Searching US Patent Collection...
Results of Search in US Patent Collection db for:
REF/7632064: 49 patents.
Hits 1 through 49
out of 49
| PAT. NO. | | Title |
| 1 |
10,989,143 |
 |
Gas turbine engine bifurcation located fan variable area nozzle
|
| 2 |
10,920,603 |
 |
Gas turbine engine forward bearing compartment architecture
|
| 3 |
10,914,315 |
 |
Gas turbine engine airfoil
|
| 4 |
10,907,579 |
 |
Gas turbine engine with geared architecture
|
| 5 |
10,907,482 |
 |
Turbine blade damper seal
|
| 6 |
10,890,245 |
 |
Epicyclic gear train
|
| 7 |
10,890,195 |
 |
Gas turbine engine airfoil
|
| 8 |
10,830,334 |
 |
Ring gear mounting arrangement with oil scavenge scheme
|
| 9 |
10,830,153 |
 |
Geared turbofan engine with power density range
|
| 10 |
10,830,130 |
 |
Geared turbofan with three turbines all counter-rotating
|
| 11 |
10,823,052 |
 |
Geared turbofan engine with targeted modular efficiency
|
| 12 |
10,808,617 |
 |
Split-zone flow metering T-tube
|
| 13 |
10,801,355 |
 |
Geared turbofan with four star/planetary gear reduction
|
| 14 |
10,794,292 |
 |
Geared turbofan gas turbine engine architecture
|
| 15 |
10,655,538 |
 |
Geared gas turbine engine with reduced fan noise
|
| 16 |
10,591,047 |
 |
Ring gear mounting arrangement with oil scavenge scheme
|
| 17 |
10,590,802 |
 |
Flexible support structure for a geared architecture gas turbine engine
|
| 18 |
10,570,855 |
 |
Gas turbine engine with geared architecture
|
| 19 |
10,527,151 |
 |
Gas turbine engine with geared architecture
|
| 20 |
10,518,893 |
 |
Variable geometry helicopter engine inlet
|
| 21 |
10,451,004 |
 |
Gas turbine engine with low stage count low pressure turbine
|
| 22 |
10,301,971 |
 |
Low pressure ratio fan engine having a dimensional relationship between
inlet and fan size
|
| 23 |
10,288,011 |
 |
Geared turbofan gas turbine engine architecture
|
| 24 |
10,288,010 |
 |
Geared turbofan gas turbine engine architecture
|
| 25 |
10,273,976 |
 |
Actively morphable vane
|
| 26 |
10,260,406 |
 |
Supercharged internal combustion engine with mixed-flow turbine
|
| 27 |
10,221,770 |
 |
Fundamental gear system architecture
|
| 28 |
10,036,351 |
 |
Geared turbofan with three co-rotating turbines
|
| 29 |
10,036,350 |
 |
Geared turbofan with three turbines all co-rotating
|
| 30 |
10,036,264 |
 |
Variable area gas turbine engine component having movable spar and shell
|
| 31 |
10,030,586 |
 |
Geared turbofan gas turbine engine architecture
|
| 32 |
9,896,966 |
 |
Tie rod for a gas turbine engine
|
| 33 |
9,840,969 |
 |
Gear system architecture for gas turbine engine
|
| 34 |
9,828,944 |
 |
Geared turbofan gas turbine engine architecture
|
| 35 |
9,752,511 |
 |
Geared architecture for high speed and small volume fan drive turbine
|
| 36 |
9,739,206 |
 |
Geared turbofan gas turbine engine architecture
|
| 37 |
9,695,751 |
 |
Geared turbofan gas turbine engine architecture
|
| 38 |
9,656,760 |
 |
Variable geometry helicopter engine inlet
|
| 39 |
9,631,558 |
 |
Geared architecture for high speed and small volume fan drive turbine
|
| 40 |
9,617,868 |
 |
Gas turbine engine variable geometry flow component
|
| 41 |
9,394,804 |
 |
Apparatus and method for rotating fluid controlling vanes in small turbine
engines and other applications
|
| 42 |
9,353,949 |
 |
Device for improved air and fuel distribution to a combustor
|
| 43 |
8,915,703 |
 |
Internally actuated inlet guide vane for fan section
|
| 44 |
8,899,915 |
 |
Geared architecture for high speed and small volume fan drive turbine
|
| 45 |
8,756,908 |
 |
Fundamental gear system architecture
|
| 46 |
8,747,055 |
 |
Geared architecture for high speed and small volume fan drive turbine
|
| 47 |
8,684,303 |
 |
Gas turbine engine compressor arrangement
|
| 48 |
8,257,021 |
 |
Gas-turbine engine with variable stator vanes
|
| 49 |
8,001,791 |
 |
Turbine engine frame having an actuated equilibrating case
|