Razvan Virgil Florea

Person

Manchester, CT, US

People

Patents Grantslast 30 patents

Information Patent Grant
Airfoil with thickened root and fan and engine incorporating same
- Patent number 10,968,747
- Issue date Apr 6, 2021
- Raytheon Technologies Corporation
- Eric D. Gray
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Non-axisymmetric fan flow path
- Patent number 10,415,505
- Issue date Sep 17, 2019
- United Technologies Corporation
- Razvan Virgil Florea
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Active airflow system and method of reducing drag for aircraft
- Patent number 10,220,939
- Issue date Mar 5, 2019
- Sikorsky Aircraft Corporation
- ByungYoung Min
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas turbine engine inlet wall design
- Patent number 9,291,101
- Issue date Mar 22, 2016
- United Technologies Corporation
- Razvan Virgil Florea
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Coupled parametric design of flow control and duct shape
- Patent number 7,610,179
- Issue date Oct 27, 2009
- United Technologies Corporation
- Razvan Florea
- G06 - COMPUTING CALCULATING COUNTING

Patents Applicationslast 30 patents

Information Patent Application
EMBEDDED ENGINES IN HYBRID BLENDED WING BODY
- Publication number 20190055006
- Publication date Feb 21, 2019
- United Technologies Corporation
- Razvan Virgil Florea
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ACTIVE AIRFLOW SYSTEM AND METHOD OF REDUCING DRAG FOR AIRCRAFT
- Publication number 20170225772
- Publication date Aug 10, 2017
- SIKORSKY AIRCRAFT CORPORATION
- ByungYoung Min
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
DRAG REDUCTION OF HIGH SPEED AIRCRAFT
- Publication number 20170096212
- Publication date Apr 6, 2017
- SIKORSKY AIRCRAFT CORPORATION
- Razvan Virgil Florea
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
NON-AXISYMMETRIC FAN FLOW PATH
- Publication number 20160186690
- Publication date Jun 30, 2016
- United Technologies Corporation
- Razvan Virgil FLOREA
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Blended Wing Body Boundary Layer Ingesting Inlet Design Integration
- Publication number 20160144972
- Publication date May 26, 2016
- United Technologies Corporation
- Razvan Virgil Florea
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
EMBEDDED ENGINES IN HYBRID BLENDED WING BODY
- Publication number 20160122005
- Publication date May 5, 2016
- United Technologies Corporation
- Razvan Virgil Florea
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Airfoil with Thickened Root and Fan and Engine Incorporating Same
- Publication number 20160003048
- Publication date Jan 7, 2016
- United Technologies Corporation
- Eric D. Gray
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Non-Axisymmetric Exit Guide Vane Design
- Publication number 20150354501
- Publication date Dec 10, 2015
- United Technologies Corporation
- Razvan Virgil Florea
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE INLET WALL DESIGN
- Publication number 20150122952
- Publication date May 7, 2015
- United Technologies Corporation
- Razvan Virgil Florea
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Coupled parametric design of flow control and duct shape
- Publication number 20060069533
- Publication date Mar 30, 2006
- United Technologies Corporation
- Razvan Florea
- G06 - COMPUTING CALCULATING COUNTING

Razvan Virgil Florea

Person

Patents Grantslast 30 patents

Airfoil with thickened root and fan and engine incorporating same

Non-axisymmetric fan flow path

Active airflow system and method of reducing drag for aircraft

Gas turbine engine inlet wall design

Coupled parametric design of flow control and duct shape

Patents Applicationslast 30 patents

EMBEDDED ENGINES IN HYBRID BLENDED WING BODY

ACTIVE AIRFLOW SYSTEM AND METHOD OF REDUCING DRAG FOR AIRCRAFT

DRAG REDUCTION OF HIGH SPEED AIRCRAFT

NON-AXISYMMETRIC FAN FLOW PATH

Blended Wing Body Boundary Layer Ingesting Inlet Design Integration

EMBEDDED ENGINES IN HYBRID BLENDED WING BODY

Airfoil with Thickened Root and Fan and Engine Incorporating Same

Non-Axisymmetric Exit Guide Vane Design

GAS TURBINE ENGINE INLET WALL DESIGN

Coupled parametric design of flow control and duct shape