PINNED FUSELAGE-TO-WING CONNECTION

PINNED FUSELAGE-TO-WING CONNECTION

An aircraft comprises a fuselage (110), a wing assembly (130), and a pinned fuselage-to-wing connection (150) including a forward pin joint (210), an aft pin joint (230), and intermediate pin joints (220) between the forward and aft pin joints. The intermediate pin joints have pins aligned in an axi...

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Hauptverfasser: LAKIC, Branko, LEIBOV, David H
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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creator LAKIC, Branko
LEIBOV, David H
description An aircraft comprises a fuselage (110), a wing assembly (130), and a pinned fuselage-to-wing connection (150) including a forward pin joint (210), an aft pin joint (230), and intermediate pin joints (220) between the forward and aft pin joints. The intermediate pin joints have pins aligned in an axial direction and are configured to slide along the axial direction without transferring axial loads from the wing assembly to the fuselage. At least one of the forward and aft pin joints is constrained to prevent translation along the axial direction.
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subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
title PINNED FUSELAGE-TO-WING CONNECTION
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