Scott D. Lewis

Person

Vernon, CT, US

People

Patents Grantslast 30 patents

Information Patent Grant
Systems and methods for manufacturing film cooling hole diffuser po...
- Patent number 11,407,065
- Issue date Aug 9, 2022
- Raytheon Corporation Inc.
- Scott D. Lewis
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Grant
Cooling arrangement including alternating pedestals for gas turbine...
- Patent number 11,352,902
- Issue date Jun 7, 2022
- AYTHEON TECHNOLOGIES CORPORATION
- Scott D. Lewis
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Combustor panel cooling hole arrangement
- Patent number 11,306,919
- Issue date Apr 19, 2022
- Raytheon Technologies Corporation
- Scott D. Lewis
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine airfoil with showerhead cooling holes near leadi...
- Patent number 11,286,787
- Issue date Mar 29, 2022
- Raytheon Technologies Corporation
- Scott D. Lewis
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Airfoil platform cooling channels
- Patent number 11,286,809
- Issue date Mar 29, 2022
- Raytheon Technologies Corporation
- Scott D Lewis
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Cooling arrangement for gas turbine engine components
- Patent number 11,168,570
- Issue date Nov 9, 2021
- Raytheon Technologies Corporation
- Scott D. Lewis
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Seal arc segment with sloped circumferential sides
- Patent number 11,156,117
- Issue date Oct 26, 2021
- Raytheon Technologies Corporation
- Scott D. Lewis
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbine engine component including an axially aligned skin core pas...
- Patent number 11,143,039
- Issue date Oct 12, 2021
- Raytheon Technologies Corporation
- Scott D. Lewis
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Dilution/effusion hole pattern for thick combustor panels
- Patent number 11,029,027
- Issue date Jun 8, 2021
- Raytheon Technologies Corporation
- Scott D. Lewis
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbine blade with slot film cooling
- Patent number 10,815,788
- Issue date Oct 27, 2020
- Raytheon Technologies Corporation
- Scott D. Lewis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
BOAS thermal protection
- Patent number 10,815,803
- Issue date Oct 27, 2020
- Raytheon Technologies Corporation
- Scott D. Lewis
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Turbine blade with tip vortex control and tip shelf
- Patent number 10,801,325
- Issue date Oct 13, 2020
- Raytheon Technologies Corporation
- Dominic J. Mongillo
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Gas turbine engine rotor including squealer tip pocket
- Patent number 10,801,331
- Issue date Oct 13, 2020
- Raytheon Technologies Corporation
- Patrick D. Couture
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Systems and methods for manufacturing film cooling hole diffuser po...
- Patent number 10,773,344
- Issue date Sep 15, 2020
- Raytheon Technologies Corporation
- Scott D. Lewis
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Grant
Turbine blade with airfoil tip vortex control
- Patent number 10,677,066
- Issue date Jun 9, 2020
- United Technologies Corporation
- Scott D. Lewis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Mateface surfaces having a geometry on turbomachinery hardware
- Patent number 10,577,936
- Issue date Mar 3, 2020
- United Technologies Corporation
- Scott D. Lewis
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Oblong purge holes
- Patent number 10,533,428
- Issue date Jan 14, 2020
- United Technologies Corporation
- Scott D. Lewis
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Cooling systems and internally-cooled engine parts having an imping...
- Patent number 10,513,931
- Issue date Dec 24, 2019
- United Technologies Corporation
- Scott D. Lewis
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Turbine engine component including an axially aligned skin core pas...
- Patent number 10,502,066
- Issue date Dec 10, 2019
- United Technologies Corporation
- Scott D. Lewis
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Cooling hole with curved metering section
- Patent number 10,422,230
- Issue date Sep 24, 2019
- United Technologies Corporation
- Scott D. Lewis
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
BOAS thermal protection
- Patent number 10,408,071
- Issue date Sep 10, 2019
- United Technologies Corporation
- Scott D. Lewis
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Large-footprint turbine cooling hole
- Patent number 10,400,607
- Issue date Sep 3, 2019
- United Technologies Corporation
- Lane Thornton
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Film cooling hole including offset diffuser portion
- Patent number 10,392,943
- Issue date Aug 27, 2019
- United Technologies Corporation
- Scott D. Lewis
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Gas turbine engine component having platform trench
- Patent number 10,364,680
- Issue date Jul 30, 2019
- United Technologies Corporation
- Bret M. Teller
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Axial skin core cooling passage for a turbine engine component
- Patent number 10,323,524
- Issue date Jun 18, 2019
- United Technologies Corporation
- Scott D. Lewis
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Axial skin core cooling passage for a turbine engine component
- Patent number 10,273,811
- Issue date Apr 30, 2019
- United Technologies Corporation
- Scott D. Lewis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine component with combined mate face and platform c...
- Patent number 10,227,875
- Issue date Mar 12, 2019
- United Technologies Corporation
- Scott D. Lewis
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Staggered crossovers for airfoils
- Patent number 10,208,603
- Issue date Feb 19, 2019
- United Technologies Corporation
- JinQuan Xu
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Mate face cooling holes for gas turbine engine component
- Patent number 10,180,067
- Issue date Jan 15, 2019
- United Technologies Corporation
- Jeffrey S. Beattie
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbine airfoil and method of cooling
- Patent number 10,156,144
- Issue date Dec 18, 2018
- United Technologies Corporation
- San Quach
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Patents Applicationslast 30 patents

