Abstract: The invention relates to a seat unit, in particular for an aircraft cabin, comprising: a seat provided with seat cushion and backrest kinematics, and a seat-base structure on which the seat is mounted, the seat-base structure comprising a frame with a tubular structure comprising: a first lower tube and a second lower tube, the first lower tube and the second lower tube each carrying at least one bolt intended to be fastened to rails, and two fastening feet for fastening the seat cushion and backrest kinematics, a fastening foot being formed by a tube connected by one of its ends to the first lower tube of the frame and by its other end to the second lower tube of the frame.

Abstract: The present invention essentially relates to a method for assembling a beam and a structural element of an aircraft seat, characterised in that it comprises: a step of producing at least one recess in an inner face of a beam passage area of the structural element, a step of inserting the beam into the beam passage area, and a step of deforming the beam such that a deformed portion of the beam penetrates into the recess of the beam passage area.

Abstract: The invention relates to a method for manufacturing a finished part comprising: a step of placing a trimmed finishing shell inside a heated mold chosen from a first mold referred to as a female mold and a second mold referred to as a male mold in the form of a punch, a step of heating a structural part made of a composite material up to its melting point, a step of placing the structural part on the finishing shell, a step of shaping the structural part against the finishing shell by means of the male mold in the form of a punch cooperating with the female mold, such that the finishing shell is fixed to the structural part that was shaped to obtain the finished part.

Abstract: The present invention essentially relates to a method for assembling a beam and a structural element of an aircraft seat, characterised in that it comprises: a step of producing at least one recess in an inner face of a beam passage area of the structural element, a step of inserting the beam into the beam passage area, and a step of deforming the beam such that a deformed portion of the beam penetrates into the recess of the beam passage area.

Abstract: Described are seating arrangements having at least one aisle column with at least one high bed seating unit and at least one low bed seating unit, and at least one non-aisle column having at least one high bed seating unit and at least one low bed seating unit. The at least one high bed seating unit in the at least one aisle column is positioned laterally proximate the at least one low bed seating unit in the at least one non-aisle column, and the at least one low bed seating unit in the at least one aisle column is positioned laterally proximate the at least one high bed seating unit in the at least one non-aisle column.

Abstract: The invention relates to a method for assembling a first metal part with a second part made of a composite material comprising at least one matrix and fibers arranged inside the matrix. The method comprises at least: a step of forming the first part, consisting in producing a plurality of teeth projecting from a contact face of the first part, two adjacent teeth being separated from each other by an interstitial space, the teeth having an end protuberance; and a step of pressing the second part against the first part, in such a way that the fibers of the composite material can penetrate inside the interstitial space defined between adjacent teeth and that the fibers are retained by the end protuberances of the teeth.

Abstract: Described are seat track fittings (100) with a stud (102) having a spacer (104) separated from a lower flange (106), and a locking mechanism (110). The locking mechanism includes an elastic fitting (112) having an upper arm (116a) and a lower arm (116b) connected by a resilient member (120). An end of the upper arm and an end the lower arm are coupled to the stud, with the end of the upper arm positioned above the spacer, and the end of the lower arm positioned above the lower flange. An activation mechanism (114) is coupled to the elastic fitting to transition the seat track fitting between unloaded, unlocked, and locked positions.

Abstract: The present invention generally relates to passenger seats. Some embodiments are related to a compact seat kinematic for moving a seat from a retracted position to an extended position. In some embodiments an intermediate component may be provided for coupling between a lower frame and an upper seat portion. The intermediate component (230) may translate in a forward direction relative to the lower frame and may translate the upper seat portion in the forward direction relative to the intermediate component. Other embodiments relate to a seat backrest recline system that may provide constant ratio of speed and force and may forgo the need for calibration.

Abstract: Arrangements of at least one column of seats for passengers of a vehicle, the column including a next-front seat unit positioned in front of a next-back seat unit. Each seat unit includes a seat having a chair position and a bed position, and a bed extension coupled to the next-front seat unit. The bed extension has a stowed position within the next-front seat unit and a deployed position that is located within a space between the next-front seat unit and the next-back seat unit that is not occupied by the seat in the next-back seat unit when the seat in the next-back seat unit is positioned in the bed position.

Abstract: The present invention generally relates to passenger aircraft seats. The disclosure focuses on a seat unit arrangement (10) for a cabin and seat units that provide different comfort positions. In some embodiments, a side cushion (14) forms part of a bed surface when the seats are converted to a bed position. In some embodiments, a bed extension (30) is deployed from a stowed position to form a part of the bed surface. In some embodiments, a seat backrest (22) does not form part of the bed surface when the seat unit is in the bed position. In some embodiments, a lounge position is provided when the seat backrest rotates toward a side cushion. In such an embodiment, the passenger may be positioned toward the side cushion such that the passenger may comfortably rest their legs on the side cushion without converting the seat to a bed position.

