A fluid module configured to be connected to an aircraft, comprising a manifold configured to direct fluid flow from an inlet to an outlet, the outlet configured to be connected to a hydraulic system of the aircraft and the inlet configured to be connected to a ground source of fluid, the manifold comprising a filter port adapted to receive a filter port; the first inlet in fluid communication with the filter port; and the outlet in fluid communication with the filter port. A method of utilizing the fluid module to provide fluid from the ground fluid source to the filter unit; filtering the fluid via the filter unit; and providing the filtered fluid from the outlet to one or more components, a reservoir of the aircraft, or combinations thereof.
FLUID MODULE
03.08.2023
Patent
Elektronische Ressource
Englisch