LANDING GEAR COMPONENTS HAVING IMPROVED JOINTS

The present disclosure includes landing gear components, such as an outer cylinder (104) of a shock strut assembly (102). The outer cylinder (104) includes one or more structural attachment pins (105) configured to engage with other components of the landing gear including pintle frames (110), drag...

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Bibliographische Detailangaben
Hauptverfasser:	Noel C., HAYNES, Marilea, MANZINI
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT ALLOYS ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING CHEMISTRY COSMONAUTICS ENGINEERING ELEMENTS AND UNITS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FERROUS OR NON-FERROUS ALLOYS FLYING SUITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS LIGHTING MEANS FOR DAMPING VIBRATION MECHANICAL ENGINEERING METALLURGY PARACHUTES PERFORMING OPERATIONS SHOCK-ABSORBERS SPRINGS THERMAL INSULATION IN GENERAL TRANSPORTING TREATMENT OF ALLOYS OR NON-FERROUS METALS WEAPONS
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Beschreibung
Zusammenfassung:	The present disclosure includes landing gear components, such as an outer cylinder (104) of a shock strut assembly (102). The outer cylinder (104) includes one or more structural attachment pins (105) configured to engage with other components of the landing gear including pintle frames (110), drag braces (106), and torque links (124). The pins (105) include a cobalt alloy mated to a cobalt containing coating (140) for improved wear resistance, which may eliminate the need for a bushing between the pin (105) and the receptacle (107) of the corresponding landing gear component.