A landing detection system (300) for a landing gear assembly of an aircraft may comprise a moveable member (309) mechanically coupled between an aircraft wheel and a strut piston (212), wherein the moveable member (309) is in communication with a strut chamber pressure of the landing gear assembly, wherein the moveable member (309) moves relative to the strut piston (212) in response to a first force applied to the aircraft wheel and the strut piston (212) strokes in response to a second force applied to the aircraft wheel.
TWO STAGE STRUT ALLOWING LOW INITIAL COMPRESSION LOAD
ZWEISTUFIGES FEDERBEIN, DAS EINE GERINGE ANFÄNGLICHE DRUCKBELASTUNG ERLAUBT
JAMBE À AMORTISSEUR À DEUX ÉTAGES PERMETTANT UNE CHARGE DE COMPRESSION INITIALE FAIBLE
2020-05-13
Patent
Elektronische Ressource
Englisch
Two stage strut allowing low initial compression load
Europäisches Patentamt | 2019
|TWO STAGE STRUT ALLOWING LOW INITIAL COMPRESSION LOAD
Europäisches Patentamt | 2018
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