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

Claim 18:
19. 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;
wherein, during a transfer of said first table element between the stowage position and the position of use, the first pivot axis is moved in linear translation in a mounting plane of 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.