Abstract: A main filter for an airplane fuel circuit or a fuel circuit for any type of mechanism, the filter having a first and second entry, which go directly into a chamber containing a filtering unit, the first entry receiving the fuel at a temperature essentially equal to that of the second entry which receives a hotter fuel which has passed through a heat exchanger. The filter prevents clogging due to ice formation on the filtering unit of the filter or at least inhibits such clogging. A fuel circuit using such a filter is also disclosed.
Type:
Grant
Filed:
January 12, 2000
Date of Patent:
June 26, 2001
Assignee:
Societe Nationale d'Etude et de Consrtuction de Moteurs
d'Aviation “SNECMA”
Inventors:
Marie Trinité Blot-Carretero, Jean-Marie Brocard