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JP4035899B2 - Gas cooler - Google Patents
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JP4035899B2 - Gas cooler - Google Patents

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Publication number
JP4035899B2
JP4035899B2 JP25151498A JP25151498A JP4035899B2 JP 4035899 B2 JP4035899 B2 JP 4035899B2 JP 25151498 A JP25151498 A JP 25151498A JP 25151498 A JP25151498 A JP 25151498A JP 4035899 B2 JP4035899 B2 JP 4035899B2
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JP
Japan
Prior art keywords
gas
heat transfer
outlet
inlet
coolant
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 - Fee Related
Application number
JP25151498A
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Japanese (ja)
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JP2000081293A (en
Inventor
和三 長谷川
浩 上藤
高志 穂刈
良行 小河
敏礼 武富
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IHI Corp
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IHI Corp
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Filing date
Publication date
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Description

【0001】
【発明の属する技術分野】
本発明は、ガスクーラに関するものである。
【0002】
【従来の技術】
ターボコンプレッサのガスクーラは、ターボ圧縮機で圧縮されて温度上昇されたガスを冷却するものであり、ターボ圧縮機の下流側に接続されている。
【0003】
図8に示すように、ガスクーラ30は、胴31の一端部にガスの入口32を設けると共に他端部にガスの出口33を設け、さらに胴31の一端面に冷却液の入口34と出口35を設け、その入口34と出口35を結んで多数の伝熱管36を胴31内に設けたものであり、伝熱管36には多数のフィン37が設けられている。
【0004】
また、胴31内には、ガス入口32から胴31内に入るガスを伝熱管36に対して直交させて流し、かつ、複数回折り返してガス出口33へ導くように流路を区画する邪魔板38,39が設けられている。
【0005】
【発明が解決しようとする課題】
ところで、図8に示すようなターボ圧縮機40とガスクーラ30を多段に接続して圧縮率を高めるようにしたターボコンプレッサの場合、レイアウト上の制約から胴31の両端に形成されるガスの出口33と入口32が段ごとに入れ替わってしまう。
【0006】
このとき、ガス出口33が冷却水入口34側の端にあるガスクーラ30は効率よくガスを冷却することができ、ガス出口33が冷却水入口34側とは反対側の端にあり、伝熱管36がガス流路を巡ってからガス出口33に至るガスクーラ41は同じフィン面積、同じ冷却水流量であってもガス出口33が冷却水入口34位置にあるガスクーラ30ほど効率よくガスを冷却することはできないという課題がある。
【0007】
そこで、本発明の目的は、上記課題を解決し、伝熱管がガス流路を巡ってからガス出口に至っても良好にガスを冷却することのできるガスクーラを提供することにある。
【0008】
【課題を解決するための手段】
上記目的を達成するために本発明は、胴の一端部にガスの入口を、他端部にガスの出口を設け、さらに胴の一端面に冷却液の入口と出口を設け、その入口と出口とを結んで胴内に多数の伝熱管を設けたガスクーラにおいて、上記胴内に、複数の邪魔板を設けて、上記ガス入口から上記ガス出口に至るガスが伝熱管に対して直交してから折り返すよう折り返し流路を形成し、その各折り返し流路の冷却液出口側伝熱管とガス出口側折り返し流路の冷却液入口側伝熱管に多数のフィンを設け、ガス入口側折り返し流路の冷却液入口側伝熱管にフィンを取り付けないようにしたものである。
【0009】
【発明の実施の形態】
本発明の好適実施の形態を添付図面に基づいて詳述する。
【0010】
図1、図2、図3及び図4に示すように、ガスクーラ1は、胴2と、胴2内に設けられた多数の伝熱管3と、伝熱管3に設けられた多数のフィン4とからなる。
【0011】
胴2は、一端側の側面(一端部)にガスの入口5を有し、他端側の側面(他端部)にガスの出口6を有する。
【0012】
また、胴2の一端側の端面(以下、一端面という)には伝熱管3に流す冷却液たる冷却水の入口7と出口8とが形成されている。具体的には、冷却液出口8はガス入口5に近接する位置に配されており、冷却液入口7は、冷却液出口8のガス流下流側に配されている。
【0013】
冷却液の入口7と出口8は、一端面上に互いに隣接して形成されており、図5に示すように、胴2の一端側には冷却液入口7から流入する冷却液を一旦溜める入口側ヘッド9が設けられると共に、伝熱管3を流れてガスクーラ1外に流出させる冷却液を一旦溜める出口側ヘッド10が設けられている。
【0014】
各伝熱管3は、銅製のチューブからなり、略U字状に形成されている。それぞれの伝熱管3は、一端を入口側ヘッド9に接続されると共に他端を出口側ヘッド10に接続されており、入口側ヘッド9に流入された冷却液を多数の伝熱管3中に分岐して流入させたのち、出口側ヘッド10内に流して合流させるようになっている。
【0015】
また、特に伝熱管3は、ガス入口5とガス出口6の近傍まで設けられており、後述するガス出入口5,6近傍まで延長されるフィン4を冷却するようになっている。
【0016】
胴2内には、ガス入口5からガス出口6に至るガスが伝熱管3に対して直交してから折り返すよう折り返し流路を区画形成し、ガスの流速を増加させるための邪魔板11,12が2枚設けられている。
【0017】
具体的には、邪魔板11,12は、ガス入口5の胴2中央側から伝熱管3に対して直交して延びる第1邪魔板11と、ガス出口6の胴2中央側から伝熱管3に対して直交して延びる第2邪魔板12とからなる。第1邪魔板11と第2邪魔板12は、互いに反対方向に延びており、邪魔板11,12先端と胴2内面との間にガスを流す折り返し部13,14を形成している。
【0018】
そして、胴2内に、ガス入口5から入って伝熱管3に対して直交するガス入口側折り返し流路15と、第1邪魔板11を挟んで折り返される中央折り返し流路16と、第2邪魔板12を挟んで再度折り返されガス出口6に接続されるガス出口側折り返し流路17とからなる折り返し流路18を形成するようになっている。
【0019】
フィン4は、冷却液出口8に接続される直線状の冷却液出口側(復路側)伝熱管19と、冷却液入口7に接続される直線状の冷却液入口側(往路側)伝熱管20のうちガス出口側折り返し流路17を横断する出口横断部21とにのみ多数設けられており、出口横断部21の冷却液入口7側には設けられていない。
【0020】
また、フィン4はガス入口側折り返し流路15にあってはガス入口5近傍まで延長するように折り返し流路18の折り返し部13,14のフィン4より大きく形成されており、ガス出口側折り返し流路17にあってはガス出口6近傍まで延長するように折り返し部13,14のフィン4より大きく形成されている。そして、伝熱管3の出口横断部21の冷却液入口7側にフィン4を設けた場合とフィン面積を同等にするようになっている。
【0021】
フィン4は、それぞれ伝熱管3の外周に略等間隔にかしめて固定されている。
【0022】
次に作用を述べる。
【0023】
