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INTERRUPTED FIN FOR HEAT EXCHANGER

机译:换热器插翅

摘要

The present invention involves a flat finheat exchanger configuration with a plurality oflouvers and a rib raised above the plane of thefin connecting adjacent tube collars. The raisedrib configuration enhances the heat transfercharacteristics of the fin, and allows for the useof thinner materials to lower cost withoutdiminishing performance. The exterior fin surface"scoops" and redirects air flow from the leadingedge to the trailing edge of the fin. This"scooping" effect directs the air flow over and inbetween the interrupted surfaces, thus breaking upair boundary layer around the fin. The louvers ofthe fin are oriented relative to the air flow insuch a manner that each louver in effect createsanother leading edge contributing to a higher heattransfer coefficient. Also, the location of theraised rib also enhances the heat transfer betweenthe fin and the circulated air. The fin collarsare also surrounded by a raised portion so thatone raised rib and its two adjacent raisedportions bordering the collar form a "dog bone"type shape. The leading and trailing edges areserrated to improve the structural rigidity andcreate turbulence in the air flow. Also, theleading and trailing edges are oriented at aslight angle, e.g., 12°, relative to the plane ofthe fin. The louvers are oriented at a slightlygreater angle than the leading and trailing edges,e.g., 20°-35°.
机译:本发明涉及扁平翅片带有多个百叶窗和在肋骨平面上方凸起的肋骨鳍片连接相邻的管颈。提出肋结构增强了热传递鳍片的特性,并允许使用较薄的材料以降低成本而无需性能下降。鳍片外表面“隐蔽”并重新引导来自前端的气流边缘到鳍的后缘。这个“ sco”效应可引导空气流过和流入在中断的表面之间,从而破裂散热片周围的空气边界层。百叶窗散热片相对于进气流定向每个百叶窗实际上产生的方式另一个导致热量上升的前沿转移系数。另外,凸起的肋骨也增强了之间的热传递鳍片和循环空气。鳍领也被凸起部分包围,一个凸起的肋骨和两个相邻的凸起与衣领接壤的部分形成“狗骨头”类型形状。前沿和后沿是锯齿状以提高结构刚度和在气流中产生湍流。另外,前缘和后缘的方向为相对于飞机平面的微小角度,例如12°鳍。百叶窗朝向比前缘和后缘更大的角度,例如20°-35°。

著录项

  • 公开/公告号CA2145943C

    专利类型

  • 公开/公告日1999-04-13

    原文格式PDF

  • 申请/专利号CA19952145943

  • 发明设计人 OBOSU CHARLES B.;

    申请日1995-03-30

  • 分类号F28F1/30;F28F13/12;

  • 国家 CA

  • 入库时间 2022-08-22 02:24:10

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