Abstract: An inert gas generating system includes a source of a gaseous mixture, and a fuel separation unit configured to receive a portion of the gaseous mixture from the source. The fuel separation unit includes a reverse selective membrane configured to separate the gaseous mixture into a condensable gas portion and a permanent gas portion. The inert gas generating system further includes a catalytic oxidation unit configured to receive and react hydrocarbon vapors within the condensable gas portion to produce an inert gas.

Abstract: Disclosed is a refrigeration system including a heat transfer fluid circulation loop configured to allow a refrigerant to circulate through the circulation loop. A purge gas outlet is in operable communication with the heat transfer fluid circulation loop. The system also includes at least one gas permeable membrane having a first side in operable communication with the purge gas outlet and a second side. The membrane includes a separation layer including a porous inorganic material with pores of a size to allow passage of contaminants through the membrane and restrict passage of the through the membrane, and a polymer coating over the separation layer. A permeate outlet is in operable communication with the second side of the membrane.

Abstract: Fuel tank inerting systems for aircraft are described. The systems include a fuel tank, a pressurized air source, an air separation module arranged between the pressurized air source and the fuel tank, the air separation module configured to generate an inerting gas from pressurized air supplied from the pressurized air source and supply the inerting gas to the fuel tank, an upstream thermal conditioning system arranged upstream of the air separation module, the upstream thermal conditioning system configured to increase a temperature of the pressurized air prior to entry into the air separation module, and a downstream thermal conditioning system arranged downstream of the air separation module, the downstream thermal conditioning system configured to decrease a temperature of the inerting gas prior to entry into the fuel tank.

Abstract: Provided are techniques that include operating a spiral contactor. The techniques include receiving, by a spiral contactor, a first fluid, and receiving a second fluid, wherein the first fluid is different than the second fluid. The techniques also include exchanging the first fluid and the second fluid using the spiral contactor, and outputting a deoxygenated fluid from the spiral contactor, wherein the deoxygenated fluid has a lower oxygen concentration than the first fluid.

Abstract: Disclosed is a refrigeration system including a heat transfer fluid circulation loop configured to allow a refrigerant to circulate therethrough. A purge gas outlet is in operable communication with the heat transfer fluid circulation loop. The system also includes at least one gas permeable membrane having a first side in operable communication with the purge gas outlet and a second side. The membrane includes a porous inorganic material with pores of a size to allow passage of contaminants through the membrane and restrict passage of the refrigerant through the membrane. The system also includes a permeate outlet in operable communication with a second side of the membrane.

Abstract: A system for degassing a hydrocarbon fluid from a hydrocarbon liquid has a plurality of hollow tube membranes. The hollow tube membranes are formed of a plastic providing an inner support body and an outer selective layer which is denser than the inner support body. The inner support body is formed of spherulitic structures. A fuel supply system and a method are also disclosed.

Abstract: A system configured for detection of corrosion of a metal substrate is disclosed. The article includes a first layer disposed over the metal substrate comprising a first electrically conductive polymer, and a first electrical conductivity sensor in sensing contact with the first layer.

Abstract: A selectively permeable membrane device for separating a first fluid from a second fluid in a flow can include a membrane conduit configured to receive the flow and to allow permeation of the first fluid therethrough, and configured to not allow permeation of the second fluid. The device can include a residence time enhancing structure disposed within the membrane conduit and configured to increase residence time of the flow within the membrane conduit.

Abstract: A fuel deoxygenation system has a deoxygenator, an ultrasound transducer, and a control. The ultrasonic transducer is operable to direct ultrasonic waves into a flow passage for a fuel connected to the deoxygenator. A gas turbine engine and a method are also disclosed.

Abstract: A filter screen includes a plate body with an upstream surface, an opposed downstream surface, and an array of apertures extending between the upstream surface and the downstream surface. A polytetrafluoroethylene-based layer overlays the upstream surface between apertures of the aperture array, the polytetrafluorethylene-based layer being conformally disposed over the upstream surface of the plate body and spanning the upstream surface between the apertures of the aperture array to slow deposition of carbonaceous deposits on the filter screen.

