Assignee
NEGULESCU DIMITRIE
DE·7 granted patents·56 citations·filing 2008–2012
Top patents by PatentIndex Score
7 records- 0185US9151501B2Gas turbine centripetal annular combustion chamber and method for flow guidanceNEGULESCU DIMITRIE·Filed 2012·Granted Oct 6, 2015·9 cites·12 claims
- 0285US8438829B2Turboprop propulsion unit with pusher propellerNEGULESCU DIMITRIE·Filed 2010·Granted May 14, 2013·12 cites·20 claims
- 0382US8256709B2Aircraft with tail propeller-engine layoutNEGULESCU DIMITRIE·Filed 2009·Granted Sep 4, 2012·17 cites·13 claims
- 0479US8834108B2Running-gap control system of an aircraft gas turbineNEGULESCU DIMITRIE·Filed 2010·Granted Sep 16, 2014·8 cites·8 claims
- 0574US8720208B2Aircraft gas turbine engineNEGULESCU DIMITRIE·Filed 2011·Granted May 13, 2014·5 cites·7 claims
- 0668US9151223B2Gas turbine combustion chamber arrangement of axial type of constructionNEGULESCU DIMITRIE·Filed 2011·Granted Oct 6, 2015·3 cites·20 claims
- 0742US8122698B2Vent for the lubricating oil system of a jet engineNEGULESCU DIMITRIE·Filed 2008·Granted Feb 28, 2012·2 cites·19 claims
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