发明名称 Aircraft system carrier element
摘要 An aircraft system carrier element includes a basic body made of a sound- and heat-insulating material, in which are formed an air conditioning duct, which is connectable to an aircraft air conditioning system and provided for supplying an aircraft compartment, and a line duct for receiving lines that are provided for supplying the aircraft compartment. The basic body includes a rear wall and a line duct cover that is fastened detachably to the rear wall. The detachable fastening of the line duct cover enables easy access to the lines for maintenance purposes, when necessary, while also protecting the lines against environmental effects in normal operation.
申请公布号 US9096306(B2) 申请公布日期 2015.08.04
申请号 US200912997497 申请日期 2009.06.09
申请人 Airbus Operations GMBH 发明人 Szarszewski Maik;Weber Christoph;Voelkner Joachim
分类号 B64D13/00;B64C1/06;B64C1/00 主分类号 B64D13/00
代理机构 Wood Herron & Evans, LLP 代理人 Wood Herron & Evans, LLP
主权项 1. An aircraft system carrier element, comprising: a basic body made of a sound- and heat-insulating material, in which are formed: an air conditioning duct, which is connectable to an aircraft air conditioning system and provided for supplying an aircraft compartment, anda line duct for receiving lines that are provided for supplying the aircraft compartment,wherein the basic body comprises a rear wall; a line duct cover that is fastened detachably to the rear wall; a first cutout formed in the rear wall at a portion of the rear wall adjacent to the line duct; and a second cutout extending through the line duct cover, the second cutout aligned with the first cutout formed in the rear wall such that the first and second cutouts are configured to collectively receive a holder extending through the first and second cutouts for fastening a wall of the aircraft compartment to an aircraft structure.
地址 Hamburg DE