Abstract: A method, a system, and a computer program product for operating a communication device. A location information of a communication device is received. Based on the location information of the communication device, it is determined whether the communication device and another communication device are co-located. Based on the determination, operation of the communication device is controlled.

Abstract: An aircraft tail section has a first tail component and a second tail component, the first tail component being positioned further forward than the second tail component with respect to a nose of the aircraft. Each tail component has two surfaces, each of the two surfaces of at least one of the first and second tail components comprises a solar panel configured to collect solar energy. Each tail component is rotatable with respect to a centerline of the aircraft such that an offset angle of between zero degrees and 180 degrees is formed between corresponding surfaces of the first and second tail components. Preferably, the tail components are rotated into (i) a takeoff and landing configuration that is substantially horizontal, and (ii) a crosswise configuration during flight such that collection of solar energy is maximized.

Abstract: An energy management system and method can include functions such as monitoring a status of the electrical energy storage device; receiving a first demand from a first power load for electrical power, and determining whether to supply the electrical power to satisfy the first demand from the electrical energy storage device or from one or more power sources connected to the energy management system. The determining can include applying an algorithm to determine a power provision arrangement based on at least one preset criteria. The algorithm can have data input that includes the status of the electrical energy storage device, one or more load characteristics of the first power load and any other loads supplied with electrical power from the energy management system, and one or more source characteristics of each of the one or more power sources. Electrical power can be supplied to the first power load in satisfaction of the first demand and in accordance with the determined power provision arrangement.

Abstract: Methods, program products, and systems for monitoring extrinsic processes are described. A monitoring process can monitor one or more target processes. The target processes can be extrinsic, e.g., not spawned by the monitoring process. The monitoring process reads a process registry to identify which processes among multiple processes to monitor. The monitoring process can send status requests to the identified target processes periodically to check whether the target processes are healthy. If a target process is terminated, the monitoring process determines whether the termination is normal (e.g., by a user), or abnormal (e.g., the target process crashed). The monitoring process can restart the abnormally terminated or hung target process.

Abstract: An example airbag assembly includes an airbag and a duct having an opening for venting gas. The duct moves between a first position where the opening is outside the airbag and a second position where the opening is inside the airbag. Inflating the airbag moves the duct between the first position and the second position.

Abstract: An example airbag assembly includes an airbag and a duct. The duct has a duct opening for venting gas. The duct is moveable between a first position where the duct opening is outside the airbag and a second position where the duct opening is inside the airbag. Inflating the airbag moves the duct between the first position and the second position. The airbag is configured to be inflated by a first stream of gas moving from the duct opening to an interior of the airbag and by a second stream of gas moving from an airbag inflator to the interior of the airbag. The first stream of gas is separate from the second stream of gas.

Abstract: An example airbag arrangement includes an airbag that is moveable to an expanded position. The airbag has a contact area. A panel is secured exclusively to the airbag. A portion of the airbag extends through an aperture in the panel when the airbag is in the expanded position. The panel alters expansion of the contact area.

Abstract: A medicament dispensing cabinet is comprised of a frame, at least one controller, and a plurality of drawers each movably carried by the frame and each defining a plurality of dispensing cells. A plurality of removable dispensing devices is provided with each one carried by one of the dispensing cells. Each of the dispensing cells further comprises a motor for providing rotary motion to one of the removable dispensing devices in response to the controller, a sensor operating in conjunction with the controller for counting medicament dispensed from one of the removable dispensing devices, a chute for receiving medicament dispensed from one of the removable dispensing devices and a chute gate for controlling access to the chute. The cabinet may additionally comprise a chute gate release responsive to the controller for controlling the chute gate and a chute gate sensor connected to the controller and responsive to the position of the chute gate.

Abstract: Systems 100, 1000, methods, and machine-interpretable programming or other instruction products for the management of data processing by multiple networked computing resources 106, 1106. In particular, the disclosure relates to the synchronization of related requests for processing of data using distributed network resources.

