An air guidance device for a vertical take-off and landing aircraft is provided. A nacelle device with a drive device is connected via a pylon device to a wing of the vertical take-off and landing aircraft and is pivotable by a pivoting device, about an axis of rotation between a first position, such as a propulsion position, and a second position, such as a lift position, relative to the pylon device. A first inlet opening of the air guidance device is arranged on the pylon device in a region in which air conveyed by the drive device in the second position impinges on the pylon device and/or in a region of maximum propeller-generated pressure.
AIR GUIDANCE DEVICE OF A VERTICAL TAKE-OFF AND LANDING AIRCRAFT, AND VERTICAL TAKE-OFF AND LANDING AIRCRAFT
2024-05-30
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |