Showing items 1–100
Gas turbine engine airfoil
Grant US-11867195-B2
United States of America
Geared turbofan engine with targeted modular efficiency
Grant US-11859538-B2
United States of America
Gas turbine engine compressor arrangement
Grant US-11846238-B2
United States of America
Gas turbine engine with idle thrust ratio
Grant US-11814968-B2
United States of America
Planetary gear system arrangement with auxiliary oil system
Grant US-11815001-B2
United States of America
Geared gas turbine engine with oil deaerator and air removal
Grant US-11814976-B2
United States of America
Operability geared turbofan engine including compressor section variable guide vanes
Grant US-11781490-B2
United States of America
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
Grant US-11781505-B2
United States of America
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
Grant US-11781447-B2
United States of America
Splitter and guide vane arrangement for gas turbine engines
Grant US-11781506-B2
United States of America
Fundamental gear system architecture
Grant US-11773786-B2
United States of America
Method of assembly for gas turbine fan drive gear system
Grant US-11773787-B2
United States of America
Gas turbine engine airfoil
Grant US-11767856-B2
United States of America
Modal noise reduction for gas turbine engine
Grant US-11754094-B2
United States of America
Rotor assembly for gas turbine engines
Grant US-11753951-B2
United States of America
High and low spool configuration for a gas turbine engine
Grant US-11754000-B2
United States of America
Engine mount system for a gas turbine engine
Grant US-11731773-B2
United States of America
Compressor flowpath
Grant US-11725670-B2
United States of America
Geared gas turbine engine with oil deaerator
Grant US-11725589-B2
United States of America
Compressor arrangement for a gas turbine engine
Grant US-11719245-B2
United States of America
Low noise turbine for geared gas turbine engine
Grant US-11719161-B2
United States of America
Gas turbine engine front center body architecture
Grant US-11713713-B2
United States of America
Flexible support structure for a geared architecture gas turbine engine
Grant US-11698007-B2
United States of America
Epicyclic gear train
Grant US-11680492-B2
United States of America
Propulsion system arrangement for turbofan gas turbine engine
Grant US-11661906-B2
United States of America
Geared turbine engine with relatively lightweight propulsor module
Grant US-11661894-B2
United States of America
Geared architecture for high speed and small volume fan drive turbine
Grant US-11635043-B2
United States of America
Turbine section of gas turbine engine
Grant US-11614036-B2
United States of America
Gas turbine engine with power density range
Grant US-11608786-B2
United States of America
Turbofan engine bearing and gearbox arrangement
Grant US-11608779-B2
United States of America
Gas turbine engine with high speed low pressure turbine section and bearing support…
Grant US-11598223-B2
United States of America
Geared gas turbine engine arrangement with core split power ratio
Grant US-11598286-B2
United States of America
Thrust efficient gas turbine engine
Grant US-11598287-B2
United States of America
Geared turbofan engine with targeted modular efficiency
Grant US-11585268-B2
United States of America
Gas turbine engine with high speed low pressure turbine section and bearing support…
Grant US-11585276-B2
United States of America
Geared turbofan arrangement with core split power ratio
Grant US-11578651-B2
United States of America
Geared turbofan with integral front support and carrier
Grant US-11578665-B2
United States of America
Gas turbine engine shaft bearing configuration
Grant US-11566586-B2
United States of America
Geared turbomachine fan and compressor rotation
Grant US-11566587-B2
United States of America
Gas turbine engine buffer system
Grant US-11560839-B2
United States of America
Low noise turbine for geared gas turbine engine
Grant US-11560849-B2
United States of America
Gas turbine engine forward bearing compartment architecture
Grant US-11549387-B2
United States of America
Method of assembly for gear system with rotating carrier
Grant US-11536204-B2
United States of America
Flexible coupling for geared turbine engine
Grant US-11536203-B2
United States of America
Turbine engine gearbox
Grant US-11525406-B2
United States of America
Geared gas turbine engine with reduced fan noise
Grant US-11512631-B2
United States of America
Turbofan engine front section
Grant US-11506084-B2
United States of America
Ring gear mounting arrangement with oil scavenge scheme
Grant US-11499624-B2
United States of America
Gas turbine engine buffer system
Grant US-11499476-B2
United States of America
Dual function cascade integrated variable area fan nozzle and thrust reverser
