Tri-cycloidal airship
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United States of America Patent
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Sep 4, 2007
Grant Date -
May 3, 2007
app pub date -
Nov 1, 2005
filing date -
Nov 1, 2005
priority date (Note) -
Expired
status (Latency Note)
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Abstract
An unmanned, lighter-than-air airship includes three omnidirectional thrust generating units. One unit is mounted at the fore-end of the airship to generate thrust in a plane that is perpendicular to the longitudinal axis of the airship. This unit controls pitch and yaw movements of the airship. The other two units are mounted on the airship equidistant from the first unit, and are located in a same midships plane that is perpendicular to the longitudinal axis. These two units generate thrust vectors that control roll movements of the airship and provide propulsion for the airship.
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