Inventor · disambiguated record
Mark Broomer
Also filed as: BROOMER MARK
13 granted patents·2 pending applications·66 citations·filing 2007–2019
88Inventor score
Top patents by PatentIndex Score
15 records- 0187US8292573B2Flange cooled turbine nozzleBROOMER MARK·Filed 2009·Granted Oct 23, 2012·32 cites·20 claims
- 0282US9670791B2Flexible finger seal for sealing a gap between turbine engine componentsUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 6, 2017·8 cites·20 claims
- 0381US10392950B2Turbine band anti-chording flangesGEN ELECTRIC·Filed 2015·Granted Aug 27, 2019·3 cites·12 claims
- 0480US10145308B2Gas turbine engine ring sealUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 4, 2018·3 cites·16 claims
- 0568US8281604B2Divergent turbine nozzleBROOMER MARK·Filed 2007·Granted Oct 9, 2012·8 cites·23 claims
- 0659US8296945B2Method for repairing a turbine nozzle segmentBROOMER MARK·Filed 2007·Granted Oct 30, 2012·7 cites·14 claims
- 0758US10280778B2Assembly for sealing a gap between components of a turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted May 7, 2019·1 cites·10 claims
- 0852US12442309B2Nozzle assembly for turbine engineGEN ELECTRIC·Filed 2019·Granted Oct 14, 2025·0 cites·18 claims
- 0952US8235652B2Turbine nozzle segmentBROOMER MARK·Filed 2007·Granted Aug 7, 2012·4 cites·14 claims
- 1048US10451204B2Low leakage duct segment using expansion joint assemblyUNITED TECHNOLOGIES CORP·Filed 2014·Granted Oct 22, 2019·0 cites·20 claims
- 1148US9879558B2Low leakage multi-directional interface for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jan 30, 2018·0 cites·20 claims
- 1247US10731493B2Gas turbine engine sealUNITED TECHNOLOGIES CORP·Filed 2014·Granted Aug 4, 2020·0 cites·18 claims
- 1345US11473437B2Turbine snap in spring sealGEN ELECTRIC·Filed 2019·Granted Oct 18, 2022·0 cites·20 claims
- 1441US2019024513A1Shield for a turbine engine airfoilGEN ELECTRIC·Filed 2017·Application pending·0 cites
- 1536US2017089211A1Turbine snap in spring sealGEN ELECTRIC·Filed 2015·Application pending·0 cites
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