Searching US Patent Collection...
Results of Search in US Patent Collection db for:
REF/3935558: 92 patents.
Hits 1 through 50
out of 92
| PAT. NO. | | Title |
| 1 |
10,920,603 |
 |
Gas turbine engine forward bearing compartment architecture
|
| 2 |
10,914,315 |
 |
Gas turbine engine airfoil
|
| 3 |
10,907,579 |
 |
Gas turbine engine with geared architecture
|
| 4 |
10,907,482 |
 |
Turbine blade damper seal
|
| 5 |
10,890,245 |
 |
Epicyclic gear train
|
| 6 |
10,890,195 |
 |
Gas turbine engine airfoil
|
| 7 |
10,830,334 |
 |
Ring gear mounting arrangement with oil scavenge scheme
|
| 8 |
10,830,178 |
 |
Gas turbine engine variable area fan nozzle control
|
| 9 |
10,830,153 |
 |
Geared turbofan engine with power density range
|
| 10 |
10,830,152 |
 |
Gas turbine engine compressor arrangement
|
| 11 |
10,823,052 |
 |
Geared turbofan engine with targeted modular efficiency
|
| 12 |
10,815,888 |
 |
Geared turbofan bearing arrangement
|
| 13 |
10,808,617 |
 |
Split-zone flow metering T-tube
|
| 14 |
10,801,355 |
 |
Geared turbofan with four star/planetary gear reduction
|
| 15 |
10,794,293 |
 |
Turbine section of high bypass turbofan
|
| 16 |
10,794,292 |
 |
Geared turbofan gas turbine engine architecture
|
| 17 |
10,781,755 |
 |
Turbine engine gearbox
|
| 18 |
10,760,488 |
 |
Geared turbofan engine gearbox arrangement
|
| 19 |
10,753,285 |
 |
Method of assembly for gas turbine fan drive gear system
|
| 20 |
10,731,563 |
 |
Compressed air bleed supply for buffer system
|
| 21 |
10,731,559 |
 |
Lubrication system for gas turbine engines
|
| 22 |
10,711,703 |
 |
Flutter sensing and control system for a gas turbine engine
|
| 23 |
10,697,375 |
 |
Flutter sensing and control system for a gas turbine engine
|
| 24 |
10,677,192 |
 |
Dual function cascade integrated variable area fan nozzle and thrust
reverser
|
| 25 |
10,655,538 |
 |
Geared gas turbine engine with reduced fan noise
|
| 26 |
10,605,351 |
 |
Oil baffle for gas turbine fan drive gear system
|
| 27 |
10,605,202 |
 |
Efficient, low pressure ratio propulsor for gas turbine engines
|
| 28 |
10,605,167 |
 |
Gas turbine engine front center body architecture
|
| 29 |
10,591,047 |
 |
Ring gear mounting arrangement with oil scavenge scheme
|
| 30 |
10,590,802 |
 |
Flexible support structure for a geared architecture gas turbine engine
|
| 31 |
10,584,660 |
 |
Geared turbomachine fan and compressor rotation
|
| 32 |
10,578,053 |
 |
Gas turbine engine variable area fan nozzle with ice management
|
| 33 |
10,577,965 |
 |
Epicyclic gear train
|
| 34 |
10,570,855 |
 |
Gas turbine engine with geared architecture
|
| 35 |
10,563,576 |
 |
Turbofan engine bearing and gearbox arrangement
|
| 36 |
10,550,852 |
 |
Gas turbine engine airfoil
|
| 37 |
10,550,714 |
 |
Gas turbine engine forward bearing compartment architecture
|
| 38 |
10,550,713 |
 |
Gas turbine engine forward bearing compartment architecture
|
| 39 |
10,544,741 |
 |
Flutter sensing and control system for a gas turbine engine
|
| 40 |
10,527,151 |
 |
Gas turbine engine with geared architecture
|
| 41 |
10,465,549 |
 |
Gas turbine engine forward bearing compartment architecture
|
| 42 |
10,451,004 |
 |
Gas turbine engine with low stage count low pressure turbine
|
| 43 |
10,436,116 |
 |
Gas turbine engine geared architecture axial retention arrangement
|
| 44 |
10,371,061 |
 |
Turbine section of high bypass turbofan
|
| 45 |
10,358,924 |
 |
Turbofan arrangement with blade channel variations
|
| 46 |
10,309,414 |
 |
Gas turbine engine airfoil
|
| 47 |
10,301,971 |
 |
Low pressure ratio fan engine having a dimensional relationship between
inlet and fan size
|
| 48 |
10,294,894 |
 |
Thrust efficient turbofan engine
|
| 49 |
10,288,011 |
 |
Geared turbofan gas turbine engine architecture
|
| 50 |
10,288,010 |
 |
Geared turbofan gas turbine engine architecture
|