公开(公告)号：US09388767B2

公开(公告)日：2016-07-12

申请号：US13573784

申请日：2012-10-03

Applicant: AIRBUS OPERATIONS (S.A.S.)

Inventor： Alain Porte ,  Grégory Albet ,  Guillaume Ring ,  Pascal Galletti

IPC: F02K1/46 ,  F02C7/047 ,  B64D33/02 ,  B64D15/04 ,  F02C7/045 ,  F02K1/82

CPC classification number: F02K1/46 ,  B64D15/04 ,  B64D33/02 ,  B64D2033/0206 ,  B64D2033/0233 ,  F02C7/045 ,  F02C7/047 ,  F02K1/827 ,  Y02T50/672

Abstract: An aircraft nacelle comprising a lip extended by an inner conduit forming an air intake, a front frame delimiting with said lip an annular channel within which hot air flows and a panel for acoustic treatment having, from outside inwardly, an acoustic resistive layer, at least one honeycomb structure and a reflective layer as well as ducts for channeling hot air, each including one inlet communicating with the annular channel and one outlet communicating with the inner conduit, wherein the panel for acoustic treatment comprises at least a stabilization chamber in the form of an annular channel with a cross-section larger than that of the ducts which extends over at least a portion of the nacelle circumference and which communicates with a plurality of ducts, the inlets and outlets not being aligned in the longitudinal direction.

Abstract translation: 一种飞机机舱，包括由形成进气口的内部管道延伸的唇缘，与所述唇缘一起限定热空气流动的环形通道的前框架和用于声学处理的面板，其外部至少从外部至少形成声阻层 一个蜂窝结构和反射层以及用于引导热空气的管道，每个管道包括与环形通道连通的一个入口和与内部管道连通的一个出口，其中用于声学处理的面板至少包括稳定室 环形通道，其横截面大于在所述机舱周边的至少一部分上延伸并且与多个管道连通的管道的横截面，所述入口和出口不在纵向方向上对齐。

公开(公告)号：US20140001284A1

公开(公告)日：2014-01-02

申请号：US13573784

申请日：2012-10-03

Applicant: AIRBUS OPERATIONS (S.A.S)

Inventor： Alain Porte ,  Grégory Albet ,  Guillaume Ring ,  Pascal Galletti

IPC: F02K1/46

CPC classification number: F02K1/46 ,  B64D15/04 ,  B64D33/02 ,  B64D2033/0206 ,  B64D2033/0233 ,  F02C7/045 ,  F02C7/047 ,  F02K1/827 ,  Y02T50/672

Abstract: An aircraft nacelle comprising a lip extended by an inner conduit forming an air intake, a front frame delimiting with said lip an annular channel within which hot air flows and a panel for acoustic treatment having, from outside inwardly, an acoustic resistive layer, at least one honeycomb structure and a reflective layer as well as ducts for channeling hot air, each including one inlet communicating with the annular channel and one outlet communicating with the inner conduit, wherein the panel for acoustic treatment comprises at least a stabilization chamber in the form of an annular channel with a cross-section larger than that of the ducts which extends over at least a portion of the nacelle circumference and which communicates with a plurality of ducts, the inlets and outlets not being aligned in the longitudinal direction.

Abstract translation: 一种飞机机舱，包括由形成进气口的内部管道延伸的唇缘，与所述唇缘一起限定热空气流动的环形通道的前框架和用于声学处理的面板，其外部至少从外部至少形成声阻层 一个蜂窝结构和反射层以及用于引导热空气的管道，每个管道包括与环形通道连通的一个入口和与内部管道连通的一个出口，其中用于声学处理的面板至少包括稳定室 环形通道，其横截面大于在所述机舱周边的至少一部分上延伸并且与多个管道连通的管道的横截面，所述入口和出口不沿纵向排列。