SL

Scott D. Lewis

RTX (Raytheon): 39 patents #128 of 15,912Top 1%
PS Penn State: 1 patents #667 of 1,788Top 40%
Overall (All Time): #79,265 of 4,157,543Top 2%
40
Patents All Time

Issued Patents All Time

Showing 25 most recent of 40 patents

Patent #TitleCo-InventorsDate
11407065 Systems and methods for manufacturing film cooling hole diffuser portion Stephen Brian Lynch, Shane Haydt 2022-08-09
11352902 Cooling arrangement including alternating pedestals for gas turbine engine components 2022-06-07
11306919 Combustor panel cooling hole arrangement 2022-04-19
11286787 Gas turbine engine airfoil with showerhead cooling holes near leading edge Dominic J. Mongillo, Atul Kohli 2022-03-29
11286809 Airfoil platform cooling channels Kyle C. Lana 2022-03-29
11168570 Cooling arrangement for gas turbine engine components 2021-11-09
11156117 Seal arc segment with sloped circumferential sides 2021-10-26
11143039 Turbine engine component including an axially aligned skin core passage interrupted by a pedestal 2021-10-12
11029027 Dilution/effusion hole pattern for thick combustor panels James B. Hoke, Jeffrey J. Lienau 2021-06-08
10815803 BOAS thermal protection Dominic J. Mongillo, Mark F. Zelesky, Bret M. Teller, Russell Deibel, Matthew S. Gleiner 2020-10-27
10815788 Turbine blade with slot film cooling Kyle C. Lana 2020-10-27
10801325 Turbine blade with tip vortex control and tip shelf Dominic J. Mongillo, Jeffrey T. Morton 2020-10-13
10801331 Gas turbine engine rotor including squealer tip pocket Patrick D. Couture, Kyle C. Lana 2020-10-13
10773344 Systems and methods for manufacturing film cooling hole diffuser portion Stephen Brian Lynch, Shane Haydt 2020-09-15
10677066 Turbine blade with airfoil tip vortex control Kyle C. Lana 2020-06-09
10577936 Mateface surfaces having a geometry on turbomachinery hardware John W. Magowan 2020-03-03
10533428 Oblong purge holes 2020-01-14
10513931 Cooling systems and internally-cooled engine parts having an impingement cavity with an undulating internal surface Kyle C. Lana 2019-12-24
10502066 Turbine engine component including an axially aligned skin core passage interrupted by a pedestal 2019-12-10
10422230 Cooling hole with curved metering section Mark F. Zelesky, Dominic J. Mongillo 2019-09-24
10408071 BOAS thermal protection Dominic J. Mongillo, Mark F. Zelesky, Bret M. Teller, Russell Deibel, Matthew S. Gleiner 2019-09-10
10400607 Large-footprint turbine cooling hole Lane Thornton, Matthew A. Devore 2019-09-03
10392943 Film cooling hole including offset diffuser portion Stephen Brian Lynch, Shane Haydt 2019-08-27
10364680 Gas turbine engine component having platform trench Bret M. Teller, Mark F. Zelesky, Brandon W. Spangler, Ricardo Trindade 2019-07-30
10323524 Axial skin core cooling passage for a turbine engine component 2019-06-18