Assignee
BROSTMEYER JOSEPH D
US·16 granted patents·3 pending applications·177 citations·filing 2010–2016
Top patents by PatentIndex Score
19 records- 0198US8789377B1Gas turbine engine with liquid metal coolingBROSTMEYER JOSEPH D·Filed 2013·Granted Jul 29, 2014·55 cites·3 claims
- 0297US9353687B1Gas turbine engine with liquid metal coolingBROSTMEYER JOSEPH D·Filed 2014·Granted May 31, 2016·30 cites·13 claims
- 0396US8209839B1Process for re-designing a distressed component used under thermal and structural loadingBROSTMEYER JOSEPH D·Filed 2010·Granted Jul 3, 2012·28 cites·5 claims
- 0495US9200983B2Apparatus and process for testing an industrial gas turbine engine and components thereofBROSTMEYER JOSEPH D·Filed 2012·Granted Dec 1, 2015·17 cites·23 claims
- 0590US9604756B1Process for testing a compressor or a combustor of a gas turbine engine using a large compressed air storage reservoirBROSTMEYER JOSEPH D·Filed 2016·Granted Mar 28, 2017·3 cites·2 claims
- 0689US8205456B1Dual heat exchanger power cycleBROSTMEYER JOSEPH D·Filed 2010·Granted Jun 26, 2012·10 cites·2 claims
- 0786US8640437B1Mini sized combined cycle power plantBROSTMEYER JOSEPH D·Filed 2011·Granted Feb 4, 2014·6 cites·5 claims
- 0885US8721265B1Multiple staged compressor with last stage airfoil coolingBROSTMEYER JOSEPH D·Filed 2013·Granted May 13, 2014·9 cites·11 claims
- 0985US8505181B1Process for re-designing a distressed component used under thermal and structural loadingBROSTMEYER JOSEPH D·Filed 2012·Granted Aug 13, 2013·7 cites·8 claims
- 1081US8277193B1Thin walled turbine blade and process for making the bladeBROSTMEYER JOSEPH D·Filed 2010·Granted Oct 2, 2012·7 cites·11 claims
- 1176US9410869B2Process for testing a compressor or a combustor of a gas turbine engine using a large compressed air storage reservoirBROSTMEYER JOSEPH D·Filed 2015·Granted Aug 9, 2016·1 cites·3 claims
- 1275US9654161B2Process for testing a compressor or a combustor of a gas turbine engine using a large compressed air storage reservoirBROSTMEYER JOSEPH D·Filed 2016·Granted May 16, 2017·1 cites·2 claims
- 1372US8250851B1Transition duct with integral guide vanesBROSTMEYER JOSEPH D·Filed 2011·Granted Aug 28, 2012·3 cites·12 claims
- 1458US9500564B2Process for testing a compressor or a combustor of a gas turbine engine using a large compressed air storage reservoirBROSTMEYER JOSEPH D·Filed 2016·Granted Nov 22, 2016·0 cites·4 claims
- 1558US2016305436A1Process for testing a compressor or a combustor of a gas turbine engine using a large compressed air storage reservoirBROSTMEYER JOSEPH D·Filed 2016·Application pending·0 cites
- 1653US9810151B2Turbine last stage rotor blade with forced driven cooling airBROSTMEYER JOSEPH D·Filed 2014·Granted Nov 7, 2017·0 cites·3 claims
- 1751US2016069264A1Gas turbine engine with turbine cooling and combustor air preheatingBROSTMEYER JOSEPH D·Filed 2014·Application pending·0 cites
- 1845US2011296870A1Apparatus and process for separating CO2 from a flue gasBROSTMEYER JOSEPH D·Filed 2010·Application pending·0 cites
- 1942US10151211B2Apparatus and process for converting an aero gas turbine engine into an industrial gas turbine engine for electric power productionBROSTMEYER JOSEPH D·Filed 2015·Granted Dec 11, 2018·0 cites·12 claims
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