Stephen W. Jorgensen
25Patents
11h-index
39Co-inventors
75Inventor score
Filing activity: Nov 14, 1988 → Oct 6, 2017
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US6568187B1 | Effusion cooled transition duct | Mechanical Engineering; Lighting; Heating | 63 | Expired |
| US6644032B1 | Transition duct with enhanced profile optimization | Mechanical Engineering; Lighting; Heating | 44 | Expired |
| US6619915B1 | Thermally free aft frame for a transition duct | Emerging Cross-Sectional Technologies | 42 | Expired |
| US4887949A | Bolt retention apparatus | Emerging Cross-Sectional Technologies | 38 | Expired |
| US6662567B1 | Transition duct mounting system | Mechanical Engineering; Lighting; Heating | 36 | Expired |
| US6675584B1 | Coated seal article used in turbine engines | Mechanical Engineering; Lighting; Heating | 32 | Expired |
| US8151570B2 | Transition duct cooling feed tubes | Mechanical Engineering; Lighting; Heating | 32 | Active |
| US6834507B2 | Convoluted seal with enhanced wear capability | Mechanical Engineering; Lighting; Heating | 25 | Expired |
| US7178340B2 | Transition duct honeycomb seal | Mechanical Engineering; Lighting; Heating | 20 | Expired |
| US4878811A | Axial compressor blade assembly | Mechanical Engineering; Lighting; Heating | 20 | Expired |
| US8322146B2 | Transition duct assembly | Mechanical Engineering; Lighting; Heating | 13 | Active |
| US8684130B1 | Damping system for combustor | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US8418474B2 | Altering a natural frequency of a gas turbine transition duct | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US7677045B2 | Gas turbine transition duct | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US10132243B2 | Mounting and dismounting device for a liner of a gas turbine and a related method | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US9752781B2 | Flamesheet combustor dome | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10571128B2 | Gas turbine fuel components | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10215418B2 | Sealing device for a gas turbine combustor | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10718525B2 | Fuel injection locations based on combustor flow path | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US9851107B2 | Axially staged gas turbine combustor with interstage premixer | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10920670B2 | Sealing device arrangement at the interface between a combustor and a turbine of a gas turbine and gas turbine with such a sealing arrangement | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US9429206B2 | Sensor mounting attachment | Physics | 1 | Active |
| US9347669B2 | Variable length combustor dome extension for improved operability | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US8196412B2 | Gas turbine transition duct profile | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US9897317B2 | Thermally free liner retention mechanism | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.