Abstract: A membrane-based air separation module includes an inlet configured to receive supply air, a first hollow fiber membrane configured to substantially remove water from the supply air to form an anhydrous air stream, and a permeate port configured to exhaust the water removed by the first hollow fiber membrane from the air separation module. The air separation module also includes a second hollow fiber membrane positioned downstream of the first hollow fiber membrane configured to receive the anhydrous air stream and substantially remove oxygen from the anhydrous air stream, an oxygen-enriched air outlet configured to exhaust the oxygen removed by the second hollow fiber membrane from the air separation module, and a nitrogen-enriched air outlet configured to supply a stream of nitrogen-enriched air to a fuel tank of an aircraft.

Abstract: An air separation module includes a shell configured to house an air separation membrane, an inlet configured to receive supply air, an oxygen-enriched air outlet configured to exhaust oxygen from the air separation module, and a nitrogen-enriched air outlet configured to supply a stream of nitrogen-enriched air to a fuel tank of an aircraft. The air separation module also includes a condition monitoring sensor integral with the air separation module and configured to measure at least one of a plurality of conditions; and a connector integral with the air separation module and configured to join the condition monitoring sensor with an electrical system of the aircraft.

Abstract: A membrane-based air separation module includes an inlet configured to receive supply air, a first hollow fiber membrane configured to substantially remove water from the supply air to form an anhydrous air stream, and a permeate port configured to exhaust the water removed by the first hollow fiber membrane from the air separation module. The air separation module also includes a second hollow fiber membrane positioned downstream of the first hollow fiber membrane configured to receive the anhydrous air stream and substantially remove oxygen from the anhydrous air stream, an oxygen-enriched air outlet configured to exhaust the oxygen removed by the second hollow fiber membrane from the air separation module, and a nitrogen-enriched air outlet configured to supply a stream of nitrogen-enriched air to a fuel tank of an aircraft.

Abstract: An air separation module includes a shell configured to house an air separation membrane, an inlet configured to receive supply air, an oxygen-enriched air outlet configured to exhaust oxygen from the air separation module, and a nitrogen-enriched air outlet configured to supply a stream of nitrogen-enriched air to a fuel tank of an aircraft. The air separation module also includes a condition monitoring sensor integral with the air separation module and configured to measure at least one of a plurality of conditions; and a connector integral with the air separation module and configured to join the condition monitoring sensor with an electrical system of the aircraft.

Abstract: A nitrogen generation system includes a bleed air source. The system also includes an air separation module having an inlet for receiving bleed air, a hollow fiber membrane for substantially removing oxygen from the bleed air to produce a stream of oxygen enriched air and a stream of nitrogen enriched air, a first outlet for exhausting the nitrogen enriched air, a second outlet for exhausting the oxygen enriched air from the air separation module. The system also includes a nitrogen enriched air line configured to receive the nitrogen enriched air and a fuel tank disposed downstream from the air separation module. The air separation module is positioned within a one of the group consisting of a gas turbine engine, a nacelle, a pylon, an aircraft wing, and combinations thereof.

Abstract: Superhydrophobic surfaces according to the invention contain micro or nanoscale hydrophobic features which can support a shear-free air-water interface between peaks in the surface topology. The surface of an engineered structure is patterned with a plurality of parallel ridges extending from the surface. The ridges have a width d and a height h, and are spaced apart by a first spacing dimension w. The ridges extend along the surface of the solid object for a predefined length l. Breaker ridges are situated between the parallel ridges, and are oriented at an angle to the parallel ridges. The breaker ridges are preferably spaced apart by a second spacing dimension. The breaker ridges and the parallel ridges are configured to define a volume wherein a gas may be situated. The engineered structure is configured to provide a reduced drag force between itself and a fluid.