Ibrahim Sezer
17Patents
4h-index
33Co-inventors
56Inventor score
Filing activity: Jun 8, 2012 → Apr 23, 2024
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US9963985B2 | Turbomachine and turbine nozzle therefor | Mechanical Engineering; Lighting; Heating | 16 | Active |
| US9816388B1 | Seal in a gas turbine engine having a shim base and a honeycomb structure with a number of cavities formed therein | Emerging Cross-Sectional Technologies | 5 | Active |
| US10472980B2 | Gas turbine seals | Emerging Cross-Sectional Technologies | 4 | Active |
| US9127557B2 | Nozzle mounting and sealing assembly for a gas turbine system and method of mounting and sealing | Emerging Cross-Sectional Technologies | 4 | Active |
| US10989068B2 | Turbine shroud including plurality of cooling passages | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US9464536B2 | Sealing arrangement for a turbine system and method of sealing between two turbine components | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US9995151B2 | Article and manifold for thermal adjustment of a turbine component | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US9464538B2 | Shroud block segment for a gas turbine | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10975724B2 | System and method for shroud cooling in a gas turbine engine | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11047248B2 | Curved seal for adjacent gas turbine components | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10837315B2 | Turbine shroud including cooling passages in communication with collection plenums | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11572803B1 | Turbine airfoil with leading edge cooling passage(s) coupled via plenum to film cooling holes, and related method | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10519861B2 | Transition manifolds for cooling channel connections in cooled structures | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11773739B2 | Curved seal for adjacent gas turbine components | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11231175B2 | Integrated combustor nozzles with continuously curved liner segments | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11525397B2 | Gas turbine component with ejection circuit for removing debris from cooling air supply | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12410730B1 | Turbine shroud and turbomachine with cooling circuit | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.