Abstract: The present invention provides an aircraft seat unit comprising a main seat, and a companion seat, the main seat and the companion seat facing each other, wherein the companion seat comprises a seat pan, providing a seat pan surface, and a moveable seat element, the moveable seat element being moveable in relation to the seat pan between a stowed position, in which the companion seat provides an additional support surface for a main passenger in the main seat, and a deployed position, in which the moveable seat element provides a backrest surface for a companion passenger in the companion seat. The invention also provides a method of deploying and a method of stowing a companion seat.

Abstract: The present invention relates to an assembly of individual seats intended to be installed in an aircraft cabin, the assembly comprising: —a first seat and a second seat, a central console arranged between the first seat and the second seat, the central console comprising a first foot area and a second foot area extending in two opposite directions, —a seat surface width of the first seat being smaller in a portion of the seat opposite the second foot area in relation to a width of a portion of the seat surface opposite the first foot area so as to increase a space between the seat surface of the first seat and the second foot area.

Abstract: Described are torque bearing assemblies for passenger seats. A torque bearing attachment (122, 222, 322, 422) includes an elongated body having a forward edge configured to mate with an aft end (140) of a seat bottom pan (120), and first and second side edges having attachment elements (136) for connecting the assembly with a passenger seat frame (108). The first and second side edges can be positioned orthogonal to the forward edge and at opposite ends of the elongated body with respect to each other.

Abstract: Described are privacy screens and privacy assemblies for passenger seats including a frame defining a perimeter of the privacy screen and shaped to partially wrap around a portion of a passenger seat, a textile shell connected with and surrounding the frame, and a sound-absorbing layer positioned within the frame and surrounded by the textile shell for conferring physical, visual, and sound privacy for an occupant.

Abstract: The invention relates to a safety belt, which is in particular intended to be installed in an aircraft seat, comprising: a closing loop comprising a male element and a female element, a first strap which is connected to the male element and a second strap which is connected to the female element, the first strap and the second strap being capable of being attached together by means of the closing loop, which can change from an open state to a closed state through cooperation between the male element and the female element, the safety belt further comprising: a system for detecting that the safety belt is in the closed stated, the system being capable of generating an information item relating to a closed state of the safety belt, and a system for detecting that the safety belt is in a mechanically tensioned state, said system being capable of generating an information item relating to a mechanically tensioned state of at least one strap of the safety belt.

Abstract: A passenger seat assembly can include a seat frame; a seat back supported by the seat frame, comprising a rearward surface, and moveable between a stowed position and a deployed position; and a monitor shroud positioned proximate to the rearward surface of the seat back and fixedly coupled to a stationary surface, wherein the monitor shroud remains stationary as the seat back moves between the stowed position and the deployed position, and the monitor shroud defines an opening that provides access to the rearward surface of the seat back.

Abstract: The invention relates to a seat, in particular for an aircraft, including: a seat support, a seat base, a backrest hinged relative to the seat base by means of a pivot link, a leg rest hinged relative to the seat base by means of a pivot link, the seat being able to move between a sitting position and a bed position in which the backrest and the leg rest are situated in a continuation of the seat base, the seat base being mounted so as to be able to slide relative to the seat support, the seat comprising at least one connecting rod, referred to as the backrest pivot connecting rod, comprising a first end connected in rotation relative to the backrest and a second end connected in rotation relative to the seat support, the leg rest being mechanically connected to the backrest by means of a connecting rod deployment device, the seat further comprising a single actuator capable alone of moving a set of components of the seat formed at least by the seat base, the backrest, and the leg rest in order to move the

Abstract: A movable close-out shroud suitably configured to substantially cover, partially block, or otherwise close out an articulating opening to a cavity, void, etc., of a first part, such as a passenger seat section. The close-out shroud is configured to move between a stored position and a close-out position.

