FUSELAGE MOUNTED LANDING GEAR

A landing gear for an aircraft. The landing gear may have a wheel/truck assembly (404), an oleo strut/support frame (402) for supporting the wheel/truck assembly, and a retraction assembly (410) attached to the oleo strut/support frame, the retraction assembly for moving the landing gear between a d...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: LONG, Michael Allan, SALMON, James Jason, BARMICHEV, Sergey D
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung:A landing gear for an aircraft. The landing gear may have a wheel/truck assembly (404), an oleo strut/support frame (402) for supporting the wheel/truck assembly, and a retraction assembly (410) attached to the oleo strut/support frame, the retraction assembly for moving the landing gear between a deployed position and a retracted position. The retraction assembly may have a pivoting trunnion brace (422) attached to the oleo strut/support frame and to a fuselage of the aircraft for positioning the wheel/truck assembly, the oleo strut/support frame and the retraction assembly at least substantially fully within the fuselage of the aircraft in the retracted position.