发明名称 Panel for an air intake of an aircraft nacelle that ensures optimized acoustic treatment and frost treatment
摘要 An acoustic treatment panel includes an acoustically resistive layer that defines a surface of an aircraft that is in contact with an aerodynamic stream, a reflective layer (50) between which are arranged at least one alveolar structure (52) with a number of cells dedicated to the acoustic treatment, and de-icing cavities (58) in which hot air circulates in contact with the acoustically resistive layer to ensure a frost treatment, characterized in that it includes holes for supplying de-icing cavities (58) with hot air and in that the capacity to treat the frost is adjusted along the zones by modifying the open surface ratio that results from the holes.
申请公布号 US8960589(B2) 申请公布日期 2015.02.24
申请号 US201012968562 申请日期 2010.12.15
申请人 Airbus Operations SAS 发明人 Porte Alain;Chelin Frédéric;Dida Stéphane;Hormiere Arnaud
分类号 B64C23/00;B64D15/04;B64D33/02;F02C7/045;F02C7/047 主分类号 B64C23/00
代理机构 Young & Thompson 代理人 Young & Thompson
主权项 1. An acoustic treatment panel, comprising: an acoustically resistive layer that defines an outer surface of an aircraft that is in contact with an aerodynamic stream; a reflective layer; and at least one alveolar structure located between the acoustically resistive layer and the reflective layer, the at least one alveolar structure comprising a plurality of cells configured for acoustic treatment, the cells being formed of elongated strips extending parallel to one another, each of the strips being delimited by two opposite side partitions and each of the strips being spaced apart from one another to form elongated de-icing cavities extending in between adjacent strips such that, during operation, hot air circulates through the de-icing cavities in contact with said acoustically resistive layer for frost treatment, wherein a rear wall, extending from opposite facing side partitions of the adjacent strips and enclosing each of the de-icing cavities between the strips, includes holes in communication with each de-icing cavity for supplying each de-icing cavity with hot air, and wherein along an entire length of the rear wall over any one de-icing cavity, a ratio of open space formed by the holes to a closed area of the rear wall along the length varies irregularly to delimit zones having differing communication with the hot air for differing capacities for frost treatment.
地址 Toulouse FR