Dimitrie NEGULESCU

Person

Berlin, DE

People

Patents Grantslast 30 patents

Information Patent Grant
Rotor blade for a turbomachine and method for the assembly of a rot...
- Patent number 10,781,699
- Issue date Sep 22, 2020
- Rolls-Royce Deutschland Ltd & Co KG
- Dimitrie Negulescu
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Adaptive aircraft engine and aircraft having an adaptive engine
- Patent number 10,450,078
- Issue date Oct 22, 2019
- Rolls-Royce Deutschland Ltd & Co KG
- Dimitrie Negulescu
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Cooled turbine runner, in particular for an aircraft engine
- Patent number 10,436,031
- Issue date Oct 8, 2019
- Rolls-Royce Deutschland Ltd & Co KG
- Joana Negulescu
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbine with cooled turbine guide vanes
- Patent number 10,378,372
- Issue date Aug 13, 2019
- Rolls-Royce Deutschland Ltd & Co KG
- Dimitrie Negulescu
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine centripetal annular combustion chamber and method for f...
- Patent number 9,151,501
- Issue date Oct 6, 2015
- Rolls-Royce Deutschland Ltd & Co KG
- Dimitrie Negulescu
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine combustion chamber arrangement of axial type of constru...
- Patent number 9,151,223
- Issue date Oct 6, 2015
- Rolls-Royce Deutschland Ltd & Co KG
- Dimitrie Negulescu
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Running-gap control system of an aircraft gas turbine
- Patent number 8,834,108
- Issue date Sep 16, 2014
- Rolls-Royce Deutschland Ltd & Co KG
- Dimitrie Negulescu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft gas turbine engine
- Patent number 8,720,208
- Issue date May 13, 2014
- Rolls-Royce Deutschland Ltd & Co KG
- Dimitrie Negulescu
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turboprop propulsion unit with pusher propeller
- Patent number 8,438,829
- Issue date May 14, 2013
- Rolls-Royce Deutschland Ltd & Co KG
- Dimitrie Negulescu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft with tail propeller-engine layout
- Patent number 8,256,709
- Issue date Sep 4, 2012
- Rolls-Royce Deutschland Ltd & Co KG
- Dimitrie Negulescu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Vent for the lubricating oil system of a jet engine
- Patent number 8,122,698
- Issue date Feb 28, 2012
- Rolls-Royce Deutschland Ltd & Co KG
- Dimitrie Negulescu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Cooled turbine rotor wheel, in particular, a high-pressure turbine...
- Patent number 7,121,797
- Issue date Oct 17, 2006
- Rolls-Royce Deutschland Ltd & Co KG
- Dimitrie Negulescu
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Air intake system of a propeller-turbine engine
- Patent number 6,817,572
- Issue date Nov 16, 2004
- Rolls-Royce Deutschland Ltd & Co. KG
- Dimitrie Negulescu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Turboprop aircraft engine
- Patent number 6,746,207
- Issue date Jun 8, 2004
- Rolls-Royce Deutschland Ltd & Co. KG
- Christian Mundt
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Bleed valve of a compressor, in particular a compressor of a bypass...
- Patent number 6,588,195
- Issue date Jul 8, 2003
- Rolls-Royce Deutschland Ltd & Co. KG
- Dimitrie Negulescu
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Turbomachine rotor blade and disk
- Patent number 6,290,464
- Issue date Sep 18, 2001
- BMW Rolls-Royce GmbH
- Dimitrie Negulescu
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbofan aircraft engine
- Patent number 6,260,352
- Issue date Jul 17, 2001
- Rolls-Royce Deutschland Ltd & Co KG
- Dimitrie Negulescu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Aircraft gas turbine engine with a liquid-air heat exchanger
- Patent number 6,000,210
- Issue date Dec 14, 1999
- BMW Rolls-Royce GmbH
- Dimitrie Negulescu
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
ROTOR BLADE FOR A TURBOMACHINE AND METHOD FOR THE ASSEMBLY OF A ROT...
- Publication number 20180066526
- Publication date Mar 8, 2018
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Dimitrie NEGULESCU
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
COOLED TURBINE RUNNER, IN PARTICULAR FOR AN AIRCRAFT ENGINE
- Publication number 20170138200
- Publication date May 18, 2017
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Joana NEGULESCU
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBINE WITH COOLED TURBINE GUIDE VANES
- Publication number 20170022836
- Publication date Jan 26, 2017
- Rolls-Royce Deutschland Ltd & Co KG
- Dimitrie NEGULESCU
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
ADAPTIVE AIRCRAFT ENGINE AND AIRCRAFT HAVING AN ADAPTIVE ENGINE
- Publication number 20160347463
- Publication date Dec 1, 2016
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Dimitrie NEGULESCU
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE
- Publication number 20160138478
- Publication date May 19, 2016
- ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
- Dimitrie NEGULESCU
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE CENTRIPETAL ANNULAR COMBUSTION CHAMBER AND METHOD FOR F...
- Publication number 20140150442
- Publication date Jun 5, 2014
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Dimitrie NEGULESCU
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE COMBUSTION CHAMBER ARRANGEMENT OF AXIAL TYPE OF CONSTRU...
- Publication number 20130086908
- Publication date Apr 11, 2013
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Dimitrie NEGULESCU
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Aircraft gas turbine engine
- Publication number 20110209458
- Publication date Sep 1, 2011
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Dimitrie NEGULESCU
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
TURBOPROP PROPULSION UNIT WITH PUSHER PROPELLER
- Publication number 20100212285
- Publication date Aug 26, 2010
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Dimitrie NEGULESCU
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
RUNNING-GAP CONTROL SYSTEM OF AN AIRCRAFT GAS TURBINE
- Publication number 20100215481
- Publication date Aug 26, 2010
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Dimitrie NEGULESCU
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
AIRCRAFT WITH TAIL PROPELLER-ENGINE LAYOUT
- Publication number 20100155526
- Publication date Jun 24, 2010
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Dimitrie NEGULESCU
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Vent for the lubricating oil system of a jet engine
- Publication number 20090025363
- Publication date Jan 29, 2009
- Dimitrie Negulescu
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Cooled turbine rotor wheel, in particular, a high-pressure turbine...
- Publication number 20050111980
- Publication date May 26, 2005
- Dimitrie Negulescu
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Turboprop engine with co-rotating two-stage high-performance propeller
- Publication number 20040179941
- Publication date Sep 16, 2004
- Dimitrie Negulescu
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Air intake system of a propeller-turbine engine
- Publication number 20030113205
- Publication date Jun 19, 2003
- Dimitrie Negulescu
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Bleed valve of a compressor, in particular a compressor of a bypass...
- Publication number 20010042368
- Publication date Nov 22, 2001
- Dimitrie Negulescu
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...

