139125 ⎘
Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages the turbine being of the radial-flow type
Cooling structure for radial turbine
#2Inertial particle separator for turbine engine
#3Gas turbine engine flow control
#4Control of clearance between aircraft rotor blades and a casing
#5Bleed expander cooling with turbine
#6Turbine blade, and turbine and gas turbine including the same
#7GEAR SYSTEM ARCHITECTURE FOR GAS TURBINE ENGINE
#8GEAR SYSTEM ARCHITECTURE FOR GAS TURBINE ENGINE
#9GEAR SYSTEM ARCHITECTURE FOR GAS TURBINE ENGINE
#10Reaction turbine and hybrid impulse reaction turbine