Tunnel wing system for lift, altitude flight, and ground effect flight
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United States of America Patent
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N/A
Issued Date -
Apr 17, 2014
app pub date -
Oct 17, 2012
filing date -
Oct 17, 2012
priority date (Note) -
Abandoned
status (Latency Note)
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Abstract
Aircraft comprising a single wing suspended under a closed sided chassis. The wing spar is mounted to the sides that enclose and channel the airflow over and under the wing to provide lift. Airflow is provided by a source located in front of the wing by means of either propeller, ducted fan or similar devise. Engines mounted on a rotational engine mount can provide downward thrust to lift front of craft to obtain an angle great enough for lift-off Once aircraft has sustained-angle for lift off engine(s) rotate to produce airflow parallel to wing for flight. Rudders mounted behind the air source and prior to the wing provide steering.
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