US2014030074A1
|
|
Gas turbine engine exhaust duct
|
US2013028712A1
|
|
Gas turbine engine systems involving tip fans
|
US2013183136A1
|
|
Start system for gas turbine engines
|
US2013000273A1
|
|
Gas-driven propulsor with tip turbine fan
|
US2009211222A1
|
|
Rear propulsor for a variable cycle gas turbine engine
|
US2009211221A1
|
|
Auxiliary propulsor for a variable cycle gas turbine engine
|
US2009185911A1
|
|
Systems and methods involving localized stiffening of blades
|
US2009145102A1
|
|
Gas turbine engine systems involving tip fans
|
US2009056309A1
|
|
Gas turbine engine systems and related methods involving multiple gas turbine cores
|
US2009067993A1
|
|
Coated variable area fan nozzle
|
US2007144141A1
|
|
Pulsed combustion fluidic nozzle
|