PRIMARY STRUCTURAL ASSEMBLY FOR AN AIRCRAFT OUTSIDE-SKIN HEAT EXCHANGER, AIRCRAFT HAVING A PRIMARY STRUCTURAL ASSEMBLY, AND METHOD FOR ATTACHING AN AIRCRAFT OUTSIDE-SKIN HEAT EXCHANGER

The invention relates to a primary structural assembly (100) for an aircraft outside-skin heat exchanger (50), the assembly comprising: an outer-skin portion (5) which defines an outer shape of the aircraft (1) and forms a portion of a hull of the aircraft (1), wherein the outer-skin portion (5) comprises at least one recess (10); a thermal-transfer fluid connection (20) which is designed to convey a thermal-transfer fluid into the recess (10); a component (50) which closes the recess (10); and at least one retaining means (30) which is arranged in or on the recess (10) and is designed to hold the component (50) closing the recess (10) in the recess (10). The invention further relates to an aircraft (10) comprising such a primary structural assembly (100) and to a method for attaching an aircraft outside-skin heat exchanger. 描述了一种用于飞行器外蒙皮换热器(50)的初级结构布置(100)，该初级结构布置包括：外蒙皮区段(5)，该外蒙皮区段限定飞行器(1)的外部形状并且构成飞行器(1)的外壳的区段，其中外蒙皮区段(5)具有至少一个凹部(10)；载热流体连接部(20)，该载热流体连接部被适配成用于将载热流体引导到凹部(10)中；封闭凹部(10)的结构元件(50)；以及布置在凹部(10)中或其上的