Low-noise aircraft, particularly at take-off and landing
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United States of America Patent
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Dec 13, 2011
Grant Date -
Aug 14, 2008
app pub date -
Apr 11, 2006
filing date -
Apr 13, 2005
priority date (Note) -
In Force
status (Latency Note)
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Abstract
An aircraft includes a rear vertical tail unit having two tail fins forming, with the rear part of a fuselage, a channel on the back of the fuselage. A turbine engine is arranged on the back of the fuselage so that gas streams generated by the turbine engine penetrate into the channel. The main landing gear of the aircraft is arranged integrally beneath the fuselage. The wings of the aircraft have a slight sweep angle and a large fineness ratio.
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