Abstract: Aspects of this disclosure relate to one or more particles that move within a container in response to a magnetic field. A measurement circuit is configured to output an indication of the magnetic field based on position of the one or more particles.

Abstract: A system may have a support structure that separates an exterior region from an interior region. The system may include a lighting system with interior and/or exterior lights with adjustable diffusers. An interior light may be used as a task light, a cabin light, a sensor indicator light, or a trim light. Adjustments to the adjustable diffusers can be used to adjust the angular spread of emitted light for operation in different lighting modes.

Abstract: Aspects of this disclosure relate to particles that can move in response to a magnetic field. A system can include a container, particles within the container, and a magnetic structure integrated with the container. The magnetic structure can magnetically interact with both an external magnetic field and the particles. Related methods are disclosed including magnetic field detection methods based on detection of particles within a container.

Abstract: The present disclosure generally relates to methods for managing charging of an electronic device.

Abstract: An in-flight entertainment (IFE) system for an aircraft includes a phased array antenna and control circuitry associated therewith to be carried by the aircraft and to generate dual antenna beams for television programming and Internet data from respective spaced apart satellites. A television programming distribution system is to be carried by the aircraft and coupled to the phased array antenna and control circuitry to provide television programming within the aircraft. At least one access point is to be carried by the aircraft and coupled to the phased array antenna and control circuitry to provide a wireless local area network (WLAN) within the aircraft for the Internet data.

Abstract: A communications system is for an aircraft carrying at least some personnel having PEDs, and the communications system may include a ground-based communications network, and a satellite-based communications network. The system may include at least one access point in the aircraft for providing a wireless local area network (WLAN) within the aircraft to receive a web content request from a given PED and transmit corresponding web content to the given PED. An air-to-ground communications device in the aircraft may cooperate with the at least one access point for sending the web content request to the ground-based communications network defining a return link. Further, a satellite communications device in the aircraft may cooperate with the at least one access point for receiving the corresponding web content from the satellite-based communications network defining a forward link.

Abstract: An in-flight entertainment (IFE) system for an aircraft includes a phased array antenna and control circuitry associated therewith to be carried by the aircraft and to generate dual antenna beams for television programming and Internet data from respective spaced apart satellites. A television programming distribution system is to be carried by the aircraft and coupled to the phased array antenna and control circuitry to provide television programming within the aircraft. At least one access point is to be carried by the aircraft and coupled to the phased array antenna and control circuitry to provide a wireless local area network (WLAN) within the aircraft for the Internet data.

Abstract: An in-flight entertainment (IFE) system for an aircraft includes a phased array antenna and control circuitry associated therewith to be carried by the aircraft and to generate dual antenna beams for television programming and Internet data from respective spaced apart satellites. A television programming distribution system is to be carried by the aircraft and coupled to the phased array antenna and control circuitry to provide television programming within the aircraft. At least one access point is to be carried by the aircraft and coupled to the phased array antenna and control circuitry to provide a wireless local area network (WLAN) within the aircraft for the Internet data.

Abstract: A system is provided that includes a control panel of a security system that protects a secured geographic area, wherein a controller enters a set-up mode in response to detecting entry of a code by an authorized user through a user interface and opening of an access door and wirelessly pairs a portable device carried by the authorized user with the control panel and registers the portable device with the controller while in the set-up mode, wherein, when operating in a normal operating mode, the controller detects the portable device and automatically forms a wireless control connection between the portable device and the control panel, and wherein the controller enters a log-on mode during set-up in response to connecting to the portable device and allows the authorized user to unlock the access door and enter a password at the controller, thereby enabling service and control from the portable device.

Abstract: A system providing a control panel of a security system that protects a secured geographic area, the controller entering a set-up mode in response to detecting entry of a code by an authorized user through the user interface and opening an access door, wirelessly pairing a portable device carried by the user with the control panel and registering the portable device with the controller while in the set-up mode, operating in the normal operating mode detecting the registered portable device and automatically forming a wireless control connection between the proximate portable device and the control panel, wherein the controller enters a log-on mode during set-up in response to connecting to the wireless device and allows the authorized user to unlock the access door and enter a password at the controller enabling service and control from the wireless device.

Abstract: An aircraft in-flight entertainment (IFE) system for an aircraft includes a radome to be carried by the aircraft, and a dual-beam satellite antenna and at least one positioner coupled thereto to be carried by the aircraft and protected by the radome. The dual-beam satellite antenna is to generate dual antenna beams for television programming and Internet data from respective spaced apart satellites. The dual-beam satellite antenna includes a first aperture for receiving the television programming, and a second aperture adjacent the first aperture for receiving the Internet data. A television programming distribution system is to be carried by the aircraft and coupled to the dual-beam satellite antenna to provide television programming within the aircraft. At least one access point is to be carried by the aircraft and coupled to the dual-beam satellite antenna to provide a wireless local area network (WLAN) within the aircraft for the Internet data.

