公开(公告)号：US08636107B2

公开(公告)日：2014-01-28

申请号：US13941044

申请日：2013-07-12

Applicant: Aircelle

Inventor： John Moutier ,  Emmanuel Anfray ,  Franck Maze ,  Herve Simon

IPC: E04B1/84 ,  B32B43/00 ,  E04B1/74

CPC classification number: F02C7/24 ,  B29C73/04 ,  B29C73/26 ,  B64D2033/0206 ,  B64F5/40 ,  Y10T29/49398 ,  Y10T29/49618 ,  Y10T29/49732 ,  Y10T29/49734 ,  Y10T156/1082

Abstract: The present disclosure relates to a method for repairing a portion of an acoustic panel for a nacelle of an aircraft turbojet engine. The panel includes an acoustic skin in which a plurality of acoustic holes are drilled, a solid skin, and a cellular acoustic structure. The cellular acoustic structure, being arranged between the acoustic skin and the solid skin, has a plurality of cells, each of which has one or more drainage openings arranged in one or more of the walls forming each cell. The method includes a step of: defining a part of the acoustic panel to be cut; forming a cutting area closed by the acoustic skin; injecting a resin through the acoustic holes; positioning a replacement cellular acoustic structure in the cutting area and on the acoustic skin; forming a solid replacement skin on the replacement cellular acoustic structure.

Abstract translation: 本公开涉及一种用于修理飞机涡轮喷气发动机的机舱的声学面板的一部分的方法。 面板包括其中钻有多个声孔的声学皮肤，固体皮肤和蜂窝声学结构。 布置在声学皮肤和固体皮肤之间的细胞声学结构具有多个单元，每个单元具有布置在形成每个单元的一个或多个壁中的一个或多个排水孔。 该方法包括以下步骤：定义待切割的声学面板的一部分; 形成由声学皮肤封闭的切割区域; 通过声孔注入树脂; 在切割区域和声学皮肤上定位更换的蜂窝声学结构; 在替代的细胞声学结构上形成固体替代皮肤。

公开(公告)号：US20130292202A1

公开(公告)日：2013-11-07

申请号：US13941044

申请日：2013-07-12

Applicant: AIRCELLE

Inventor： John MOUTIER ,  Emmanuel Anfray ,  Franck Maze ,  Herve Simon

IPC: B64F5/00 ,  F02C7/24

CPC classification number: F02C7/24 ,  B29C73/04 ,  B29C73/26 ,  B64D2033/0206 ,  B64F5/40 ,  Y10T29/49398 ,  Y10T29/49618 ,  Y10T29/49732 ,  Y10T29/49734 ,  Y10T156/1082

Abstract: The present disclosure relates to a method for repairing a portion of an acoustic panel for a nacelle of an aircraft turbojet engine. The panel includes an acoustic skin in which a plurality of acoustic holes are drilled, a solid skin, and a cellular acoustic structure. The cellular acoustic structure, being arranged between the acoustic skin and the solid skin, has a plurality of cells, each of which has one or more drainage openings arranged in one or more of the walls forming each cell. The method includes a step of: defining a part of the acoustic panel to be cut; forming a cutting area closed by the acoustic skin; injecting a resin through the acoustic holes; positioning a replacement cellular acoustic structure in the cutting area and on the acoustic skin; forming a solid replacement skin on the replacement cellular acoustic structure.

Abstract translation: 本公开涉及一种用于修理飞机涡轮喷气发动机的机舱的声学面板的一部分的方法。 面板包括其中钻有多个声孔的声学皮肤，固体皮肤和蜂窝声学结构。 布置在声学皮肤和固体皮肤之间的细胞声学结构具有多个单元，每个单元具有布置在形成每个单元的一个或多个壁中的一个或多个排水孔。 该方法包括以下步骤：定义待切割的声学面板的一部分; 形成由声学皮肤封闭的切割区域; 通过声孔注入树脂; 在切割区域和声学皮肤上定位更换的蜂窝声学结构; 在替代的细胞声学结构上形成固体替代皮肤。