首页> 外国专利> AIR INLET FOR AN AIRCRAFT TURBINE ENGINE, AN AIRCRAFT PROVIDED WITH SUCH AN AIR INLET, AND A METHOD OF OPTIMIZING THE OPERATION OF AN AIRCRAFT TURBINE ENGINE WITH THE HELP OF AN AIR INLET

AIR INLET FOR AN AIRCRAFT TURBINE ENGINE, AN AIRCRAFT PROVIDED WITH SUCH AN AIR INLET, AND A METHOD OF OPTIMIZING THE OPERATION OF AN AIRCRAFT TURBINE ENGINE WITH THE HELP OF AN AIR INLET

机译：飞机涡轮发动机的进气口，带有这种进气口的飞机以及一种通过进气口帮助优化涡轮发动机的工作方法

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摘要

The present invention relates to an air inlet (10) for a turbine engine (2) of an aircraft (1), the air inlet comprising an air delivery duct (20) defined by a side wall (21) and extended by a dynamic inlet duct (30), said dynamic inlet duct (30) extending along a dynamic axis (AX1) towards a front flow section (31), said dynamic inlet duct (30) being provided with a grid (40) for protection against ingesting foreign bodies. The grid (40) is suitable for moving in translation along said dynamic axis (AX1) relative to said front flow section (31), and said air inlet (10) includes at least one lateral inlet (50) arranged in said side wall (21) and cover means (41) for covering said lateral inlet (50) that are movable relative to said lateral inlet (50), said air inlet (10) including movement means (60) controlled by said movement in translation of the grid (40) to request movement of said cover means (41) relative to said lateral inlet (50).

机译：用于飞机（ 1 ）的涡轮发动机（ 2 ）的进气口（ 10 ），该进气口包括由侧壁（ 21 ）限定并由动态进气管（ 30 ）延伸的空气输送管（ 20 ），所述动态进气管沿动态轴（AX 1 ）朝向前流段（ 31 ）延伸的管道（ 30 ），所述动态入口管道（ 30 ）带有一个网格（ 40 ），以防止异物进入。网格（ 40 ）适用于相对于所述前流段（ 31 ）沿所述动态轴（AX 1 ）平移，所述进气口（ 10 ）包括布置在所述侧壁（ 21 ）中的至少一个横向进气口（ 50 ）和盖装置（< B> 41 ）以覆盖相对于所述侧向入口（ 50 ）可移动的所述侧向入口（ 50 ），所述空气入口（ 10 ）包括受网格平移（ 40 ）的所述移动控制的移动装置（ 60 ），以请求所述覆盖装置（ 41 < / B>）相对于所述横向入口（ 50 ）。 展开▼

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公开/公告号US2011108676A1

专利类型

公开/公告日2011-05-12

原文格式PDF

申请/专利权人 MARC COLAPRISCO;VICTOR GERIN-ROZE;
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申请/专利号US20100941467

发明设计人 MARC COLAPRISCO;VICTOR GERIN-ROZE;
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申请日2010-11-08

分类号B64D33/02;

国家 US

入库时间 2022-08-21 18:16:26

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机译：飞机涡轮发动机的进气口，装有这种进气口的飞机，以及通过进气口优化飞机涡轮发动机的操作的过程

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机译：飞机涡轮发动机的进气口，装有这种进气口的飞机，以及通过进气口优化飞机涡轮发动机的操作的过程

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