Constantine Baltas

Person

Manchester, CT, US

People

Patents Grantslast 30 patents

Information Patent Grant
Gas turbine engine bifurcation located fan variable area nozzle
- Patent number 11,391,240
- Issue date Jul 19, 2022
- Raytheon Technologies Corporation
- Constantine Baltas
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Acoustic liner with varied properties
- Patent number RE48980
- Issue date Mar 22, 2022
- Raytheon Technologies Corporation
- Jonathan Gilson
Information Patent Grant
Gas turbine engine bifurcation located fan variable area nozzle
- Patent number 10,989,143
- Issue date Apr 27, 2021
- Raytheon Technologies Corporation
- Constantine Baltas
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Split-zone flow metering T-tube
- Patent number 10,808,617
- Issue date Oct 20, 2020
- Raytheon Technologies Corporation
- Jorge I. Farah
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Variable fan nozzle using shape memory material
- Patent number 10,371,001
- Issue date Aug 6, 2019
- United Technologies Corporation
- Constantine Baltas
- F03 - MACHINES OR ENGINES FOR LIQUIDS WIND, SPRING WEIGHT AND MISCELLANEOUS M...
Information Patent Grant
Noise reducing vane
- Patent number 10,287,987
- Issue date May 14, 2019
- United Technologies Corporation
- Constantine Baltas
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Geared turbofan engine having a reduced number of fan blades and im...
- Patent number 10,184,340
- Issue date Jan 22, 2019
- United Technologies Corporation
- Constantine Baltas
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Acoustic liner with varied properties
- Patent number 10,066,548
- Issue date Sep 4, 2018
- United Technologies Corporation
- Jonathan Gilson
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Gas turbine engine bifurcation located fan variable area nozzle
- Patent number 9,885,313
- Issue date Feb 6, 2018
- United Technologes Corporation
- Constantine Baltas
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Variable fan nozzle using shape memory material
- Patent number 9,328,695
- Issue date May 3, 2016
- United Technologies Corporation
- Constantine Baltas
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Rotor with flattened exit pressure profile
- Patent number 9,017,037
- Issue date Apr 28, 2015
- United Technologies Corporation
- Constantine Baltas
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Corrugated core cowl for a gas turbine engine
- Patent number 8,857,151
- Issue date Oct 14, 2014
- United Technologies Corporation
- Constantine Baltas
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine having variable flow through a bifurcation havin...
- Patent number 8,418,471
- Issue date Apr 16, 2013
- United Technologies Corporation
- Constantine Baltas
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Corrugated core cowl for a gas turbine engine
- Patent number 8,291,689
- Issue date Oct 23, 2012
- United Technologies Corporation
- Constantine Baltas
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine with a variable exit area fan nozzle, nacelle as...
- Patent number 8,256,225
- Issue date Sep 4, 2012
- United Technologies Corporation
- Constantine Baltas
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

