首页> 外国专利> ACOUSTIC STRUCTURE ALVEOLAIRE FOR TURBOJETACTOR AND TURBOJETACTOR INCORPORATING AT LEAST ONE SUCH STRUCTURE

ACOUSTIC STRUCTURE ALVEOLAIRE FOR TURBOJETACTOR AND TURBOJETACTOR INCORPORATING AT LEAST ONE SUCH STRUCTURE

机译:涡轮射流器和涡轮射流器的声学结构泡孔包含至少一种这样的结构

摘要

A cellular acoustic structure for a turbojet engine includes a closed wall. The closed wall includes at least two faces having acoustically transparent areas and acoustic reflective areas. The closed wall is filled with a plurality of cells, and the acoustic reflective areas are disposed within the closed wall so that an acoustic path of aerial sound vibrations travels through the acoustically transparent areas, penetrates inside the cells and reflects on the acoustic reflective areas. In particular, the acoustic path in some of the cells has a depth greater than a half of the thickness of the cellular acoustic structure.
机译:用于涡轮喷气发动机的蜂窝声学结构包括封闭壁。封闭壁包括至少两个面,所述至少两个面具有声透明区域和声反射区域。封闭壁中填充有多个单元,并且声反射区域布置在封闭壁内,使得空中声振动的声路穿过声透明区域,穿透单元内部并在声反射区域上反射。特别地,某些单元中的声路径的深度大于蜂窝声结构的厚度的一半。

著录项

  • 公开/公告号FR2985287B1

    专利类型

  • 公开/公告日2018-02-23

    原文格式PDF

  • 申请/专利权人 AIRCELLE;

    申请/专利号FR20120050073

  • 发明设计人 XAVIER CAZUC;JEAN PHILIPPE JORET;

    申请日2012-01-04

  • 分类号F02C7/24;F02C7;F02K3/06;

  • 国家 FR

  • 入库时间 2022-08-21 12:33:21

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