Zodiac Seats UK Limited

Safran Seats Gb Limited

Robert Gow

Paul Morgan

The present invention provides a table arrangementfor use in an aircraft seat module, the table arrangement comprising a first table element suitable for being movably mounted to a mounting structure of the aircraft seat module, the first table element being provided with a first table surface, a second table element provided with a second table surface substantially parallel to the first table surface, wherein the second table element is mounted to the first table element, such that the second table element is moveable from a first position with respect to the first table element to a second position with respect to the first table element, the second position being transformed from the first position within the plane of the second table element. The present invention also provides an aircraft seat module, an aircraft and a method of deploying a table arrangement.

Table arrangement

The present invention provides a table arrangement comprising a table moveably mounted to a table mounting structure, a compensation arrangement connected between the table and table mounting structure for reducing the force required to lift the table from a lowered position to a raised position, and a damper arrangement for reducing the speed of the table as it moves from the raised position to the lowered position, wherein the compensation arrangement is mounted on a shaft, such that as the table is lowered, the shaft rotates about its longitudinal axis and wherein the damping arrangement is arranged to act on the shaft to reduce the speed of its rotation about its longitudinal axis. The invention also provides an aircraft seat module and a method of deploying or stowing a table arrangement.

A table arrangement including a support member rotatably mounted to a base structure, a table element translatably mounted to the support member, and a locking mechanism is described. The locking mechanism may include a first locking member connected to the support member to rotate with the support member between non-aligned and aligned configurations with respect to the second locking member, and a second locking member. The first or second locking member may be translatably mounted with respect to the other locking member between a first engagement position and a second engagement position, wherein, when the first locking member is in the aligned configuration, the first or second locking member can translate into the second engagement position. The table arrangement may be deployed and stowed.

Table

The present invention provides table arrangement comprising a housing that has an open configuration and a closed configuration, a table, which, when in a stowed configuration is at least partially housed in the housing, and when in a presented configuration, is partially protruding from the housing, and an activation mechanism for opening and closing the housing, which is linked by a mechanical linkage to the table or housing such that when the activation mechanism closes the housing, the table changes from the presented configuration to the stowed configuration. The invention also provides an aircraft seat module, an aircraft and a method of stowing a table arrangement.

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Chepstow, United Kingdom

Robert Gow