of the fin 2, the development of the temperature boundary layer of the airflow A generated on the surface of the fin 2 is interrupted, the thickness of the boundary layer becomes thinner, and the louver surface 3b is inclined. Even by changing the flow direction of the airflow A and turbulating the flow, a large amount of heat is transferred between the airflow 3 beso A and the fins 2.

発明が解決しようとする問題点 しかしながら上記のような構成では、ルーバー片3の通
風抵抗が大きいために、第8図に示すように気流Aはル
ーバー片3の無い部分、すなわちルーバー片3の両端の
外側に片寄って流れ、ルーバー片30両端の外側では気
流Aの温度境界層が十分に分断できずに下流へ行くに従
って厚くなると共に、ルーバー片3の内側を流れる気流
Aの速度が遅くなるためにルーバー片3表面に生じる温
度境界層も厚いものとなシ、特に気流入方向に長い熱交
換器の場合に極端に熱伝達率が低下するという問題点を
有していた。
Problems to be Solved by the Invention However, in the above configuration, since the ventilation resistance of the louver piece 3 is large, the airflow A is directed to the portion where the louver piece 3 is not present, that is, both ends of the louver piece 3, as shown in FIG. The temperature boundary layer of the airflow A cannot be sufficiently separated on the outside of both ends of the louver piece 30, and it becomes thicker as it goes downstream, and the speed of the airflow A flowing inside the louver piece 3 becomes slower. In addition, the temperature boundary layer formed on the surface of the louver piece 3 is also thick, which has the problem of extremely lowering the heat transfer coefficient, especially in the case of a heat exchanger that is long in the air inflow direction.

本発明は上記問題点に鑑み、気流方向に長い熱交換器に
おいても平均的に大きい熱伝達率が得られる熱交換器を
提供するものである。
In view of the above-mentioned problems, the present invention provides a heat exchanger that can obtain a high average heat transfer coefficient even in a heat exchanger that is long in the direction of airflow.

問題点を解決するための手段 上記問題点を解決するために本発明の熱交換器は、フィ
ン表面に前縁部が気流と対向するスリット片を設け、か
つこのスリット片の脚部が気流方向に対してスリット片
内側へ傾側を持つという構成を備えたものである。
Means for Solving the Problems In order to solve the above problems, the heat exchanger of the present invention has a slit piece provided on the fin surface with a front edge facing the airflow, and a leg of this slit piece facing the airflow direction. It has a structure in which the slit piece has an inwardly inclined side.

作  用 本発明は上記した構成によって、スリット片は気流方向
を大きく変えないため、ルーバー片に比べて通風抵抗が
少なく、フィン間を流れる気流がスリット片のない部分
、ずなわぢスリット片の両端の外側へ極端に片寄って流
れることはなく、しかもスリット片両端の脚部が気流方
向に対してスリット片内側へ傾斜を持っているだめに、
スリット片両端の外側を流れる気流がスリット片内側へ
引き寄せられるためにスリット片内側を流れる気流が加
速されることとなり、スリット片によって気流の温度境
界層を分断して境界層を薄くする効果が大きくなり、気
流とフィンの間の熱伝達率が極めて向上することとなる
Effect: Due to the above-described configuration, the slit piece does not greatly change the direction of airflow, so there is less ventilation resistance than a louver piece, and the airflow flowing between the fins is directed to the part without the slit piece and both ends of the slit piece. The air does not flow extremely toward the outside of the air, and the legs at both ends of the slit are inclined toward the inside of the slit with respect to the airflow direction.
The airflow flowing on the outside of both ends of the slit piece is drawn to the inside of the slit piece, so the airflow flowing inside the slit piece is accelerated, and the slit piece has a large effect of dividing the temperature boundary layer of the airflow and thinning the boundary layer. As a result, the heat transfer coefficient between the airflow and the fins is greatly improved.

実施例 以下本発明の一実施例の熱交換器について、図面を参照
しながら説明する。
EXAMPLE Hereinafter, a heat exchanger according to an example of the present invention will be described with reference to the drawings.

第1図は本発明の一実施例における熱交換器の6ページ 斜視図を示すものである。第1図において、4は蛇行状
に屈曲した偏平管で、鉛直方向で直管部4′を平行に備
えている。5は偏平管4の向い合う直管部4′相互間に
水平に設けられたフィンで、波形状に一定間隔で偏平管
4に固定されている。6はフィン5の表面に設けられた
スリット片で、フィン5の両面に気流B方向で交互に設
けである。
FIG. 1 shows a 6-page perspective view of a heat exchanger in an embodiment of the present invention. In FIG. 1, reference numeral 4 denotes a flat tube bent in a meandering manner, and is provided with straight tube portions 4' parallel to each other in the vertical direction. Fins 5 are provided horizontally between the opposing straight pipe portions 4' of the flat tube 4, and are fixed to the flat tube 4 at regular intervals in a wave shape. Reference numeral 6 denotes slit pieces provided on the surface of the fin 5, which are alternately provided on both sides of the fin 5 in the direction of the air flow B.

