Aircraft with a fuselage substantially designed as an aerodynamic lifting body
Number of patents in Portfolio can not be more than 2000
United States of America Patent
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Sep 11, 2001
Grant Date -
N/A
app pub date -
Nov 1, 1999
filing date -
Jan 4, 1997
priority date (Note) -
Expired
status (Latency Note)
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Abstract
An aircraft has a fuselage designed essentially as an aerostatic lift body. Combined lift and propulsion devices are articulated on the fuselage, are provided with propellers and form propulsion units and which in each case can tilt between a lift position, in which the respective propeller rotation plane is essentially horizontal and a propulsion position, in which the respective propeller rotation plane is essentially vertical. Additionally the propeller rotation plane has all-round inclination relative to the output shaft of the associated drive device.
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