VERTICAL TAKEOFF AND LANDING AIRCRAFT
Number of patents in Portfolio can not be more than 2000
United States of America
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Issued Date -
Oct 3, 2024
app pub date -
Jun 10, 2024
filing date -
Jun 10, 2024
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Abstract
An aircraft defines a vertical direction and includes a fuselage and a propulsion system comprising a power source and a plurality of vertical thrust electric fans driven by the power source. A wing extends from the fuselage. The plurality of vertical thrust electric fans are arranged along a length of the wing along a lengthwise direction of the wing. The wing comprises a diffusion assembly along the lengthwise direction of the wing and includes a first diffusion member positioned downstream of at least one of the plurality of vertical thrust electric fans. The first diffusion member defines a curved shape relative to a longitudinal direction of the aircraft. The longitudinal direction is generally perpendicular to the lengthwise direction of the wing.
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