Add to ORKGA gas turbine engine has a fairing and an air intake that includes an air inlet embedded within the fairing for supplying free stream atmospheric air to a gas generator
An aircraft assembly is disclosed and includes a fuselage including a turbine engine mounted within ...
Nozzle exit configurations and associated systems and methods are disclosed. An aircraft system in a...
Development of a gas turbine powertrain with a 30% fuel economy improvement over a comparable S1 rec...
A gas turbine engine has an inlet duct formed to have a shape with a first ellipse in one half and a...
A mixer assembly for a gas turbine engine is provided, including a main mixer with fuel injection ho...
A gas turbine engine includes a gear assembly and a bypass flow passage that includes an inlet and a...
A nozzle assembly for a dual gas turbine engine propulsion system includes a housing mountable proxi...
A propulsion system for an aircraft includes first and second turbine engines mounted within a fusel...
A gas turbine engine has a core engine incorporating a core engine turbine. A fan rotor is driven by...
A combustor assembly includes a first wall, a second wall, a bulkhead and a plurality of fuel inject...
An engine system has a gas generator, a bi-fi wall surrounding at least a portion of the gas generat...
An endwall treatment for a gas turbine engine having at least one rotor blade extending from a rotat...
An aircraft includes a fuselage including a propulsion system supported within an aft portion. A thr...
One embodiment of the present invention is a unique gas turbine engine system. Another embodiment is...
A mixer assembly for a gas turbine engine is provided, including a main mixer, and a pilot mixer hav...
An aircraft assembly is disclosed and includes a fuselage including a turbine engine mounted within ...
Nozzle exit configurations and associated systems and methods are disclosed. An aircraft system in a...
Development of a gas turbine powertrain with a 30% fuel economy improvement over a comparable S1 rec...
A gas turbine engine has an inlet duct formed to have a shape with a first ellipse in one half and a...
A mixer assembly for a gas turbine engine is provided, including a main mixer with fuel injection ho...
A gas turbine engine includes a gear assembly and a bypass flow passage that includes an inlet and a...
A nozzle assembly for a dual gas turbine engine propulsion system includes a housing mountable proxi...
A propulsion system for an aircraft includes first and second turbine engines mounted within a fusel...
A gas turbine engine has a core engine incorporating a core engine turbine. A fan rotor is driven by...
A combustor assembly includes a first wall, a second wall, a bulkhead and a plurality of fuel inject...
An engine system has a gas generator, a bi-fi wall surrounding at least a portion of the gas generat...
An endwall treatment for a gas turbine engine having at least one rotor blade extending from a rotat...
An aircraft includes a fuselage including a propulsion system supported within an aft portion. A thr...
One embodiment of the present invention is a unique gas turbine engine system. Another embodiment is...
A mixer assembly for a gas turbine engine is provided, including a main mixer, and a pilot mixer hav...
An aircraft assembly is disclosed and includes a fuselage including a turbine engine mounted within ...
Nozzle exit configurations and associated systems and methods are disclosed. An aircraft system in a...
Development of a gas turbine powertrain with a 30% fuel economy improvement over a comparable S1 rec...