139123 ⎘
Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor being of the positive-displacement type
Dual-pressure jet engine and device for work done by compressed air thereof
#2Control device, control method, and program
#3Method of operating an engine assembly
#4TURBINE CLEARANCE CONTROL SYSTEM AND METHOD FOR IMPROVED VARIABLE CYCLE GAS TURBINE ENGINE FUEL BURN
#5Revolving outer body rotary vane compressor or expander
#6Compressor blade mounting arrangement
#7POSITIVE DISPLACEMENT POWER EXTRACTION COMPENSATION DEVICE
#8Quasi-isobaric heat engine
#9Combustion engine with feedback gear/rotary pump input
#10Hybrid worm gas turbine engine
#11Low volumetric compression ratio integrated turbo-compound rotary engine
#12Axial flow positive displacement gas generator with combustion extending into an expansion section
#13Gas turbine engine system
#14Gas turbine engine
#15Rotary vane engine and thermodynamic cycle
#16Gas turbine engine system
#17Integrated microturbine system