Ardeshir Riahi
34Patents
9h-index
41Co-inventors
75Inventor score
Filing activity: Jun 15, 2001 → Jul 15, 2021
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US9856739B2 | Turbine blades with tip portions having converging cooling holes | Emerging Cross-Sectional Technologies | 26 | Active |
| US6554562B2 | Combustor hot streak alignment for gas turbine engine | Emerging Cross-Sectional Technologies | 24 | Expired |
| US6792757B2 | Gas turbine combustor heat shield impingement cooling baffle | Emerging Cross-Sectional Technologies | 22 | Expired |
| US9546554B2 | Gas turbine engine components with blade tip cooling | Emerging Cross-Sectional Technologies | 14 | Active |
| US9394798B2 | Gas turbine engines with turbine airfoil cooling | Emerging Cross-Sectional Technologies | 14 | Active |
| US8292581B2 | Air cooled turbine blades and methods of manufacturing | Emerging Cross-Sectional Technologies | 11 | Active |
| US9546603B2 | Engine systems and methods for removing particles from turbine air | Emerging Cross-Sectional Technologies | 10 | Active |
| US9115586B2 | Axially-split radial turbine | Emerging Cross-Sectional Technologies | 9 | Active |
| US8206108B2 | Turbine blades and methods of manufacturing | Emerging Cross-Sectional Technologies | 9 | Active |
| US8777567B2 | Turbine blades, turbine assemblies, and methods of manufacturing turbine blades | Emerging Cross-Sectional Technologies | 9 | Active |
| US7223072B2 | Gas turbine engine including airfoils having an improved airfoil film cooling configuration and method therefor | Emerging Cross-Sectional Technologies | 7 | Expired |
| US8277169B2 | Turbine rotor cooling flow system | Emerging Cross-Sectional Technologies | 7 | Active |
| US9719362B2 | Turbine nozzles and methods of manufacturing the same | Emerging Cross-Sectional Technologies | 6 | Active |
| US10683763B2 | Turbine blade with integral flow meter | Emerging Cross-Sectional Technologies | 4 | Active |
| US9885245B2 | Turbine nozzles and cooling systems for cooling slip joints therein | Emerging Cross-Sectional Technologies | 4 | Active |
| US8297935B2 | Turbine blades and methods of forming modified turbine blades and turbine rotors | Emerging Cross-Sectional Technologies | 4 | Active |
| US10655476B2 | Gas turbine engines with airfoils having improved dust tolerance | Emerging Cross-Sectional Technologies | 4 | Active |
| US11506060B1 | Radial turbine rotor for gas turbine engine | Emerging Cross-Sectional Technologies | 3 | Active |
| US11021965B2 | Engine components with cooling holes having tailored metering and diffuser portions | Emerging Cross-Sectional Technologies | 3 | Active |
| US9506365B2 | Gas turbine engine components having sealed stress relief slots and methods for the fabrication thereof | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10641106B2 | Gas turbine engines with improved airfoil dust removal | Emerging Cross-Sectional Technologies | 2 | Active |
| US10605086B2 | Turbine engines with ceramic vanes and methods for manufacturing the same | Emerging Cross-Sectional Technologies | 2 | Active |
| US9988932B2 | Bi-cast turbine nozzles and methods for cooling slip joints therein | Emerging Cross-Sectional Technologies | 2 | Active |
| US8292587B2 | Turbine blade assemblies and methods of manufacturing the same | Emerging Cross-Sectional Technologies | 2 | Active |
| US9844826B2 | Methods for manufacturing a turbine nozzle with single crystal alloy nozzle segments | Emerging Cross-Sectional Technologies | 1 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.