首页> 外国专利> Bypass jet engine i.e. counterflow engine, for use in aircraft, has front blower deflecting fresh air around specified degrees in collecting cavity of core engine, where fresh air is sucked in front of outer housing of core engine

Bypass jet engine i.e. counterflow engine, for use in aircraft, has front blower deflecting fresh air around specified degrees in collecting cavity of core engine, where fresh air is sucked in front of outer housing of core engine

机译:旁路喷气发动机,即用于飞机的逆流发动机,其前鼓风机将新鲜空气以一定程度偏转到核心发动机的收集腔中,在那里新鲜空气被吸入核心发动机外壳的前面

摘要

The engine has a core engine (1) whose outer housing (3) is formed with a cavity for a fresh air channel. Fresh air is sucked in front of the housing and drawn behind a front blower (2) and into a collecting cavity of the core engine. 180 degree deflection of the air is made by low and high pressure sections (6, 7) of a compressor and high and low pressure sections (9, 10) of a power turbine under increase of temperature by compression and energy supply in a combustion chamber (8) against flight direction of an aircraft. The blower deflects the air around 90 degrees in the collecting cavity.
机译:该发动机具有核心发动机(1),其外部壳体(3)形成有用于新鲜空气通道的腔。新鲜空气被吸入壳体的前面,并在前鼓风机(2)的后面被吸入并进入核心发动机的收集腔。空气的180度偏转是由压缩机的低压部分和高压部分(6、7)和动力涡轮的高压部分和低压部分(9、10)在燃烧室中通过压缩和能量供应而在温度升高时产生的(8)反对飞机的飞行方向。鼓风机使空气在收集腔中偏转约90度。

著录项

  • 公开/公告号DE102010022932A1

    专利类型

  • 公开/公告日2011-12-08

    原文格式PDF

  • 申请/专利权人 SEEFLUTH CHRISTIAN;

    申请/专利号DE20101022932

  • 发明设计人 ANTRAG AUF NICHTNENNUNG;

    申请日2010-06-04

  • 分类号F02K3/04;F02C3/04;

  • 国家 DE

  • 入库时间 2022-08-21 17:05:35

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