Matthew R. Feulner
28Patents
8h-index
40Co-inventors
75Inventor score
Filing activity: Sep 24, 1997 → May 26, 2023
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US6195982A | Apparatus and method of active flutter control | Mechanical Engineering; Lighting; Heating | 39 | Expired |
| US6059522A | Compressor stall diagnostics and avoidance | Mechanical Engineering; Lighting; Heating | 34 | Expired |
| US6010303A | Apparatus and method of predicting aerodynamic and aeromechanical instabilities in turbofan engines | Mechanical Engineering; Lighting; Heating | 24 | Expired |
| US6574965B1 | Rotor tip bleed in gas turbine engines | Emerging Cross-Sectional Technologies | 21 | Expired |
| US9540944B2 | Real time model based compressor control | Mechanical Engineering; Lighting; Heating | 21 | Active |
| US10040577B2 | Modified start sequence of a gas turbine engine | Mechanical Engineering; Lighting; Heating | 15 | Active |
| US10125691B2 | Bowed rotor start using a variable position starter valve | Emerging Cross-Sectional Technologies | 13 | Active |
| US10457401B2 | Dual-use air turbine system for a gas turbine engine | Emerging Cross-Sectional Technologies | 11 | Active |
| US10774788B2 | Particle extraction system for a gas turbine engine | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US9909497B2 | Combined stability and customer bleed with dirt, water and ice rejection | Emerging Cross-Sectional Technologies | 4 | Active |
| US10625881B2 | Modified start sequence of a gas turbine engine | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US9291064B2 | Anti-icing core inlet stator assembly for a gas turbine engine | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10293951B2 | Takeoff power management system and method for gas turbine engines | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US11674407B2 | Systems and methods for controlling blade tip clearances | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11473510B2 | Active multi-effector control of high pressure turbine clearances | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10060284B2 | Engine inlet total air temperature sensor | Physics | 1 | Active |
| US10167783B2 | Low pressure compressor variable vane control for two-spool turbofan or turboprop engine | Emerging Cross-Sectional Technologies | 1 | Active |
| US10495006B2 | Variable geometry gas turbine engine for use in inclement weather | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11339678B2 | Systems and methods for controlling blade tip clearances | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11754000B2 | High and low spool configuration for a gas turbine engine | Emerging Cross-Sectional Technologies | 0 | Active |
| US11719245B2 | Compressor arrangement for a gas turbine engine | Emerging Cross-Sectional Technologies | 0 | Active |
| US9982689B2 | Apparatus and method for water and ice flow management in a gas turbine engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10718272B2 | Variable-geometry boundary layer diverter | Emerging Cross-Sectional Technologies | 0 | Active |
| US10787277B2 | Modified start sequence of a gas turbine engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11391205B2 | Anti-icing core inlet stator assembly for a gas turbine engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.