Aircraft connector for fluid transfer
AssigneeAirbus Operations GmbH
InventorHenry EDWARDS
Life of this patent
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Abstract
An aircraft having a port over which a first connector is mounted for connecting to a second connector to transfer fluid to and/or from the aircraft is disclosed. The first connector includes a first fluid path extending from the port towards an aircraft fluid tank and a second, different, fluid path which extends from the port towards an aircraft fluid tank.
Claims20
An aircraft comprising a port over which a first connector is mounted for connecting to a second, complementary connector to transfer fluid to and/or from the aircraft, the first connector including a first fluid path extending from the port towards an aircraft fluid tank and a second, different, fluid path extending from the port towards an aircraft fluid tank.
A method of transferring fluids to and/or from an aircraft, comprising:
- providing an aircraft having a port over which is mounted a first connector, the first connector connected to a second connector to form a connection, the first connector including a first fluid path extending from the port towards an aircraft fluid tank and a second, different, fluid path extending from the port towards an aircraft fluid tank;
- transferring a first fluid through the first fluid path to transfer the first fluid to or from the aircraft;
- and
- transferring a second fluid through the second fluid path to transfer the second fluid to or from the aircraft.
Dependencies are inferred from the claim text.