An aircraft has a ducted thruster. The ducted thruster includes a duct having an inner wall, a stator hub disposed within the duct, a first stator extending along a first longitudinal axis between the inner wall and the stator hub, and a second stator. The second stator extends along a second longitudinal axis between the inner wall and the stator hub. The second longitudinal axis is either (1) substantially perpendicular to the first longitudinal axis or (2) substantially parallel to the first longitudinal axis and offset from the first longitudinal axis.
DUCTED THRUSTERS
2020-09-17
Patent
Elektronische Ressource
Englisch
OMAE2017-61085 Improved Sustainable Speed due to Thrusters With Ducted Propellers
British Library Conference Proceedings | 2017
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