7 Patents
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- US121634642024Turbine Engine Core and Bypass Flows Having a Defined Fan-turbine Radial Distance
ROLLS-ROYCE PLC
0 cites - US120122162024Support Structure for Attaching a Gas Turbine Engine to an Aircraft Pylon
ROLLS-ROYCE PLC
0 cites - 0 cites
- US119455952024Support Structure for Attaching a Gas Turbine Engine to an Aircraft Pylon
ROLLS-ROYCE PLC
0 cites - 0 cites