JPS5923981Y2 - Heat exchanger with fins - Google Patents

Heat exchanger with fins

Info

Publication number
JPS5923981Y2
JPS5923981Y2 JP1979001643U JP164379U JPS5923981Y2 JP S5923981 Y2 JPS5923981 Y2 JP S5923981Y2 JP 1979001643 U JP1979001643 U JP 1979001643U JP 164379 U JP164379 U JP 164379U JP S5923981 Y2 JPS5923981 Y2 JP S5923981Y2
Authority
JP
Japan
Prior art keywords
heat exchanger
fins
group
exchanger tubes
airflow
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
Application number
JP1979001643U
Other languages
Japanese (ja)
Other versions
JPS55105785U (en
Inventor
真 小畑
正明 安立
幸助 小松原
聡 丹野
Original Assignee
松下電器産業株式会社
松下冷機株式会社
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 松下電器産業株式会社, 松下冷機株式会社 filed Critical 松下電器産業株式会社
Priority to JP1979001643U priority Critical patent/JPS5923981Y2/en
Publication of JPS55105785U publication Critical patent/JPS55105785U/ja
Application granted granted Critical
Publication of JPS5923981Y2 publication Critical patent/JPS5923981Y2/en
Expired legal-status Critical Current

Links

Description

【考案の詳細な説明】 近年、空調機器の低騒音化に伴なって熱交換器の前面風
速を1m/s以下にする設計傾向が強まっており、この
ような低風速域における熱交換器の性能向上が課題とな
っている。
[Detailed description of the idea] In recent years, with the reduction in noise from air conditioning equipment, there has been a growing trend to design heat exchangers with front wind speeds of 1 m/s or less. Improving performance is an issue.

本考案は上記のような要望にかなう熱交換器の構成を提
示するものであり、特に伝熱管後流の死水域をフィン形
状によって減少させ、空気側伝熱面における熱伝達率の
著しい向上を図るものである。
The present invention proposes a structure of a heat exchanger that satisfies the above-mentioned demands.In particular, the dead area downstream of the heat transfer tubes is reduced by the fin shape, and the heat transfer coefficient on the air side heat transfer surface is significantly improved. This is what we aim to do.

従来、この種の熱交換器は、第1図aに示すように、一
定間隔で平行に並べられた平板フィン群1とこのフィン
群1に直角に挿入された管群2から構成され、空気はフ
ィン1′間を白ぬき矢印方向に流動して管2′内流体と
熱交換を行う。
Conventionally, this type of heat exchanger, as shown in FIG. The fluid flows between the fins 1' in the direction of the white arrow and exchanges heat with the fluid in the tube 2'.

そして、フィン1′間の管2′まわりの熱流体特性は、
第1図すに示すように、管2′に白ぬき矢印方向の低風
速気流が流動する場合、管表面のよどみ点がらの角度θ
が70〜80°で流れが剥離し、前後流部に斜線で示す
死水域3が生じ、そのために、この死水域での空気側熱
伝達率が著しく低下するので、熱交換器としての伝熱性
能が低いという欠点を有していた。
The thermal fluid characteristics around the tube 2' between the fins 1' are:
As shown in Figure 1, when a low wind velocity airflow flows through the pipe 2' in the direction of the white arrow, the angle θ from the stagnation point on the pipe surface
The flow separates between 70 and 80°, creating a dead area 3 shown by diagonal lines in the front and downstream parts.As a result, the air side heat transfer coefficient in this dead area decreases significantly, so it is difficult to conduct heat as a heat exchanger. It had the disadvantage of low performance.

本考案は、以上のような問題点を考察し、これを解決し
たものである。
The present invention has been developed by considering the above-mentioned problems and solving them.

以下本考案の一実施例を第2図a、l)により詳細な説
明を行う。
Hereinafter, one embodiment of the present invention will be explained in detail with reference to FIGS. 2a and 2).

第2図aは本考案の一実施例を示すフィン付熱交換器の
断面図であり、フィン4に一定間隔でバアーリングされ
たフィンカラ一部4aに伝熱管5が挿入されており、そ
して、気流に沿い伝熱管5の一部周囲のフィン4には、
低風速域において伝熱管5まわりに理想的な流線の形状
を実現すると同時に気流の剥離を防止する波形状の整流
溝6を設けている。
FIG. 2a is a cross-sectional view of a finned heat exchanger showing an embodiment of the present invention, in which heat transfer tubes 5 are inserted into fin collar portions 4a that are barred at regular intervals on the fins 4, and the airflow The fins 4 partially surrounding the heat exchanger tubes 5 along the
Wave-shaped rectifying grooves 6 are provided around the heat exchanger tubes 5 in a low wind speed region to realize an ideal streamline shape and at the same time prevent separation of airflow.