Information Patent Application
COOLING ARRANGEMENT INCLUDING ALTERNATING PEDESTALS FOR GAS TURBINE...
- Publication number 20220065129
- Publication date Mar 3, 2022
- Raytheon Technologies Corporation
- Scott D. Lewis
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
SYSTEMS AND METHODS FOR MANUFACTURING FILM COOLING HOLE DIFFUSER PO...
- Publication number 20200368851
- Publication date Nov 26, 2020
- Raytheon Technologies Corporation
- Scott D. Lewis
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Application
TURBINE ENGINE COMPONENT INCLUDING AN AXIALLY ALIGNED SKIN CORE PAS...
- Publication number 20200149414
- Publication date May 14, 2020
- United Technologies Corporation
- Scott D. Lewis
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
COMBUSTOR PANEL COOLING HOLE ARRANGEMENT
- Publication number 20200124282
- Publication date Apr 23, 2020
- United Technologies Corporation
- SCOTT D. LEWIS
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
DILUTION/EFFUSION HOLE PATTERN FOR THICK COMBUSTOR PANELS
- Publication number 20200109854
- Publication date Apr 9, 2020
- United Technologies Corporation
- Scott D. Lewis
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
BOAS THERMAL PROTECTION
- Publication number 20190383153
- Publication date Dec 19, 2019
- United Technologies Corporation
- Scott D. Lewis
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
SYSTEMS AND METHODS FOR MANUFACTURING FILM COOLING HOLE DIFFUSER PO...
- Publication number 20180361512
- Publication date Dec 20, 2018
- United Technologies Corporation
- Scott D. Lewis
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
OBLONG PURGE HOLES
- Publication number 20180347379
- Publication date Dec 6, 2018
- United Technologies Corporation
- SCOTT D. LEWIS
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
AIRFOIL IMPINGEMENT CAVITY
- Publication number 20180306038
- Publication date Oct 25, 2018
- United Technologies Corporation
- Scott D. Lewis
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
AIRFOIL PLATFORM COOLING CHANNELS
- Publication number 20180306058
- Publication date Oct 25, 2018
- United Technologies Corporation
- Scott D. Lewis
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
TURBINE BLADE WITH TIP VORTEX CONTROL AND TIP SHELF
- Publication number 20180274368
- Publication date Sep 27, 2018
- United Technologies Corporation
- Dominic J. Mongillo
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
FILM COOLING HOLE INCLUDING OFFSET DIFFUSER PORTION
- Publication number 20180230811
- Publication date Aug 16, 2018
- United Technologies Corporation
- Scott D. Lewis
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
TURBINE BLADE WITH SLOT FILM COOLING
- Publication number 20180216472
- Publication date Aug 2, 2018
- United Technologies Corporation
- Scott D. Lewis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
LARGE AREA RATIO COOLING HOLES
- Publication number 20180135520
- Publication date May 17, 2018
- United Technologies Corporation
- SCOTT D. LEWIS
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE AIRFOIL WITH SHOWERHEAD COOLING HOLES NEAR LEADI...
- Publication number 20180073369
- Publication date Mar 15, 2018
- United Technologies Corporation
