Rudolf Stanka
27Patents
3h-index
47Co-inventors
63Inventor score
Filing activity: Aug 24, 1998 → May 17, 2019
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US6217282A | Vane elements adapted for assembly to form a vane ring of a gas turbine | Mechanical Engineering; Lighting; Heating | 31 | Expired |
| US10001083B2 | Turbofan aircraft engine | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US9771827B2 | Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine | Emerging Cross-Sectional Technologies | 4 | Active |
| US9416676B2 | Gas turbine | Emerging Cross-Sectional Technologies | 3 | Active |
| US8591182B2 | Device for suspending guide blades | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US9695699B2 | Securing blade assortment | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US9657581B2 | Rotor for a turbomachine | Emerging Cross-Sectional Technologies | 1 | Active |
| US10753213B2 | Wear-resistant shield for a rotating blade of a gas turbine | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US9617863B2 | Gas turbine stage | Emerging Cross-Sectional Technologies | 1 | Active |
| US10502084B2 | Module for a gas turbine | Emerging Cross-Sectional Technologies | 1 | Active |
| US10914181B2 | Blade or vane for turbomachine with different diffusion protective coatings and method for manufacture thereof | Emerging Cross-Sectional Technologies | 1 | Active |
| US8708638B2 | Apparatus and method for active gap monitoring for a continuous flow machine | Emerging Cross-Sectional Technologies | 1 | Active |
| US9982566B2 | Turbomachine, sealing segment, and guide vane segment | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US9822657B2 | Gas turbine | Emerging Cross-Sectional Technologies | 1 | Active |
| US9752455B2 | Component support and turbomachine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10151208B2 | Guide vane arrangement | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11268398B2 | Gas turbine with axially moveable outer sealing ring with respect to housing against a direction of flow in an assembled state | Emerging Cross-Sectional Technologies | 0 | Active |
| US10895162B2 | Guide vane segment for a turbomachine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11125088B2 | Stacking of rotor blades on centroids | Emerging Cross-Sectional Technologies | 0 | Active |
| US10480341B2 | Run-in coating for an outer air seal of a turbomachine | Emerging Cross-Sectional Technologies | 0 | Active |
| US10808561B2 | Seal arrangement for a turbomachine, method for manufacturing a seal arrangement and turbomachine | Emerging Cross-Sectional Technologies | 0 | Active |
| USRE48320E1 | Gas turbine | General | 0 | Active |
| US10370989B2 | Guide vane segment with radical securing elements | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10125627B2 | Method for disassembly and assembly of a rotor of a gas turbine | Emerging Cross-Sectional Technologies | 0 | Active |
| US11092012B2 | Turbomachine component arrangement | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.