139131 ⎘
Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage of the centripetal type
Aircraft engine having two radially offset turbines
#2Removable mechanical part for acoustic insulation of an air inlet casing
#3MULTISTAGE COMPRESSOR-EXPANDER TURBOMACHINE CONFIGURATION
#4Gas turbine auxiliary power unit
#5Jet engine having fan blades with air and exhaust gas flow channels
#6Reverse-flow gas turbine engine
#7Forward-swept impellers and gas turbine engines employing the same
#8Gas turbine fuel injector having flow guide for receiving air flow
#9Bi-directional compression fan rotor for a gas turbine engine
#10Combined pump system for engine TMS AOC reduction and ECS loss elimination
#11BOUNDARY LAYER EFFECT TURBINE
#12Engine
#13Integrated gearless and nonlubricated auxiliary power unit