NOSE LANDING GEAR ASSEMBLY FOR USE WITH AN AIRCRAFT

NOSE LANDING GEAR ASSEMBLY FOR USE WITH AN AIRCRAFT

A nose landing gear assembly (108) includes an oleo strut (136), a forward brace (110) including a forward brace first end (112) and a forward brace second end (114). The forward brace first end (112) is pivotably coupled to the nose gear bay (106) of a high wing aircraft about a first pivot axis (1...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: KARAPETIAN, Michael S, LEE, Hao
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:A nose landing gear assembly (108) includes an oleo strut (136), a forward brace (110) including a forward brace first end (112) and a forward brace second end (114). The forward brace first end (112) is pivotably coupled to the nose gear bay (106) of a high wing aircraft about a first pivot axis (116). The assembly also includes an aft brace (118) including an aft brace first end (120) and an aft brace second end (124). The aft brace first end (120) is pivotably coupled to the nose gear bay (106) about a second pivot axis (122), and the aft brace second end (124) is pivotably coupled to the oleo strut (136). An actuator (126) includes an actuator first end (128) and an actuator second end (130). The actuator second end (130) is coupled to the nose gear bay (106) and the actuator first end (128) coupled to the forward brace (110). The actuator (126) is configured to move the nose landing gear assembly (108) between a retracted position and an extended position.