そして相隣る段方向の前記伝熱管間でかつ相隣る整流溝
が近接した位置でフィン上に整流溝と同一方向に突出す
る突起7を設けている。
A protrusion 7 protruding in the same direction as the rectifying groove is provided on the fin at a position between the heat exchanger tubes in the direction of adjacent stages and adjacent to the rectifying groove.

第2図すは第2図aのA−A’線における断面図であり
、波形状の整流溝6.突起7の断面形状を示している。
FIG. 2 is a sectional view taken along line AA' in FIG. 2a, and shows the wave-shaped rectifying groove 6. The cross-sectional shape of the protrusion 7 is shown.

そして、フィン4と伝熱管5から構成されるフィン付熱
交換器に白ぬき矢印方向に気流が流動すると、伝熱管5
まわりの熱流体特性は、つぎのようになる。
When the airflow flows in the direction of the white arrow in the finned heat exchanger composed of the fins 4 and the heat exchanger tubes 5, the heat exchanger tubes 5
The surrounding thermal fluid characteristics are as follows.

すなわち、空気は相隣る段方向の前記伝熱管5間でかつ
相隣る整流溝6が近接した位置を通過する時最も速度が
大きくなる。
That is, the speed of air is highest when it passes between the heat exchanger tubes 5 in the direction of adjacent stages and through a position where adjacent rectifying grooves 6 are close to each other.

そしてその位置で整流溝と同一方向に突出した突起7に
衝突するため、渦流が生じる。
At that position, it collides with the protrusion 7 that protrudes in the same direction as the rectifying groove, so that a vortex is generated.

しかも、生じた渦流は近接して同一方向に突出している
整流溝に沿うように流れを規制されるため、より活性化
される。
Furthermore, the generated eddy current is regulated to flow along the rectifying grooves protruding in the same direction in close proximity, so that it is further activated.

その結果フィン表面および伝熱管表面の境界層の厚さが
薄くなり、流体とフィン表面および伝熱管表面との熱伝
達率が著しく向上する。
As a result, the thickness of the boundary layer on the fin surface and the heat exchanger tube surface becomes thinner, and the heat transfer coefficient between the fluid and the fin surface and the heat exchanger tube surface increases significantly.

その後伝熱管5表面のよどみ点からの角度±70〜80
°で剥離されようとした気流は伝熱管5の周囲のフィン
4にわたって設けた波形状の整流溝6により、剥離を防
止され、伝熱管5表面に沿って、流動する為に、伝熱管
5後流の死水域8は著しく減少する。
After that, the angle from the stagnation point on the surface of the heat exchanger tube 5 ±70 to 80
The airflow that was about to be separated at the temperature of The dead area 8 of the stream is significantly reduced.

したがって、突起7に衝突して発生した渦流はフィン4
表面上を流れて、フィン4表面および伝熱管5表面の境
界層の厚さを薄くして流体とフィン4および伝熱管5と
の間の熱伝達率を著しく向上させると共に気流の剥離を
防止する波形状の整流溝6によって伝熱管5後流域にお
いても死水域が著しく減少し伝熱管5と気流の熱交換が
十分行える為に熱交換器の伝熱性能が大幅に向上する。
Therefore, the vortex generated by colliding with the protrusion 7 is caused by the fin 4
The fluid flows over the surface to reduce the thickness of the boundary layer on the surfaces of the fins 4 and the heat exchanger tubes 5, significantly improving the heat transfer coefficient between the fluid and the fins 4 and the heat exchanger tubes 5, and preventing separation of airflow. The wave-shaped rectifying grooves 6 significantly reduce the dead area in the downstream region of the heat exchanger tubes 5, and sufficient heat exchange between the heat exchanger tubes 5 and the airflow can be performed, so that the heat transfer performance of the heat exchanger is greatly improved.

また、波形状の整流溝6によって、伝熱管5表面まわり
に理想的な流線の形状を実現すると共に、気流の剥離を
防止しているためにフィン4間を通過する気流の圧力損
失は小さくできる。
In addition, the wave-shaped rectifying grooves 6 create an ideal streamline shape around the surface of the heat exchanger tube 5, and prevent separation of the airflow, so the pressure loss of the airflow passing between the fins 4 is small. can.

なお、本実施例では整流溝3の断面形状は鋸歯形状であ
るが、その他の形状例えばミゾ形状であっても、同時の
効果を有することは明らかである。
In this embodiment, the cross-sectional shape of the rectifying groove 3 is a sawtooth shape, but it is clear that other shapes, such as a groove shape, can also have the same effect.

