SHOCK ABSORBERS
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United States of America Patent
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N/A
Issued Date -
Jul 18, 2013
app pub date -
Jul 16, 2012
filing date -
Aug 5, 2011
priority date (Note) -
Abandoned
status (Latency Note)
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Abstract
Adjusting device (1) for an aircraft landing gear shock absorber (2), such that the length (3) of said shock absorber (2) can be varied to change the aircraft attitude for operations on ground, wherein the adjusting device (1) is directly connected to a shock absorber (2) by a supply line (16), the adjusting device (1) comprising an actuating element (13) that moves in a chamber (17) filled with a fluid (20), the actuating element (13) being displaced by means of a drive shaft (12) driven by a driving device (11), the displacement of the actuating element (13) in the chamber (17) causing the addition or removal of fluid (20) in the shock absorber (2), therefore varying the length (3) of said shock absorber (2). The invention also refers to an aircraft landing gear comprising such an adjusting device (1).
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