冷却液入口7から冷却液を流し、ガス入口5から冷却すべきガスを流入させると、冷却液は入口側ヘッド9内に流入し、入口側ヘッド9から各伝熱管3内に分岐されて流れる。そして、冷却液は、冷却液入口側伝熱管20内を流れてガス入口側折り返し流路15と中央折り返し流路16とを横断し、ガス出口側折り返し流路17の出口横断部21に流れる。
【0024】
このとき、冷却液入口側伝熱管20にはガス出口側折り返し流路17の出口横断部21に至るまでフィン4は設けられていないため、ガス入口側折り返し流路15と中央折り返し流路16では熱交換は行われず、冷却液は冷えたままの状態で出口横断部21に至り、出口横断部21に設けられたフィン4で始めてガスと熱交換される。
【0025】
そして、冷却液は冷却液出口側伝熱管19内へ流れ、ガス出口側折り返し流路17、中央折り返し流路16、ガス入口側折り返し流路15の順に横断して出口側ヘッド10内に流れて合流される。
【0026】
ガスは、ガス入口5から胴2内に流入し、ガス入口側折り返し流路15を伝熱管3と直交するようにして流れる。このとき、ガス入口5近傍の冷却液出口側伝熱管19内を流れる冷却液は冷却液出口近傍の比較的温まった冷却液であるが、フィン4はガス入口5近傍まで延びて大きく、かつ、熱交換するガスも胴2内で最も温度の高い最上流のガスであるため良好に熱交換される。
【0027】
そして、冷却液入口側伝熱管20と交差して折り返し、中央折り返し流路16へ流れて再度冷却液入口側伝熱管20と交差する。このとき、冷却液入口側伝熱管20にはフィン4が設けられておらず、冷却液入口側伝熱管20の表面積もフィン4の表面積と比較すると微々たるものであるため、冷却液−ガス間の熱交換はほとんど行われず、冷却液は暖められない。
【0028】
その後、ガスは、冷却液出口側伝熱管19と交差して折り返し、ガス出口側折り返し流路17へ流れて再度冷却液出口側伝熱管19と交差する。このとき、冷却液出口側伝熱管19にはフィン4が設けられており、ガスは中央折り返し流路16で冷却液出口側伝熱管19と熱交換をして冷却されたあと、ガス出口側折り返し流路17で冷却液出口側伝熱管19と熱交換をしてさらに冷却される。ガスは、冷却液下流で熱交換をしたあと上流へ移って熱交換するため効率よく良好に熱交換される。
【0029】
そして、ガスはガス出口6へ向かって流れ、冷却液入口側伝熱管20と交差して最後の熱交換をしたあとガス出口6から流出される。このとき、冷却液入口側伝熱管20内の冷却液は、冷却液入口7から流入されたときとほとんど変わらない低い温度であるため、ガスと冷却液との温度差は大きく、また、フィン4が折り返し部13,14よりも大きく形成されているため、ガスは流入時の冷却液温近くまで冷却される。
【0030】
このように、冷却液出口側伝熱管19とガス出口側折り返し流路17の冷却液入口側伝熱管20に多数のフィン4を設け、ガス入口側折り返し流路15の冷却液入口側伝熱管20にフィン4を取り付けないようにしたため、ガス出口6に冷たい冷却液を流すことができ、ガス出口6でガスと冷却液の温度差を大きくすることにより、図6に示すように、結果としてガスを効率よく良好に冷却することができる。
【0031】
なお、伝熱管3はU字状のものに限るものではなく、図8に示すように、直線状としてもよい。この場合、胴2の他端側に水室22を形成し、伝熱管を入口側ヘッド9と水室22を接続する往路側伝熱管(冷却液入口側伝熱管)23と、水室22と出口側ヘッド10を接続する復路側伝熱管(冷却液出口側伝熱管)24とからなるものとするとよい。
【0032】
【発明の効果】
以上要するに本発明によれば、伝熱管がガス流路を巡ってからガス出口に至っても良好にガスを冷却することができる。
【図面の簡単な説明】
【図1】本発明の好適実施の形態を示すガスクーラの平面図である。
【図2】図1のII−II線矢視図である。
【図3】図1の側面図である。
【図4】図1のIV−IV線矢視図である。
【図5】ガスクーラの概略使用説明図である。
【図6】ガスクーラの性能比較を表すグラフである。
【図7】他の実施の形態のガスクーラの平面図である。
【図8】従来のガスクーラの使用状態を示す概略使用説明図である。
【符号の説明】
1 ガスクーラ
2 胴
3 伝熱管
4 フィン
5 ガス入口
6 ガス出口
7 冷却液入口
8 冷却液出口
11 邪魔板
12 邪魔板
15 ガス入口側折り返し流路
17 ガス出口側折り返し流路
18 折り返し流路
19 冷却液出口側伝熱管
20 冷却液入口側伝熱管
[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a gas cooler.
[0002]
[Prior art]
The gas cooler of the turbo compressor cools the gas whose temperature has been increased by being compressed by the turbo compressor, and is connected to the downstream side of the turbo compressor.
[0003]
As shown in FIG. 8, the gas cooler 30 is provided with a gas inlet 32 at one end of a cylinder 31, a gas outlet 33 at the other end, and a coolant inlet 34 and outlet 35 at one end of the cylinder 31. And a large number of heat transfer tubes 36 are provided in the body 31 by connecting the inlet 34 and the outlet 35 thereof, and the heat transfer tubes 36 are provided with a number of fins 37.
[0004]
Further, a baffle plate that divides the flow path in the cylinder 31 so that the gas entering the cylinder 31 from the gas inlet 32 flows perpendicularly to the heat transfer tube 36 and is led back to the gas outlet 33 by being bent a plurality of times. 38 and 39 are provided.
[0005]
[Problems to be solved by the invention]
By the way, in the case of a turbo compressor in which the turbo compressor 40 and the gas cooler 30 as shown in FIG. 8 are connected in multiple stages so as to increase the compression rate, gas outlets 33 formed at both ends of the cylinder 31 due to layout restrictions. And the entrance 32 is changed for each stage.
[0006]
At this time, the gas cooler 30 with the gas outlet 33 at the end on the cooling water inlet 34 side can efficiently cool the gas, and the gas outlet 33 is at the end on the opposite side to the cooling water inlet 34 side, so The gas cooler 41 from the gas flow path to the gas outlet 33 can cool the gas as efficiently as the gas cooler 30 in which the gas outlet 33 is located at the cooling water inlet 34 position even if the same fin area and the same cooling water flow rate are used. There is a problem that you can not.