以上のように、本考案は、一定間隔で平行に並べられた
フィン群と、このフィン群に直角に挿入された伝熱管群
から構成され、この伝熱管群周囲のフィン部に波形状の
整流溝を設けると共に相隣る段方向の前記伝熱管間でか
つ相隣る整流溝が近接した位置でフィン上に整流溝と同
一方向に突出する突起を設けることにより、突起によっ
て渦流を発生せしめて、フィン表面の境界層の厚さを薄
くして流体とフィンとの間の熱伝達率を著しく大きくす
ることができるとともに、しかも気流の剥離を防止する
波形状の整流溝により管群を流れ抜ける主流、伝熱管側
への運動量変化を与えて、伝熱管後流の死水域を減少で
き、これが流体とフィンとの間の熱伝達率の向上をさら
に増大させるものであり、熱交換器としての多くの実用
上の効果を奏し得るものである。
As described above, the present invention consists of a group of fins arranged in parallel at regular intervals and a group of heat exchanger tubes inserted at right angles to the group of fins. In addition to providing grooves, protrusions protruding in the same direction as the rectifying grooves are provided on the fins at positions where adjacent rectifying grooves are close to each other between the heat exchanger tubes in the direction of adjacent stages, thereby generating a vortex flow by the protrusions. By reducing the thickness of the boundary layer on the fin surface, the heat transfer coefficient between the fluid and the fins can be significantly increased, and in addition, the wave-shaped rectifying grooves prevent the airflow from separating, allowing it to flow through the tube group. By imparting a momentum change to the mainstream and the heat transfer tube side, the dead zone downstream of the heat transfer tube can be reduced, which further increases the improvement in the heat transfer coefficient between the fluid and the fins, making it suitable for use as a heat exchanger. This can have many practical effects.

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

第1図aは従来の熱交換器の斜視図、第1図すは同伝熱
管の熱流体特性図、第2図aは本考案の一実施例を示す
フィン付熱交換器の断面図、第2図すは第2図aのA−
A’線における断面図である。 4・・・・・・フィン、5・・・・・・伝熱管、6・・
・・・・整流溝、7・・・・・・突起。
Fig. 1a is a perspective view of a conventional heat exchanger, Fig. 1 is a thermal fluid characteristic diagram of the heat exchanger tube, Fig. 2a is a sectional view of a finned heat exchanger showing an embodiment of the present invention, Figure 2 is A- in Figure 2 a.
It is a sectional view taken along the A' line. 4...fins, 5...heat exchanger tubes, 6...
... Rectifying groove, 7... Protrusion.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 一定間隔で平行に並べられたフィン群と、このフィン群
に直角に挿入された伝熱管群がら構成され、前記伝熱管
群周囲の前記フィン群に、波形状の整流溝を設けると共
に相隣る段方向の前記伝熱管間でかつ相隣る整流溝が近
接した位置でフィン上に整流溝と同一方向に突出する突
起を設けたフィン付熱交換器。
It is composed of a group of fins arranged in parallel at regular intervals and a group of heat exchanger tubes inserted at right angles to the group of fins, and a wave-shaped rectifying groove is provided in the group of fins around the group of heat exchanger tubes, and a groove is provided between adjacent stages. A heat exchanger with fins, wherein protrusions projecting in the same direction as the flow straightening grooves are provided on the fins at positions where adjacent flow straightening grooves are close to each other and between the heat exchanger tubes in the direction.
JP1979001643U 1979-01-11 1979-01-11 Heat exchanger with fins Expired JPS5923981Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1979001643U JPS5923981Y2 (en) 1979-01-11 1979-01-11 Heat exchanger with fins

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1979001643U JPS5923981Y2 (en) 1979-01-11 1979-01-11 Heat exchanger with fins

Publications (2)

Publication Number Publication Date
JPS55105785U JPS55105785U (en) 1980-07-24
JPS5923981Y2 true JPS5923981Y2 (en) 1984-07-16

Family

ID=28803972

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1979001643U Expired JPS5923981Y2 (en) 1979-01-11 1979-01-11 Heat exchanger with fins

Country Status (1)

Country Link
JP (1) JPS5923981Y2 (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5181635A (en) * 1975-01-14 1976-07-17 Tokyo Seimitsu Co Ltd Suiheiichi oyobi keishanobichoseisochi
JPS533807U (en) * 1976-06-29 1978-01-13

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5181635A (en) * 1975-01-14 1976-07-17 Tokyo Seimitsu Co Ltd Suiheiichi oyobi keishanobichoseisochi
JPS533807U (en) * 1976-06-29 1978-01-13

Also Published As

Publication number Publication date
JPS55105785U (en) 1980-07-24

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