Abstract: A method comprises storing first transaction data for a first transaction producing a first version of a first dataset, second transaction data for a second transaction transforming a first version of the first dataset to a second version of the first dataset, and third transaction data for a third transaction transforming the second version of the first dataset to a third version of the first dataset; storing dependency information indicating a first dependency of the third transaction on the second transaction and a second dependency of the second transaction on the first transaction; receiving a first instruction to revoke a first permission of a first user to access the second version of the first dataset; automatically revoking a certain permission of the first user to access the third version of the first dataset based on the dependency information.

Abstract: A method of deception detection based upon ocular information of a subject provides a video camera configured to record a close-up view of a subject's eye. A cognitive state model is configured to determine a high to a low cognitive load experienced by the subject. An emotional state model is configured to determine a high to a low state of arousal experienced by the subject. After asking a question, the ocular information is processed to identify changes in ocular signals of the subject. The cognitive state and emotional state models are evaluated based solely on the changes in ocular signals where a probability of the subject being either truthful or deceptive is estimated for a binary output.

Abstract: A cockpit center console armrest includes a base member configured for mounting to a floor, an extending member mechanically coupled to the base member, and an armrest mechanically coupled to the extending member. The extending member includes an inner telescoping member configured for sliding within an outer telescoping member for adjusting a height of the armrest. A lever exposed on an underside of the armrest is configured for actuating a release mechanism. The release mechanism is configured for releasably securing the inner telescoping member to the outer telescoping member. A pivot axis pivotably couples the extending member to the base member such that the extending member is rotatable for rotating the armrest between a deployed orientation and a retracted orientation.

Abstract: A cockpit center console armrest includes a base member configured for mounting to a floor, an extending member mechanically coupled to the base member, and an armrest mechanically coupled to the extending member. The extending member includes an inner telescoping member configured for sliding within an outer telescoping member for adjusting a height of the armrest. A lever exposed on an underside of the armrest is configured for actuating a release mechanism. The release mechanism is configured for releasably securing the inner telescoping member to the outer telescoping member. A pivot axis pivotably couples the extending member to the base member such that the extending member is rotatable for rotating the armrest between a deployed orientation and a retracted orientation.

Abstract: A substructure in an aircraft cabin includes a drawer-insert accepting portion that defines multiple racks. Each rack may receive an exchangeable drawer insert. A module-accepting portion of the substructure defines an opening that includes a supporting surface, a back wall which extends upward and outward, and a lateral side wall. A module is provided for optionally installing in the module-accepting portion. The module has concealed areas upon installing that include: (i) a base adapted to rest on the supporting surface, (ii) a side wall adapted to abut the lateral side wall, and (iii) a rear wall adapted to abut the back wall. The module has exposed surfaces upon installing that are adapted to match an existing profile of the drawer-insert accepting portion. The module-accepting portion is configured for stowing cargo in a first mode and for receiving the module in a second mode. The module may include a locking assembly.

Abstract: A substructure in an aircraft cabin includes a drawer-insert accepting portion that defines multiple racks. Each rack may receive an exchangeable drawer insert. A module-accepting portion of the substructure defines an opening that includes a supporting surface, a back wall which extends upward and outward, and a lateral side wall. A module is provided for optionally installing in the module-accepting portion. The module has concealed areas upon installing that include: (i) a base adapted to rest on the supporting surface, (ii) a side wall adapted to abut the lateral side wall, and (iii) a rear wall adapted to abut the back wall. The module also has exposed surfaces upon installing that are adapted to match an existing profile of the drawer-insert accepting portion. The module-accepting portion is configured for stowing cargo in a first mode and for receiving the module in a second mode.

Abstract: A multi-function credenza includes at least one cabinet with a first top surface and a seat adjacent the cabinet. The seat has a convertible seat back for converting to a second top surface adjacent to the first top surface when the seat is stowed. A multi-function credenza in an aircraft cabin includes a first cabinet that has a first inboard panel and a first top surface, a second cabinet that has a second inboard panel and a second top surface, and a stowable seat located between the first cabinet and the second cabinet. A stowable seat includes a seat back that has a first side adapted for seating in a first mode and a second side adapted as a working surface in a second mode. The seat back articulates between the first mode and the second mode for deploying and stowing the seat, respectively.