Abstract: Described are passenger seats having a seat frame and a seat bottom slidingly and pivotally attached to the seat frame that, when the passenger seats are reclined, are configured to articulate forward from an upright configuration of the passenger seat to a second seat position corresponding to a reclined configuration of the passenger seat. The seat bottom can include an aft articulating mechanism that defines a declining first path in an aft-to-forward direction to cause the aft end of the seat bottom to drop when the seat bottom articulates forward; and a forward articulating mechanism connected with the seat bottom near a forward end of the seat bottom that defines a second path shaped to cause the forward end of the seat bottom to move upward when the seat bottom articulates forward, such that the seat bottom tilts aft in response to articulating forward when the passenger seat is reclined.

Abstract: A system for securing a passenger seat to a track can include a fitting coupled with or forming a portion of the passenger seat; a shear plunger coupled with the fitting including a shear plunger body defining a shear plunger locking surface; a guide pin assembly that may include a guide pin movable along a lift axis between a retracted state and an extended state and a locking member extending laterally from the guide pin that may travel in response to a movement of the guide pin from the retracted state to the extended state and may engage the shear plunger locking surface in response to a rotation of the guide pin in the extended state; and a quick install tool operable to raise and twist the guide pin assembly such that the locking member is held in tension against the shear plunger locking surface.

Abstract: Described are tray tables having a shroud and a core assembly. The shroud may form an outer surface of the tray table. The core assembly may be within the shroud and may include a top sheet, a bottom sheet, and a honeycomb core. The honeycomb core may be between the top sheet and the bottom sheet. The honeycomb core may define a plurality of cells.

Abstract: A passenger seat includes a spreader frame structure and a seat back pivotally attached to the spreader frame structure. At least one cable can pass through apertures between the seat back and the spreader frame structure. The seat can rotate between an upright configuration wherein the seat back is in a deployed position, and a break over configuration wherein the seat back is in a stowed position. The length of the at least one cable between the aperture in the seat back and the aperture in the spreader frame structure is approximately the same in the upright configuration and in the break over configuration.

Abstract: Described are tray table tuning mechanisms for a passenger seat. The tray table tuning mechanisms can include a pivot limiting member, a paddle arm deployment member, an adjustment plate, and a paddle arm. The paddle arm deployment member and the adjustment plate may be pivoted relative to the pivot limiting member. The paddle arm can include at least one stop member and may be pivotably coupled to the paddle arm deployment member. Additionally, the paddle arm may be pivoted between a stowed state and a deployed state. In the deployed state, the stop member can abut a portion of the adjustment plate to limit rotation of the paddle arm deployment member in a first direction.

Abstract: The present invention relates to a passenger seat (10), in particular for an aircraft cabin, comprising: —a headrest (11), —a backrest (12), —a seat member (13) and —at least one loudspeaker (18) for broadcasting a sound signal to a passenger, —the passenger seat (10) further comprising: —at least one detection means (20) for detecting the presence of the passenger or a part of the passenger's body, and —a control unit (24) configured to selectively command the activation or deactivation of the loudspeaker (18) and/or the modification of a characteristic of a sound signal broadcast by the loudspeaker (18) in accordance with at least one information item from: —an information item relating to the presence of the passenger or a part of the passenger's body determined using the detection means (20), or —an information item concerning the state of the aircraft cabin or aircraft.

Abstract: Described is a frame component for a passenger seat assembly. The frame includes a tubular frame component having a first portion and a second portion. The bent portion bends the frame at a non-zero angle within a plane. The tubular frame component includes a variable inner diameter such that the first portion of the tubular frame component has a first wall thickness and the bent portion of the tubular frame component has a second wall thickness that is different from the first wall thickness.

Abstract: A leg assembly for a passenger seat includes a base member (102), a leg (104B), and an adjuster (106). The leg includes an upper end (110) and a lower end (112). The upper end of the leg includes an aperture (126) configured to receive a base frame tube, and the lower end is pivotally connected to the base member such that the leg is pivotable forward and aft from a base position. The adjuster is configured to pivotally position the leg relative to the base member.

Abstract: Described are tray table assemblies for a passenger seat, such as an aircraft passenger seat. The tray table assembly includes a tray table with a top surface and a holder assembly. The holder assembly includes a first holder pivotably attached to the tray table and a second holder pivotably attached to the first holder.