Inventor · disambiguated record
Dimitrie Negulescu
Also filed as: NEGULESCU DIMITRIE
18 granted patents·2 pending applications·289 citations·filing 1996–2017
94Inventor score
Files withNEGULESCU DIMITRIE7ROLLS ROYCE DEUTSCHLAND6ROLLS ROYCE DEUTSCHLAND LTD & CO KG4BMW ROLLS ROYCE GMBH2
Top patents by PatentIndex Score
20 records- 0186US6000210AAircraft gas turbine engine with a liquid-air heat exchangerBMW ROLLS ROYCE GMBH·Filed 1996·Granted Dec 14, 1999·80 cites·13 claims
- 0285US9151501B2Gas turbine centripetal annular combustion chamber and method for flow guidanceNEGULESCU DIMITRIE·Filed 2012·Granted Oct 6, 2015·9 cites·12 claims
- 0385US8438829B2Turboprop propulsion unit with pusher propellerNEGULESCU DIMITRIE·Filed 2010·Granted May 14, 2013·12 cites·20 claims
- 0485US6588195B2Bleed valve of a compressor, in particular a compressor of a bypass aero-engineROLLS ROYCE DEUTSCHLAND·Filed 2000·Granted Jul 8, 2003·40 cites·18 claims
- 0582US8256709B2Aircraft with tail propeller-engine layoutNEGULESCU DIMITRIE·Filed 2009·Granted Sep 4, 2012·17 cites·13 claims
- 0679US8834108B2Running-gap control system of an aircraft gas turbineNEGULESCU DIMITRIE·Filed 2010·Granted Sep 16, 2014·8 cites·8 claims
- 0778US10378372B2Turbine with cooled turbine guide vanesROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2016·Granted Aug 13, 2019·3 cites·14 claims
- 0874US8720208B2Aircraft gas turbine engineNEGULESCU DIMITRIE·Filed 2011·Granted May 13, 2014·5 cites·7 claims
- 0968US9151223B2Gas turbine combustion chamber arrangement of axial type of constructionNEGULESCU DIMITRIE·Filed 2011·Granted Oct 6, 2015·3 cites·20 claims
- 1067US10450078B2Adaptive aircraft engine and aircraft having an adaptive engineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2016·Granted Oct 22, 2019·1 cites·17 claims
- 1167US6290464B1Turbomachine rotor blade and diskBMW ROLLS ROYCE GMBH·Filed 1999·Granted Sep 18, 2001·49 cites·8 claims
- 1265US10781699B2Rotor blade for a turbomachine and method for the assembly of a rotor blade for a turbomachineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2017·Granted Sep 22, 2020·1 cites·17 claims
- 1360US6817572B2Air intake system of a propeller-turbine engineROLLS ROYCE DEUTSCHLAND·Filed 2002·Granted Nov 16, 2004·16 cites·20 claims
- 1455US6260352B1Turbofan aircraft engineROLLS ROYCE DEUTSCHLAND·Filed 1998·Granted Jul 17, 2001·25 cites·8 claims
- 1550US7121797B2Cooled turbine rotor wheel, in particular, a high-pressure turbine rotor wheel for an aircraft engineROLLS ROYCE DEUTSCHLAND·Filed 2004·Granted Oct 17, 2006·13 cites·13 claims
- 1642US8122698B2Vent for the lubricating oil system of a jet engineNEGULESCU DIMITRIE·Filed 2008·Granted Feb 28, 2012·2 cites·19 claims
- 1741US6746207B1Turboprop aircraft engineROLLS ROYCE DEUTSCHLAND·Filed 2003·Granted Jun 8, 2004·5 cites·12 claims
- 1839US2016138478A1Gas turbine engineROLLS ROYCE DEUTSCHLAND·Filed 2015·Application pending·0 cites
- 1938US2004179941A1Turboprop engine with co-rotating two-stage high-performance propellerFiled 2004·Application pending·0 cites
- 2037US10436031B2Cooled turbine runner, in particular for an aircraft engineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2016·Granted Oct 8, 2019·0 cites·8 claims
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