AIRCRAFT FUEL SYSTEM WITH CYCLONIC SEPARATOR
An aircraft fuel system comprising: a fuel tank (20); and a cyclonic separator (1). The cyclonic separator comprises: a separation chamber; an inlet (2) in fluid communication with the fuel tank (20) and the separation chamber; a fuel outlet (4) in fluid communication with the separation chamber; an...
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Main Authors | , |
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Format | Patent |
Language | English French German |
Published |
23.10.2019
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Abstract | An aircraft fuel system comprising: a fuel tank (20); and a cyclonic separator (1). The cyclonic separator comprises: a separation chamber; an inlet (2) in fluid communication with the fuel tank (20) and the separation chamber; a fuel outlet (4) in fluid communication with the separation chamber; and a water outlet (3). The cyclonic separator is adapted to discharge water from the water outlet (3) and relatively less dense liquid fuel from the fuel outlet (4), and wherein the cyclonic separator (1) further comprises a permeation member (22) formed from a water-permeable material which enables water in the separation chamber to flow through the water-permeable material and out of the water outlet (3), but substantially prevents liquid fuel in the separation chamber from doing so. |
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AbstractList | An aircraft fuel system comprising: a fuel tank (20); and a cyclonic separator (1). The cyclonic separator comprises: a separation chamber; an inlet (2) in fluid communication with the fuel tank (20) and the separation chamber; a fuel outlet (4) in fluid communication with the separation chamber; and a water outlet (3). The cyclonic separator is adapted to discharge water from the water outlet (3) and relatively less dense liquid fuel from the fuel outlet (4), and wherein the cyclonic separator (1) further comprises a permeation member (22) formed from a water-permeable material which enables water in the separation chamber to flow through the water-permeable material and out of the water outlet (3), but substantially prevents liquid fuel in the separation chamber from doing so. |
Author | Lam, Joseph K-W Lisle-Taylor, Stephen |
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DocumentTitleAlternate | FLUGZEUGKRAFTSTOFFSYSTEM MIT FLIEHKRAFTABSCHEIDER SYSTÈME DE CARBURANT D'AÉRONEFS AVEC SÉPARATEUR À CYCLONE |
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Notes | Application Number: EP20160170286 |
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RelatedCompanies | Airbus Operations Limited |
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Snippet | An aircraft fuel system comprising: a fuel tank (20); and a cyclonic separator (1). The cyclonic separator comprises: a separation chamber; an inlet (2) in... |
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SubjectTerms | AIRCRAFT APPARATUS USING FREE VORTEX FLOW, e.g. CYCLONES ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CENTRIFUGAL APPARATUS OR MACHINES FOR CARRYING-OUT PHYSICAL ORCHEMICAL PROCESSES CHEMISTRY COSMONAUTICS CRACKING HYDROCARBON OILS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS FUELS LUBRICANTS METALLURGY MINERAL WAXES PARACHUTES PEAT PERFORMING OPERATIONS PETROLEUM, GAS OR COKE INDUSTRIES PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL PRODUCTION OF LIQUID HYDROCARBON MIXTURES, e.g. BY DESTRUCTIVEHYDROGENATION, OLIGOMERISATION, POLYMERISATION RECOVERY OF HYDROCARBON OILS FROM OIL-SHALE, OIL-SAND, ORGASES REFINING MIXTURES MAINLY CONSISTING OF HYDROCARBONS REFORMING OF NAPHTHA SEPARATION TECHNICAL GASES CONTAINING CARBON MONOXIDE TRANSPORTING |
Title | AIRCRAFT FUEL SYSTEM WITH CYCLONIC SEPARATOR |
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