Searching US Patent Collection...

	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	10,830,178		Gas turbine engine variable area fan nozzle control
10	10,830,153		Geared turbofan engine with power density range
11	10,830,152		Gas turbine engine compressor arrangement
12	10,823,052		Geared turbofan engine with targeted modular efficiency
13	10,815,888		Geared turbofan bearing arrangement
14	10,808,617		Split-zone flow metering T-tube
15	10,801,355		Geared turbofan with four star/planetary gear reduction
16	10,794,293		Turbine section of high bypass turbofan
17	10,794,292		Geared turbofan gas turbine engine architecture
18	10,781,755		Turbine engine gearbox
19	10,774,653		Composite gas turbine engine component with lattice structure
20	10,760,488		Geared turbofan engine gearbox arrangement
21	10,753,285		Method of assembly for gas turbine fan drive gear system
22	10,731,563		Compressed air bleed supply for buffer system
23	10,731,559		Lubrication system for gas turbine engines
24	10,731,473		Gas turbine engine component having engineered vascular structure
25	10,711,703		Flutter sensing and control system for a gas turbine engine
26	10,697,375		Flutter sensing and control system for a gas turbine engine
27	10,677,192		Dual function cascade integrated variable area fan nozzle and thrust reverser
28	10,662,781		Gas turbine engine component having vascular engineered lattice structure
29	10,655,538		Geared gas turbine engine with reduced fan noise
30	10,605,351		Oil baffle for gas turbine fan drive gear system
31	10,605,202		Efficient, low pressure ratio propulsor for gas turbine engines
32	10,605,167		Gas turbine engine front center body architecture
33	10,605,092		Cooling hole with shaped meter
34	10,591,047		Ring gear mounting arrangement with oil scavenge scheme
35	10,590,802		Flexible support structure for a geared architecture gas turbine engine
36	10,584,660		Geared turbomachine fan and compressor rotation
37	10,578,053		Gas turbine engine variable area fan nozzle with ice management
38	10,578,018		Geared turbofan engine gearbox arrangement
39	10,577,965		Epicyclic gear train
40	10,570,855		Gas turbine engine with geared architecture
41	10,570,746		Gas turbine engine component having vascular engineered lattice structure
42	10,563,867		CMC articles having small complex features for advanced film cooling
43	10,563,576		Turbofan engine bearing and gearbox arrangement
44	10,550,852		Gas turbine engine airfoil
45	10,550,714		Gas turbine engine forward bearing compartment architecture
46	10,550,713		Gas turbine engine forward bearing compartment architecture
47	10,544,741		Flutter sensing and control system for a gas turbine engine
48	10,539,026		Gas turbine engine component with cooling holes having variable roughness
49	10,527,151		Gas turbine engine with geared architecture
50	10,519,778		Gas turbine engine component with converging/diverging cooling passage