Honeywell Patente

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In some examples, a cooling system defines a first flow path for a first gas stream and a second flow path for a second gas stream. The cooling system is configured to merge the first gas stream and the second gas stream to produce a mixed gas stream and provide the mixed gas stream to cool a brake assembly of a wheel. Control circuitry is configured to adjust a flow rate of the second gas stream based on a pressure and/or other flow parameter of the first gas stream. In examples, the control circuitry is configured to initiate and/or substantially cease cooling to the brake assembly based on a temperature signal indicative of a temperature of the brake assembly.

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A vapor cycle cooling system includes first and second compressor (112B) systems in parallel with one another, each compressor system including a motor, a motor controller (180, 280, 380, 480), and a first compressor (112A, 212A) in series with a second compressor (112B);a condenser (102, 202, 302) fluidically coupled to each compressor system;a filter drier (138, 238, 338), in series with, and fluidically coupled to the condenser (102, 202, 302);a first expansion device in series with, and fluidically coupled to, a flash heat exchanger (106, 206), the flash heat exchanger (106, 206) fluidically coupled to a second expansion device, the second expansion device fluidically coupled to a first evaporator (266), the first evaporator (266) fluidically coupled to each compressor system;a system controller (180, 280, 380, 480) electrically coupled to each motor controller (180, 280, 380, 480);and a motor and motor controller (180, 280, 380, 480) cooling loop fluidically coupled to the filter drier (138, 238, 338) and each motor, wherein the vapor cycle cooling system is configured to cool one or more thermal loads (264) for a vehicle.

In some examples, a stator assembly includes a stator body including a base portion and a plurality of stator teeth projecting radially inward from the base portion. The stator assembly further includes an electrically conductive member wound about a tooth of the plurality of stator teeth to define a winding about the tooth, the winding comprising a single layer of the conductive member and including a plurality of turns of the electrically conductive member, wherein the electrically conductive member has a thickness in the radial direction that is less than its width in a direction perpendicular to the radial direction.

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Devices, methods, and systems having insect guards in devices and systems for aspirated smoke, gas, or air quality monitoring are described herein. One aspirated smoke, gas, or air quality monitoring unit includes a detector module that includes at least one particulate sensing chamber within the detector module and an air inlet connecting the sampling tube to the particulate sensing chamber allowing communication of air from the sampling tube to the particulate sensing chamber; and a spiral shaped insect guard positioned within the inlet.

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Methods, apparatuses and systems for providing dehumidification providing dehumidification for gas detecting components are disclosed herein. An example apparatus may comprise: a flow sensing component configured to detect a flow rate associated with a flowing media in a flow channel of the apparatus; and a controller component in electronic communication with the flow sensing component that is configured to receive a flow rate indication from the flow sensing component, and in response to determining that the flow rate indication satisfies a null condition threshold, apply an exponential smoothing function with a variable alpha value to condition an output signal of the apparatus.

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Disclosed are methods, systems, and non-transitory computer-readable medium for vehicle navigation processing. For instance, the method may include scanning for one or more terminals (111-117, 122, 124, 131-133) within a predetermined vicinity of the vehicle (131-133) via a low latency communication network and receiving positional data of the one or more terminals via the low latency communication network. The method may further include receiving directional data of the one or more terminals relative to the vehicle, determining a first location of the vehicle relative to the one or more terminals based on the directional data, and determining a second location of the vehicle relative to the environment based on the positional data and the first location.

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Embodiments of the present disclosure provide for generation and use of multiple representations of a processing plant, for example a refinery plant. In some embodiments a first representation is utilized to visualize the component(s) and/or connection(s) of the processing plant, with a second representation utilized to process one or more aspect(s) of the processing plant. The first representation in some embodiments represents the physical components and/or connections between such components to enable intuitive visualization and monitoring of the components thereof. The second representation in some embodiments represents a virtualized representation of the physical components and/or connections between such components in a manner that is better processable via one or more computing process(es). Such processing is performable to generate data for controlling configuration and/or operation of component(s) in the processing plant.

A method in an aircraft for identifying valid runway intersections for takeoff is provided. The method comprises: estimating a runway length required for takeoff based on aircraft parameters; estimating, at each of a plurality of runway intersections, a corrected runway length at the runway intersection by applying an elevation correction, a temperature correction, and a gradient correction; determining, based on the estimated runway length required for takeoff and the corrected runway length at each of the plurality of runway intersections, each valid runway intersection from the plurality of runway intersections whose corrected runway length is long enough for use by the aircraft for takeoff and each invalid runway intersection from the plurality of runway intersections whose corrected runway length is not long enough for use by the aircraft for takeoff; and signaling an aircraft display device to display on a map depicting the takeoff runway each invalid runway intersection.

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Methods and system for alerting descent with respect to at least one of minimum sector altitude, minimum safe altitude and terrain clearance floor in an aircraft. The methods and systems receive at least one of a minimum sector altitude value, a minimum safe altitude value and a terrain clearance floor value based on a flight plan of the aircraft or a location of the aircraft. A movement trajectory of the aircraft is predicted. The aircraft predicted movement trajectory is evaluated with respect to the at least one of the minimum sector altitude value, the minimum safe altitude value and the terrain clearance floor value. An alert is output when the evaluation predicts convergence of the aircraft predicted movement trajectory and the at least one of the minimum sector altitude value, the minimum safe altitude value and the terrain clearance floor value.

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Embodiments of the present disclosure provide techniques for generating emissions impact-optimized optimized paths. The techniques may include identifying input data set for a target vehicle operation, the input data set; determining using a machine learning optimization model, an emissions impact-optimized path based on the input data set and historical emissions impact data associated with a plurality of historical vehicle operations; evaluating the emissions impact-optimized path, based on one or more validation engines, to generate an evaluation output; and determining a validated emissions impact-optimized path for the target vehicle operation based on the emissions impact-optimized path and the evaluation output.

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