Assignee
TODOROVIC PREDRAG
DE·15 granted patents·1 pending application·139 citations·filing 2008–2012
Top patents by PatentIndex Score
16 records- 0195US8776946B2Gas turbine exhaust coneTODOROVIC PREDRAG·Filed 2012·Granted Jul 15, 2014·22 cites·12 claims
- 0293US8479877B2Gas-turbine exhaust cone with three-dimensionally profiled partition wall and plate-type wall elementTODOROVIC PREDRAG·Filed 2012·Granted Jul 9, 2013·16 cites·16 claims
- 0393US8307945B2Gas-turbine exhaust coneTODOROVIC PREDRAG·Filed 2011·Granted Nov 13, 2012·17 cites·20 claims
- 0489US8938944B2Aircraft gas-turbine engine with oil cooler in the engine cowlingTODOROVIC PREDRAG·Filed 2012·Granted Jan 27, 2015·13 cites·20 claims
- 0586US8690098B2Air ejector nozzle tube for an oil heat exchanger of an aircraft engineTODOROVIC PREDRAG·Filed 2011·Granted Apr 8, 2014·12 cites·20 claims
- 0685US8220586B2Noise-reduced aircraft engine and method for reducing noise emissions of an aircraft engineTODOROVIC PREDRAG·Filed 2010·Granted Jul 17, 2012·11 cites·11 claims
- 0784US9719421B2Gas-turbine engine with telescope-type air inlet of the engine cowling (nacelle)TODOROVIC PREDRAG·Filed 2012·Granted Aug 1, 2017·10 cites·10 claims
- 0882US8408008B2Scoop of a running-gap control system of an aircraft gas turbineTODOROVIC PREDRAG·Filed 2010·Granted Apr 2, 2013·13 cites·16 claims
- 0979US9328694B2Aviation gas turbine thrust reversing deviceTODOROVIC PREDRAG·Filed 2012·Granted May 3, 2016·6 cites·10 claims
- 1076US8678319B2De-icing device of an aircraft gas-turbine engineTODOROVIC PREDRAG·Filed 2012·Granted Mar 25, 2014·5 cites·13 claims
- 1173US8833515B2Method for the production of a sound absorber, especially for a gas turbine exhaust coneTODOROVIC PREDRAG·Filed 2012·Granted Sep 16, 2014·4 cites·13 claims
- 1268US8783412B2Sound absorber for a gas turbine exhaust cone, and method for the production thereofTODOROVIC PREDRAG·Filed 2012·Granted Jul 22, 2014·3 cites·16 claims
- 1368US8480032B2Aircraft de-icing device and engine nacelle of an aircraft gas turbine with de-icing deviceTODOROVIC PREDRAG·Filed 2010·Granted Jul 9, 2013·4 cites·19 claims
- 1465US8850824B2Aircraft gas turbine with variable bypass nozzle by deforming elementTODOROVIC PREDRAG·Filed 2012·Granted Oct 7, 2014·3 cites·10 claims
- 1557US2009103975A1Attaching elementTODOROVIC PREDRAG·Filed 2008·Application pending·0 cites
- 1642US8782896B2Method for the manufacture of an ejector nozzle tubeTODOROVIC PREDRAG·Filed 2009·Granted Jul 22, 2014·0 cites·12 claims
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