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Compact air-to-air heat exchanger for jet engine application

机译:紧凑型空对空热交换器,用于喷气发动机

摘要

A structurally compact air-to-air heat exchanger, for a gas turbine engine of the fan bypass type, that permits a lower percentage of cooling air, than is presently needed in the art, to cool effectively the hot turbine, and its parts, of the engine. This goal is achieved, in part, by using a portion of the cool flow of fan air as a heat sink, without disturbing the flow of the fan air stream. The heat exchanger is disposed internal of the engine, and, it includes a plurality of flow tubes through which flows the hot cooling air, with the flow tubes positioned in a crossflow relationship with and to a portion of the cool flow of fan air. Three (3) variations of the preferred embodiment of the heat exchanger also are taught.
机译:一种结构紧凑的空对空热交换器,用于风扇旁路类型的燃气涡轮发动机,与现有技术相比,它所允许的冷却空气百分比较低,以有效地冷却热涡轮机及其零件,的引擎。该目标部分地通过将一部分风扇空气的冷流用作散热器来实现,而不会干扰风扇空气流的流动。热交换器设置在发动机内部,并且包括多个流管,使热的冷却空气流过该流管,并且流管以与风扇空气的一部分冷流成交叉关系的方式定位。还教导了热交换器的优选实施例的三(3)种变型。

著录项

  • 公开/公告号US4187675A

    专利类型

  • 公开/公告日1980-02-12

    原文格式PDF

  • 申请/专利权人 U S OF AMERICA AIR FORCE SECRETARY;

    申请/专利号US19770842139

  • 发明设计人 THOMAS G. WAKEMAN;

    申请日1977-10-14

  • 分类号F02C7/18;

  • 国家 US

  • 入库时间 2022-08-22 17:07:20

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