A landing detection system for a landing gear assembly of an aircraft may comprise a moveable member mechanically coupled between an aircraft wheel and a strut piston, wherein the moveable member is in communication with a strut chamber pressure of the landing gear assembly, wherein the moveable member moves relative to the strut piston in response to a first force applied to the aircraft wheel and the strut piston strokes in response to a second force applied to the aircraft wheel.
TWO STAGE STRUT ALLOWING LOW INITIAL COMPRESSION LOAD
12.07.2018
Patent
Elektronische Ressource
Englisch
Two stage strut allowing low initial compression load
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