Aircraft door hinge mechanism

Miscellaneous hardware (e.g. – bushing – carpet fastener – caster – Hinge – Having plural hinge axes

Patent

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Details

244905, 2441295, 49246, E05D 306, E05D 1528, B64C 114

Patent

active

052896153

ABSTRACT:
A hinge assembly (14) for attaching a translating-motion-type aircraft door (10) to an aircraft fuselage (12) is disclosed. The hinge assembly (14) includes a fitting (28) that is pivotally attached to the portion of the aircraft fuselage (14) adjacent the door opening (16) in the fuselage in which the door (10) is normally seated. The door is attached to the hinge fitting (28) by way of a universal shaft (30) that is rotatably attached to the free end of the hinge fitting (28). A drivebelt (32) is anchored at one end to the aircraft fuselage (12) and is attached at the opposed end to the universal shaft (30) so as to move in unison with the shaft. When the hinge assembly (14) of this invention is opened, the hinge fitting (28) pulls on the drivebelt (32) so as to cause its movement and the subsequent movement of the universal shaft (30). The universal shaft (30) is rotated about the hinge fitting (28) so as to maintain the door (10) attached thereto in a constant angular relationship relative to the longitudinal axis of the aircraft fuselage (12).

REFERENCES:
patent: 2702400 (1955-02-01), Marple
patent: 3004303 (1961-10-01), Wilmer
patent: 3016261 (1962-01-01), Tatter
patent: 4025104 (1977-05-01), Grossbach et al.
patent: 4607812 (1986-08-01), De Haan et al.
patent: 4720065 (1988-01-01), Hamatani

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