Markus Schlemmer
25Patents
3h-index
45Co-inventors
59Inventor score
Filing activity: Jun 21, 2010 → May 13, 2022
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US9322281B2 | Shroud segment to be arranged on a blade | Mechanical Engineering; Lighting; Heating | 9 | Active |
| US9500088B2 | Blade rim segment for a turbomachine and method for manufacture | Emerging Cross-Sectional Technologies | 5 | Active |
| US9982559B2 | Blade or vane for a turbomachine and axial turbomachine | Emerging Cross-Sectional Technologies | 4 | Active |
| US10570752B2 | Impulse element module for a turbomachine | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10689983B2 | Pulse body module with bearing protection | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10436044B2 | Guide vane segment for a turbomachine | Emerging Cross-Sectional Technologies | 3 | Active |
| US10428668B2 | Vane segment with peripheral securing | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10458248B2 | Blade channel, blade cascade and turbomachine | Emerging Cross-Sectional Technologies | 2 | Active |
| US10526901B2 | Turbomachine blade assembly | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US11002140B2 | Guide vane segment | Emerging Cross-Sectional Technologies | 1 | Active |
| US10370989B2 | Guide vane segment with radical securing elements | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11898618B2 | Arrangement for reducing oscillation | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US9777588B2 | Brush seal system for sealing a gap between components of a thermal gas turbine that may be moved relative to one another | Emerging Cross-Sectional Technologies | 0 | Active |
| US11499437B2 | Sealing apparatus for a turbomachine, seal-carrier ring element for a sealing apparatus, and turbomachine | Emerging Cross-Sectional Technologies | 0 | Active |
| US11867080B2 | Integrally bladed turbomachine rotor | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US9482099B2 | Rotor blade for a turbomachine and turbomachine | Emerging Cross-Sectional Technologies | 0 | Active |
| US10550720B2 | Guide vane segment | Emerging Cross-Sectional Technologies | 0 | Active |
| US10024192B2 | Ceramic component for a turbomachine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10808561B2 | Seal arrangement for a turbomachine, method for manufacturing a seal arrangement and turbomachine | Emerging Cross-Sectional Technologies | 0 | Active |
| US10865651B2 | Sealing assembly for a fluid kinetic machine, method for producing a sealing assembly as well as fluid kinetic machine | Emerging Cross-Sectional Technologies | 0 | Active |
| US10655483B2 | Run-up surface for the guide-vane shroud plate and the rotor-blade base plate | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10544696B2 | Stabilized sealing ring for a turbomachine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US9359903B2 | Gas turbine and guide blade for a housing of a gas turbine | Emerging Cross-Sectional Technologies | 0 | Active |
| US10895162B2 | Guide vane segment for a turbomachine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10415425B2 | Turbomachine stage | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.