An aircraft fuel tank inerting system is disclosed. An aircraft fuel tank inerting system may include a paramagnetic pump arranged to apply a magnetic field to a source of gas to provide a motivational force for removing oxygen from said gas. A paramagnetic pump may include a series of magnetic field generating elements configured to provide a sequence of discrete spaced apart magnetic fields. The series of magnetic field generating elements may include a series of spaced apart pairs of magnetic field generating elements. Each spaced apart pair of magnetic field generating elements may be arranged to generate a respective spaced apart magnetic field, of the sequence of discrete spaced apart magnetic fields, across an airspace therebetween.
FUEL TANK INERTING
KRAFTSTOFFTANKINERTISIERUNG
INERTAGE DE RÉSERVOIR DE CARBURANT
2020-01-01
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Wiley | 2009
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