Luis A. Tapia

Person

Tempe, AZ, US

People

Patents Grantslast 30 patents

Information Patent Grant
Gas turbine component with cooling aperture having shaped inlet and...
- Patent number 11,220,918
- Issue date Jan 11, 2022
- Honeywell International Inc.
- Jeff Howe
- B22 - CASTING POWDER METALLURGY
Information Patent Grant
Gas turbine component with cooling aperture having shaped inlet and...
- Patent number 11,208,900
- Issue date Dec 28, 2021
- Honeywell International Inc.
- Jeff Howe
- B22 - CASTING POWDER METALLURGY
Information Patent Grant
Gas turbine component with cooling aperture having shaped inlet and...
- Patent number 10,830,052
- Issue date Nov 10, 2020
- Honeywell International Inc.
- Jeff Howe
- B22 - CASTING POWDER METALLURGY
Information Patent Grant
Airfoil with leading edge convective cooling system
- Patent number 10,669,862
- Issue date Jun 2, 2020
- Honeywell International Inc.
- Luis Tapia
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine components with lateral and forward sweep film c...
- Patent number 10,113,433
- Issue date Oct 30, 2018
- Honeywell International Inc.
- Mark C. Morris
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbine rotor assemblies with improved slot cavities
- Patent number 9,777,575
- Issue date Oct 3, 2017
- Honeywell International Inc.
- Luis Tapia
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine components with film cooling holes having cylind...
- Patent number 9,650,900
- Issue date May 16, 2017
- Honeywell International Inc.
- Malak Fouad Malak
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbine blade airfoils including film cooling systems, and methods...
- Patent number 9,562,437
- Issue date Feb 7, 2017
- Honeywell International Inc.
- Vighneswara Rao Kollati
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Grant
Turbine blade airfoils including showerhead film cooling systems, a...
- Patent number 9,228,440
- Issue date Jan 5, 2016
- Honeywell International Inc.
- Vighneswara Rao Kollati
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine components with cooling hole trenches
- Patent number 8,628,293
- Issue date Jan 14, 2014
- Honeywell International Inc.
- Dhinagaran Ramachandran
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Gas turbine engine components with improved film cooling
- Patent number 8,529,193
- Issue date Sep 10, 2013
- Honeywell International Inc.
- Jyothishkumar Venkataramanan
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Seal plates for directing airflow through a turbine section of an e...
- Patent number 8,444,387
- Issue date May 21, 2013
- Honeywell International Inc.
- Mark C. Morris
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Turbine engine components
- Patent number 8,371,814
- Issue date Feb 12, 2013
- Honeywell International Inc.
- Dhinagaran Ramachandran
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
High effectiveness cooled turbine blade
- Patent number 7,625,178
- Issue date Dec 1, 2009
- Honeywell International Inc.
- Mark C. Morris
- B22 - CASTING POWDER METALLURGY

