Timothy A. Fox
27Patents
8h-index
35Co-inventors
71Inventor score
Filing activity: Sep 19, 2008 → Jun 28, 2018
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US8752386B2 | Air/fuel supply system for use in a gas turbine engine | Mechanical Engineering; Lighting; Heating | 42 | Active |
| US8375726B2 | Combustor assembly in a gas turbine engine | Mechanical Engineering; Lighting; Heating | 40 | Active |
| US8272218B2 | Spiral cooled fuel nozzle | Mechanical Engineering; Lighting; Heating | 30 | Active |
| US8511087B2 | Fuel injector and swirler assembly with lobed mixer | Mechanical Engineering; Lighting; Heating | 30 | Active |
| US9016066B2 | Combustor assembly in a gas turbine engine | Mechanical Engineering; Lighting; Heating | 28 | Active |
| US8661779B2 | Flex-fuel injector for gas turbines | Mechanical Engineering; Lighting; Heating | 16 | Active |
| US10704786B2 | Fuel injector including a lobed mixer and vanes for injecting alternate fuels in a gas turbine | Mechanical Engineering; Lighting; Heating | 8 | Active |
| US8769955B2 | Self-regulating fuel staging port for turbine combustor | Mechanical Engineering; Lighting; Heating | 8 | Active |
| US8991192B2 | Fuel nozzle assembly for use as structural support for a duct structure in a combustor of a gas turbine engine | Mechanical Engineering; Lighting; Heating | 7 | Active |
| US9395082B2 | Combustor resonator section with an internal thermal barrier coating and method of fabricating the same | Emerging Cross-Sectional Technologies | 4 | Active |
| US8549859B2 | Combustor apparatus in a gas turbine engine | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US9163841B2 | Cast manifold for dry low NOx gas turbine engine | Emerging Cross-Sectional Technologies | 3 | Active |
| US10139111B2 | Dual outlet nozzle for a secondary fuel stage of a combustor of a gas turbine engine | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10443855B2 | Flexible fuel combustion system for turbine engines | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US9562692B2 | Nozzle with multi-tube fuel passageway for gas turbine engines | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US8955328B2 | Burner arrangement | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US9488105B2 | Gas turbine assembly and method therefor | Emerging Cross-Sectional Technologies | 0 | Active |
| US9157370B2 | Burner assembly | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US9746185B2 | Circumferential biasing and profiling of fuel injection in distribution ring | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US9151171B2 | Stepped inlet ring for a transition downstream from combustor basket in a combustion turbine engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10095218B2 | Method and computer-readable model for additively manufacturing ducting arrangement with injector assemblies forming a shielding flow of air | Physics | 0 | Active |
| US10359194B2 | Film cooling hole arrangement for acoustic resonators in gas turbine engines | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US9291102B2 | Interface ring for gas turbine fuel nozzle assemblies | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10309655B2 | Cooling system for fuel nozzles within combustor in a turbine engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11092338B2 | Method for constructing impingement/effusion cooling features in a component of a combustion turbine engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.