Abstract: Described are base frame assemblies (10) for a passenger seat including a main frame (12) with a seat support structure (16) and a lateral support structure (18), wherein the lateral support structure (18) includes two seat fittings (28), and the seat support structure includes one seat fitting (30), and a secondary frame (14) pivotally coupled to the main frame (16), wherein the secondary frame (14) includes one seat fitting (50). A passenger seat (20) and a surrounding monument (26) are mounted to the base frame assembly (10).

Abstract: Described are seat track fittings (100) with a stud (102) having a spacer (104) separated from a lower flange (106), and a locking mechanism (110). The locking mechanism includes an elastic fitting (112) having an upper arm (116a) and a lower arm (116b) connected by a resilient member (120). An end of the upper arm and an end the lower arm are coupled to the stud, with the end of the upper arm positioned above the spacer, and the end of the lower arm positioned above the lower flange. An activation mechanism (114) is coupled to the elastic fitting to transition the seat track fitting between unloaded, unlocked, and locked positions.

Abstract: Embodiments of the present invention provide an improved pivot articulation for a kinematic seat. Certain embodiments provide an elastic pivot that is formed as flexion weaves that connect upper and lower portions of a seat back. The flexion weaves may be inner and outer legs that are curved in configuration or that have bent dimensions.

Abstract: Described are seating arrangements having at least one aisle column with at least one high bed seating unit and at least one low bed seating unit, and at least one non-aisle column having at least one high bed seating unit and at least one low bed seating unit. The at least one high bed seating unit in the at least one aisle column is positioned laterally proximate the at least one low bed seating unit in the at least one non-aisle column, and the at least one low bed seating unit in the at least one aisle column is positioned laterally proximate the at least one high bed seating unit in the at least one non-aisle column.

Abstract: An airbag system assembly configured to be positioned in the interior of a vehicle that includes an aft wall configured to be positioned forward of a passenger seat and an airbag system. The aft wall includes front and aft surfaces and the aft wall includes a first flap that is formed by a plurality of weakness lines in at least the front surface thereof. The airbag system includes at least a first airbag module having a first airbag support plate with front and aft surfaces. The first airbag support plate is secured to the front surface of the aft wall, and the first airbag support plate includes a first airbag that is configured to deploy in the event of a crash condition and that is disposed on the aft surface of the first airbag support plate. The first airbag is positioned adjacent the first flap.

Abstract: Embodiments of the present invention provide an airbag system formed of a plurality of tubular structures.

Abstract: Described are arrangements of at least one column of seats for passengers of a vehicle, the column including a next-front seat unit positioned in front of a next-back seat unit, wherein each seat unit includes a seat having a chair position and a bed position, and a bed extension coupled to the next-front seat unit. The bed extension has a stowed position within the next-front seat unit and a deployed position that is located within a space between the next-front seat unit and the next-back seat unit that is not occupied by the seat in the next-back seat unit when the seat in the next-back seat unit is positioned in the bed position.

Abstract: The present invention generally relates to passenger seats. Some embodiments are related to a compact seat kinematic for moving a seat from a retracted position to an extended position. In some embodiments an intermediate component may be provided for coupling between a lower frame and an upper seat portion. The intermediate component (230) may translate in a forward direction relative to the lower frame and may translate the upper seat portion in the forward direction relative to the intermediate component. Other embodiments relate to a seat backrest recline system that may provide constant ratio of speed and force and may forgo the need for calibration.

Abstract: The present invention generally relates to passenger aircraft seats. The disclosure focuses on a seat unit arrangement (10) for a cabin and seat units that provide different comfort positions. In some embodiments, a side cushion (14) forms part of a bed surface when the seats are converted to a bed position. In some embodiments, a bed extension (30) is deployed from a stowed position to form a part of the bed surface. In some embodiments, a seat backrest (22) does not form part of the bed surface when the seat unit is in the bed position. In some embodiments, a lounge position is provided when the seat backrest rotates toward a side cushion. In such an embodiment, the passenger may be positioned toward the side cushion such that the passenger may comfortably rest their legs on the side cushion without converting the seat to a bed position.

Abstract: Described are base frame assemblies (10) for a passenger seat including a main frame (12) with a seat support structure (16) and a lateral support structure (18), wherein the lateral support structure (18) includes two seat fittings (28), and the seat support structure includes one seat fitting (30), and a secondary frame (14) pivotally coupled to the main frame (16), wherein the secondary frame (14) includes one seat fitting (50). A passenger seat (20) and a surrounding monument (26) are mounted to the base frame assembly (10).