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Heat Exchanger of a Turbomachine

机译:涡轮机的热交换器

摘要

The invention relates to a heat exchanger of an air circulation channel of a turbomachine, the heat exchanger being configured so as to have fluid to be cooled passing through it and including a plurality of fins protruding from a support surface, the heat exchanger being characterized in that each fin includes a base and a preferably continuous leading face which extends axially from the base in the air circulation direction while tapering from upstream to downstream along an axis parallel with the support surface.
机译:涡轮机的空气循环通道的热交换器技术领域本发明涉及一种涡轮机的空气循环通道的热交换器,该热交换器被构造成使得待冷却的流体流经该热交换器,并且包括从支撑表面突出的多个翅片。每个散热片包括一个基部和一个优选连续的引导面,该引导面从该基部沿空气循环方向轴向延伸,同时沿与支撑表面平行的轴从上游到下游逐渐变细。

著录项

  • 公开/公告号GB2523243B

    专利类型

  • 公开/公告日2020-03-04

    原文格式PDF

  • 申请/专利权人 SNECMA;

    申请/专利号GB20140023062

  • 发明设计人 IMANE GHAZLANE;GABRIELA PHILIPPART;

    申请日2014-12-23

  • 分类号F02C7/12;F01D25/12;

  • 国家 GB

  • 入库时间 2022-08-21 11:00:08

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