Patents Applicationslast 30 patents

Information Patent Application
GAS TURBINE COMPONENT WITH COOLING APERTURE HAVING SHAPED INLET AND...
- Publication number 20210003019
- Publication date Jan 7, 2021
- HONEYWELL INTERNATIONAL INC.
- Jeff Howe
- B22 - CASTING POWDER METALLURGY
Information Patent Application
AIRFOIL WITH LEADING EDGE CONVECTIVE COOLING SYSTEM
- Publication number 20200018172
- Publication date Jan 16, 2020
- HONEYWELL INTERNATIONAL INC.
- Luis Tapia
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE COMPONENT WITH COOLING APERTURE HAVING SHAPED INLET AND...
- Publication number 20200011186
- Publication date Jan 9, 2020
- HONEYWELL INTERNATIONAL INC.
- Jeff Howe
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
GAS TURBINE COMPONENT WITH COOLING APERTURE HAVING SHAPED INLET AND...
- Publication number 20180073368
- Publication date Mar 15, 2018
- HONEYWELL INTERNATIONAL INC.
- Jeff Howe
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBINE ROTOR ASSEMBLIES WITH IMPROVED SLOT CAVITIES
- Publication number 20150204194
- Publication date Jul 23, 2015
- Honeywell International Inc.
- Luis Tapia
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBINE BLADE AIRFOILS INCLUDING FILM COOLING SYSTEMS, AND METHODS...
- Publication number 20140356188
- Publication date Dec 4, 2014
- Honeywell International, Inc.
- Vighneswara Rao Kollati
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Application
TURBINE BLADE AIRFOILS INCLUDING SHOWERHEAD FILM COOLING SYSTEMS, A...
- Publication number 20140154096
- Publication date Jun 5, 2014
- Honeywell International Inc.
- Vighneswara Rao Kollati
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
GAS TURBINE ENGINE COMPONENTS WITH LATERAL AND FORWARD SWEEP FILM C...
- Publication number 20140099189
- Publication date Apr 10, 2014
- Honeywell International Inc.
- Mark C. Morris
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
GAS TURBINE ENGINE COMPONENTS WITH COOLING HOLE TRENCHES
- Publication number 20130315710
- Publication date Nov 28, 2013
- Honeywell International Inc.
- Vighneswara Rao Kollati
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE ENGINE COMPONENTS WITH FILM COOLING HOLES HAVING CYLIND...
- Publication number 20130294889
- Publication date Nov 7, 2013
- Honeywell International Inc.
- Malak Fouad Malak
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
GAS TURBINE ENGINE COMPONENTS WITH COOLING HOLE TRENCHES
- Publication number 20110311369
- Publication date Dec 22, 2011
- Honeywell International Inc.
- Dhinagaran Ramachandran
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
SEAL PLATES FOR DIRECTING AIRFLOW THROUGH A TURBINE SECTION OF AN E...
- Publication number 20110123325
- Publication date May 26, 2011
- Honeywell International Inc.
- Mark C. Morris
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE ENGINE COMPONENTS WITH IMPROVED FILM COOLING
- Publication number 20110123312
- Publication date May 26, 2011
- Honeywell International Inc.
- Jyothishkumar Venkataramanan
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
TURBINE ENGINE COMPONENTS
- Publication number 20100329846
- Publication date Dec 30, 2010
- Honeywell International Inc.
- Dhinagaran Ramachandran
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
High effectiveness cooled turbine blade
- Publication number 20080056908
- Publication date Mar 6, 2008
- Honeywell International, Inc.
- Mark C. Morris
- B22 - CASTING POWDER METALLURGY
Information Patent Application
Method to augment heat transfer using chamfered cylindrical depress...
- Publication number 20070201980
- Publication date Aug 30, 2007
- Honeywell International, Inc.
- Mark C. Morris
- B22 - CASTING POWDER METALLURGY

Luis A. Tapia

Person

Patents Grantslast 30 patents

Gas turbine component with cooling aperture having shaped inlet and...

Gas turbine component with cooling aperture having shaped inlet and...

Gas turbine component with cooling aperture having shaped inlet and...

Airfoil with leading edge convective cooling system

Gas turbine engine components with lateral and forward sweep film c...

Turbine rotor assemblies with improved slot cavities

Gas turbine engine components with film cooling holes having cylind...

Turbine blade airfoils including film cooling systems, and methods...

Turbine blade airfoils including showerhead film cooling systems, a...

Gas turbine engine components with cooling hole trenches

Gas turbine engine components with improved film cooling

Seal plates for directing airflow through a turbine section of an e...

Turbine engine components

High effectiveness cooled turbine blade

Patents Applicationslast 30 patents

GAS TURBINE COMPONENT WITH COOLING APERTURE HAVING SHAPED INLET AND...

AIRFOIL WITH LEADING EDGE CONVECTIVE COOLING SYSTEM

GAS TURBINE COMPONENT WITH COOLING APERTURE HAVING SHAPED INLET AND...

GAS TURBINE COMPONENT WITH COOLING APERTURE HAVING SHAPED INLET AND...

TURBINE ROTOR ASSEMBLIES WITH IMPROVED SLOT CAVITIES

TURBINE BLADE AIRFOILS INCLUDING FILM COOLING SYSTEMS, AND METHODS...

TURBINE BLADE AIRFOILS INCLUDING SHOWERHEAD FILM COOLING SYSTEMS, A...

GAS TURBINE ENGINE COMPONENTS WITH LATERAL AND FORWARD SWEEP FILM C...

GAS TURBINE ENGINE COMPONENTS WITH COOLING HOLE TRENCHES

GAS TURBINE ENGINE COMPONENTS WITH FILM COOLING HOLES HAVING CYLIND...

GAS TURBINE ENGINE COMPONENTS WITH COOLING HOLE TRENCHES

SEAL PLATES FOR DIRECTING AIRFLOW THROUGH A TURBINE SECTION OF AN E...

GAS TURBINE ENGINE COMPONENTS WITH IMPROVED FILM COOLING

TURBINE ENGINE COMPONENTS

High effectiveness cooled turbine blade

Method to augment heat transfer using chamfered cylindrical depress...