またスリット片6は、脚部6aとスリット部6bとから
なり、脚部6aは気流B方向に対してスリット片内側へ
傾斜を持っている。
Further, the slit piece 6 is composed of a leg portion 6a and a slit portion 6b, and the leg portion 6a has an inclination toward the inside of the slit piece with respect to the direction of the airflow B.

以上のように構成された熱交換器について、以下その動
作について説明する。
The operation of the heat exchanger configured as above will be described below.

フィン6のフィン間を流れる気流Bと偏平管4の管内を
流れる熱媒体の間で、フィン5及び偏平管4を介して熱
交換が行なわれる。その際、フィン5の表面に生じる気
流Bの温度境界層はスリット片6によって分断され境界
層厚さは薄いものとなる。また、スリット片6のスリッ
ト部6bは気流Bと平行になっているため、極端に通風
抵抗を増大させることは々く、気流Bがスリット片6の
A− 無い部分、すなわちスリット片6両端の外側へ極端に片
寄って流れることはない。しかもスリット片6両端の脚
部6aによってスリット片6両端の外側を流れる気流B
がスリット片6の内側へ引き寄せられるためにスリット
片6内側を流れる気流が加速されることとなり、気流B
の温度境界層はより薄いものとなって気流Bとフィン5
の熱伝達率が下流側へ行っても低下することはなく、平
均的に大きい熱伝達率を得ることができる。
Heat exchange is performed between the airflow B flowing between the fins of the fins 6 and the heat medium flowing inside the flat tube 4 via the fins 5 and the flat tube 4. At this time, the temperature boundary layer of the airflow B generated on the surface of the fin 5 is divided by the slit piece 6, and the thickness of the boundary layer becomes thin. In addition, since the slit portion 6b of the slit piece 6 is parallel to the airflow B, it is unlikely that the ventilation resistance will be extremely increased. It does not flow excessively toward the outside. Moreover, the airflow B flowing on the outside of both ends of the slit piece 6 due to the legs 6a at both ends of the slit piece 6
is drawn to the inside of the slit piece 6, the airflow flowing inside the slit piece 6 is accelerated, and the airflow B
The temperature boundary layer becomes thinner, and airflow B and fin 5
The heat transfer coefficient does not decrease even if it goes downstream, and a high heat transfer coefficient can be obtained on average.

以上のように本実施例によれば、フィン6の表面にスリ
ット片6を設け、かつスリット片6の脚部6aを気流B
方向に対してスリット片6内側へ傾斜させることにより
、気流Bの下流側へ行っても気流Bとフィン60間の熱
伝達率を低下させることなく、気流B方向に長い熱交換
器においても大きい熱伝達率を維持して伝熱性能の向上
がはかれる。
As described above, according to this embodiment, the slit piece 6 is provided on the surface of the fin 6, and the leg part 6a of the slit piece 6 is connected to the air flow B.
By inclining the slit piece 6 inward with respect to the direction, the heat transfer coefficient between the airflow B and the fins 60 does not decrease even when going downstream of the airflow B, and is large even in a heat exchanger that is long in the direction of the airflow B. Heat transfer performance is improved by maintaining the heat transfer coefficient.

発明の効果 以上のように本発明は、フィン表面にスリット片を設け
、かつスリット片の脚部を気流方向に対7ページ してスリット片内側へ傾斜させることにより、気流方向
に長い熱交換器でも下流側へ行くに従って気流とフィン
の間の熱伝達率を低下させることはなく伝熱性能の優れ
た熱交換器を得ることができる。
Effects of the Invention As described above, the present invention provides a heat exchanger that is long in the airflow direction by providing slit pieces on the fin surface and inclining the legs of the slit pieces inward in the airflow direction. However, as it goes downstream, the heat transfer coefficient between the airflow and the fins does not decrease, making it possible to obtain a heat exchanger with excellent heat transfer performance.