Abstract: In one aspect, a cannulation site selection apparatus includes a flexible member, a first marking on the flexible member, and an array of cannulation site selection markings on the flexible member, wherein the array of cannulation site selection markings is positioned at a set distance from the first marking, and wherein the cannulation site selection markings are spaced at set distances from one another.

Abstract: An adaptable skylight includes a frame facing an interior of an enclosure having an opening for allowing light to pass. An opacity-control pane adjacent the opening allows a variable amount of light to pass, and an artificial light source illuminates the frame. An aircraft skylight assembly includes a variable pane, an artificial light source for illuminating portions of the skylight assembly, and a controller configured for adjusting an amount of external light transmission through the variable pane and an amount of artificial light illumination. An internal ambiance lighting system includes the adaptable skylight having a dimmable pane for providing transmission of a variable amount of external light into an enclosure, the artificial light illuminates the frame surrounding the adaptable skylight, and the controller automatically adjusts external light transmission through the adaptable skylight and illumination of the frame based on a lighting preference.

Abstract: In one aspect, a cannulation site selection apparatus includes a flexible member, a first marking on the flexible member, and an array of cannulation site selection markings on the flexible member, wherein the array of cannulation site selection markings is positioned at a set distance from the first marking, and wherein the cannulation site selection markings are spaced at set distances from one another.

Abstract: A substructure in an aircraft cabin includes a drawer-insert accepting portion that defines multiple racks. Each rack may receive an exchangeable drawer insert. A module-accepting portion of the substructure defines an opening that includes a supporting surface, a back wall which extends upward and outward, and a lateral side wall. A module is provided for optionally installing in the module-accepting portion. The module has concealed areas upon installing that include: (i) a base adapted to rest on the supporting surface, (ii) a side wall adapted to abut the lateral side wall, and (iii) a rear wall adapted to abut the back wall. The module also has exposed surfaces upon installing that are adapted to match an existing profile of the drawer-insert accepting portion. The module-accepting portion is configured for stowing cargo in a first mode and for receiving the module in a second mode.

Abstract: An adaptable skylight includes a frame facing an interior of an enclosure having an opening for allowing light to pass. An opacity-control pane adjacent the opening allows a variable amount of light to pass, and an artificial light source illuminates the frame. An aircraft skylight assembly includes a variable pane, an artificial light source for illuminating portions of the skylight assembly, and a controller configured for adjusting an amount of external light transmission through the variable pane and an amount of artificial light illumination. An internal ambiance lighting system includes the adaptable skylight having a dimmable pane for providing transmission of a variable amount of external light into an enclosure, the artificial light illuminates the frame surrounding the adaptable skylight, and the controller automatically adjusts external light transmission through the adaptable skylight and illumination of the frame based on a lighting preference.

Abstract: A multi-function credenza includes at least one cabinet with a first top surface and a seat adjacent the cabinet. The seat has a convertible seat back for converting to a second top surface adjacent to the first top surface when the seat is stowed. A multi-function credenza in an aircraft cabin includes a first cabinet that has a first inboard panel and a first top surface, a second cabinet that has a second inboard panel and a second top surface, and a stowable seat located between the first cabinet and the second cabinet. A stowable seat includes a seat back that has a first side adapted for seating in a first mode and a second side adapted as a working surface in a second mode. The seat back articulates between the first mode and the second mode for deploying and stowing the seat, respectively.

Abstract: A carrier composition having magnetite with a diameter of from about 80 microns to about 150 microns, and wherein the carrier has a conductivity of from about 10?8 to about 10?11 (ohms-cm)?1 and a carrier breakdown voltage of from about 20 to about 200 volts, and a developer composition with toner and this carrier composition, and also including a developer housing apparatus and an electrostatographic apparatus comprising the developer housing apparatus.