PROPULSION SYSTEM FOR AN AIRCRAFT, AIRCRAFT HAVING A PROPULSION SYSTEM, AND METHOD FOR OPERATING AN AIRCRAFTThe invention relates to a propulsion system (11) for an aircraft (1) which is designed to operate with a liquid and a gaseous fuel, comprising - at least one engine (2) with a combustion chamber (6) …DRIVE·Apr 29·2 min readFollowB64D37/02ROLLS ROYCE DEUTSCHLAND LTD & CO KG [DE]
GAS TURBINE ENGINE FUEL SYSTEMA fuel system for a hydrogen fuelled gas turbine engine (201) comprises a main hydrogen fuel storage unit (104) configured to store liquid hydrogen. The main fuel storage unit (104) comprises an ullag…DRIVE·Mar 11·1 min readFollowB64D37/02ROLLS ROYCE PLC [GB]
OVER-PRESSURE VENT SYSTEM FOR AN AIRCRAFT FUEL TANKAn over-pressure vent (OPV) system (150) is provided for a fuel tank (102) of an aircraft (800). The OPV system (150) includes an OPV valve (152) configured to be coupled in fluid communication with a…DRIVE·Feb 11·1 min readFollowB64D37/02BOEING CO [US]
AIRCRAFT FUEL STORAGE SYSTEMDisclosed is an aircraft fuel storage system comprising: a fuel tank comprising a chamber for storing fuel, the chamber comprising a first side, a second side, and a base connecting the first side to …DRIVE·Dec 10·2 min readFollowB64D37/02AIRBUS OPERATIONS LTD [GB]
