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DE13 patents

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US8075279B2Dec 13, 2011

Coated turbine blade

AHMAD FATHI8 citations82
US9238976B2Jan 19, 2016

Guide vane system for a turbomachine having segmented guide vane carriers

AHMAD FATHI5 citations69
US8602741B2Dec 10, 2013

Turbine vane for a stationary gas turbine

AHMAD FATHI5 citations69
US8574671B2Nov 5, 2013

Method for adjusting the coolant consumption within actively cooled components, and component

AHMAD FATHI6 citations67
US8267659B2Sep 18, 2012

Turbine blade

AHMAD FATHI6 citations66
US8607455B2Dec 17, 2013

Method for the production of coated turbine moving blades and moving-blade ring for a rotor of an axial-throughflow turbine

AHMAD FATHI4 citations62
US8545169B2Oct 1, 2013

Cooled turbine blade for a gas turbine and use of such a turbine blade

AHMAD FATHI2 citations62
US8956116B2Feb 17, 2015

Cooling of a gas turbine component designed as a rotor disk or turbine blade

AHMAD FATHI2 citations60
US8109712B2Feb 7, 2012

Method of producing a turbine or compressor component, and turbine or compressor component

AHMAD FATHI2 citations60
US8951016B2Feb 10, 2015

Rotor blade for an axial flow turbomachine and mounting for such a rotor blade

AHMAD FATHI2 citations57
US9862002B2Jan 9, 2018

Process for producing a layer system

AHMAD FATHI0 citations48
US9188015B2Nov 17, 2015

Elongate component having longitudinal grains with different widths

AHMAD FATHI0 citations47
US8865255B2Oct 21, 2014

Method for assessing the coolant consumption within actively cooled components

AHMAD FATHI0 citations40