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发明授权
CN106882392B 具有包括两个枢转地安装的排放部段的热空气排放件的飞行器 有权

具有包括两个枢转地安装的排放部段的热空气排放件的飞行器
摘要：
一种具有至少一个发动机的飞行器(1)，该发动机在飞行器的操作中产生热空气流(7)，该飞行器设有至少一个热空气排放件(6)以排出所产生的热空气流(7)，该排放件包括至少一个第一排放部段(6a)，其藉由相关联的偏轴旋转接头(10)以可转动的方式安装于至少一个第二排放部段(6b)，其中还设有致动构件(11)，该致动构件适合于在操作中将转动力矩施加于至少一个第二排放部段以使其纵向轴线(6g)相对于至少一个第一排放部段的纵向轴线(6e)偏移预定偏移角度(12b)。本发明还涉及一种操作热空气排放件(6)的方法。本发明能使得能减小飞行器承载结构部件由于热空气流而过度升温，从而能可靠地防止这些承载结构部件受损或破坏。
摘要（英）：

The invention is related to an aircraft with at least one engine that generates a hot air flow (7) in operation of the aircraft, wherein at least one hot air exhaust (6) is provided for exhausting the generated hot air flow (7), the at least one hot air exhaust (6) comprising at least one first exhaust section (6a) that is mounted in a rotatable manner to at least one second exhaust section (6b) via an associated off-axis swivel joint (10), wherein an actuating member (11) is provided that is adapted for applying a turning moment to the at least one second exhaust section (6b) in operation of the aircraft in order to displace a longitudinal axis (6g) of the at least one second exhaust section (6b) with respect to a longitudinal axis (6e) of the at least one first exhaust section (6a) by a predetermined displacement angle (12b).

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