[0007]
Accordingly, an object of the present invention is to provide a gas cooler that can solve the above-mentioned problems and can cool the gas satisfactorily even if the heat transfer tube goes around the gas flow path and reaches the gas outlet.
[0008]
[Means for Solving the Problems]
In order to achieve the above object, the present invention provides a gas inlet at one end of a cylinder, a gas outlet at the other end, and an inlet and outlet for cooling liquid at one end of the cylinder. In the gas cooler in which a large number of heat transfer tubes are provided in the cylinder, a plurality of baffle plates are provided in the cylinder, and the gas from the gas inlet to the gas outlet is orthogonal to the heat transfer tube. A folded flow path is formed so as to be folded, and a large number of fins are provided in the cooling liquid outlet side heat transfer tubes of the respective folded flow paths and the cooling liquid inlet side heat transfer tubes of the gas outlet side folded flow paths to cool the gas inlet side folded flow paths. The fin is not attached to the liquid inlet side heat transfer tube.
[0009]
DETAILED DESCRIPTION OF THE INVENTION
Preferred embodiments of the present invention will be described in detail with reference to the accompanying drawings.
[0010]
As shown in FIGS. 1, 2, 3, and 4, the gas cooler 1 includes a body 2, a number of heat transfer tubes 3 provided in the body 2, and a number of fins 4 provided in the heat transfer tubes 3. Consists of.
[0011]
The body 2 has a gas inlet 5 on one side surface (one end) and a gas outlet 6 on the other side surface (other end).
[0012]
In addition, an inlet 7 and an outlet 8 of cooling water, which is a coolant flowing through the heat transfer tube 3, are formed on one end face (hereinafter referred to as one end face) of the body 2. Specifically, the coolant outlet 8 is disposed at a position close to the gas inlet 5, and the coolant inlet 7 is disposed on the gas flow downstream side of the coolant outlet 8.
[0013]
The coolant inlet 7 and the outlet 8 are formed adjacent to each other on one end face, and as shown in FIG. 5, at one end of the body 2, an inlet for temporarily storing the coolant flowing in from the coolant inlet 7. A side head 9 is provided, and an outlet side head 10 for temporarily storing a coolant that flows through the heat transfer tube 3 and flows out of the gas cooler 1 is provided.
[0014]
Each heat transfer tube 3 is made of a copper tube and is formed in a substantially U shape. Each heat transfer tube 3 has one end connected to the inlet side head 9 and the other end connected to the outlet side head 10. The coolant flowing into the inlet side head 9 is branched into a large number of heat transfer tubes 3. Then, it flows into the outlet-side head 10 and joins.
[0015]
In particular, the heat transfer tube 3 is provided up to the vicinity of the gas inlet 5 and the gas outlet 6 and cools the fins 4 extended to the vicinity of gas inlets 5 and 6 described later.
[0016]
A baffle flow path is defined in the cylinder 2 so that the gas from the gas inlet 5 to the gas outlet 6 is folded after being orthogonal to the heat transfer tube 3, and baffles 11 and 12 for increasing the gas flow rate. Are provided.
[0017]
Specifically, the baffle plates 11 and 12 include a first baffle plate 11 extending perpendicularly to the heat transfer tube 3 from the center side of the body 2 of the gas inlet 5, and the heat transfer tube 3 from the center side of the body 2 of the gas outlet 6. The second baffle plate 12 extends perpendicularly to the second baffle plate 12. The first baffle plate 11 and the second baffle plate 12 extend in directions opposite to each other, and folding portions 13 and 14 for flowing gas are formed between the front ends of the baffle plates 11 and 12 and the inner surface of the body 2.
