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Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor the compressor being of the centrifugal type
IMPROVED TURBOMACHINE FOR HYBRID AIRCRAFT
#2IMPROVED PROPULSIVE ASSEMBLY FOR A MULTI-ENGINE HYBRID AIRCRAFT
#3Aircraft engine having two radially offset turbines
#4HYBRID-ELECTRIC PROPULSION SYSTEM EQUIPPED WITH A COUPLER FOR SWITCHING BETWEEN MODES OF OPERATION
#5Advanced 2-spool turboprop engine
#6Recovered-cycle aircraft turbomachine
#7Gas turbine engine
#8Starter/generator
#9Turboshaft gas turbine engine and expansion ratio relationship
#10Centrifugal impeller for gas turbine engine
#11Advanced 2-spool turboprop engine
#12STARTER/GENERATOR
#13Turbine engine with single wall cantilevered architecture
#14Integrated power generation and compression train, and method
#15Centrifugal gas compressor
#16Turbine rotor with low over-speed requirements
#17Turboshaft engine embeddable in a reduction gearbox
#18Geared gas turbine engine
#19Decoupled gas turbine engine
#20Bearing support for a hot section of a turboshaft engine, and an associated turboshaft engine
#21Non-lubricated architecture for a turboshaft engine
#22Combined pump system for engine TMS AOC reduction and ECS loss elimination
#23Turboshaft engine with parallel shafts
#24ENGINE-LOAD CONNECTION STRATEGY
#25Rotor containment element with frangible connections
#26Turbine engine including a reversible electric machine
#27COMPRESSOR SYSTEM AND METHOD FOR GAS LIQUEFACTION SYSTEM
#28Single stage dual-entry centriafugal compressor, radial turbine gas generator
#29ROTORCRAFT FITTED WITH TURBINE ENGINES
#30Rotor containment element with frangible connections
#31Method for producing gas turbines and gas turbine assembly