Aircraft with a hot air exhaust that comprises two pivotally mounted exhaust sections
Number of patents in Portfolio can not be more than 2000
United States of America
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-
Jan 7, 2020
Grant Date -
Jun 22, 2017
app pub date -
Nov 30, 2016
filing date -
Nov 30, 2016
priority date (Note) -
In Force
status (Latency Note)
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Abstract
An aircraft with at least one engine that generates a hot air flow in operation of the aircraft, wherein at least one hot air exhaust is provided for exhausting the generated hot air flow, the at least one hot air exhaust comprising at least one first exhaust section that is mounted in a rotatable manner to at least one second exhaust section via an associated off-axis swivel joint, wherein an actuating member is provided that is adapted for applying a turning moment to the at least one second exhaust section in operation of the aircraft in order to displace a longitudinal axis of the at least one second exhaust section with respect to a longitudinal axis of the at least one first exhaust section by a predetermined displacement angle.
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