[0018]
Then, a gas inlet-side folded flow path 15 that enters the barrel 2 through the gas inlet 5 and is orthogonal to the heat transfer tube 3, a central folded flow path 16 that is folded with the first baffle plate 11 interposed therebetween, and a second baffle A folded channel 18 including a gas outlet side folded channel 17 that is folded again and is connected to the gas outlet 6 with the plate 12 interposed therebetween is formed.
[0019]
The fin 4 includes a linear coolant outlet side (return path side) heat transfer tube 19 connected to the coolant outlet 8 and a linear coolant inlet side (outward side) heat transfer tube 20 connected to the coolant inlet 7. Among them, a large number of them are provided only at the outlet crossing portion 21 that crosses the gas outlet side folded flow path 17, and are not provided at the coolant inlet 7 side of the outlet crossing portion 21.
[0020]
Further, the fin 4 is formed to be larger than the fin 4 of the folded portions 13 and 14 of the folded flow path 18 so as to extend to the vicinity of the gas inlet 5 in the gas inlet-side folded flow path 15. The passage 17 is formed larger than the fins 4 of the folded portions 13 and 14 so as to extend to the vicinity of the gas outlet 6. And the fin area is made equal to the case where the fin 4 is provided on the coolant inlet 7 side of the outlet crossing portion 21 of the heat transfer tube 3.
[0021]
The fins 4 are caulked and fixed to the outer periphery of the heat transfer tube 3 at substantially equal intervals.
[0022]
Next, the operation will be described.
[0023]
When a coolant is supplied from the coolant inlet 7 and a gas to be cooled is supplied from the gas inlet 5, the coolant flows into the inlet head 9 and branches from the inlet head 9 into the heat transfer tubes 3 to flow. . Then, the coolant flows through the coolant inlet side heat transfer tube 20, crosses the gas inlet side return channel 15 and the center return channel 16, and flows to the outlet crossing portion 21 of the gas outlet side return channel 17.
[0024]
At this time, since the fin 4 is not provided in the coolant inlet side heat transfer tube 20 up to the outlet crossing portion 21 of the gas outlet side folded channel 17, the gas inlet side folded channel 15 and the central folded channel 16 No heat exchange is performed, and the coolant reaches the outlet crossing portion 21 in a state of being cooled, and heat exchange with the gas starts at the fins 4 provided on the outlet crossing portion 21.
[0025]
Then, the coolant flows into the coolant outlet side heat transfer tube 19 and flows into the outlet side head 10 across the gas outlet side folded channel 17, the central folded channel 16, and the gas inlet side folded channel 15 in this order. Merged.
[0026]
The gas flows into the body 2 from the gas inlet 5 and flows through the gas inlet-side folded flow path 15 so as to be orthogonal to the heat transfer tube 3. At this time, the coolant flowing in the coolant outlet side heat transfer pipe 19 near the gas inlet 5 is a relatively warm coolant near the coolant outlet, but the fin 4 extends to the vicinity of the gas inlet 5 and is large, and The heat exchange gas is also the most upstream gas having the highest temperature in the cylinder 2, so that the heat exchange is performed well.
[0027]
Then, it intersects with the coolant inlet side heat transfer tube 20 and turns back, flows into the center return passage 16 and again intersects with the coolant inlet side heat transfer tube 20. At this time, the fin 4 is not provided in the cooling liquid inlet side heat transfer tube 20, and the surface area of the cooling liquid inlet side heat transfer tube 20 is slightly smaller than the surface area of the fin 4. The heat exchange is hardly performed and the coolant is not warmed.
