首页> 外国专利> APPARATUS FOR INCREASING THE HEAT TRANSFER TO THE APPARATUS FOR INCREASING THE HEAT TRANSFER TO THE COOLANT ON THE INSIDE OF A NOZZLE WALL OF EXPANDERCOOLANT ON THE INSIDE OF A NOZZLE WALL OF EXPANDER CYCLE ROCKET ENGINES CYCLE ROCKET ENGINES

APPARATUS FOR INCREASING THE HEAT TRANSFER TO THE APPARATUS FOR INCREASING THE HEAT TRANSFER TO THE COOLANT ON THE INSIDE OF A NOZZLE WALL OF EXPANDERCOOLANT ON THE INSIDE OF A NOZZLE WALL OF EXPANDER CYCLE ROCKET ENGINES CYCLE ROCKET ENGINES

机译:在膨胀剂循环火箭发动机的喷嘴壁内的膨胀剂的喷嘴壁内,将热量增加到冷却剂的传递的装置

摘要

The invention relates to an apparatus for increasing the heat transfer to the coolant on the inside of a nozzle wall provided with coolant channels of expander cycle rocket engines. To achieve this the invention proposes that, to disturb the boundarylayer at the nozzle wall and thereby increasing the beat transfer, the inside of the nozzle wall feeing the flame has a particularly chosen increased surface roughness of such a magnitude that it penetrates the viscous sub-layer of the boundary layer at the nozzle wall.
机译:本发明涉及一种用于增加到喷嘴壁内侧上的冷却剂的热传递的设备,该喷嘴壁设有膨胀循环火箭发动机的冷却剂通道。为了达到这一目的,本发明提出,为了扰动喷嘴壁处的边界层并由此增加节拍传递,对火焰进行火焰作用的喷嘴壁内部具有特别选择的增大的表面粗糙度,其程度使其可以穿透粘性的亚表面。喷嘴壁上边界层的一层。

著录项

  • 公开/公告号UA70364C2

    专利类型

  • 公开/公告日2002-02-15

    原文格式PDF

  • 申请/专利权人 VOLVO AERO CORPORATION VOLVO AERO CORPORATION;

    申请/专利号UA20010117853

  • 发明设计人

    申请日2001-03-16

  • 分类号F02K9/97;

  • 国家 UA

  • 入库时间 2022-08-22 00:43:26

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