Abstract: A method for providing landing assistance for an aircraft is provided. The method analyzes terrain data; identifies one or more landing zones, based on analyzing the terrain data, each of the one or more landing zones comprising a flat area lacking obstacles to aircraft landing; and presents the one or more landing zones via a display element onboard the aircraft.

Abstract: Methods and devices for scheduling operation of residential energy consumption devices are described herein. One device includes a memory and a processor. The processor can be configured to execute executable instructions stored in the memory to form a number of chains of residential energy consumption devices, wherein each of the number of chains includes different devices, determine which of the number of chains has a largest total energy consumption over a particular period of time, and determine, for the devices in the chain having the largest total energy consumption over the particular period of timed of time, an operational schedule having a lowest possible cost.

Abstract: In some examples, an integrated circuit system includes a plurality of integrated circuit layers. At least one of the integrated circuit layers includes an integrated circuit die, which may not include any through-silicon vias that provide a pathway to an adjacent integrated circuit layer, and an interposer portion, which includes electrically conductive through-vias. The interposer portion may facilitate communication of the integrated circuit die with other integrated circuit layers of the integrated circuit system. In some examples, the stacked integrated circuit system may include more than one integrated circuit die, which may be in the same integrated circuit layer as at least one other integrated circuit die, or may be in a different integrated circuit layer.

Abstract: Aluminum iron based alloys and methods for producing the same are provided. In an exemplary embodiment, a method for producing an aluminum iron based alloy includes melting an aluminum iron based alloy to form a melt. The aluminum iron based alloy includes iron at about 2.0 to about 7.5 weight percent, silicon at about 0.5 to about 3.0 weight percent, aluminum at about 86 to about 97.5 weight percent, and one or more of manganese, vanadium, chromium, molybdenum, tungsten, niobium, zirconium, cerium, erbium, magnesium, calcium, scandium, ytterbium, yttrium, or tantalum at about 0.05 to about 3.5 weight percent. The melt is solidified at about 105 degrees centigrade per second of faster to form particulates. The particulates are degassed at a degassing temperature of about 400 to about 500 degrees centigrade.

Abstract: Embodiments relate generally to methods and systems for detecting pressure. A pressure sensor assembly may comprise a sensor unit having a pressure input port on one side, the sensor unit comprising a printed circuit board; a pressure sensor secured to a side of the printed circuit board; a support secured to the side of the printed circuit board, the support circumferentially surrounding the pressure sensor and defining the pressure input port; and a media isolation layer comprising a first media isolation layer applied adjacent to the pressure sensor, and a second media isolation layer comprising a material different from the first media isolation layer located between the first media isolation layer and the pressure input port, wherein the media isolation layer is configured to transfer a pressure caused by a sense media to the pressure sensor.

Abstract: GBAS includes reference receivers, processing module, and communication device. Processing module checks GNSS satellite measurements to determine proximity of GNSS satellite measurement's IPP to IGPs derived from SBAS geostationary satellites. Processing module determines that GNSS satellite measurement is safe for mitigation using overbounded Vertical Ionosphere Gradient standard deviation sigma-vig (?vig) when IGPs possess acceptable GIVE values. Processing module determines whether number of GNSS satellite measurements determined safe for mitigation using ?vig are able to produce VPL that meets VAL required for precision approach.

Abstract: A method and system for an onboard reporting system capable of detecting keywords in voice data and considering the keywords in combination with respective predefined instructions is provided. The provided system uses, for each keyword, predefined instructions to validate the keyword prior to sending a report.

Abstract: A single event effects (SEE) immune linear voltage regulator includes an input node, an output node, a first transistor control logic, a second transistor control logic, a first transistor, and a second transistor. The regulator is configured such that when the first transistor is operating in linear regulation mode, the second transistor automatically operates in saturation mode, and the voltage at the output node is controlled by the first transistor and the first transistor control logic to be substantially equal to the first reference voltage. Conversely, when the second transistor is operating in linear regulation mode, the first transistor automatically operates in saturation mode, and the voltage at the output node is controlled by the second transistor and the second transistor control logic to be substantially equal to the second reference voltage.

Abstract: Heating, ventilation, and air conditioning (HVAC) controllers are described herein. One method includes receiving an approximate relationship between each of a number of controlled and manipulated variables of an HVAC system, designating one of the number of controlled variables as a primary controlled variable, determining operating parameters for each of the number of manipulated variables that maintain the primary controlled variable based, at least in part, on the approximate relationship between the primary controlled variable and each respective manipulated variable, and determining operating parameters for each of the number of manipulated variables that maintain each of the other controlled variables based, at least in part, on the approximate relationship between each respective other controlled variable and each respective manipulated variable and the determined operating parameters for each of the number of manipulated variables that maintain the primary controlled variable.

Abstract: Systems and methods for regulating weather information collection are provided. In one embodiment, a method for managing the collection of weather information comprises: determining whether or not a weather data processing system is in a state open to receiving weather information; communicating to a first aircraft when the weather data processing system is in a state open to receiving weather information; and upon receiving weather information at the weather data processing system from the first aircraft, transmitting a signal indicating that the weather data processing system is not in a state open to receiving weather information.

Abstract: In some examples, a method for forming a carbon fiber preform includes depositing, via a print head of a three-dimensional printing system, a first plurality of carbon fibers to form a first layer of carbon fibers in approximately an x-y plane, wherein the first plurality of carbon fibers are deposited around an array of carbon fiber filaments extending in approximately a z-axis direction relative to the x-y plane.

