Patent ID: 11890980
Assignee: AIRBUS OPERATIONS LIMITED
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 0:
1. A table arrangement for an aircraft, the table arrangement comprising:
a mounting element to be fastened to a fastening structure element, said mounting element defining a mounting plane;
a first table element connected to said mounting element, said first table element being pivotable relative to said mounting element about a first pivot axis between a stowage position, in which said first table element extends substantially parallel to said mounting plane defined by said mounting element, and a position of use, in which said first table element extends substantially perpendicular to said mounting plane defined by said mounting element; and
a second table element connected to said first table element, said second table element being arranged substantially parallel to said first table element and being rotatable relative to said first table element about an axis of rotation arranged parallel to said mounting plane when said first table element is in the position of use; and
said second table element being pivotable into an overlapping position, in which said first and second table elements overlap one another to a maximum, and into a working position, in which a longitudinal axis of said first table element encloses an angle of approximately 80 to 120° with a longitudinal axis of said second table element;
said second table element being pivotable relative to said first table element about the axis of rotation between the overlapping position and the working position, and
when said first table element is in the stowage position, said second table element is displaceable relative to said first table element in a direction parallel to the longitudinal axis of said first table element and the longitudinal axis of said second table element.