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AssigneesDaimler-Benz Aerospace AG, Tupolev AG
InventorsFranz Grafwallner, Peter Luger, Helmuth Peller, Martin Muller, Valentin V. Malyshev, Sergei B. Galperin, Igor V. Golov
Estimating the term…
Fuel supply system for multijet airplanes using cryogenic fuel with one tank or one tank group for each engine or for all engines on one side of the longitudinal central plane of the airplane, and, if desired, with an additional, common tank or an additional, common tank group for all engines. A transfer line with shut-off valve leads from each tank/tank group associated with a defined engine or with the engines of one side of the airplane to at least one other tank/tank group and/or, if desired, to the tank/tank group common to all engines. If desired, at least one transfer line leads from the common tank/tank group to at least one other tank/tank group.
A fuel supply system for multijet airplanes using cryogenic fuel such as hydrogen, the airplane having an engine on one side of a central plane and having an engine on the other side of the central plane, the system comprising:
A fuel supply system for multijet airplanes using hydrogen as a cryogenic fuel, the airplane having an engine on one side of a central plane and having an engine on the other side of the central plane, the fuel system comprising:
The fuel supply system for multijet airplanes using cryogenic fuel, the airplane having an engine on one side of a central plane and having an engine on the other side of the central plane, the fuel system comprising:
Dependencies are inferred from the claim text.