Negulescu; Dimitrie

Patent Applications and Registrations

Patent applications and USPTO patent grants for Negulescu; Dimitrie.The latest application filed is for "rotor blade for a turbomachine and method for the assembly of a rotor blade for a turbomachine".

Company Profile

1.21.18

Negulescu; Dimitrie - Berlin DE

*profile and listings may contain filings by different individuals or companies with the same name. Review application materials to confirm ownership/assignment.

Patent Activity

Patent	Date
Rotor blade for a turbomachine and method for the assembly of a rotor blade for a turbomachine Grant 10,781,699 - Negulescu Sept	2020-09-22
Adaptive aircraft engine and aircraft having an adaptive engine Grant 10,450,078 - Negulescu Oc	2019-10-22
Cooled turbine runner, in particular for an aircraft engine Grant 10,436,031 - Negulescu , et al. O	2019-10-08
Turbine with cooled turbine guide vanes Grant 10,378,372 - Negulescu , et al. A	2019-08-13
Rotor Blade For A Turbomachine And Method For The Assembly Of A Rotor Blade For A Turbomachine App 20180066526 - NEGULESCU; Dimitrie	2018-03-08
Cooled Turbine Runner, In Particular For An Aircraft Engine App 20170138200 - NEGULESCU; Joana ; et al.	2017-05-18
Turbine With Cooled Turbine Guide Vanes App 20170022836 - NEGULESCU; Dimitrie ; et al.	2017-01-26
Adaptive Aircraft Engine And Aircraft Having An Adaptive Engine App 20160347463 - NEGULESCU; Dimitrie	2016-12-01
Gas Turbine Engine App 20160138478 - NEGULESCU; Dimitrie	2016-05-19
Gas turbine centripetal annular combustion chamber and method for flow guidance Grant 9,151,501 - Negulescu October 6, 2	2015-10-06
Gas turbine combustion chamber arrangement of axial type of construction Grant 9,151,223 - Negulescu October 6, 2	2015-10-06
Running-gap control system of an aircraft gas turbine Grant 8,834,108 - Negulescu , et al. September 16, 2	2014-09-16
Gas Turbine Centripetal Annular Combustion Chamber And Method For Flow Guidance App 20140150442 - Negulescu; Dimitrie	2014-06-05
Aircraft gas turbine engine Grant 8,720,208 - Negulescu May 13, 2	2014-05-13
Turboprop propulsion unit with pusher propeller Grant 8,438,829 - Negulescu May 14, 2	2013-05-14
Gas Turbine Combustion Chamber Arrangement Of Axial Type Of Construction App 20130086908 - Negulescu; Dimitrie	2013-04-11
Aircraft with tail propeller-engine layout Grant 8,256,709 - Negulescu September 4, 2	2012-09-04
Vent for the lubricating oil system of a jet engine Grant 8,122,698 - Negulescu , et al. February 28, 2	2012-02-28
Aircraft gas turbine engine App 20110209458 - NEGULESCU; Dimitrie	2011-09-01
Running-gap Control System Of An Aircraft Gas Turbine App 20100215481 - NEGULESCU; Dimitrie ; et al.	2010-08-26
Turboprop Propulsion Unit With Pusher Propeller App 20100212285 - NEGULESCU; Dimitrie	2010-08-26
Aircraft With Tail Propeller-engine Layout App 20100155526 - NEGULESCU; Dimitrie	2010-06-24
Vent for the lubricating oil system of a jet engine App 20090025363 - Negulescu; Dimitrie ; et al.	2009-01-29
Cooled turbine rotor wheel, in particular, a high-pressure turbine rotor wheel for an aircraft engine Grant 7,121,797 - Negulescu , et al. October 17, 2	2006-10-17
Cooled turbine rotor wheel, in particular, a high-pressure turbine rotor wheel for an aircraft engine App 20050111980 - Negulescu, Dimitrie ; et al.	2005-05-26
Air intake system of a propeller-turbine engine Grant 6,817,572 - Negulescu , et al. November 16, 2	2004-11-16
Turboprop engine with co-rotating two-stage high-performance propeller App 20040179941 - Negulescu, Dimitrie	2004-09-16
Turboprop aircraft engine Grant 6,746,207 - Mundt , et al. June 8, 2	2004-06-08
Bleed valve of a compressor, in particular a compressor of a bypass aero-engine Grant 6,588,195 - Negulescu July 8, 2	2003-07-08
Air intake system of a propeller-turbine engine App 20030113205 - Negulescu, Dimitrie ; et al.	2003-06-19
Bleed valve of a compressor, in particular a compressor of a bypass aero-engine App 20010042368 - Negulescu, Dimitrie	2001-11-22
Aircraft gas turbine engine with a liquid-air heat exchanger Grant 6,000,210 - Negulescu December 14, 1	1999-12-14

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