Dimitrie NEGULESCU

Person

Patents Grantslast 30 patents

Rotor blade for a turbomachine and method for the assembly of a rot...

Adaptive aircraft engine and aircraft having an adaptive engine

Cooled turbine runner, in particular for an aircraft engine

Turbine with cooled turbine guide vanes

Gas turbine centripetal annular combustion chamber and method for f...

Gas turbine combustion chamber arrangement of axial type of constru...

Running-gap control system of an aircraft gas turbine

Aircraft gas turbine engine

Turboprop propulsion unit with pusher propeller

Aircraft with tail propeller-engine layout

Vent for the lubricating oil system of a jet engine

Cooled turbine rotor wheel, in particular, a high-pressure turbine...

Air intake system of a propeller-turbine engine

Turboprop aircraft engine

Bleed valve of a compressor, in particular a compressor of a bypass...

Turbomachine rotor blade and disk

Turbofan aircraft engine

Aircraft gas turbine engine with a liquid-air heat exchanger

Patents Applicationslast 30 patents

ROTOR BLADE FOR A TURBOMACHINE AND METHOD FOR THE ASSEMBLY OF A ROT...

COOLED TURBINE RUNNER, IN PARTICULAR FOR AN AIRCRAFT ENGINE

TURBINE WITH COOLED TURBINE GUIDE VANES

ADAPTIVE AIRCRAFT ENGINE AND AIRCRAFT HAVING AN ADAPTIVE ENGINE

GAS TURBINE ENGINE

GAS TURBINE CENTRIPETAL ANNULAR COMBUSTION CHAMBER AND METHOD FOR F...

GAS TURBINE COMBUSTION CHAMBER ARRANGEMENT OF AXIAL TYPE OF CONSTRU...

Aircraft gas turbine engine

TURBOPROP PROPULSION UNIT WITH PUSHER PROPELLER

RUNNING-GAP CONTROL SYSTEM OF AN AIRCRAFT GAS TURBINE

AIRCRAFT WITH TAIL PROPELLER-ENGINE LAYOUT

Vent for the lubricating oil system of a jet engine

Cooled turbine rotor wheel, in particular, a high-pressure turbine...

Turboprop engine with co-rotating two-stage high-performance propeller

Air intake system of a propeller-turbine engine

Bleed valve of a compressor, in particular a compressor of a bypass...