Method for determining the filterability of jet fuel...

Details Method for determining the filterability of jet fuel... Method for determining the filterability of jet fuel...

G - Physics

01

N

G01N 33/22 (2006.01) B01D 17/00 (2006.01) B01D 35/00 (2006.01) C10G 33/08 (2006.01) G01N 33/28 (2006.01)

Patent

CA 2716709

It has been discovered that jet fuel containing enhanced thermal stability additives and water can be delivered with a final water content of 15 ppm or less via existing jet fuel distribution system by controlling the fuel flow rate through the fuel delivery system comprising one or more filter coalescers and separator systems, said controlled fuel flow rate being determined by passing a sample of actual fuel through a sample of the fuel filter at various fuel flow rates to identify the flowrate at which the fuel effluent contains 15 ppm or less.

Il a été découvert que le carburant aviation contenant des additifs améliorés de stabilité thermique et de l'eau peut être fourni avec une teneur en eau finale égale ou inférieure à 15 ppm, par l'intermédiaire d'un système de distribution de carburant aviation existant, par le réglage du débit de carburant au moyen du système d'approvisionnement en carburant, qui comprend un ou plusieurs systèmes de filtres coalesceurs et séparateurs. On détermine ledit débit en faisant passer un échantillon de carburant réel à travers un échantillon du filtre à carburant, à divers débits de carburant, afin d'identifier le débit auquel l'effluent de carburant présente une teneur en eau égale ou inférieure à 15 ppm.

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