LEVERED LANDING GEAR WITH INNER SHOCK STRUT

A levered landing gear (110) including a first shock strut (200) having a longitudinal axis (LAX), a second shock strut (300) disposed concentrically with the first shock strut (200) along the longitudinal axis (LAX) such that the first shock strut (200) and the second shock strut (300) extend along...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser:	Mellor, Mitchell
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS LIGHTING MEANS FOR DAMPING VIBRATION MECHANICAL ENGINEERING PERFORMING OPERATIONS SHOCK-ABSORBERS SPRINGS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A levered landing gear (110) including a first shock strut (200) having a longitudinal axis (LAX), a second shock strut (300) disposed concentrically with the first shock strut (200) along the longitudinal axis (LAX) such that the first shock strut (200) and the second shock strut (300) extend along a common extension axis (EX), and a truck lever (220) coupled to both the first shock strut (200) and the second shock strut (300) such that the second shock strut (300) pivots the truck lever (220) relative to the first shock strut (200).