Assignee
AHMAD FATHI
DE·13 granted patents·20 pending applications·42 citations·filing 2004–2013
Top patents by PatentIndex Score
33 records- 0172US8574671B2Method for adjusting the coolant consumption within actively cooled components, and componentAHMAD FATHI·Filed 2012·Granted Nov 5, 2013·6 cites·7 claims
- 0269US9238976B2Guide vane system for a turbomachine having segmented guide vane carriersAHMAD FATHI·Filed 2010·Granted Jan 19, 2016·5 cites·9 claims
- 0361US8075279B2Coated turbine bladeAHMAD FATHI·Filed 2007·Granted Dec 13, 2011·8 cites·14 claims
- 0460US8956116B2Cooling of a gas turbine component designed as a rotor disk or turbine bladeAHMAD FATHI·Filed 2010·Granted Feb 17, 2015·2 cites·11 claims
- 0558US8951016B2Rotor blade for an axial flow turbomachine and mounting for such a rotor bladeAHMAD FATHI·Filed 2010·Granted Feb 10, 2015·2 cites·10 claims
- 0654US8267659B2Turbine bladeAHMAD FATHI·Filed 2008·Granted Sep 18, 2012·6 cites·9 claims
- 0753US8607455B2Method for the production of coated turbine moving blades and moving-blade ring for a rotor of an axial-throughflow turbineAHMAD FATHI·Filed 2008·Granted Dec 17, 2013·4 cites·14 claims
- 0851US8602741B2Turbine vane for a stationary gas turbineAHMAD FATHI·Filed 2009·Granted Dec 10, 2013·5 cites·13 claims
- 0950US8865255B2Method for assessing the coolant consumption within actively cooled componentsAHMAD FATHI·Filed 2011·Granted Oct 21, 2014·0 cites·3 claims
- 1048US2014248157A1Blade or vane of differing roughness and production processAHMAD FATHI·Filed 2013·Application pending·0 cites
- 1147US8545169B2Cooled turbine blade for a gas turbine and use of such a turbine bladeAHMAD FATHI·Filed 2006·Granted Oct 1, 2013·2 cites·11 claims
- 1247US8109712B2Method of producing a turbine or compressor component, and turbine or compressor componentAHMAD FATHI·Filed 2007·Granted Feb 7, 2012·2 cites·18 claims
- 1345US9862002B2Process for producing a layer systemAHMAD FATHI·Filed 2012·Granted Jan 9, 2018·0 cites·15 claims
- 1445US2012285652A1Liner for a Die BodyAHMAD FATHI·Filed 2011·Application pending·0 cites
- 1545US2012103554A1Process for optimizing a core dieAHMAD FATHI·Filed 2011·Application pending·0 cites
- 1644US2013330203A1Method for producing a protective layer for a rotor bladeAHMAD FATHI·Filed 2011·Application pending·0 cites
- 1744US2014099209A1Gas turbine component, method for its production and casting mold for use of this methodAHMAD FATHI·Filed 2013·Application pending·0 cites
- 1843US2013233451A1Shot peening in combination with an heat treatment and a componentAHMAD FATHI·Filed 2011·Application pending·0 cites
- 1943US2012118524A1Core die with variable pins and process for producing a coreAHMAD FATHI·Filed 2011·Application pending·0 cites
- 2042US2012273153A1Casting mold having a stabilized inner casting core, casting method and casting partAHMAD FATHI·Filed 2010·Application pending·0 cites
- 2142US2012031579A1Method for producing a negative mold for casting a turbine blade and mold for producing a wax model of a gas turbineAHMAD FATHI·Filed 2010·Application pending·0 cites
- 2242US2009074572A1Cooled gas turbine guide blade for a gas turbine, use of a gas turbine guide blade and method for operating a gas turbineAHMAD FATHI·Filed 2008·Application pending·0 cites
- 2341US2011255956A1Gas turbine having cooling insertAHMAD FATHI·Filed 2009·Application pending·0 cites
- 2441US2013156599A1Turbine blade for a gas turbineAHMAD FATHI·Filed 2011·Application pending·0 cites
- 2540US2012100008A1Annular flow channel section for a turbomachineAHMAD FATHI·Filed 2010·Application pending·0 cites
- 2640US2011176930A1Turbine vane for a gas turbine and casting core for the production of suchAHMAD FATHI·Filed 2009·Application pending·0 cites
- 2739US9188015B2Elongate component having longitudinal grains with different widthsAHMAD FATHI·Filed 2009·Granted Nov 17, 2015·0 cites·20 claims
- 2839US2012039718A1Casting apparatus for producing a turbine rotor blade of a gas turbine and turbine rotor bladeAHMAD FATHI·Filed 2010·Application pending·0 cites
- 2939US2010068069A1Turbine BladeAHMAD FATHI·Filed 2007·Application pending·0 cites
- 3039US2008000063A1Component with a Filled RecessAHMAD FATHI·Filed 2005·Application pending·0 cites
- 3139US2009252612A1Blade and gas turbineAHMAD FATHI·Filed 2004·Application pending·0 cites
- 3237US2014255652A1Surface having specially formed recesses and componentAHMAD FATHI·Filed 2012·Application pending·0 cites
- 3337US2012070310A1Axial turbomachine rotor having blade coolingAHMAD FATHI·Filed 2010·Application pending·0 cites
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