Abstract: Use of a bubble-generating mechanism in a production environment is described, The bubble generating mechanism may be used to facilitate the separation of a target fluid from a non-target fluid in the production environment, such as by creating a gradient of the fluids or creating separate and distinct zones of the fluids to be separated. The target fluid can then be preferentially recovered from the production environment based on the gradient or distinct zones.

Abstract: An inlet air conditioning system for a gas turbine includes an inlet duct for the with an air flow path to provide inlet air to the gas turbine; evaporative cooling media disposed in the air flow path; a water chiller; and a circulation pump that circulates water through the water chiller and the evaporative media in series. The chiller is configured to chill the water to below ambient wet-bulb temperature before the water is circulated to the evaporative cooling media. A power plant includes a gas turbine including a compressor, a combustion system, and a turbine section; a load; and the inlet air conditioning system.

Abstract: According to embodiments of the present invention, an air conduction sensor for detecting a sound from a user is provided. The air conduction sensor includes a housing comprising an opening, wherein a rim of the opening is configured to at least substantially attach to a skin or a clothing of the user; a microphone coupled to the housing such that there is an air gap between the microphone and the skin or the clothing, and wherein the microphone is configured to detect the sound. A system and a method for monitoring a health condition of a user are also provided.

Abstract: In a first embodiment, a system, including an exhaust duct configured to flow an exhaust gas, and an air injection system coupled to the exhaust duct, wherein the air injection system comprises a first air injector configured to inject air into the exhaust duct to assist flow of the exhaust gas through the exhaust duct.

Abstract: A metal sheathed cable includes an optical unit and a control unit helically twisted together, a grounding wire unit distributed in the gaps between the optical unit and the control unit to form an inner layer cable core, a filler watertightly filled into gaps among the optical unit, the control unit and the grounding wire unit, and a taped covering arranged outside the inner layer cable core; a power unit and a filling core helically twisted around the inner layer cable core, the grounding wire unit distributed in the gap between the power unit and the filling core, the filler watertightly filled into gaps among the power unit, the grounding wire unit and the filling core, and the taped covering arranged outside the outer layer cable core; an inner protective layer wrapped outside the outer layer core, and a sheathing layer twisted outside the inner protective layer.

Abstract: The present application provides a media pad for cooling an inlet air flow to a compressor of a gas turbine engine. The media pad may include a first media sheet with a chevron corrugated surface having a first mist eliminator and a second media sheet with a wavy corrugated surface having a second mist eliminator.

Abstract: A thermostatic valve includes a housing and a thermostatic actuating element, and the thermostatic actuating element includes a main body in which a thermosensitive substance is provided. The housing has an open end which is closed by a cap assembly. The thermostatic valve includes a first elastic element and a second elastic element, wherein the first elastic element is provided at a side of the cap assembly, and has one end abutting against the cap assembly, and another end directly abutting against or indirectly abutting against the piston at least during a moving process; the second elastic element is provided at a side of the third port, and has one end abutting against an inner wall or a bottom wall of the cavity of the housing, and another end abutting against the main body.

Abstract: Integrated circuit packages with openings surrounding a conductive via on a substrate layer are disclosed. An integrated circuit package may include a substrate layer with upper and lower surfaces. A conductive via may extend between the upper and lower surfaces of the substrate layer. The integrated circuit package further includes multiple openings in the substrate layer that may be distributed evenly in the substrate layer surrounding the conductive via. The multiple openings reduce signal insertion loss of the conductive via.

Abstract: The present application provides a power augmentation system for use with a gas turbine engine. The power augmentation system may include a compressor discharge manifold, an inlet bleed heat system in communication with the compressor discharge manifold via an inlet bleed heat line, and an auxiliary compressor in communication with the compressor discharge manifold via the inlet bleed heat line.

Abstract: The present application provides an inlet air cooling system for cooling a flow air in a gas turbine engine. The inlet air cooling system may include an inlet filter house, a transition piece, an inlet duct, and an inlet ultrasonic water atomization system positioned about the inlet filter house, the transition piece, or the inlet duct to cool the flow of air.

