Abstract: The invention relates to an item of furniture, in particular for an aircraft seat, comprising: a frame, a movable element, a pivot connection for rotating the movable element relative to the frame between a folded position and a deployed position, a locking finger, a cam provided with a locking recess and an elastic member for biasing, when it is under tension, the locking finger inside the locking recess when the movable element is in the folded position, such that pressure on the movable element causes the elastic member to rotate the movable element and release the locking finger from the locking recess to enable the movable element to rotate towards the deployed position in a second direction of rotation.

Abstract: The invention relates to an item of furniture, in particular for an aircraft seat, comprising: a frame, a movable element, a pivot connection for rotating the movable element relative to the frame between a folded position and a deployed position, a locking finger, a cam provided with a locking recess and an elastic member for biasing, when it is under tension, the locking finger inside the locking recess when the movable element is in the folded position, such that pressure on the movable element causes the elastic member to rotate the movable element and release the locking finger from the locking recess to enable the movable element to rotate towards the deployed position in a second direction of rotation.

Abstract: The invention relates to a method for integrating and executing a software application to be implemented by a medical imaging platform running a file system. Such a method comprises a step of reading an agreement dedicated to a software application, the agreement comprising the access paths for input and/or output directories of the file system in order to write and/or read the values of the input/output data of the software application. The invention further relates to a medical imaging platform suitable for implementing such a method for integrating and executing software applications.

Abstract: A seat that can be converted between an upright position and a bed position, includes a mechanism for deploying an armrest, The mechanism includes a first guide connection comprising a first roller mechanically connected to the moving part associated with the seat-cushion portion, the first roller collaborating with a first slot formed in the armrest, and a second guide connection comprising a second roller mechanically connected to a fixed part, the second roller collaborating with a second slot formed in the armrest, such that a movement of the seat-cushion portion of the seat as the seat transitions from the upright position to the bed position causes the armrest to move from the up position to the down position.

Abstract: A seat that can be converted between an upright position and a bed position, includes a mechanism for deploying an armrest, The mechanism includes a first guide connection comprising a first roller mechanically connected to the moving part associated with the seat-cushion portion, the first roller collaborating with a first slot formed in the armrest, and a second guide connection comprising a second roller mechanically connected to a fixed part, the second roller collaborating with a second slot formed in the armrest, such that a movement of the seat-cushion portion of the seat as the seat transitions from the upright position to the bed position causes the armrest to move from the up position to the down position.

Abstract: The present invention relates essentially to a double-door module for aircraft seats, characterized in that it comprises: a first door that is mobile in translation between a stowed position and a deployed position, a second door that is mobile in translation between a stowed position and a deployed position, the first door and the second door overlapping completely when the first door and the second door are simultaneously in the stowed position, and a control system comprising a device for locking and unlocking the first door and/or the second door.

Abstract: The present invention relates essentially to a double-door module for aircraft seats, characterized in that it comprises: a first door that is mobile in translation between a stowed position and a deployed position, a second door that is mobile in translation between a stowed position and a deployed position, the first door and the second door overlapping completely when the first door and the second door are simultaneously in the stowed position, and a control system comprising a device for locking and unlocking the first door and/or the second door.