Abstract: Examples are disclosed that relate to a mobile device configured to change a feature set in response to detecting that a case is attached to the mobile device. One example provides a method enacted on a mobile device. The method comprises operating the mobile device with a first feature set. The first feature set comprises one or more features enabled when a case is not attached to the mobile device. The method further comprises detecting that the case is attached to the mobile device and an identity of the case by using a magnetic sensor. The method further comprises operating the mobile device with a second feature set that is different from the first feature set in response to detecting that the case is attached to the mobile device. The second feature set is selected based upon the identity of the case.

Abstract: The invention refers to a device (100) for detecting a working status of a medical implant (130), like a stent or bone implant, wherein a micro device (131) is integrated in and/or attached to the implant and comprises a magneto-mechanical oscillator configured to transduce a magnetic excitation field into a magnetic response field, wherein the response field is indicative of a temperature change of the micro device. The device comprises a transmit/receive unit (110) adapted to generate the excitation field, detect the response field, and transduce the detected response field into an electric response signal, and a controller (120) adapted to control the transmit/receive unit and further adapted to determine a change in a temperature of the micro device based on the electric response signal, and to determine the working status of the medical implant based on the determined change in the temperature of the micro device.

Abstract: A method of controlling an engine for a propeller-driven aircraft, including setting an initial maximum power limit, wherein the initial maximum power limit is associated with a maximum allowable thrust for an aircraft, receiving an indication that a predetermined aircraft condition is satisfied, and setting an updated maximum power limit.

Abstract: A method of controlling an engine for a propeller-driven aircraft, including setting an initial maximum power limit, wherein the initial maximum power limit is associated with a maximum allowable thrust for an aircraft, receiving an indication that a predetermined aircraft condition is satisfied, and setting an updated maximum power limit.

Abstract: A syngas treatment plant is configured to remove sulfurous compounds and carbon dioxide from shifted or un-shifted syngas in a configuration having a decarbonization section and a desulfurization section. Most preferably, the solvent in the decarbonization section is regenerated and cooled by flashing, while the solvent is regenerated in the desulfurization section via stripping using external heat, and it is still further preferred that carbonylsulfide is removed in the desulfurization section via hydrolysis, and that the so produced hydrogen sulfide is removed in a downstream absorber.

Abstract: A syngas treatment plant is configured to remove sulfurous compounds and carbon dioxide from shifted or un-shifted syngas in a configuration having a decarbonization section and a desulfurization section. Most preferably, the solvent in the decarbonization section is regenerated and cooled by flashing, while the solvent is regenerated in the desulfurization section via stripping using external heat, and it is still further preferred that carbonylsulfide is removed in the desulfurization section via hydrolysis, and that the so produced hydrogen sulfide is removed in a downstream absorber.

Abstract: A filter system has a first filter from which solvent is recovered in a cleaning cycle using a rinse fluid in forward flow, and from which particulates are removed using flush gas in reverse flow. At least part of the solvent and the flush gas are recycled to the system and in still further preferred aspects, filtration of the solvent continues during the cleaning cycle via a bypass circuit through which the solvent is routed to a second filter.

Abstract: LNG vapor from an LNG storage vessel is absorbed using C3 and heavier components provided by a fractionator that receives a mixture of LNG vapors and the C3 and heavier components as fractionator feed. In such configurations, refrigeration content of the LNG liquid from the LNG storage vessel is advantageously used to condense the LNG vapor after separation. Where desired, a portion of the LNG liquid may also be used as fractionator feed to produce LPG as a bottom product.

Abstract: A plant includes an absorber (103) that operates in a gas phase supercritical region and removes an acid gas from a feed stream (9) at high recovery of the feed stream (10) while producing a high purity acid gas stream (36). Particularly preferred plants include gas purification plants that receive a feed gas with at least 5 mol % carbon dioxide at a pressure of at least 3000 psi.

Abstract: Contemplated plants comprise an acid gas removal unit (102) that receives a compressed gas from an injection gas compressor (107), wherein acid gas is removed from the compressed gas in the acid gas removal unit (102) at a pressure of about of above pipeline pressure.

Abstract: A device for verifying the calibration of an infrared sensor includes a body configured to be placed in orbit. The body defines a spin axis and an outer surface. The outer surface has an infrared radiant intensity that is substantially independent of the viewing angle between the spin axis of the body and the infrared sensor. The device may be used for on-orbit verification of the calibration coefficients associated with each pixel of an infrared sensor, including linearity calibration and verification of the resolution capability of the sensor. The calibration coefficients may be verified over the entire sensing capability range of the infrared sensor. After a thermal model of the device is developed, the device operates passively and provides a known source of infrared radiation observable during the device's entire orbital lifetime. The device may be designed to automatically de-orbit from space after a predictable time in orbit.

Abstract: A plant includes an absorber (103) that operates in a gas phase supercritical region and removes an acid gas from a feed stream (9) at high recovery of the feed stream (10) while producing a high purity acid gas stream (36). Particularly preferred plants include gas purification plants that receive a feed gas with at least 5 mol % carbon dioxide at a pressure of at least 3000 psi.

Abstract: A compact, portable, radio-controlled on/off valve for use with a garden hose has low energy consumption by using a water-powered motor for driving the valve into open and closed positions. The on/off valve has a pilot device for starting water flow through the water-powered motor. A low-power local electrical energy source, such as a battery pack, powers the pilot device and a receiver for receiving control signals. Upon receiving a control signal, the pilot device is energized briefly to start water flow through the water-powered motor. The water-powered motor then moves the valve from a closed position to an open position, or from an open position to a closed position.