Abstract: A turbocharger includes a variable-nozzle turbine having a variable vane assembly formed as a cartridge. A pipe-shaped insert of the cartridge fits into an axial bore in the turbine housing. The variable vane assembly includes a nozzle ring to which the variable vanes are mounted. A composite heat shroud is disposed between and axially compressed between the turbocharger's center housing and the nozzle ring. The heat shroud is constructed such that heating of the shroud causes the shroud to deform so as to increase the axial preload exerted by the shroud. In one embodiment the heat shroud is a two-layer structure in which the two layers are formed of different materials having different coefficients of thermal expansion.

Abstract: A method of predicting a parameter for an aircraft includes detecting an actual approach profile of the aircraft. The actual approach profile includes an actual approach angle. The method also includes comparing, by a processor, the actual approach profile to a predetermined approach profile to determine a difference between the actual and predetermined approach profiles. The predetermined approach profile includes a predetermined approach angle. The method further includes determining, by the processor, an effective approach angle by combining the actual approach angle and the predetermined approach angle according to a factor that varies based on the difference between the actual and predetermined approach profiles. Moreover, the method includes determining, by the processor, the predicted parameter based on the effective approach angle.

Abstract: Systems and methods for verified threat detection are provided. Some systems can include a sensor monitoring an ambient region and an image capturing device, wherein, upon the sensor detecting an alarm condition in the ambient region, the image capturing device is activated for capturing an image of the ambient region to determine whether the image is consistent with the alarm condition.

Abstract: Systems and methods for measuring velocity with a radar altimeter are provided. In at least one embodiment a method for measuring velocity magnitude of a platform in relation to a surface comprises transmitting a radar beam, wherein the radar beam is aimed toward a surface; receiving a plurality of reflected signals, wherein the plurality of reflected signals correspond to portions of the transmitted radar beam that are reflected by a plurality of portions of the surface; and applying Doppler filtering to the plurality of signals to form at least one Doppler beam. The method also comprises identifying range measurements within each Doppler beam in the at least one Doppler beam; and calculating the velocity magnitude based on the range measurements of the at least one Doppler beam.

Abstract: Disclosed is an integrated manufacturing process to co-produce (E) 1-chloro-3,3,3-trifluoropropene, (E) 1,3,3,3-tetrafluoropropene, and 1,1,1,3,3-pentafluoro-propane starting from a single starting feed material or a mixture of unsaturated hydrochlorocarbon feed materials comprising 1,1,1,3-tetrachloropropene and/or 1,1,3,3-tetrachloropropene. The process includes a combined liquid or vapor phase reaction/purification operation which directly produces (E) 1-chloro-3,3,3-trifluoro-propene (1233zd (E)) from these feed materials, which may also include 240fa. In the second liquid phase fluorination reactor 1233zd (E) is contacted with HF in the presence of catalyst to produce 1,1,1,3,3-pentafluoropropane (245fa) with high conversion and selectivity. A third reactor is used for dehydrofluorination of 245fa to produce (E) 1,3,3,3-tetrafluoropropene (1234ze (E)) by contacting in the liquid phase with a caustic solution or in the vapor phase using a dehydrofluorination catalyst.

Abstract: This invention pertains to a method for removing acidic impurity from halogenated olefins, especially methods for removing acidic impurity from halogenated propenes, and even more particularly to methods for removing acidic impurity from 1,3,3,3-tetrafluoro-1-propene (HFO-1234ze), 2,3,3,3-tetrafluoro-1-propene (HFO-1234yf), 1-chloro-3,3,3-trifluoro-1-propene (HCFO-1233zd), and 2-chloro-3,3,3-trifluoro-1-propene (HCFO-1233xf). The method is conducted by passing the halogenated olefin stream, in liquid or gas form, through a solid adsorbent bed, which contains at least one acid reactive agent.

Abstract: A constant current regulator for airfield ground lighting is described herein. For example, one or more embodiments include a power converter configured to receive a signal from an alternating current (AC) mains, where the power converter includes a number of bi-directional switches, a transformer configured to isolate the AC signal from an airfield ground lighting circuit, and a rectifier configured to convert the signal from the AC mains from AC to direct current (DC), an inverter configured to convert the DC signal from the power converter and convert the DC to AC, an output filter configured to receive the AC signal from the inverter and send the AC signal to the airfield ground lighting circuit, and a controller configured to switch the number of bi-directional switches of the power converter to allow an input voltage and current of the signal from the AC mains to be in phase.

Abstract: A low powered system for providing sufficient current to a fuel control mechanism drive. The system may have a fuel control mechanism pick circuit that has an energy storage mechanism for providing a large amount of current for a short time to the fuel control mechanism drive. A safety switch may be enabled with a special signal to let current flow to the fuel control mechanism drive to operate a corresponding fuel control mechanism for controlling fuel to a pilot light or heating element. The pilot light or heating element may provide heat to a thermoelectric source that generates electrical power from the heat. The electrical power may go to a single DC-to-DC converter and voltage clamp for providing a voltage source to a microcontroller and other circuits of the system. The pick circuit may prevent a harmful reverse flow of current from the storage mechanism to the thermoelectric source.

Abstract: A composition comprising from about 40 weight percent to about 99.9 weight percent of at least one C1-C5 hydrofluorocarbon, from about 0.1 weight percent to about 50 weight percent of CF3I, and from about 0.1 weight percent to about 10 weight percent of at least one C1-C6 hydrocarbon and the use of these composition for in methods of the recharging of refrigeration systems.