发明名称 Support plate for the passage of systems between two zones with different pressurizations of an aircraft
摘要 A support plate for the passage of systems between two zones at different pressurizations of an aircraft, in the region of a bulkhead separating the two zones. The support plate comprises a connection plate including at least one retaining element and at least one sealing joint and is provided with a plurality of holes intended for the passage of an assembly of systems which have to pass through said bulkhead.
申请公布号 US9321519(B2) 申请公布日期 2016.04.26
申请号 US201414285787 申请日期 2014.05.23
申请人 Airbus Operations SAS 发明人 Tomasi Marc;Lieven Patrick;Delahaye Romain;De Kergommeaux Matthieu
分类号 B64C1/10;F16L3/00;F16L5/12 主分类号 B64C1/10
代理机构 Greer, Burns & Crain, Ltd. 代理人 Greer, Burns & Crain, Ltd.
主权项 1. An aircraft comprising: a pressurized zone; a non-pressurized zone; a bulkhead separating the pressurized zone from the non-pressurized zone; and a support plate for the passage of systems between pressurized zone and the non-pressurized zone positioned within an opening in the bulkhead, said support plate comprising: a connection plate,said connection plate comprising at least one retaining element and at least one sealing joint arranged on the periphery of at least one face of the connection plate,said connection plate further comprising at least one electrical connector and at least one hydraulic connector passing through the opening in said bulkhead, andwherein said retaining element is provided with two branches, of which one is intended to come to contact with a face of the connection plate and of which the other is suitable for being fixed on a structural element.
地址 Toulouse FR