Landing gear
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United States of America Patent
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May 6, 2014
Grant Date -
Jan 6, 2011
app pub date -
Aug 13, 2010
filing date -
Apr 7, 2003
priority date (Note) -
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Abstract
An aircraft landing gear is arranged such that in its deployed position it is configured to reduce, during the approach on landing, the noise generated by the interaction of the landing gear and the air flowing past the landing gear. Various means are described to reduce the amount of turbulent air flow generated in the region of the landing gear, including inverting and fairing the nose-gear shock-absorbing leg, providing faired twin in-line oleos and providing fairings that produce shielding air curtains.
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