FAN FOR AIRCRAFT INTERIOR
Number of patents in Portfolio can not be more than 2000
United States of America
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Issued Date -
Feb 20, 2025
app pub date -
Jun 6, 2024
filing date -
Jun 6, 2024
priority date (Note) -
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Abstract
A fan structure for the interior of an aircraft. The fan structure includes: a structure of an aircraft interior defining an aperture, a spindle configured to be rotatably driven about its axis by a motor, a central hub mounted on the spindle and a plurality of blades extending outwardly from the central hub. The base of each of the plurality of blades is connected to the central hub and the tip of each of the plurality of blades is connected to an adjacent blade or the central hub, such that each of the plurality of blades forms a closed surface with an adjacent blade or the central hub. The plurality of blades are located in the aperture of the structure of an aircraft interior. The fan structure is configured to move a gas from a first side of the aperture to a second side of the aperture.
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