Hinge mechanism for aircraft door
AssigneeThe Boeing Company
InventorsAlex Maraghe, Miloslav Puncoch
Life of this patent
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Abstract
A passenger door is connected to an aircraft fuselage by a hinge mechanism having an elongated goose-neck hinge member. One end of the hinge-member is pivotally connected to an idler crank arm that is pivotally connected to the fuselage. The other end of the goose-neck member is pivotally connected to the door. A guide arm connected to the door and carried by the idler crank arm controls door movement. An end of the guide arm has a pin that follows a groove in an "S"-shaped guide track. The shape of the track causes the guide arm to initially pivot and translate the door partially inwardly into the fuselage during opening movement, and then swing the door outwardly until it is parallel with the fuselage's outer surface.
Claims4
A hinge mechanism for mounting a door to an entryway in a wall, comprising:
- an idler crank arm having first and second ends, said first end being pivotally connected to said wall;
- a goose-neck member having first and second ends, wherein said first end of said member is pivotally connected to said idler crank arm's second end, and wherein said second end of said member is pivotally connected to said door near a side edge of said door;
- a guide arm having first and second ends, wherein one of said guide arm ends is pivotally connected to said door at a position nearer the side edge of said door than the position where said second end of said goose-neck member is pivotally connected to said door, in a manner so that said guide arm moves in response to opening and closing movement of said door, said guide arm being supportably connected to said idler crank arm in a manner so that said guide arm may both pivot and translate as said guide arm moves;
- an "S"-shaped track connected to said wall;
- and
- cam follower means for causing the other end of said guide arm to follow the direction of said track's shape as said guide arm moves.
Dependencies are inferred from the claim text.