Christopher Drake

Person

Atlanta, GA, US

People

Patents Grantslast 30 patents

Information Patent Grant
Sealed combustor liner panel for a gas turbine engine
- Patent number 10,816,201
- Issue date Oct 27, 2020
- Raytheon Technologies Corporation
- Christopher Drake
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Swirler mount interface for gas turbine engine combustor
- Patent number 10,598,381
- Issue date Mar 24, 2020
- United Technologies Corporation
- Christopher Drake
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Gas turbine engine wave geometry combustor liner panel
- Patent number 10,508,808
- Issue date Dec 17, 2019
- United Technologies Corporation
- Christopher Drake
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine combustor liner panel
- Patent number 10,352,566
- Issue date Jul 16, 2019
- United Technologies Corporation
- Christopher Drake
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Dual anti surge and anti rotation feature on first vane support
- Patent number 10,337,354
- Issue date Jul 2, 2019
- United Technologies Corporation
- Christopher Drake
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Flow splitting first vane support for gas turbine engine
- Patent number 10,190,425
- Issue date Jan 29, 2019
- United Technologies Corporation
- Christopher Drake
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Gas turbine engine wall assembly with circumferential rail stud arc...
- Patent number 10,088,161
- Issue date Oct 2, 2018
- United Technologies Corporation
- Christopher Drake
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Swirler mount interface for gas turbine engine combustor
- Patent number 10,088,166
- Issue date Oct 2, 2018
- United Technologies Corporation
- Christopher Drake
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Grant
Tube fed tangential on-board injector for gas turbine engine
- Patent number 9,777,634
- Issue date Oct 3, 2017
- United Technologies Corporation
- Christopher Drake
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Patents Applicationslast 30 patents

Information Patent Application
GAS TURBINE ENGINE WALL ASSEMBLY WITH CIRCUMFERENTIAL RAIL STUD ARC...
- Publication number 20170159935
- Publication date Jun 8, 2017
- United Technologies Corporation
- Christopher Drake
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
CONDUCTIVE PANEL SURFACE COOLING AUGMENTATION FOR GAS TURBINE ENGIN...
- Publication number 20160370008
- Publication date Dec 22, 2016
- United Technologies Corporation
- Christopher Drake
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
COMBUSTOR PANEL WITH MULTIPLE ATTACHMENTS
- Publication number 20160245518
- Publication date Aug 25, 2016
- United Technologies Corporation
- Christopher Drake
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
FLOW SPLITTING FIRST VANE SUPPORT FOR GAS TURBINE ENGINE
- Publication number 20160215633
- Publication date Jul 28, 2016
- Christopher Drake
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
SEALED COMBUSTOR LINER PANEL FOR A GAS TURBINE ENGINE
- Publication number 20160201914
- Publication date Jul 14, 2016
- United Technologies Corporation
- Christopher Drake
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
VENA CONTRACTA SWIRLING DILUTION PASSAGES FOR GAS TURBINE ENGINE CO...
- Publication number 20160201908
- Publication date Jul 14, 2016
- United Technologies Corporation
- Christopher Drake
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
DUAL ANTI SURGE AND ANTI ROTATION FEATURE ON FIRST VANE SUPPORT
- Publication number 20160194981
- Publication date Jul 7, 2016
- Christopher Drake
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
SWIRLER MOUNT INTERFACE FOR GAS TURBINE ENGINE COMBUSTOR
- Publication number 20160169521
- Publication date Jun 16, 2016
- United Technologies Corporation
- Christopher Drake
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Application
SWIRLER MOUNT INTERFACE FOR GAS TURBINE ENGINE COMBUSTOR
- Publication number 20160153660
- Publication date Jun 2, 2016
- United Technologies Corporation
- Christopher Drake
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Application
GAS TURBINE ENGINE COMBUSTOR LINER PANEL
- Publication number 20160123592
- Publication date May 5, 2016
- United Technologies Corporation
- Christopher Drake
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
GAS TURBINE ENGINE COMBUSTOR LINER PANEL
- Publication number 20160116166
- Publication date Apr 28, 2016
- United Technologies Corporation
- Christopher DRAKE
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
GAS TURBINE ENGINE WAVE GEOMETRY COMBUSTOR LINER PANEL
- Publication number 20160109128
- Publication date Apr 21, 2016
- United Technologies Corporation
- Christopher Drake
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TUBE FED TANGENTIAL ON-BOARD INJECTOR FOR GAS TURBINE ENGINE
- Publication number 20150068210
- Publication date Mar 12, 2015
- United Technologies Corporation
- Christopher Drake
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Christopher Drake

Person

Patents Grantslast 30 patents

Sealed combustor liner panel for a gas turbine engine

Swirler mount interface for gas turbine engine combustor

Gas turbine engine wave geometry combustor liner panel

Gas turbine engine combustor liner panel

Dual anti surge and anti rotation feature on first vane support

Flow splitting first vane support for gas turbine engine

Gas turbine engine wall assembly with circumferential rail stud arc...

Swirler mount interface for gas turbine engine combustor

Tube fed tangential on-board injector for gas turbine engine

Patents Applicationslast 30 patents

GAS TURBINE ENGINE WALL ASSEMBLY WITH CIRCUMFERENTIAL RAIL STUD ARC...

CONDUCTIVE PANEL SURFACE COOLING AUGMENTATION FOR GAS TURBINE ENGIN...

COMBUSTOR PANEL WITH MULTIPLE ATTACHMENTS

FLOW SPLITTING FIRST VANE SUPPORT FOR GAS TURBINE ENGINE

SEALED COMBUSTOR LINER PANEL FOR A GAS TURBINE ENGINE

VENA CONTRACTA SWIRLING DILUTION PASSAGES FOR GAS TURBINE ENGINE CO...

DUAL ANTI SURGE AND ANTI ROTATION FEATURE ON FIRST VANE SUPPORT

SWIRLER MOUNT INTERFACE FOR GAS TURBINE ENGINE COMBUSTOR

SWIRLER MOUNT INTERFACE FOR GAS TURBINE ENGINE COMBUSTOR

GAS TURBINE ENGINE COMBUSTOR LINER PANEL

GAS TURBINE ENGINE COMBUSTOR LINER PANEL

GAS TURBINE ENGINE WAVE GEOMETRY COMBUSTOR LINER PANEL

TUBE FED TANGENTIAL ON-BOARD INJECTOR FOR GAS TURBINE ENGINE