Abstract: A system and method are provided for a short take-off and landing/vertical take-off and landing aircraft that stores required take-off power in the form of primarily an electric fan engine, and secondarily in the form of an internal combustion engine, wherein the combined power of the electric fan and internal combustion engines can cause the STOL/VTOL A/C to take-off in substantially less amount of time and space than other STOL/VTOL A/C, and further wherein the transition from vertical to horizontal thrust is carefully executed to rapidly rise from the take-off position to a forward flight position, thereby minimizing the necessity for a larger electric fan engine.

Abstract: A medicament dispensing cabinet is comprised of a frame, at least one controller, and a plurality of drawers each movably carried by the frame and each defining a plurality of dispensing cells. A plurality of removable dispensing devices is provided with each one carried by one of the dispensing cells. Each of the dispensing cells further comprises a motor for providing rotary motion to one of the removable dispensing devices in response to the controller, a sensor operating in conjunction with the controller for counting medicament dispensed from one of the removable dispensing devices, a chute for receiving medicament dispensed from one of the removable dispensing devices and a chute gate for controlling access to the chute. The cabinet may additionally comprise a chute gate release responsive to the controller for controlling the chute gate and a chute gate sensor connected to the controller and responsive to the position of the chute gate.

Abstract: An example airbag arrangement includes an airbag that moves between an expansion-constrained position and an expanded position. A tether adjacent an exterior surface of the airbag moves with the airbag between a shorter position and a longer position. The tether remains intact in the shorter position and the longer position. When the tether is in the shorter position, the tether holds the airbag in the expansion-constrained position.

Abstract: A system and method for assembling and operating a solar powered aircraft, composed of one or more modular constituent wing panels. Each wing panel includes at least one hinge interface that is configured to rotationally interface with a complementary hinge interface on another wing panel. When a first and second wing panel are coupled together via the rotational interface, they can rotate with respect to each other within a predetermined angular range. The aircraft further comprises a control system that is configured to acquire aircraft operating information and atmospheric information and use the same alter the angle between the wing panels, even if there are multiple wing panels. One or more of the wing panels can include photovoltaic cells and/or solar thermal cells to convert solar radiation energy or solar heat energy into electricity, that can be used to power electric motors.

Abstract: The present disclosure relates to an aircraft having a fuselage. The fuselage may have a plurality of frame members, a cabin formed within the fuselage, a floor defining a portion of the cabin, a center section of seats disposed on the floor, a crown positioned above a center section of seats, and a crew rest module. The crew rest module may have an entrance module defined by at least two entrance module peripheral walls and having a seating area, and a bunk module being separate from the seating area and being defined by at least three bunk module peripheral walls. The entrance module peripheral walls and the bunk module peripheral walls may be sized to fit through a passenger door of a substantially assembled aircraft.

Abstract: An administration server in a database management system retrieves log files in a plurality of formats from a plurality of clients through helper programs running on the clients. The plurality of clients can include Web servers, application servers, and database servers. The log files can be generated by software modules on the clients. An administration engine converts log entries in the log files into a unified format for display. The converted log entries can be stored in a log database. Upon a user request, the administration server presents the log entries to the user in a log viewer. The log viewer can display log entries originated from heterogeneous software modules in a unified view.

Abstract: A passenger airbag module includes opposite side walls connected by a rear wall. The side walls each include at least one inward projection that traps a semi-cylindrical retainer between the projections and the rear wall. The retainer holds the inflator and airbag within the housing. End walls connect the side walls with interlocking channels thereby preventing the side walls from releasing the retainer, inflator and airbag.

Abstract: The invention discloses several types of fastener, fastening systems, fastener assemblies and related areas. In particular, the invention discloses a releasable fastening system (150) which has a pin (152) with a locking cavity (163). The pin is intended for insertion in an aperture (154). A locking means (158, 160) engages the locking cavity (163) of the pin (152) when the pin (152) is received in the aperture (154). The system (150) also includes unlocking means (162) which includes material adapted to contract when activated. When a material contracts, engagement means (158) included in the locking means (158, 160), disengage the locking cavity (154).

Abstract: A system for deploying a deployable structure in an aircraft, comprising a drogue parachute, at least one deployable structure, a riser line attached to the drogue parachute and the at least one deployable structure, wherein when the drogue parachute is deployed, a tension is applied to the riser line, and a parachute deployment system, wherein the parachute deployment system is configured to utilize the applied tension to deploy the at least one deployable structure.