Abstract: A fuel and/or lubricant system for an engine can include an engine component configured to be in fluid communication with the fuel and/or lubricant, and an alternating current (AC) source electrically connected to the engine component to create an electric field of alternating polarity to subject particles within the fuel and/or lubricant to dielectrophoresis as the fuel and/or lubricant passes through the electric field to prevent deposits from forming on the engine component. In certain embodiments, the engine component can be a filter screen configured to filter the fuel and/or lubricant to subject particles within the fuel and/or lubricant to dielectrophoresis as the fuel and/or lubricant passes through the filter screen.

Abstract: A method may comprise preparing a radical-neutralizing composition comprising a cerium compound and a carrier; applying the radical-neutralizing composition to a passageway surface of a lubricant passageway in a lubricant system component; and/or drying the radical-neutralizing composition to form a radical-neutralizing coating on the passageway surface comprising cerium oxide.

Abstract: A fuel tank inerting system uses a catalytic oxidation unit to combust fuel from the fuel tank to produce inert gas, simultaneously working with a gas separator that removes dissolved carbon dioxide from the fuel before it is cycled to the thermal management system (TMS) or the engine. This prevents cavitation of carbon dioxide (gaseous bubbling) within the fuel at varying temperatures while in flight.

Abstract: A passive fuel additives dosing system includes a membrane-based contactor within a cartridge, an additive within the membrane-based contactor, a fuel inlet to the cartridge and a fuel outlet from the cartridge. The membrane-based contactor is arranged within the cartridge such that, with fuel in the cartridge, a fuel contact area with the membrane-based contactor is dependent on a fuel flow rate to passively dispense a proportional amount of the additive into the fuel.

Abstract: A system for generating inert gas includes a source of pressurized air. An air separation module including at least one permeable membrane is operable to separate the pressurized air into oxygen-enriched air and inert gas-enriched air. A fuel tank containing a fuel is arranged downstream from said air separation module. The inert gas-enriched air output from said air separation module interacts with said fuel to remove dissolved oxygen from said fuel.

Abstract: A fuel tank inerting system uses a catalytic oxidation unit to combust fuel from the fuel tank to produce inert gas, simultaneously working with a gas separator that removes dissolved carbon dioxide from the fuel before it is cycled to the thermal management system (TMS) or the engine. This prevents cavitation of carbon dioxide (gaseous bubbling) within the fuel at varying temperatures while in flight.

Abstract: A fuel tank inerting system includes an air separation module with an oxygen permeable membrane and a variable vacuum source in fluid communication with the air separation module. The variable vacuum source provides an adjustable vacuum to the permeate side of the oxygen permeable membrane in the air separation module, driving production of inert gas for fuel tank inerting or fire suppression.

Abstract: A system for generating inert gas includes a source of pressurized air. An air separation module including at least one permeable membrane is operable to separate the pressurized air into oxygen-enriched air and inert gas-enriched air. A fuel tank containing a fuel is arranged downstream from said air separation module. The inert gas-enriched air output from said air separation module interacts with said fuel to remove dissolved oxygen from said fuel.

Abstract: An inert gas generating system includes a source of a liquid hydrocarbon fuel, and a fractioning unit configured to receive a portion of the liquid hydrocarbon fuel from the source. The fractioning unit includes a perm-selective membrane configured to separate the portion of the liquid hydrocarbon fuel into substantially sulfur-free vapors and a sulfur-containing remainder. The system further includes a catalytic oxidation unit configured to receive and react the substantially sulfur-free vapors to produce an inert gas.

Abstract: A chemical scavenging component includes a porous body that has a radical-scavenging material. The radical-scavenging material has a composition of, by weight, greater than 50% of cerium oxide that is chemically active with regard to oxygen-containing radicals.