Vertical take-off and landing aircraft with adjustable center-of-gravity position
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United States of America Patent
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N/A
Issued Date -
Jun 1, 2006
app pub date -
Jun 24, 2005
filing date -
Jun 24, 2004
priority date (Note) -
Abandoned
status (Latency Note)
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Abstract
A vertical take-off and landing aircraft includes a device for generating lift, which includes at least one drivable rotor, which is mounted to be rotatable about a rotor pivot axis, which extends parallel to the vertical axis of the aircraft. The aircraft further includes a device for generating propulsion, which displaces the center of gravity of the aircraft within a plane running normal to the rotor pivot axis.
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