Grant US-11499502-B2
United States of America
Turbine section of high bypass turbofan
Grant US-11486311-B2
United States of America
Gas turbine engine shaft bearing configuration
Grant US-11486269-B2
United States of America
Turbine section of high bypass turbofan
Grant US-11480108-B2
United States of America
Gas turbine engine with blade channel variations
Grant US-11466572-B2
United States of America
Gas turbine engine with non-epicyclic gear reduction system
Grant US-11459957-B2
United States of America
Gas turbine engine with axial movable fan variable area nozzle
Grant US-11454193-B2
United States of America
Oil baffle for gas turbine fan drive gear system
Grant US-11448310-B2
United States of America
Geared turbofan engine with a high ratio of thrust to turbine volume
Grant US-11448124-B2
United States of America
Gas turbine engine front architecture
Grant US-11408372-B2
United States of America
Gas turbine engine airfoil
Grant US-11408436-B2
United States of America
Gas turbine engine variable area fan nozzle control
Grant US-11401889-B2
United States of America
Flutter sensing and control system for a gas turbine engine
Grant US-11396847-B2
United States of America
Gas turbine engine airfoil
Grant US-11391294-B2
United States of America
Elongated geared turbofan with high bypass ratio
Grant US-11391216-B2
United States of America
Gas turbine engine bifurcation located fan variable area nozzle
Grant US-11391240-B2
United States of America
Geared gas turbine engine with gear driving low pressure compressor and fan at a common…
Grant US-11384657-B2
United States of America
Ring gear mounting arrangement with oil scavenge scheme
Grant US-11378039-B2
United States of America
Geared turbofan engine with targeted modular efficiency
Grant US-11371427-B2
United States of America
Turbine section of high bypass turbofan
Grant US-11346289-B2
United States of America
Geared turbofan engine with power density range
Grant US-11346286-B2
United States of America
Method of assembly for gas turbine fan drive gear system
Grant US-11339726-B2
United States of America
Epicyclic gear train
Grant US-11319831-B2
United States of America
Modal noise reduction for gas turbine engine
Grant US-11300141-B2
United States of America
Gas turbine engine forward bearing compartment architecture
Grant US-11293299-B2
United States of America
Gas turbine engine with low stage count low pressure turbine and engine mounting…
Grant US-11286883-B2
United States of America
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
Grant US-11286811-B2
United States of America
Gas turbine engine buffer system
Grant US-11286852-B2
United States of America
Geared turbofan engine gearbox arrangement
Grant US-11280267-B2
United States of America
Geared gas turbine engine with oil deaerator and air removal
Grant US-11248494-B2
United States of America
Turbine section of high bypass turbofan
Grant US-11242805-B2
United States of America
Geared turbine engine with relatively lightweight propulsor module
Grant US-11236679-B2
United States of America
Ring gear mounting arrangement with oil scavenge scheme
Grant US-11221066-B2
United States of America
Turbine section of high bypass turbofan
Grant US-11215123-B2
United States of America
Geared turbofan arrangement with core split power ratio
Grant US-11215143-B2
United States of America
Gas turbine engine airfoil
Grant US-11209013-B2
United States of America
Thrust efficient turbofan engine
Grant US-11199159-B2
United States of America
Gas turbine engine airfoil
Grant US-11193497-B2
United States of America
Gas turbine engine airfoil
Grant US-11193496-B2
United States of America
Geared turbofan with non-epicyclic gear reduction system
Grant US-11187160-B2
United States of America
Variable area fan nozzle with wall thickness distribution
Grant US-11181074-B2
United States of America
Flexible support structure for a geared architecture gas turbine engine
Grant US-11174936-B2
United States of America
Low noise turbine for geared gas turbine engine
Grant US-11168614-B2
United States of America
Gas turbine engine with axial movable fan variable area nozzle
Grant US-11162456-B2
United States of America
Gas turbine engine shaft bearing configuration
Grant US-11149689-B2
United States of America
Turbine section of high bypass turbofan
Grant US-11149650-B2
United States of America
Low noise turbine for geared gas turbine engine
Grant US-11143109-B2
United States of America
Flexible coupling for geared turbine engine
Grant US-11136920-B2
United States of America
Geared turbofan arrangement with core split power ratio
Grant US-11125155-B2
United States of America
Fundamental gear system architecture
Grant US-11125167-B2
United States of America
Showing items 1–100