High traction on demand aircraft landing gear system
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United States of America Patent
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Oct 4, 2016
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N/A
app pub date -
May 1, 2013
filing date -
Jul 24, 2012
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Abstract
A traction-on-demand landing gear tire control system and methods are presented. An outer tire of an aircraft wheel is depressurized to a depressurized state in response to a non-optimal aircraft landing condition. An inner tire of the aircraft wheel contacts the outer tire in response to the depressurized state, and a plurality of traction studs are deployed to protrude from the outer tire in response to the inner tire contacting the outer tire.
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