A structural cooling system for an aircraft. A component (100) for an aircraft (200) and an aircraft (200) comprising such a component are provided. The component (100) comprises at least one heat source (110), a housing (140) surrounding the at least one heat source (110), at least one heat exchanger (120), at least one heat sink (130), at least one structural suspension element (150) and an air conduit (170). Each of the at least one structural suspension element (150) is attached to an inner surface of the housing (140) and supports one or more of the at least one heat source (110) within the housing (140). The heat sink (130) is part of the housing (140) and is configured to direct air from an interior of the housing (140) to an exterior of the housing (140). Each of the at least one heat exchanger (120) is thermally coupled to at least one of the at least one heat source (110). Each of the at least one heat exchanger (120) is fluidly connected to one of the at least one radiator (130) via an inlet line (160) and a return line (161) for coolant. The air conduit (170) is configured to direct ambient air from the outside through the housing (140), through each of the at least one structural suspension element (150), and through the heat sink (130) out of the housing (140).

    用于飞行器的结构性冷却系统。提供了一种用于飞行器(200)的部件(100)和包括这种部件的飞行器(200)。所述部件(100)包括至少一个热源(110)、包围所述至少一个热源(110)的壳体(140)、至少一个热交换器(120)、至少一个散热器(130)、至少一个结构性悬挂元件(150)和空气导管(170)。所述至少一个结构性悬挂元件(150)中的每一个附接到所述壳体(140)的内表面,并支撑所述壳体(140)内的所述至少一个热源(110)中的一个或多个热源。所述散热器(130)是所述壳体(140)的一部分,并被构造用以将空气从所述壳体(140)的内部引导到所述壳体(140)的外部。所述至少一个热交换器(120)中的每一个热耦合到所述至少一个热源(110)中的至少一个热源。所述至少一个热交换器(120)中的每一个经由用于冷却剂的入口管线(160)和返回管线(161)流体地连接到所述至少一个散热器(130)中的一个散热器。所述空气导管(170)被构造用以引导来自外部的环境空气通过所述壳体(140),经过所述至少一个结构性悬挂元件(150)中的每一个结构性悬挂元件,并经过所述散热器(130)离开所述壳体(140)。


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    Titel :

    Structural cooling system for aircraft


    Weitere Titelangaben:

    用于飞行器的结构性冷却系统


    Beteiligte:

    Erscheinungsdatum :

    2023-11-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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