Add to ORKGA gas turbine engine includes a core flow passage, a bypass flow passage, and a propulsor arranged at an inlet of the bypass flow passage and the core flow passage. The propulsor includes a row of propulsor blades. The row includes no more than 20 of the propulsor blades. The propulsor has a pressure ratio between about 1.2 and about 1.7 across the propulsor blades
The solar fuels generator includes an ionically conductive separator between a gaseous first phase a...
The low pressure turbine for the energy efficient engine is a five-stage configuration with moderate...
A method of measuring a residence time in a gas-turbine engine is disclosed that includes measuring ...
A gas turbine engine includes a gear assembly and a bypass flow passage that includes an inlet and a...
A combustor assembly includes a first wall, a second wall, a bulkhead and a plurality of fuel inject...
A gas turbine engine has a core engine incorporating a core engine turbine. A fan rotor is driven by...
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 propulsion system for an aircraft includes first and second turbine engines mounted within a fusel...
A gas turbine engine has a fairing and an air intake that includes an air inlet embedded within the ...
A nozzle assembly for a dual gas turbine engine propulsion system includes a housing mountable proxi...
An improved acoustic liner for turbine engines is disclosed. The acoustic liner may include a straig...
An aircraft assembly is disclosed and includes a fuselage including a turbine engine mounted within ...
An endwall treatment for a gas turbine engine having at least one rotor blade extending from a rotat...
A rotor blade comprises an airfoil extending radially from a root section to a tip section and axial...
The solar fuels generator includes an ionically conductive separator between a gaseous first phase a...
The low pressure turbine for the energy efficient engine is a five-stage configuration with moderate...
A method of measuring a residence time in a gas-turbine engine is disclosed that includes measuring ...
A gas turbine engine includes a gear assembly and a bypass flow passage that includes an inlet and a...
A combustor assembly includes a first wall, a second wall, a bulkhead and a plurality of fuel inject...
A gas turbine engine has a core engine incorporating a core engine turbine. A fan rotor is driven by...
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 propulsion system for an aircraft includes first and second turbine engines mounted within a fusel...
A gas turbine engine has a fairing and an air intake that includes an air inlet embedded within the ...
A nozzle assembly for a dual gas turbine engine propulsion system includes a housing mountable proxi...
An improved acoustic liner for turbine engines is disclosed. The acoustic liner may include a straig...
An aircraft assembly is disclosed and includes a fuselage including a turbine engine mounted within ...
An endwall treatment for a gas turbine engine having at least one rotor blade extending from a rotat...
A rotor blade comprises an airfoil extending radially from a root section to a tip section and axial...
The solar fuels generator includes an ionically conductive separator between a gaseous first phase a...
The low pressure turbine for the energy efficient engine is a five-stage configuration with moderate...
A method of measuring a residence time in a gas-turbine engine is disclosed that includes measuring ...