An economy class (Y class) private suite includes a continuous seatback and a stowable aisle-side panel. The continuous seatback covers the gaps between seats of a 3-seat or 4-seat PAX and the stowable aisle-side panel slides to close off the PAX from the aisle when desirable. Each seat in the PAX includes an extension element to extend from the anterior surface of the seat cushion and establish a substantially flat surface including the seat cushions and extension elements. A separate padded element may be placed over the substantially flat surface. Each seatback cushion in the PAX is removable and reconfigurable as a reclining support or expanded armrest.

An aircraft interior structure may include a galley section with a galley cart portion and a passenger seating section proximate to a passenger compartment. The galley cart portion may include at least one galley cart cavity configured to receive one or more galley carts. The galley cart portion may be accessible from a floor area of an aircraft cabin. The passenger seating section may include a footwell. The footwell may be integrated or may be part of an auxiliary aircraft interior structure. The footwell may be at least partially inserted within the galley cart section. The footwell may be surrounded at least in part within the galley section by the at least one galley cart cavity. The footwell may correspond to an aircraft seat within the passenger compartment. The aircraft seat may be configured to form a bed surface when the aircraft seat is in a lie-flat position.

A seat assembly includes a base structure having at least one of a seat pan shell and a backrest shell, and one or more attachment structures configured to removably couple at least one of the seat pan shell and the backrest shell to a seat surface arrangement or a utility surface arrangement. The base structure is convertible between a passenger seat and a utility element based on the coupling of the seat surface arrangement or the utility surface arrangement, respectively, to the base structure.

An aircraft passenger seating unit and aircraft seating arrangements including seating units, each seating unit configured as a window-facing seating unit or as an aisle-facing seating unit. Each individual seating unit including first and second laterally adjacent seats mounted on a common platform and oriented at an angle to a longitudinal aircraft axis. A forwardmost point of each of the first and second seats, when in an upright sitting position, resides along a plane common to both the first and second passenger seats perpendicular to the longitudinal aircraft axis to allow longitudinal alignment of rows and increased seating density.

The present invention relates to a console for a seat unit comprising: an upper wall forming a table surface on which a passenger can place objects, a cavity, an articulated arm fixed to an internal face of the cavity, said articulated arm comprising a holding device for a portable electronic device provided with a screen, said articulated arm being movable between a stored position, in which the articulated arm is located inside the cavity, and a extended position in which the articulated arm is at least in part outside the cavity.

An aircraft passenger compartment suite may include a first side with a first display device, a second side with a second display device, and a privacy divider separating the first side and the second side. The first display device may be configured to actuate between a first deployed position and a first stowed position via a first stowage mechanism. The second display device may be configured to actuate between a second deployed position and a second stowed position via a second stowage mechanism. The privacy divider may include one or more panels configured to actuate between a panel deployed position and a panel stowed position. The privacy divider may be open when at least one of the first display device is in the first stowed position, the second display device is in the second stowed position, or the one or more panels are in the panel stowed position.

A sleeping assist device for providing help for both obese and non-obese passengers to sleep while traveling on an airplane consists of a primary model for non-obese passengers and a second model for obese passengers. The primary device includes an adjustable length support tube that rests on the lap of the passenger during use. A face sleeping cushion is adjusted in height using a pair of tubes with a tube locking mechanism that can be locked to set the height. A pair of locking mechanisms are attached to a cushion support plate and allow the tilt angle of the face cushion to be adjusted. An adjustable length belt attached to the cushion support plate is used to hold the device securely using two airplane seat mounting brackets. A security ring is welded to the lower tube to prevent the device being used as a weapon by use of a steel wire cable that attaches to the security ring and to a second ring mounted to the passenger seat mounting frame.

The secondary device for obese passengers also includes an adjustable length support tube that rests on the lap of the passenger during use. A face sleeping cushion is adjusted in height using a locking mechanism that can be locks the position between the lower tube and a first bar. The first bar and a second bar connected to the cushion support plate are fixed in both angular and translational position by using a thumb screw to adjust cushion tilt and a locking mechanism to adjust the translation of the second bar. An adjustable length belt attached to the cushion support plate is used to hold the device securely using two airplane seat mounting brackets. A security ring is welded to the lower tube to prevent the device being used as a weapon by use of a steel wire cable that attaches to the security ring and to a second ring mounted to the passenger seat mounting frame.

A device for controlling a balance of an urban air mobility, may include a receiver configured to receive occupant information related to the urban air mobility from a cloud server; and a controller configured to control the balance of the urban air mobility according to the received occupant information.

An aircraft monument for use in a cabin of an aircraft includes a monument assembly and a seat assembly. The monument assembly includes a frame having a plurality of walls defining a compartment. The plurality of walls include a first end wall having a forward section at a forward plane of the frame. The compartment is defined rearward of the forward section. The seat assembly is forward of the frame. The seat assembly has a shell configured to at least partially surround a passenger seat. The shell has a rear rearward of the forward plane of the frame.

An aircraft seating module (20) includes a seating mount (26) having a horizontal mounting rail (28) integrally joined to a vertical mounting post (30) at an adjoining elbow (32). The rail (28) includes a mounting boss (34) longitudinally spaced from the post (30) for attachment to an aircraft cabin seat track (18). Both the rail (28) and post (30) include mounting holes (38) for attaching a passenger seat (22) and appended furniture (24) directly to the seating mount (26) and in turn indirectly to the seat track (18) in the cabin floor (12).