[0028]
Thereafter, the gas crosses over the coolant outlet side heat transfer tube 19 and turns back, flows into the gas outlet side return flow passage 17 and crosses the coolant outlet side heat transfer tube 19 again. At this time, the cooling liquid outlet side heat transfer tubes 19 are provided with fins 4, and the gas is cooled by exchanging heat with the cooling liquid outlet side heat transfer tubes 19 in the central return flow path 16, and then turned back on the gas outlet side. Heat is exchanged with the coolant outlet side heat transfer tube 19 in the flow path 17 for further cooling. Since the gas exchanges heat downstream of the coolant and then moves upstream to exchange heat, the gas is efficiently and well exchanged.
[0029]
Then, the gas flows toward the gas outlet 6, crosses the coolant inlet side heat transfer tube 20, and flows out from the gas outlet 6 after the final heat exchange. At this time, the coolant in the coolant inlet side heat transfer tube 20 has a low temperature that is almost the same as that when it flows in from the coolant inlet 7, so that the temperature difference between the gas and the coolant is large, and the fin 4 Is formed larger than the folded portions 13 and 14, the gas is cooled to near the coolant temperature at the time of inflow.
[0030]
As described above, the cooling liquid outlet side heat transfer tube 19 and the cooling liquid inlet side heat transfer tube 20 of the gas outlet side folded flow channel 17 are provided with a large number of fins 4, and the cooling liquid inlet side heat transfer tube 20 of the gas inlet side folded flow channel 15 is provided. Since the fin 4 is not attached to the gas outlet 6, it is possible to allow a cold coolant to flow through the gas outlet 6. By increasing the temperature difference between the gas and the coolant at the gas outlet 6, as shown in FIG. Can be efficiently and satisfactorily cooled.
[0031]
The heat transfer tube 3 is not limited to a U-shape, and may be linear as shown in FIG. In this case, a water chamber 22 is formed on the other end of the body 2, a heat transfer tube is connected to the head 9 on the inlet side and the water chamber 22, a forward heat transfer tube (coolant inlet side heat transfer tube) 23, It is good to consist of the return side heat exchanger tube (coolant outlet side heat exchanger tube) 24 which connects the outlet side head 10.
[0032]
【The invention's effect】
In short, according to the present invention, it is possible to cool the gas satisfactorily even if the heat transfer tube goes around the gas flow path and reaches the gas outlet.
[Brief description of the drawings]
FIG. 1 is a plan view of a gas cooler showing a preferred embodiment of the present invention.
2 is a view taken along the line II-II in FIG.
FIG. 3 is a side view of FIG. 1;
4 is a view taken in the direction of arrows IV-IV in FIG. 1;
FIG. 5 is a schematic illustration of the use of a gas cooler.
FIG. 6 is a graph showing a performance comparison of gas coolers.
FIG. 7 is a plan view of a gas cooler according to another embodiment.
FIG. 8 is a schematic explanatory diagram showing a usage state of a conventional gas cooler.
[Explanation of symbols]
1 Gas cooler 2 Body 3 Heat transfer tube 4 Fin 5 Gas inlet 6 Gas outlet 7 Coolant inlet 8 Coolant outlet 11 Baffle plate 12 Baffle plate 15 Gas inlet side folded flow path 17 Gas outlet side folded flow path 18 Folded flow path 19 Cooling liquid Outlet side heat transfer tube 20 Coolant inlet side heat transfer tube

