| 14 |
10,823,260 |
 |
Transmission device for splitting torque between two coaxial gears, in
particular for a planetary gearing for aeronautic applications, and
method for manufacturing and assembling said transmission device
|
| 15 |
10,823,052 |
 |
Geared turbofan engine with targeted modular efficiency
|
| 16 |
10,823,051 |
 |
Geared turbofan engine with high compressor exit temperature
|
| 17 |
10,816,078 |
 |
Systems and methods for a gas turbine engine with combined
multi-directional gearbox deflection limiters and dampers
|
| 18 |
10,815,888 |
 |
Geared turbofan bearing arrangement
|
| 19 |
10,808,621 |
 |
Gas turbine engine having support structure with swept leading edge
|
| 20 |
10,808,617 |
 |
Split-zone flow metering T-tube
|
| 21 |
10,801,355 |
 |
Geared turbofan with four star/planetary gear reduction
|
| 22 |
10,794,293 |
 |
Turbine section of high bypass turbofan
|
| 23 |
10,794,292 |
 |
Geared turbofan gas turbine engine architecture
|
| 24 |
10,794,291 |
 |
Geared turbofan architecture for regional jet aircraft
|
| 25 |
10,787,971 |
 |
Flexible coupling for geared turbine engine
|
| 26 |
10,787,970 |
 |
Flexible coupling for geared turbine engine
|
| 27 |
10,781,755 |
 |
Turbine engine gearbox
|
| 28 |
10,760,488 |
 |
Geared turbofan engine gearbox arrangement
|
| 29 |
10,753,285 |
 |
Method of assembly for gas turbine fan drive gear system
|
| 30 |
10,731,563 |
 |
Compressed air bleed supply for buffer system
|
| 31 |
10,731,559 |
 |
Lubrication system for gas turbine engines
|
| 32 |
10,731,510 |
 |
Gas turbine engine with fluid damper
|
| 33 |
10,724,479 |
 |
Thrust efficient turbofan engine
|
| 34 |
10,724,445 |
 |
Method of assembly for fan drive gear system with rotating carrier
|
| 35 |
10,724,431 |
 |
Buffer system that communicates buffer supply air to one or more portions
of a gas turbine engine
|
| 36 |
10,711,703 |
 |
Flutter sensing and control system for a gas turbine engine
|
| 37 |
10,697,375 |
 |
Flutter sensing and control system for a gas turbine engine
|
| 38 |
10,677,192 |
 |
Dual function cascade integrated variable area fan nozzle and thrust
reverser
|
| 39 |
10,662,880 |
 |
Turbine section of high bypass turbofan
|
| 40 |
10,655,538 |
 |
Geared gas turbine engine with reduced fan noise
|
| 41 |
10,648,383 |
 |
Planetary gear system arrangement with auxiliary oil system
|
| 42 |
10,634,053 |
 |
Electric windmill pump for gearbox durability
|
| 43 |
10,605,351 |
 |
Oil baffle for gas turbine fan drive gear system
|
| 44 |
10,605,259 |
 |
Gas turbine engine airfoil
|
| 45 |
10,605,202 |
 |
Efficient, low pressure ratio propulsor for gas turbine engines
|
| 46 |
10,605,172 |
 |
Low noise turbine for geared gas turbine engine
|
| 47 |
10,605,167 |
 |
Gas turbine engine front center body architecture
|
| 48 |
10,605,112 |
 |
Fan drive gear system spline oil lubrication scheme
|
| 49 |
10,605,104 |
 |
Multi-circuit lubrication system for a turbine engine
|
| 50 |
10,605,092 |
 |
Cooling hole with shaped meter
|