An articulating motor mount assembly including a first frame segment attachable to an airframe of an aircraft. A second frame segment is rotatably coupled to the first frame segment in a plane oblique to a longitudinal axis of the first frame segment. A third frame segment is rotatably coupled to the second frame segment in a plane oblique to a longitudinal axis of the second frame segment and configured to carry a thrust device. A first actuator is positioned to rotate the second frame segment relative to the first frame segment and a second actuator is positioned to rotate the third frame segment relative to the second frame segment.
Articulating motor mount
03.06.2025
Patent
Elektronische Ressource
Englisch
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