|
JP2019065834A
|
|
Flow control method for super high bypass ratio ducted turbo fan
|
|
JP2018059491A
|
|
Flow control method of ultrahigh bypass ratio variable cycle turbofan
|
|
JP2012251542A
|
|
Variable cycle engine
|
|
JP2012067738A
|
|
Low noise supersonic propeller
|
|
JP2011069342A
|
|
Supersonic aircraft propulsion system
|
|
JP2009057955A
|
|
Inter-turbine-bypass variable-cycle engine for supersonic aircraft
|
|
WO2005085620A1
|
|
Variable cycle engine for propelling subsonic aircraft
|
|
JP2002221092A
|
|
High bypass ratio turbo-fan engine with variable jet nozzle
|
|
JP2002054503A
|
|
High bypass ratio variable cycle engine for subsonic aircraft
|
|
JP2000220524A
|
|
Variable cycle engine of bleed air method
|
|
JPH11303682A
|
|
Double bypass engine
|
|
JPH09287520A
|
|
Double bypass engine
|
|
JPH0960557A
|
|
Double bypass engine
|
|
JPH07301150A
|
|
Cross compound turbofan
|
|
JPH06317180A
|
|
Cross compound type fan engine
|
|
JPH05312005A
|
|
Turbo fan engine with variable low pressure turbine stationary blade
|
|
JPH0486333A
|
|
Regenerative cycle gas turbine of one compressor and input high-to-low pressure output turbine type
|
|
JPH03290024A
|
|
Two-shaft type intermediate pressure power turbine regeneration type gas turbine
|
|
JPH03930A
|
|
Two-shaft type regenerative gas turbine
|
|
JPH0255830A
|
|
Supercharge system for internal combustion engine
|
