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发明公开
CN102224070A 飞机或航天器的结构部件和飞机或航天器的机身部件装置 失效 - 权利终止

飞机或航天器的结构部件和飞机或航天器的机身部件装置
摘要：
在飞机或航天器的结构部件(2)的方案中，其包括：机身部分连接区域(10)，用于连接到相关的机身部分(5)并具有与所述相关的机身部分(5)近似相等的热膨胀系数；内部连接区域(11)，用于连接到相关的安装元件并具有与所述相关的安装元件近似相等的热膨胀系数；以及分隔区域(12)，用于连接所述机身部分连接区域(10)和所述内部连接区域(11)，其中所述区域(10、12、11)中的至少一个具有高传热阻(R13、R14、R15)。
摘要（英）：

The invention relates to a structural component (2) of an aircraft or spacecraft comprising a fuselage section connection area (10) for connecting to an associated fuselage section (5) having a thermal expansion coefficient that is approximately aligned with the associated fuselage section (5); an inner connection area (11) for connecting to an associated installation element having a thermal expansion coefficient that is approximately aligned with the associated installation element; and a separating area (12) for connecting the fuselage section connection area (10) and the inner connection area (11), wherein at least one of the areas (10, 11, 12) has a high thermal resistance (R13, R14, R15).

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