首页> 外国专利> Defrosting procedure forced-fluid, the air inlet cover of a jet engine and device for its practice.

Defrosting procedure forced-fluid, the air inlet cover of a jet engine and device for its practice.

机译:除霜程序为强制流体,喷气发动机的进气口盖及其实施装置。

摘要

Defrost procedure housing air inlet (5) of a jet engine, comprising a lip air inlet (6), a system (10, 1) deicing the feed lip with a hot fluid under pressure and means (11) acoustic attenuation forming an integral part of a given area of ​​said lip, characterized in that consists of forming the said acoustic attenuation means by separate islands (12, 24, 28) each constituted by a sandwich comprising an acoustically resistive porous layer forming a part (13, 13¿) of the outer envelope of the blowing channel delimited by the said air inlet lip, a honeycomb core mono or pluricapa and a reflector (15, 15¿) in forming or coating the reflector of each of the islets by a common element (15, 15¿) extending over all the islands (12, 24, 28), in effecting communication between the spaces defined or tre islets, on the one hand with the inside of the lip (5) and, on the other hand, with the outside of the cover (5) so that a forced circulation of de-icing fluid is engendered from inside the lip outward of said cover or through the spaces defined between the islets.
机译:包含喷气发动机的进气口(5)的除霜程序,其包括唇形进气口(6),在压力下用热流体对进料唇进行除冰的系统(10、1)和形成整体部分的声衰减装置(11)所述唇的给定区域的特征在于,其特征在于,其包括通过单独的岛(12、24、28)形成所述声衰减装置,每个岛由包含构成部分(13、13′)的抗声多孔层的三明治构成。 )由所述进气口唇缘界定的吹气通道的外壳,一个蜂窝芯单核或复核纤维和一个反射器(15、15′),用于通过共用元件(15, 15′)在所有岛(12、24、28)上延伸,从而在限定的或三岛的空间之间实现连通,一方面与唇部(5)的内部连通,另一方面与唇部(5)的外部连通盖(5)的顶部,以便从唇缘内部产生除冰液的强制循环所述盖的上方或穿过胰岛之间限定的空间。

著录项

  • 公开/公告号ES2236472T3

    专利类型

  • 公开/公告日2005-07-16

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE (SOCIETE PAR ACTIONS SIMPLIFIEE);

    申请/专利号ES20020362001T

  • 发明设计人 PORTE ALAIN;

    申请日2002-02-12

  • 分类号B64D15/04;B64C1/40;

  • 国家 ES

  • 入库时间 2022-08-21 22:14:39

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