Claims (1)

胴の一端部にガスの入口を、他端部にガスの出口を設け、さらに胴の一端面に冷却液の入口と出口を設け、その入口と出口とを結んで胴内に多数の伝熱管を設けたガスクーラにおいて、上記胴内に、複数の邪魔板を設けて、上記ガス入口から上記ガス出口に至るガスが伝熱管に対して直交してから折り返すよう折り返し流路を形成し、その各折り返し流路の冷却液出口側伝熱管とガス出口側折り返し流路の冷却液入口側伝熱管に多数のフィンを設け、ガス入口側折り返し流路の冷却液入口側伝熱管にフィンを取り付けないようにしたことを特徴とするガスクーラ。A gas inlet is provided at one end of the cylinder, a gas outlet is provided at the other end, a cooling liquid inlet and outlet are provided at one end of the cylinder, and a number of heat transfer tubes are connected to the cylinder by connecting the inlet and the outlet. In the gas cooler, a plurality of baffle plates are provided in the cylinder, and a folding flow path is formed so that the gas from the gas inlet to the gas outlet is folded after being orthogonal to the heat transfer tube. Provide a large number of fins on the coolant outlet side heat transfer tube of the return channel and the coolant inlet side heat transfer tube of the gas outlet side return channel, and do not attach the fins to the coolant inlet side heat transfer tube of the gas inlet side return channel A gas cooler characterized by that.
JP25151498A 1998-09-04 1998-09-04 Gas cooler Expired - Fee Related JP4035899B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP25151498A JP4035899B2 (en) 1998-09-04 1998-09-04 Gas cooler

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP25151498A JP4035899B2 (en) 1998-09-04 1998-09-04 Gas cooler

Publications (2)

Publication Number Publication Date
JP2000081293A JP2000081293A (en) 2000-03-21
JP4035899B2 true JP4035899B2 (en) 2008-01-23

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Family Applications (1)

Application Number Title Priority Date Filing Date
JP25151498A Expired - Fee Related JP4035899B2 (en) 1998-09-04 1998-09-04 Gas cooler

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Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006145092A (en) * 2004-11-17 2006-06-08 Max Co Ltd Air conditioning system and building
FR2978538B1 (en) * 2011-07-25 2015-06-19 Valeo Systemes Thermiques HEAT EXCHANGER PLATE.
CN202734605U (en) * 2012-07-18 2013-02-13 汉纬尔机械(上海)有限公司 Air-cooling cooler
CN104180704B (en) * 2014-07-25 2016-01-20 山东旺泰机械科技有限公司 Baffling assembly and welded type plate type heat exchanger

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