- Scott D. Lewis
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
GROOVED SEAL ARRANGEMENT FOR TURBINE ENGINE
- Publication number 20170362951
- Publication date Dec 21, 2017
- Scott D. Lewis
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
GAS TURBINE ENGINE ROTOR INCLUDING SQUEALER TIP POCKET
- Publication number 20170350255
- Publication date Dec 7, 2017
- United Technologies Corporation
- Patrick D. Couture
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SEAL ARC SEGMENT WITH SLOPED CIRCUMFERENTIAL SIDES
- Publication number 20170306781
- Publication date Oct 26, 2017
- United Technologies Corporation
- SCOTT D. LEWIS
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
COOLING SYSTEMS AND INTERNALLY-COOLED ENGINE PARTS HAVING AN IMPING...
- Publication number 20170175538
- Publication date Jun 22, 2017
- United Technologies Corporation
- Scott D. Lewis
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBINE BLADE WITH AIRFOIL TIP VORTEX CONTROL
- Publication number 20170145828
- Publication date May 25, 2017
- United Technologies Corporation
- Scott D. Lewis
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
TURBINE BLADE WITH AIRFOIL TIP VORTEX CONTROL
- Publication number 20170145827
- Publication date May 25, 2017
- United Technologies Corporation
- Scott D. Lewis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRFOIL PLATFORM COOLING CORE CIRCUITS WITH ONE-WALL HEAT TRANSFER...
- Publication number 20170145834
- Publication date May 25, 2017
- United Technologies Corporation
- SCOTT D. LEWIS
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
GROOVED SEAL ARRANGEMENT FOR TURBINE ENGINE
- Publication number 20170145848
- Publication date May 25, 2017
- Scott D. Lewis
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
COOLING HOLES OF TURBINE
- Publication number 20170101870
- Publication date Apr 13, 2017
- United Technologies Corporation
- Scott D. Lewis
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBINE AIRFOIL AND METHOD OF COOLING
- Publication number 20170089206
- Publication date Mar 30, 2017
- United Technologies Corporation
- San Quach
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
STAGGERED CROSSOVERS FOR AIRFOILS
- Publication number 20170081958
- Publication date Mar 23, 2017
- United Technologies Corporation
- JinQuan Xu
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
COOLING HOLE WITH CURVED METERING SECTION
- Publication number 20170081959
- Publication date Mar 23, 2017
- United Technologies Corporation
- Scott D. Lewis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE COMPONENT MATEFACE SURFACES
- Publication number 20170022839
- Publication date Jan 26, 2017
- United Technologies Corporation
- Scott D. Lewis
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
GAS TURBINE ENGINE AIRFOIL SQUEALER POCKET COOLING HOLE CONFIGURATION
- Publication number 20170002663
- Publication date Jan 5, 2017
- United Technologies Corporation
- San Quach
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
AIRFOIL IMPINGEMENT CAVITY
- Publication number 20160333701
- Publication date Nov 17, 2016
- United Technologies Corporation
- Scott D. Lewis
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Scott D. Lewis

