Abstract: The present invention relates to an aircraft seat unit, comprising: a seat that can be moved between a seated position and a reclining position and a privacy shield extending at least partly around the seat, the privacy shield comprising a fixed portion and a movable portion that can be moved relative to the fixed portion, the movable portion being movable between: a retracted position in which the movable portion delimits, with the fixed portion, a partially enclosed space around the seat to give the passenger privacy and a deployed position in which the movable portion is at a distance from the seat so as to free up space for accessing the seat.

Abstract: The invention relates to a support pallet comprising: a body, lock attachment means each created in a portion of the body, the lock attachment means each making it possible to establish an attachment between the body and a seat rail lock or with an intermediate connecting part, seat unit attachment means each created in a portion of the body, the seat unit attachment means each making it possible to establish a connection between the body and an element of the seat unit, the portions of the body comprising the lock attachment means and the portions of the body comprising the seat unit attachment means, and the rest of the body forming a single monolithic part.

Abstract: The invention mainly relates to a detachable device for closing a space inside an airplane, comprising: a frame comprising at least one upright, the frame comprising at least one attachment interface with a structural element, a curtain assembly comprising a flexible curtain, a roller around which the flexible curtain can be wound, and at least one guide device comprising an electric-motor actuator, the guide device being capable of translationally guiding the flexible curtain relative to the upright such that the flexible curtain can be moved in a direction of movement parallel to a longitudinal direction of the upright between a stowed position in which the flexible curtain is mainly wound around the roller and an extended position in which the flexible curtain is mainly unwound relative to the roller.

Abstract: Disclosed is a lightweight seat (100) that includes a seat base (102), a seat bottom (103) attached to an upper portion of the seat base, a seat back (101) attached to a rear portion of the seat bottom, and a seat belt assembly (150) secured to the seat bottom. The seat belt assembly may include a strap (104) attached to an underside of the seat bottom and extending from a first end adjacent to first side of the seat bottom to a second end adjacent to a second side of the seat bottom and a seat belt disposed adjacent to an upper side of the seat bottom, wherein a first end of the seat belt is attached to the first end of the strap and a second end of the seat belt is attached to the second end of the strap.

Abstract: The invention relates to an aircraft seat attachment (100) including a body (20), a plunger (30), and an activation lever (50). The activation lever (50) includes a locking system (54) adapted to go from an open position corresponding to a free state of the activation lever (50) to a closed position corresponding to a locked state of the activation lever (50). The attachment also enables, in a locked state of said attachment, clamping of a seat rail between at least one boss (22) of said body (20) and the plunger (30), which includes a system (41) for maintaining by friction a force clamping the attachment to the rail in the locked state so that the activation lever (50) does not participate in maintaining said clamping force.

Abstract: Disclosed is a lightweight seat (100) that includes a seat base (102), a seat bottom (103) attached to an upper portion of the seat base, a seat back (101) attached to a rear portion of the seat bottom, and a seat belt assembly (150) secured to the seat bottom. The seat belt assembly may include a strap (104) attached to an underside of the seat bottom and extending from a first end adjacent to first side of the seat bottom to a second end adjacent to a second side of the seat bottom and a seat belt disposed adjacent to an upper side of the seat bottom, wherein a first end of the seat belt is attached to the first end of the strap and a second end of the seat belt is attached to the second end of the strap.

Abstract: This invention concerns mainly a handle system with two locking latches (7, 8) called “self-locking”, independent one from the other for locking, but fitted with a single unlocking paddle (6). This system is fitted with indicators, which: detect the door's opening and closing and indicate separately the locking of the two latches (7, 8).

Abstract: Described are tray table assemblies having a table body (12), a support arm (14) comprising a support portion (18) coupled to the table body and a coupling portion (20), a center console (44) comprising a table storage compartment (52) and a track (44), wherein the track (44) is located between the table storage compartment (52) and a location forward of the table storage compartment, and the table storage compartment (52) is located above an armrest support (42), and a linkage comprising a head (28) and a base (30), wherein the head (28) is rotatably coupled to the coupling portion (29) of the support arm (14), and the base (30) is slidingly coupled to the track (40). The table body may configured to slide between a stowed position within the table storage compartment to a raised position and to rotate between the raised position and a deployed position forward of a passenger seat.

Abstract: The invention relates to an aircraft seat attachment (100) including a body (20), a plunger (30), and an activation lever (50). The activation lever (50) includes a locking system (54) adapted to go from an open position corresponding to a free state of the activation lever (50) to a closed position corresponding to a locked state of the activation lever (50). The attachment also enables, in a locked state of said attachment, clamping of a seat rail between at least one boss (22) of said body (20) and the plunger (30), which includes a system (41) for maintaining by friction a force clamping the attachment to the rail in the locked state so that the activation lever (50) does not participate in maintaining said clamping force.

Abstract: This invention concerns mainly a handle system with two locking latches (7,8) called “self-locking”, independent one from the other for locking, but fitted with a single unlocking paddle (6). This system is fitted with indicators, which: detect the door's opening and closing and indicate separately the locking of the two latches (7, 8).