Abstract: A video file system for an aircraft carrying a person having a personal electronic device (PED) for displaying video files includes a ground-based video server and an aircraft-based video system. The ground-based video server stores video files, with each video file being updatable from an available status to an unavailable status. The aircraft-based video system copies video files from the ground-based video server while the aircraft is on the ground. A determination is made, via communications with the ground-based video server and while the aircraft is on the ground, whether a given video file has been updated from the available status to the unavailable status. The PED is permitted to display the given video file if it has the available status, and is not permitted to display the given video file if it has the unavailable status.

Abstract: Systems and methods for riser coupling are disclosed. A riser coupling system comprises a riser joint connector comprising a first tubular assembly coupled to a second tubular assembly. The riser coupling system further comprises a spider assembly which receives the riser joint connector and has a connector actuation tool. The connector actuation tool comprises a dog assembly, a clamping tool and a splined member. The dog assembly selectively extends a dog to engage the riser joint connector. The clamping tool couples the first tubular assembly and the second tubular assembly. Finally, the splined member actuates a locking member of the riser joint connector.

Abstract: A communications system is for an aircraft carrying at least some personnel having PEDs, and the communications system may include a ground-based communications network, and a satellite-based communications network. The system may include at least one access point in the aircraft for providing a wireless local area network (WLAN) within the aircraft to receive a web content request from a given PED and transmit corresponding web content to the given PED. An air-to-ground communications device in the aircraft may cooperate with the at least one access point for sending the web content request to the ground-based communications network defining a return link. Further, a satellite communications device in the aircraft may cooperate with the at least one access point for receiving the corresponding web content from the satellite-based communications network defining a forward link.

Abstract: A method for drilling a wellbore includes drilling the wellbore by injecting drilling fluid into a top of a tubular string disposed in the wellbore at a first flow rate and rotating a drill bit. The tubular string includes: the drill bit disposed on a bottom thereof, tubular joints connected together, a longitudinal bore therethrough, a port through a wall thereof, and a sleeve operable between an open position where the port is exposed to the bore and a closed position where a wall of the sleeve is disposed between the port and the bore. The method further includes moving the sleeve to the open position; and injecting drilling fluid into the port at a second flow rate while adding a tubular joint(s) to the tubular string. The injection of drilling fluid into the tubular string is continuously maintained between drilling and adding the joint(s).

Abstract: Systems and methods for riser coupling are disclosed. A riser coupling system comprises a riser joint connector comprising a first tubular assembly coupled to a second tubular assembly. The riser coupling system further comprises a spider assembly which receives the riser joint connector and has a connector actuation tool. The connector actuation tool comprises a dog assembly, a clamping tool and a splined member. The dog assembly selectively extends a dog to engage the riser joint connector. The clamping tool couples the first tubular assembly and the second tubular assembly. Finally, the splined member actuates a locking member of the riser joint connector.

Abstract: An in-flight entertainment (IFE) system for an aircraft includes a phased array antenna and control circuitry associated therewith to be carried by the aircraft and to generate dual antenna beams for television programming and Internet data from respective spaced apart satellites. A television programming distribution system is to be carried by the aircraft and coupled to the phased array antenna and control circuitry to provide television programming within the aircraft. At least one access point is to be carried by the aircraft and coupled to the phased array antenna and control circuitry to provide a wireless local area network (WLAN) within the aircraft for the Internet data.

Abstract: An in-flight entertainment (IFE) system for an aircraft includes a phased array antenna and control circuitry associated therewith to be carried by the aircraft and to generate dual antenna beams for television programming and Internet data from respective spaced apart satellites. A television programming distribution system is to be carried by the aircraft and coupled to the phased array antenna and control circuitry to provide television programming within the aircraft. At least one access point is to be carried by the aircraft and coupled to the phased array antenna and control circuitry to provide a wireless local area network (WLAN) within the aircraft for the Internet data.

Abstract: Embodiments of the invention generally relate to tools and methods for hanging and/or expanding liner strings. In one embodiment, a method of hanging a liner assembly from a previously installed tubular in a wellbore includes running the liner assembly and a setting tool into the wellbore using a run-in string. The setting tool includes an isolation valve and the liner assembly includes a liner hanger and a liner string. The method further includes sending an instruction signal from the surface to the isolation valve, wherein the isolation valve closes in response to the instruction signal and isolates a setting pressure in the setting tool from the liner string; and increasing fluid pressure in the setting tool, thereby setting the liner hanger.

Abstract: A method for drilling a wellbore includes drilling the wellbore by injecting drilling fluid into a top of a tubular string disposed in the wellbore at a first flow rate and rotating a drill bit. The tubular string includes: the drill bit disposed on a bottom thereof, tubular joints connected together, a longitudinal bore therethrough, a port through a wall thereof, and a sleeve operable between an open position where the port is exposed to the bore and a closed position where a wall of the sleeve is disposed between the port and the bore. The method further includes moving the sleeve to the open position; and injecting drilling fluid into the port at a second flow rate while adding a tubular joint(s) to the tubular string. The injection of drilling fluid into the tubular string is continuously maintained between drilling and adding the joint(s).