Person

Patents Grantslast 30 patents

Systems and methods for manufacturing film cooling hole diffuser po...

Cooling arrangement including alternating pedestals for gas turbine...

Combustor panel cooling hole arrangement

Gas turbine engine airfoil with showerhead cooling holes near leadi...

Airfoil platform cooling channels

Cooling arrangement for gas turbine engine components

Seal arc segment with sloped circumferential sides

Turbine engine component including an axially aligned skin core pas...

Dilution/effusion hole pattern for thick combustor panels

Turbine blade with slot film cooling

BOAS thermal protection

Turbine blade with tip vortex control and tip shelf

Gas turbine engine rotor including squealer tip pocket

Systems and methods for manufacturing film cooling hole diffuser po...

Turbine blade with airfoil tip vortex control

Mateface surfaces having a geometry on turbomachinery hardware

Oblong purge holes

Cooling systems and internally-cooled engine parts having an imping...

Turbine engine component including an axially aligned skin core pas...

Cooling hole with curved metering section

BOAS thermal protection

Large-footprint turbine cooling hole

Film cooling hole including offset diffuser portion

Gas turbine engine component having platform trench

Axial skin core cooling passage for a turbine engine component

Axial skin core cooling passage for a turbine engine component

Gas turbine engine component with combined mate face and platform c...

Staggered crossovers for airfoils

Mate face cooling holes for gas turbine engine component

Turbine airfoil and method of cooling

Patents Applicationslast 30 patents

COOLING ARRANGEMENT INCLUDING ALTERNATING PEDESTALS FOR GAS TURBINE...

SYSTEMS AND METHODS FOR MANUFACTURING FILM COOLING HOLE DIFFUSER PO...

TURBINE ENGINE COMPONENT INCLUDING AN AXIALLY ALIGNED SKIN CORE PAS...

COMBUSTOR PANEL COOLING HOLE ARRANGEMENT

DILUTION/EFFUSION HOLE PATTERN FOR THICK COMBUSTOR PANELS

BOAS THERMAL PROTECTION

SYSTEMS AND METHODS FOR MANUFACTURING FILM COOLING HOLE DIFFUSER PO...

OBLONG PURGE HOLES

AIRFOIL IMPINGEMENT CAVITY

AIRFOIL PLATFORM COOLING CHANNELS

TURBINE BLADE WITH TIP VORTEX CONTROL AND TIP SHELF

FILM COOLING HOLE INCLUDING OFFSET DIFFUSER PORTION

TURBINE BLADE WITH SLOT FILM COOLING

LARGE AREA RATIO COOLING HOLES

GAS TURBINE ENGINE AIRFOIL WITH SHOWERHEAD COOLING HOLES NEAR LEADI...

GROOVED SEAL ARRANGEMENT FOR TURBINE ENGINE

GAS TURBINE ENGINE ROTOR INCLUDING SQUEALER TIP POCKET

SEAL ARC SEGMENT WITH SLOPED CIRCUMFERENTIAL SIDES

COOLING SYSTEMS AND INTERNALLY-COOLED ENGINE PARTS HAVING AN IMPING...

TURBINE BLADE WITH AIRFOIL TIP VORTEX CONTROL

TURBINE BLADE WITH AIRFOIL TIP VORTEX CONTROL

AIRFOIL PLATFORM COOLING CORE CIRCUITS WITH ONE-WALL HEAT TRANSFER...

GROOVED SEAL ARRANGEMENT FOR TURBINE ENGINE

COOLING HOLES OF TURBINE

TURBINE AIRFOIL AND METHOD OF COOLING

STAGGERED CROSSOVERS FOR AIRFOILS

COOLING HOLE WITH CURVED METERING SECTION

GAS TURBINE ENGINE COMPONENT MATEFACE SURFACES

GAS TURBINE ENGINE AIRFOIL SQUEALER POCKET COOLING HOLE CONFIGURATION

AIRFOIL IMPINGEMENT CAVITY