Inventor · disambiguated record
Martin Hoeger
Also filed as: HOEGER MARTIN
11 granted patents·4 pending applications·234 citations·filing 1997–2018
89Inventor score
Top patents by PatentIndex Score
15 records- 0190US8573941B2Tandem blade designHOEGER MARTIN·Filed 2010·Granted Nov 5, 2013·20 cites·8 claims
- 0288US6017186ARotary turbomachine having a transonic compressor stageMTU MUENCHEN GMBH·Filed 1997·Granted Jan 25, 2000·175 cites·24 claims
- 0383US7553129B2Flow structure for a gas turbineMTU AERO ENGINES GMBH·Filed 2005·Granted Jun 30, 2009·15 cites·21 claims
- 0479US10746131B2Turbine module for a turbomachineMTU Aero Engines AG·Filed 2018·Granted Aug 18, 2020·3 cites·15 claims
- 0571US9382806B2Intermediate housing of a gas turbine having an outer bounding wall having a contour that changes in the circumferential direction upstream of a supporting rib to reduce secondary flow lossesHOEGER MARTIN·Filed 2012·Granted Jul 5, 2016·5 cites·10 claims
- 0668US7789631B2Compressor of a gas turbine and gas turbineMTU AERO ENGINES GMBH·Filed 2005·Granted Sep 7, 2010·5 cites·13 claims
- 0766US7517192B2Flow structure for a gas turbineMTU AERO ENGINES GMBH·Filed 2005·Granted Apr 14, 2009·7 cites·20 claims
- 0859US9920640B2Extruded profile for manufacturing a blade of an outlet guide vaneMTU Aero Engines AG·Filed 2015·Granted Mar 20, 2018·1 cites·23 claims
- 0948US9822706B2Gas turbine subassemblyMTU Aero Engines AG·Filed 2015·Granted Nov 21, 2017·0 cites·11 claims
- 1044US8992172B2Turbo engineHOEGER MARTIN·Filed 2009·Granted Mar 31, 2015·3 cites·9 claims
- 1144US2007177979A1Vane comprising a transition zoneMTU AERO ENGINES GMBH·Filed 2005·Application pending·0 cites
- 1243US11371370B2Flow arrangement for placing in a hot gas duct of a turbomachineMTU Aero Engines AG·Filed 2018·Granted Jun 28, 2022·0 cites·11 claims
- 1342US2014064951A1Root bow geometry for airfoil shaped vaneJUREK RENEE J·Filed 2012·Application pending·0 cites
- 1436US2013051996A1Transition channel of a turbine unitHOEGER MARTIN·Filed 2012·Application pending·0 cites
- 1529US2015300259A1Aircraft engineMTU Aero Engines AG·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →