首页> 外国专利> New form of nozzle for aircraft engine combustion chambers for reduced emissions has turbulence guides in fuel channel and attached fitting with cross-piece mounted within it that provides turbulent flow of liquid within nozzle

New form of nozzle for aircraft engine combustion chambers for reduced emissions has turbulence guides in fuel channel and attached fitting with cross-piece mounted within it that provides turbulent flow of liquid within nozzle

机译：用于飞机发动机燃烧室的新型喷嘴，用于减少排放，在燃料通道中具有湍流导向装置，并在其内部安装有横档的附装配件可在喷嘴内提供液体的湍流

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摘要

The nozzle is provided for the flow of liquid fuel into the combustion chamber and has turbulence guides (3) in the fuel channel (2) and a fitting (4) attached to the nozzle housing (1) with a cross-piece (5) mounted within it that provides turbulent flow of the liquid within the nozzle.

机译：喷嘴用于使液体燃料流入燃烧室，并在燃料通道（2）中具有湍流导向装置（3），以及通过横档（5）连接到喷嘴壳体（1）的配件（4）。安装在其中的喷嘴可提供喷嘴内液体的湍流。

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公开/公告号DE102006045943A1

专利类型
公开/公告日2008-04-03

原文格式PDF
申请/专利权人 BOGUSLAJEW WJATSCHESLAW;WOLKOW IGOR;DOLMATOW ANATOLIJ;DOLMATOW DMITRIJ;SHEMANJUK PAWEL;
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申请/专利号DE20061045943
发明设计人 DOLMATOW DMITRIJ;BOGUSLAJEW WJATSCHESLAW;WOLKOW IGOR;DOLMATOW ANATOLIJ;SHEMANJUK PAWEL;
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申请日2006-09-28
分类号F23D11/38;F23R3/28;B05B1/00;
国家 DE
入库时间 2022-08-21 19:49:43

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