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US08439297B2 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 有权
用于飞行器涡轮发动机的空气入口，具有这种空气入口的飞行器，以及在空气入口的帮助下优化飞机涡轮发动机的操作的方法

  • Patent Title: 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
  • Patent Title (中): 用于飞行器涡轮发动机的空气入口，具有这种空气入口的飞行器，以及在空气入口的帮助下优化飞机涡轮发动机的操作的方法
  • Application No.: US12941467
    Application Date: 2010-11-08
  • Publication No.: US08439297B2
    Publication Date: 2013-05-14
  • Inventor: Marc Colaprisco , Victor Gerin-Roze
  • Applicant: Marc Colaprisco , Victor Gerin-Roze
  • Applicant Address: FR Marignane Cedex
  • Assignee: Eurocopter
  • Current Assignee: Eurocopter
  • Current Assignee Address: FR Marignane Cedex
  • Agency: Brooks Kushman P.C.
  • Priority: FR0905435 20091112
  • Main IPC: B64D33/02
  • IPC: B64D33/02
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
Abstract:
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).
Abstract(Chinese):

本发明涉及一种用于飞机（1）的涡轮发动机（2）的空气入口（10），空气入口包括由侧壁（21）限定并由动力入口延伸的空气输送管道（20） （30），所述动态入口管道（30）沿着动态轴线（AX1）朝着前部流动部分（31）延伸，所述动力入口管道（30）设置有格栅（40），用于防止吸收异物 。 格栅（40）适于沿所述动态轴线（AX1）相对于所述前部流动部分（31）平移移动，并且所述空气入口（10）包括布置在所述侧壁中的至少一个侧向入口（50） 21）和用于覆盖相对于所述侧向入口（50）可移动的所述侧向入口（50）的盖装置（41），所述进气口（10）包括由所述网格平移中的所述运动控制的运动装置（60） 40）以请求所述盖装置（41）相对于所述侧向入口（50）的移动。

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