Stephen K. Kramer
54Patents
8h-index
74Co-inventors
81Inventor score
Filing activity: Dec 20, 1996 → Jun 10, 2024
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US6627019B2 | Process for making ceramic matrix composite parts with cooling channels | Emerging Cross-Sectional Technologies | 48 | Expired |
| US7954325B2 | Gas turbine combustor | Emerging Cross-Sectional Technologies | 37 | Active |
| US9863322B2 | Selectively deoxygenated stored fuel system | Emerging Cross-Sectional Technologies | 37 | Active |
| US7100360B2 | Pulsed combustion engine | Mechanical Engineering; Lighting; Heating | 18 | Expired |
| US7665307B2 | Dual wall combustor liner | Mechanical Engineering; Lighting; Heating | 15 | Active |
| US5899076A | Flame disgorging two stream tangential entry nozzle | Mechanical Engineering; Lighting; Heating | 14 | Expired |
| US10316686B2 | High response turbine tip clearance control system | Emerging Cross-Sectional Technologies | 12 | Active |
| US5761897A | Method of combustion with a two stream tangential entry nozzle | Mechanical Engineering; Lighting; Heating | 9 | Expired |
| US5896739A | Method of disgorging flames from a two stream tangential entry nozzle | Mechanical Engineering; Lighting; Heating | 8 | Expired |
| US5791562A | Conical centerbody for a two stream tangential entry nozzle | Mechanical Engineering; Lighting; Heating | 8 | Expired |
| US10801730B2 | Combustor panel mounting systems and methods | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US5908160A | Centerbody for a two stream tangential entry nozzle | Mechanical Engineering; Lighting; Heating | 5 | Expired |
| US8800290B2 | Combustor | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US11215367B2 | Mounting a ceramic component to a non-ceramic component in a gas turbine engine | Emerging Cross-Sectional Technologies | 5 | Active |
| US8028528B2 | Annular gas turbine combustor | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US5735466A | Two stream tangential entry nozzle | Mechanical Engineering; Lighting; Heating | 4 | Expired |
| US10690346B2 | Washer for combustor assembly | Emerging Cross-Sectional Technologies | 3 | Active |
| US11112114B2 | Combustor panels for gas turbine engines | Emerging Cross-Sectional Technologies | 3 | Active |
| US10168052B2 | Combustor bulkhead heat shield | Emerging Cross-Sectional Technologies | 3 | Active |
| US10941937B2 | Combustor liner with gasket for gas turbine engine | Emerging Cross-Sectional Technologies | 2 | Active |
| US12038177B1 | Fuel injector assembly for gas turbine engine with fuel, air and steam injection | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10670275B2 | Cooling configurations for combustor attachment features | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US11181005B2 | Gas turbine engine assembly with mid-vane outer platform gap | Emerging Cross-Sectional Technologies | 2 | Active |
| US10935431B2 | Sensor arrangement for measuring gas turbine combustor temperatures | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US9494109B2 | Pivoting ball stop for exhaust duct liner hanger | Emerging Cross-Sectional Technologies | 1 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.