Abstract: An integrated circuit package substrate may include a core layer and dielectric layers formed on top and bottom surfaces of the core layer. Routing traces such as stripline structures may be formed in some of the dielectric layers, whereas plated through hole (PTH) structures may be formed through the core layer. A first pair of PTHs that carry a first differential signal may be orthogonally intertwined with a second pair of PTHs that carry a second differential signal. Solder balls formed at the surface of the package substrate may include a first pair of solder balls that convey a first differential signal that is orthogonally intertwined with respect to a second pair of solder balls that convey a second differential signal. The package substrate may be mounted on a printed circuit board (PCB). Differential PCB vias could use the same BGA orthogonal pattern described above.

Abstract: A system includes a gas turbine system, including an air intake system that includes a housing, a first plurality of air conditioning coils, a second plurality of air conditioning coils that is downstream relative to the first plurality, and a baffle extending between each of the first and second pluralities of air conditioning coils, wherein the baffle is configured to direct an air flow through the first or second pluralities of air conditioning coils in a closed position, and the baffle is configured to enable air flow to bypass the first and second pluralities of coils in an opened position.

Abstract: A heat exchanger and a gas-fired furnace including the same are provided. The heat exchanger includes at least two heat exchange shell enclosures; and at least three rows of heat exchange tubes arranged along a furnace air flow path. Each of the heat exchange tubes defines a leaving-tube-end and an entering-tube-end, two adjacent rows are spaced from each other, the at least three rows of heat exchange tubes are connected in a leaving-tube-end to entering-tube-end fashion sequentially via the at least two heat exchange shell enclosures to define a substantially serpentine flue gas passage.

Abstract: Embodiments of the present disclosure provide an assembly including a fibrous medium having a plurality of substantially corrugated channels therein, the plurality of substantially corrugated channels being permeable to a flow of fluid therethrough; a distributor in contact with the fibrous medium, and including an aperture therein for transmitting a liquid coolant through the distributor; and at least two acoustic shields coupled to the fibrous medium and proximal to opposing sides of the distributor.

Abstract: A thermal management system for an electric vehicle includes a device for cooling one or more heat generating components, an in-cabin heat exchanger, and a heat pump device. The heat pump device includes a compressor, a first heat exchanger, a throttling element, and a second heat exchanger which are connected through pipelines and form a first loop. The first heat exchanger and the second heat exchanger are both dual channel exchangers. The device for cooling one or more heat generating components forms a second loop with the second channel of the first heat exchanger, and forms a third loop with the second channel of the second heat exchanger. The in-cabin heat exchanger forms a fourth loop with the second channel of the second heat exchanger. Only one of the second, third, and fourth loops is not shut off at any given time.

Abstract: The present application provides a media pad for cooling an inlet air flow to a compressor of a gas turbine engine. The media pad may include a first media sheet with a chevron corrugated surface having a first mist eliminator and a second media sheet with a wavy corrugated surface having a second mist eliminator.

Abstract: Embodiments of the present disclosure provide an assembly including a fibrous medium having a plurality of substantially corrugated channels therein, the plurality of substantially corrugated channels being permeable to a flow of fluid therethrough; a distributor in contact with the fibrous medium, and including an aperture therein for transmitting a liquid coolant through the distributor; and at least two acoustic shields coupled to the fibrous medium and proximal to opposing sides of the distributor.

Abstract: The present application provides an inlet heat exchanger for cooling an inlet air flow in a compressor of a gas turbine engine. The inlet air exchanger may include a media pad with a number of media sheets having a substantially three-dimensional contoured shape made from non-woven synthetic fibers and a heat exchange medium flowing from a top to a bottom of the media pad to exchange heat with the inlet air flow.

Abstract: An integrated coil and fin system in a gas turbine inlet. The integrated system includes at least one wavy, non-planar, fin integrated with at least one heating/cooling coil, wherein the at least one coil is configured to heat or cool air moving through the gas turbine inlet, and wherein the at least one non-planar fin is configured to remove moisture in the air moving through the gas turbine inlet. In one embodiment, at least one hook can be included at an end or along a length of at least one non-planar fin.

Abstract: The present application provides an inlet bleed heat system for supplying a flow of bleed air to a flow of incoming air into a compressor of a gas turbine engine. The inlet bleed heat system may include an air knife and a silencer panel. The air knife may include a compressor bleed air port in communication with the flow of bleed air and a discharge gap to discharge the flow of bleed air into the flow of incoming air. The air knife may and the silencer panel may form an integrated air knife/silencer panel.