Abstract: The current invention pertains to a computer-implemented method, a method, a use thereof, a computer system and a computer program product for determining a potential for anomalous activity by a suspect user, particularly for detecting fraud and most particularly for detecting money laundering.

Abstract: The current invention pertains to a computer-implemented method, a method, a use thereof, a computer system and a computer program product for determining a potential for anomalous activity by a suspect user, particularly for detecting fraud and most particularly for detecting money laundering.

Abstract: A seat assembly for a vehicle includes a backrest. A tray table is moveably coupled to the backrest. The tray table is configured to be moved between a stowed position and a deployed position. A literature pocket is formed in the backrest. The literature pocket is disposed between the tray table in the stowed position and a rear surface of the backrest. In an embodiment, a device support is moveably coupled to the literature pocket. The device support is moveable between a support stowed position and a support deployed position that is configured to support a device.

Abstract: The current invention pertains to a computer-implemented method, a method, a use thereof, a computer system and a computer program product for determining a potential for anomalous activity by a suspect user, particularly for detecting fraud and most particularly for detecting money laundering.

Abstract: Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.

Abstract: An overhead stowage bin assembly having a bin structure with a lower panel and an open side that defines a front of the stowage bin assembly. The lower panel has a leading edge that is arranged at the front of the stowage bin assembly. A cover is formed by base plates and a central plate and is secured to the lower panel to form a passage. The central plate has protruding ribs that are aligned to increase the stiffness of the cover and the rigidity of the lower panel. A threshold has walls that are connected to each other and define a channel. The leading edge of the lower panel is received within the channel such that the threshold walls mate with opposite surfaces of the lower panel so as to grip the leading edge of the panel and further enhance the stiffness of the lower panel.

Abstract: A seat assembly for a vehicle includes a backrest. A tray table is moveably coupled to the backrest. The tray table is configured to be moved between a stowed position and a deployed position. A literature pocket is formed in the backrest. The literature pocket is disposed between the tray table in the stowed position and a rear surface of the backrest. In an embodiment, a device support is moveably coupled to the literature pocket. The device support is moveable between a support stowed position and a support deployed position that is configured to support a device.

Abstract: Systems and methods are provided for integrating a fluidized coking process with a catalyst-enhanced coke gasification process. The catalyst for the gasification process can correspond to calcium oxide, a thermally decomposable calcium salt, a potassium salt such as potassium carbonate, or a combination thereof. Examples of suitable calcium salts can include, but are not limited to, calcium hydroxide, calcium nitrate, and calcium carbonate. The calcium oxide, potassium salts, and/or thermally decomposable calcium salts can be introduced into the integrated system, for example, as part of the feed into the coker. It has been unexpectedly discovered that using catalytic gasification as part of an integrated fluidized coking and gasification process can result in an overhead gas stream from the gasifier with increased energy content and/or overhead gas pressure.

Abstract: Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.

Abstract: Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.

Abstract: Components and systems of an aircraft seating assembly are disclosed. The aircraft seating assembly can include a seat pan, a connection frame, and one or more mounts for removably coupling the seat pan to the connection frame. The aircraft seating assembly can include a back support having a removably coupled cushioning member. The aircraft seating assembly can include a tilt system which can allow the back support to articulate relative to the connection frame. The aircraft seating assembly can include a retention system coupled to the back support, the retention system can retain an object in place when in a closed configuration.

Abstract: Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.

Abstract: Components and systems of an aircraft seating assembly are disclosed. The aircraft seating assembly can include an adjustable headrest that allows the headrest to be translated and/or rotated relative to a seat, a storage sleeve, and/or a spreader. The aircraft seating assembly can include an energy absorption system. The energy absorption system can include bracket which can control pivoting of a seat back relative to the bracket when subject to forces exceeding a threshold force. The energy absorption system can include a movable wall coupled to the seat.

Abstract: Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.

Abstract: Components and systems of an aircraft seating assembly are disclosed. The aircraft seating assembly can include a seat pan, a connection frame, and one or more mounts for removably coupling the seat pan to the connection frame. The aircraft seating assembly can include a back support having a removably coupled cushioning member. The aircraft seating assembly can include a tilt system which can allow the back support to articulate relative to the connection frame. The aircraft seating assembly can include a retention system coupled to the back support, the retention system can retain an object in place when in a closed configuration.

Abstract: Dynamic support systems (10) include a plurality of support members (12), a base material (14), and a support layer (18). Each support member (12) has an upper support surface (20) extending from a first end of a stud (22), and a spherical member (28) extending from a second end of the stud. The base material (14) includes a plurality of receptacles (40) having a socket (42) with a recessed area (52) for positioning a spring (56). The support layer (18) also includes a plurality of apertures (64) that are positioned over the receptacles (40) and allow the studs (22) to extend there through.

Abstract: Described are seat units having a lower support structure with at least two leg supports, each leg support integrally formed into an arcuate shape, and an upper support structure having a seat pan and seat back integrally formed into a single component. Each leg support is coupled to at least two base frame tubes by insertion of each base frame tube through an aperture in each of the leg supports, wherein the aperture is shaped to prevent rotation of the leg support about a longitudinal axis of each of the at least two base frame tubes. Each seat support is coupled to the base frame tubes by insertion of each base frame tube through a slot in each of the upper support structure.

Abstract: Components and systems of an aircraft seating assembly are disclosed. The aircraft seating assembly can include an adjustable headrest that allows the headrest to be translated and/or rotated relative to a seat, a storage sleeve, and/or a spreader. The aircraft seating assembly can include an energy absorption system. The energy absorption system can include bracket which can control pivoting of a seat back relative to the bracket when subject to forces exceeding a threshold force. The energy absorption system can include a movable wall coupled to the seat.

Abstract: Components and systems of an aircraft seating assembly are disclosed. The aircraft seating assembly can include a seat pan, a connection frame, and one or more mounts for removably coupling the seat pan to the connection frame. The aircraft seating assembly can include a back support having a removably coupled cushioning member. The aircraft seating assembly can include a tilt system which can allow the back support to articulate relative to the connection frame. The aircraft seating assembly can include a retention system coupled to the back support, the retention system can retain an object in place when in a closed configuration.

Abstract: Dynamic support systems (10) include a plurality of support members (12), a base material (14), and a support layer (18). Each support member (12) has an upper support surface (20) extending from a first end of a stud (22), and a spherical member (28) extending from a second end of the stud. The base material (14) includes a plurality of receptacles (40) having a socket (42) with a recessed area (52) for positioning a spring (56). The support layer (18) also includes a plurality of apertures (64) that are positioned over the receptacles (40) and allow the studs (22) to extend there through.