Information Patent Application
GAS TURBINE ENGINE BIFURCATION LOCATED FAN VARIABLE AREA NOZZLE
- Publication number 20210215120
- Publication date Jul 15, 2021
- Raytheon Technologies Corporation
- Constantine Baltas
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE BIFURCATION LOCATED FAN VARIABLE AREA NOZZLE
- Publication number 20180274483
- Publication date Sep 27, 2018
- United Technologies Corporation
- Constantine Baltas
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
SPLIT-ZONE FLOW METERING T-TUBE
- Publication number 20170342904
- Publication date Nov 30, 2017
- One Financial Plaza
- Jorge I. Farah
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
VARIABLE FAN NOZZLE USING SHAPE MEMORY MATERIAL
- Publication number 20160138416
- Publication date May 19, 2016
- United Technologies Corporation
- Constantine Baltas
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Geared Turbofan Engine Having a Reduced Number of Fan Blades and Im...
- Publication number 20160003049
- Publication date Jan 7, 2016
- United Technologies Corporation
- Constantine BALTAS
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
ACOUSTIC LINER WITH VARIED PROPERTIES
- Publication number 20150369127
- Publication date Dec 24, 2015
- United Technologies Corporation
- Jonathan GILSON
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GEARED GAS TURBINE ENGINE INTEGRATED WITH A VARIABLE AREA FAN NOZZL...
- Publication number 20150252751
- Publication date Sep 10, 2015
- Constantine Baltas
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
REDUCTION IN JET FLAP INTERACTION NOISE WITH GEARED TURBINE ENGINE
- Publication number 20150233298
- Publication date Aug 20, 2015
- Constantine Baltas
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NOISE REDUCING VANE
- Publication number 20140348630
- Publication date Nov 27, 2014
- United Technologies Corporation
- Constantine Baltas
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ROTOR WITH FLATTENED EXIT PRESSURE PROFILE
- Publication number 20130189117
- Publication date Jul 25, 2013
- United Technologies Corporation
- Constantine Baltas
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
CORRUGATED CORE COWL FOR A GAS TURBINE ENGINE
- Publication number 20130034432
- Publication date Feb 7, 2013
- Constantine Baltas
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE BIFURCATION LOCATED FAN VARIABLE AREA NOZZLE
- Publication number 20120102915
- Publication date May 3, 2012
- Constantine Baltas
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
CORRUGATED CORE COWL FOR A GAS TURBINE ENGINE
- Publication number 20100089028
- Publication date Apr 15, 2010
- Constantine Baltas
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
VARIABLE FAN NOZZLE USING SHAPE MEMORY MATERIAL
- Publication number 20100037588
- Publication date Feb 18, 2010
- Constantine Baltas
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE ENGINE WITH A VARIABLE EXIT AREA FAN NOZZLE, NACELLE AS...
- Publication number 20100008764
- Publication date Jan 14, 2010
- Constantine Baltas
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE BIFURCATION LOCATED IN A FAN VARIABLE AREA NOZZLE
- Publication number 20090288387
- Publication date Nov 26, 2009
- Constantine Baltas
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Constantine Baltas

Person

Patents Grantslast 30 patents

Gas turbine engine bifurcation located fan variable area nozzle

Acoustic liner with varied properties

Gas turbine engine bifurcation located fan variable area nozzle

Split-zone flow metering T-tube

Variable fan nozzle using shape memory material

Noise reducing vane

Geared turbofan engine having a reduced number of fan blades and im...

Acoustic liner with varied properties

Gas turbine engine bifurcation located fan variable area nozzle

Variable fan nozzle using shape memory material

Rotor with flattened exit pressure profile

Corrugated core cowl for a gas turbine engine

Gas turbine engine having variable flow through a bifurcation havin...

Corrugated core cowl for a gas turbine engine

Gas turbine engine with a variable exit area fan nozzle, nacelle as...

Patents Applicationslast 30 patents

GAS TURBINE ENGINE BIFURCATION LOCATED FAN VARIABLE AREA NOZZLE

GAS TURBINE ENGINE BIFURCATION LOCATED FAN VARIABLE AREA NOZZLE

SPLIT-ZONE FLOW METERING T-TUBE

VARIABLE FAN NOZZLE USING SHAPE MEMORY MATERIAL

Geared Turbofan Engine Having a Reduced Number of Fan Blades and Im...

ACOUSTIC LINER WITH VARIED PROPERTIES

GEARED GAS TURBINE ENGINE INTEGRATED WITH A VARIABLE AREA FAN NOZZL...

REDUCTION IN JET FLAP INTERACTION NOISE WITH GEARED TURBINE ENGINE

NOISE REDUCING VANE

ROTOR WITH FLATTENED EXIT PRESSURE PROFILE

CORRUGATED CORE COWL FOR A GAS TURBINE ENGINE

GAS TURBINE ENGINE BIFURCATION LOCATED FAN VARIABLE AREA NOZZLE

CORRUGATED CORE COWL FOR A GAS TURBINE ENGINE

VARIABLE FAN NOZZLE USING SHAPE MEMORY MATERIAL

GAS TURBINE ENGINE WITH A VARIABLE EXIT AREA FAN NOZZLE, NACELLE AS...

GAS TURBINE ENGINE BIFURCATION LOCATED IN A FAN VARIABLE AREA NOZZLE