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

第1図は本発明の一実施例における熱交換器のフィン形
状、を示す要部断面図、第2図は同第1図の熱交換器の
要部斜視図、第3図は第1図のD−D線の断面を通過す
る気流の風速分布図、第4図は第1図のC−C線の断面
図、第6図は従来の熱交換器の形状を示す斜視図、第6
図は第5図のフィン形状を示す要部断面図、第7図は第
6図の要部斜視図、第8図は第6図のF−F線の断面を
通過する気流の風速分布図、第9図は第6図のE −E
線の断面図である。 4・・・・・・偏平管、6・・・・・・フィン、6・・
・・・・スリット片、6a・・・・・・脚部、6b・・
・・・・スリット部。 代理人の氏名 弁理士 中 尾 敏 男 ほか1名菓 
25!I
FIG. 1 is a sectional view of a main part showing the fin shape of a heat exchanger according to an embodiment of the present invention, FIG. 2 is a perspective view of a main part of the heat exchanger shown in FIG. 1, and FIG. Figure 4 is a cross-sectional view taken along line C-C in Figure 1. Figure 6 is a perspective view showing the shape of a conventional heat exchanger.
The figure is a cross-sectional view of the main part showing the fin shape of Fig. 5, Fig. 7 is a perspective view of the main part of Fig. 6, and Fig. 8 is a wind speed distribution diagram of the airflow passing through the cross section taken along line F-F in Fig. 6. , Figure 9 is E-E of Figure 6.
FIG. 4... Flat tube, 6... Fin, 6...
...Slit piece, 6a... Leg, 6b...
...Slit part. Name of agent: Patent attorney Toshio Nakao and one other name
25! I

Claims (1)

【特許請求の範囲】[Claims] 蛇行状に屈曲した偏平管と、前記偏平管の間に波形状に
重積したフィンとを備え、前記フィン表面に前縁部が気
流と対向するスリット片を設け、かつこのスリット片の
脚部が気流方向に対してスリット片内側へ傾斜を持つこ
とを特徴とする熱交換器。
A flat tube bent in a meandering manner and a fin stacked in a wave shape between the flat tubes, a slit piece having a front edge facing the airflow is provided on the surface of the fin, and a leg portion of the slit piece is provided. A heat exchanger characterized in that the slit has an inclination toward the inside of the slit with respect to the airflow direction.
JP25147485A 1985-11-08 1985-11-08 Heat exchanger Pending JPS62112997A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP25147485A JPS62112997A (en) 1985-11-08 1985-11-08 Heat exchanger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP25147485A JPS62112997A (en) 1985-11-08 1985-11-08 Heat exchanger

Publications (1)

Publication Number Publication Date
JPS62112997A true JPS62112997A (en) 1987-05-23

Family

ID=17223350

Family Applications (1)

Application Number Title Priority Date Filing Date
JP25147485A Pending JPS62112997A (en) 1985-11-08 1985-11-08 Heat exchanger

Country Status (1)

Country Link
JP (1) JPS62112997A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009015805A1 (en) * 2007-07-31 2009-02-05 Behr Gmbh & Co. Kg Fin for a heat exchanger
JP2010025476A (en) * 2008-07-22 2010-02-04 Daikin Ind Ltd Heat exchanger
CN102032831A (en) * 2009-09-28 2011-04-27 无锡市鑫盛换热器制造有限公司 Radiating fin
EP2096397A3 (en) * 2007-10-08 2013-07-17 Behr GmbH & Co. KG Fin for a heat exchanger and manufacturing method
CN103502765A (en) * 2011-10-19 2014-01-08 松下电器产业株式会社 Heat exchanger
CN103782123A (en) * 2011-09-05 2014-05-07 夏普株式会社 Parallel flow heat exchanger and air conditioner wherein same is installed
US20190390922A1 (en) * 2018-06-25 2019-12-26 Getac Technology Corporation Enhanced heat dissipation module, cooling fin struture and stamping method thereof

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009015805A1 (en) * 2007-07-31 2009-02-05 Behr Gmbh & Co. Kg Fin for a heat exchanger
EP2096397A3 (en) * 2007-10-08 2013-07-17 Behr GmbH & Co. KG Fin for a heat exchanger and manufacturing method
JP2010025476A (en) * 2008-07-22 2010-02-04 Daikin Ind Ltd Heat exchanger
CN102032831A (en) * 2009-09-28 2011-04-27 无锡市鑫盛换热器制造有限公司 Radiating fin
CN103782123A (en) * 2011-09-05 2014-05-07 夏普株式会社 Parallel flow heat exchanger and air conditioner wherein same is installed
CN103502765A (en) * 2011-10-19 2014-01-08 松下电器产业株式会社 Heat exchanger
US20190390922A1 (en) * 2018-06-25 2019-12-26 Getac Technology Corporation Enhanced heat dissipation module, cooling fin struture and stamping method thereof
US10921066B2 (en) * 2018-06-25 2021-02-16 Getac Technology Corporation Enhanced heat dissipation module, cooling fin structure and stamping method thereof

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