Jack R. Shekleton
111Patents
22h-index
26Co-inventors
90Inventor score
Filing activity: Nov 19, 1973 → Jul 19, 1999
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US4891936A | Turbine combustor with tangential fuel injection and bender jets | Mechanical Engineering; Lighting; Heating | 48 | Expired |
| US4928479A | Annular combustor with tangential cooling air injection | Mechanical Engineering; Lighting; Heating | 40 | Expired |
| US4373325A | Combustors | Mechanical Engineering; Lighting; Heating | 39 | Expired |
| US5024058A | Hot gas generator | Mechanical Engineering; Lighting; Heating | 36 | Expired |
| US5966926A | Liquid fuel injector purge system | Mechanical Engineering; Lighting; Heating | 36 | Expired |
| US4815277A | Integrated power unit | Mechanical Engineering; Lighting; Heating | 34 | Expired |
| US4470262A | Combustors | Mechanical Engineering; Lighting; Heating | 31 | Expired |
| US5207054A | Small diameter gas turbine engine | Mechanical Engineering; Lighting; Heating | 29 | Expired |
| US4949545A | Turbine wheel and nozzle cooling | Mechanical Engineering; Lighting; Heating | 29 | Expired |
| US6065281A | Liquid fuel injector and injector system for a small gas turbine engine | Mechanical Engineering; Lighting; Heating | 29 | Expired |
| US6082112A | Liquid fuel injector | Mechanical Engineering; Lighting; Heating | 28 | Expired |
| US4008039A | Low emission burners and control systems therefor | Emerging Cross-Sectional Technologies | 28 | Expired |
| USRE34962E | Annular combustor with tangential cooling air injection | General | 28 | Expired |
| US5214911A | Method and apparatus for high altitude starting of gas turbine engine | Mechanical Engineering; Lighting; Heating | 27 | Expired |
| US6178751A | Liquid fuel injector system | Mechanical Engineering; Lighting; Heating | 27 | Expired |
| US4989404A | Turbine engine with high efficiency fuel atomization | Mechanical Engineering; Lighting; Heating | 25 | Expired |
| US5095694A | Fuel purging system for a turbine engine | Mechanical Engineering; Lighting; Heating | 24 | Expired |
| US5263316A | Turbine engine with airblast injection | Mechanical Engineering; Lighting; Heating | 23 | Expired |
| US5277022A | Air blast fuel injecton system | Mechanical Engineering; Lighting; Heating | 23 | Expired |
| US4819423A | Integrated power unit | Mechanical Engineering; Lighting; Heating | 23 | Expired |
| US4862693A | Fuel injector for a turbine engine | Mechanical Engineering; Lighting; Heating | 22 | Expired |
| US5317864A | Tangentially directed air assisted fuel injection and small annular combustors for turbines | Emerging Cross-Sectional Technologies | 22 | Expired |
| US5261224A | High altitude starting two-stage fuel injection apparatus | Mechanical Engineering; Lighting; Heating | 21 | Expired |
| US4794754A | Low cost annular combustor | Emerging Cross-Sectional Technologies | 21 | Expired |
| US4974415A | Staged, coaxial multiple point fuel injection in a hot gas generator | Mechanical Engineering; Lighting; Heating | 21 | Expired |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.