Aircraft landing gear
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United States of America Patent
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Oct 18, 2016
Grant Date -
Sep 29, 2016
app pub date -
Jul 30, 2014
filing date -
Jul 31, 2013
priority date (Note) -
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status (Latency Note)
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Abstract
The invention relates to an aircraft landing gear, particularly a front landing gear with at least one EHDC unit, which has at least one electric motor and at least one hydraulic pump, whereby at least one adjusting device is provided for the adjustment of the position of the aircraft landing gear, whereby the adjusting device comprises at least one actuator for driving the adjusting device, whereby the steering angle and/or the steering speed and/or the retraction speed and/or the extension speed and/or the end position damping and/or the position of the adjusting device can be controlled or adjusted by means of the electric motor driving the at least one actuator of the adjusting device by means of the hydraulic pump.
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