Inventor · disambiguated record
Marco Link
Also filed as: LINK MARCO
5 granted patents·6 pending applications·28 citations·filing 2010–2021
76Inventor score
Top patents by PatentIndex Score
11 records- 0185US8800292B2Heat shield element arrangement and method for installing a heat shield elementBöttcher Andreas·Filed 2010·Granted Aug 12, 2014·13 cites·18 claims
- 0269US8721270B2Passage wall section for an annular flow passage of an axial turbomachine with radial gap adjustmentGRAEFE RICHARD·Filed 2011·Granted May 13, 2014·7 cites·15 claims
- 0368US10408135B2Method for operating a gas turbine below the nominal power thereofSIEMENS AG·Filed 2014·Granted Sep 10, 2019·3 cites·13 claims
- 0465US9574449B2Internally coolable component for a gas turbine with at least one cooling ductEIFEL MARCEL·Filed 2012·Granted Feb 21, 2017·5 cites·6 claims
- 0542US2015007573A1Annular-combustion-chamber bypassSIEMENS AG·Filed 2013·Application pending·0 cites
- 0642US2023144467A1Method for operating a gas burner and gas burner for performing the methodVIESSMANN CLIMATE SOLUTIONS SE·Filed 2021·Application pending·0 cites
- 0742US2015027128A1Heat-shield element for a compressor-air bypass around the combustion chamberSIEMENS AG·Filed 2013·Application pending·0 cites
- 0840US9915166B2Gas turbine and method for operating the gas turbineSIEMENS AG·Filed 2014·Granted Mar 13, 2018·0 cites·7 claims
- 0937US2016010566A1Method for operating a gas turbine below its rated powerSIEMENS AG·Filed 2014·Application pending·0 cites
- 1035US2012230829A1Turbine or compressor bladeBENKLER FRANCOIS·Filed 2010·Application pending·0 cites
- 1132US2013101422A1Fastening assembly for blades of turbomachines having axial flow and method for producing such an assemblyBULLINGER PATRICK·Filed 2011·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →