A discharge string for an aircraft for discharging water from the interior of the aircraft is shown and claimed, the discharge string having a conduit extending in a conduit direction from a connector end to a discharge end. A connector end is provided for connection to another conduit in the interior of the aircraft through which water flows into the drain string. A discharge end is provided for discharging water into the surrounding area of the aircraft. The pipe comprises a plastic in which an electrically conductive material is embedded, by means of which the pipe can be electrically heated by a heating current conducted through the electrically conductive material. The proportion of the conductive material embedded in the pipe increases in the direction of the pipe from the connector end to the discharge end of the pipe per unit length in such a way that the heating power per unit length introduced into the pipe increases from the connector end to the discharge end.
示出并要求保护一种用于飞行器的排放管柱,排放管柱用于从飞行器的内部排放水,排放管柱具有管道,管道在管道方向上从连接器端部延伸到排放端部。提供连接器端部以用于连接到飞行器的内部中的另一管道,水通过该另一管道流入排放管柱。提供排放端部以用于将水排放到飞行器的周围区域中。管道包含塑料,导电材料被嵌入到塑料中,通过导电材料,管道可以通过经导电材料传导的加热电流而被电加热。管道中嵌入的导电材料的比例沿管道方向在每单位长度上从管道的连接器端部向排放端部增加,其方式为使得被引入到管道中的每单位长度的加热功率从连接器端部向排放端部增加。
Discharge pipe column
排放管柱
13.01.2023
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Steering pipe column telescopic structure and steering pipe column assembly
Europäisches Patentamt | 2015
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