AIRCRAFT LANDING GEAR COMPRISING A MAIN DAMPER AND AN ANTI-SHIMMY SECONDARY DAMPER
An aircraft landing gear (1) comprises: an axle (2), a leg (3) extending along a main axis of the leg (Z) and having a first part (3a) carrying the axle (2) and a second part (3b), a main damper (5) arranged to damp axial displacements of the first leg portion (3a) with respect to the second leg por...
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Main Authors | , , |
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Format | Patent |
Language | English |
Published |
15.02.2018
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Subjects | |
Online Access | Get full text |
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