Inventor · Untersiggenthal, CH

Stefan Irmisch

11Patents
7h-index
18Co-inventors
55Inventor score

Filing activity: Nov 17, 2003 → May 24, 2012

Most-cited inventions

PatentTitleAreaCited byStatus
US8414264B2 Method for producing a gas turbine component which is to be coated, with exposed holes, device for carrying out the method, and coatable turbine blade with film cooling holes Mechanical Engineering; Lighting; Heating 34 Active
US7467922B2 Cooled turbine blade or vane for a gas turbine, and use of a turbine blade or vane of this type Mechanical Engineering; Lighting; Heating 24 Active
US7300253B2 Gas turbine blade or vane and platform element for a gas turbine blade or vane ring of a gas turbine, supporting structure for securing gas turbine blades or vanes arranged in a ring, gas turbine blade or vane ring and the use of a gas turbine blade or vane ring Mechanical Engineering; Lighting; Heating 17 Expired
US9169741B2 Turbomachine clearance control configuration using a shape memory alloy or a bimetal Mechanical Engineering; Lighting; Heating 15 Active
US9267382B2 Rotating machine Mechanical Engineering; Lighting; Heating 10 Active
US7584669B2 Method for recording microstructural changes in a component Emerging Cross-Sectional Technologies 7 Expired
US7967568B2 Gas turbine component with reduced cooling air requirement Mechanical Engineering; Lighting; Heating 7 Active
US9255488B2 Sealing arrangement for a thermal machine Mechanical Engineering; Lighting; Heating 6 Active
US8206093B2 Gas turbine with a gap blocking device Mechanical Engineering; Lighting; Heating 4 Active
US9022726B2 Thermally loaded, cooled component Emerging Cross-Sectional Technologies 3 Active
US7207108B2 Process for producing a turbine blade or vane Emerging Cross-Sectional Technologies 1 Expired

Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.