Vortex tube assembly
OwnerHenry EDWARDSinventor
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OwnerHenry EDWARDSinventor
Estimating the term…
A vortex tube assembly for an aircraft enclosure inerting system has a plenum chamber and a swirl generator which has an inlet passage that allows air in the plenum chamber to enter a vortex chamber whereupon the air can be centrifugally separated into nitrogen enriched air (NEA) and oxygen enriched air (OEA). A throttle pin is positioned within the inlet passage, an outer surface of the throttle pin and an inner surface of the inlet passage co-operatively defining a flow path for air to enter the vortex chamber from the plenum chamber. The throttle pin is movable between a restrictive position and a permissive position, with the flow path being more constricted when the throttle pin is in the restrictive position than when the throttle pin is in the permissive position. The throttle pin is biased to the permissive position and movable to the restrictive position against this bias.
A vortex tube assembly for centrifugally separating an inlet air flow into a nitrogen-enriched air (NEA) flow and an oxygen-enriched air (OEA) flow in an aircraft enclosure inerting system, the vortex tube assembly comprising:
A method of controlling separation of an inlet air flow into a nitrogen-enriched air (NEA) flow and an oxygen-enriched air (OEA) flow using a vortex tube assembly which comprises:
Dependencies are inferred from the claim text.