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1. 发明申请

US20090283641A1 AIRCRAFT WITH CONNECTION ELEMENT FOR CONNECTING A CONDUIT SYSTEM TO COOLING AGGREGATES IN AIRCRAFT CABINS 有权
标题翻译：具有连接元件的连接元件用于冷却航空仓库中的集合体的飞机
公开(公告)号：US20090283641A1
公开(公告)日：2009-11-19
申请号：US12472221
申请日：2009-05-26
申请人： Theo DE BUHR
发明人： Theo DE BUHR
IPC分类号： B64C1/00
CPC分类号： B64D11/04 , F16L41/00 , Y02T50/46
摘要： The invention relates to an aircraft with a connection element for connecting at least one first conduit element or the like positioned in a supply chamber of an aircraft with at least one second conduit element positioned in a cabin chamber of the aircraft, wherein supply chamber and cabin chamber are separated from each other by means of a separation element, substantially comprising a connection part comprising fastening elements for fastening the first and second conduit element.Known connection elements have the disadvantage that there occur sealing problems due to the fastening of the fastening element at the outside of the connection part at the end facing the cabin chamber. A further disadvantage is that the connection elements protrude into the cabin chamber and form stumble edges there.In that at least the fastening element for the fastening the conduit element of the cabin chamber is provided within the connection part, there may be realised a compact structural shape which does not protrude from the separating element into the cabin chamber, and which may in addition be reliably sealed.
摘要翻译：本发明涉及一种具有连接元件的飞行器，该连接元件用于连接位于飞行器的供应室中的至少一个第一导管元件等，其中至少一个第二导管元件定位在飞机的舱室中，其中供应室和舱室室通过分离元件彼此分离，基本上包括连接部分，该连接部分包括用于紧固第一和第二导管元件的紧固元件。已知的连接元件具有这样的缺点，即由于紧固元件在面向机舱的端部处的连接部分的外部处的紧固而出现密封问题。另一个缺点是连接元件突出到舱室中并在那里形成绊倒边缘。因为至少用于紧固舱室的管道元件的紧固元件设置在连接部分内，所以可以实现紧凑的结构形状，其不会从分离元件突出到舱室中，并且可以另外可靠密封。

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