Abstract: A support device for an aircraft cabin interior layout assembly comprises a fixed frame extending according to a longitudinal direction; and a table comprising a tray deployable relative to the frame between a retracted configuration and a deployed configuration. The tray extends horizontally in the retracted configuration and in the deployed configuration and is displaceable in rotation about a first axis of rotation, substantially parallel, while remaining horizontal between the retracted configuration and the deployed configuration. The tray is displaceable in translation relative to the frame in the longitudinal direction between a first position of use and a second position of use when the tray is in the deployed configuration, while being fixed in rotation about the first rotation axis.

Abstract: An aircraft seat structure with tapered base, and associated aircraft cabin, the seat structure includes a frame and a turret arranged above the frame, the turret being mounted rotatably relative to the frame about a vertical axis between a nominal rest configuration. The seat structure is oriented along a main direction and at least one configuration pivoted about the vertical axis relative to the nominal configuration. The seat structure further includes a main displacement carriage, movable along the main direction with respect to the frame and a seat pan support. The main displacement carriage is supported by the turret, being mounted movably in translation relative to the turret along the main direction in the nominal configuration, the main displacement carriage supporting the seat pan support.

Abstract: A portion of an aircraft includes a fuselage. The fuselage includes a ceiling and a lateral portion of fuselage delimiting a cabin. The cabin trim panel also includes at least one technical equipment item mounted on the lateral portion of fuselage and at least one trim panel intended for at least partially concealing from the cabin, the at least one technical equipment item. The at least one trim panel is mounted rotatable about a horizontal axis of rotation on the ceiling between a trimming position so the trim panel at least partially conceals the at least one technical equipment item from the cabin by being held on the lateral portion of fuselage and a maintenance position so the trim panel is arranged at a distance from the lateral portion of fuselage in a substantially vertical plane to free access to the at least one technical equipment item.

Abstract: A reclining aircraft seat structure, and associated aircraft cabin, the structure includes a base, a carriage, supported by the base, the carriage including a front edge and a rear edge, a seat pan support, articulated on the carriage about a transverse front axis, located between the front edge and the rear edge and a backrest support, articulated with respect to the seat pan support, about a transverse rear axis, located to the rear of the front axis. The structure also includes an actuator including a deployable rod between a retracted position and a deployed position, the deployable rod being articulated on a lower arm of the backrest support in a rear articulation point. The rear articulation point is located behind the front articulation axis over at least part of the travel of the deployable rod between the retracted position and the deployed position.

Abstract: A support device for an aircraft cabin interior layout assembly comprises a fixed frame extending according to a longitudinal direction; and a table comprising a tray deployable relative to the frame between a retracted configuration and a deployed configuration. The tray extends horizontally in the retracted configuration and in the deployed configuration and is displaceable in rotation about a first axis of rotation, substantially parallel, while remaining horizontal between the retracted configuration and the deployed configuration. The tray is displaceable in translation relative to the frame in the longitudinal direction between a first position of use and a second position of use when the tray is in the deployed configuration, while being fixed in rotation about the first rotation axis.