|
DE19515966A1
|
|
Turbo engine for supersonic aircraft with deceleration thrust and attitude control
|
|
DE4321175A1
|
|
Meridian compressor with integrated 2-circuit fan for turbo gas generators for driving aircraft and orbital carrier stages
|
|
DE4223930A1
|
|
Tangential blower for turbo engines
|
|
DE4129357A1
|
|
Tangential blower for turbo engines
|
|
DE4121995A1
|
|
Aircraft turbo-propulsion unit - uses second and third stages of turbine to drive rotors of tangential fan
|
|
DE4117933A1
|
|
Gas turbine unit for hypersonic aircraft - has axial compressor and blower replaced by tangential blower
|
|
DE4113976A1
|
|
Hyper-sonic aircraft engine - has speed matching of tangential blower rollers on drive turbine facilitated and noise radiation reduced
|
|
DE4111396A1
|
|
Propulsion unit for hypersonic aircraft - has gas generators mounted inside duct of rectangular cross=section
|
|
DE3841174A1
|
|
Propeller fan
|
|
DE3834511A1
|
|
Propeller fan
|
|
DE3734624A1
|
|
Propeller fan
|
|
DE3614311A1
|
|
Propulsion system for aircraft
|
|
DE3227328A1
|
|
Gas-turbine jet engine having force-control properties for use on aircraft which take off on their tails
|
|
DE2735886A1
|
|
Auxiliary inlet unit for gas turbine compressor - has regulated transverse blowers connected by channels centrally to compressor inlet
|
|
DE2618719A1
|
|
Stability control for VSTOL aircraft - has small axial turbine on main shaft to generate lateral correction impulses
|
