GAS TURBINE ENGINEA fuel system (200) for a hydrogen fuelled aircraft propulsion system (103) comprises a tank (104) configured to store hydrogen, a first inductor (436a-c) provided within the tank (104) and configured…DRIVE·Nov 19·1 min readFollowB64D37/10ROLLS ROYCE PLC [GB]
A hydraulic damping apparatusA hydraulic damping apparatus 2 comprising a conduit 4 for a hydraulic fluid having a port 12 in a wall of the conduit 4; a resonator 6 having a chamber 9 and a neck 10, the neck 10 being arranged to …DRIVE·Nov 28·2 min readFollowB64D37/10ROLLS ROYCE PLC [GB]
