Vertical takeoff and landing aircraft
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United States of America Patent
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-
May 24, 2005
Issued Date -
N/A
app pub date -
Apr 16, 2003
filing date -
Apr 16, 2003
priority date (Note) -
Expired
status (Latency Note)
Importance
Abstract
A vertical takeoff and landing aircraft, which includes pivotal wing and engine assemblies on a fuselage with tail assemblies extending from each of the wing assemblies and the engines being operable in turbo prop or pure jet mode, wherein the aircraft is configured such that it can be landed or taken off vertically or in a horizontal mode along a runway.
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