Alan Roy Stuart
47Patents
13h-index
39Co-inventors
81Inventor score
Filing activity: Feb 2, 1976 → Mar 6, 2020
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US5317877A | Intercooled turbine blade cooling air feed system | Emerging Cross-Sectional Technologies | 292 | Expired |
| US4790133A | High bypass ratio counterrotating turbofan engine | Mechanical Engineering; Lighting; Heating | 174 | Expired |
| US5927644A | Double failsafe engine mount | Emerging Cross-Sectional Technologies | 114 | Expired |
| US5190441A | Noise reduction in aircraft propellers | Emerging Cross-Sectional Technologies | 84 | Expired |
| US5921500A | Integrated failsafe engine mount | Performing Operations; Transporting | 68 | Expired |
| US4621978A | Counterrotating power turbine | Emerging Cross-Sectional Technologies | 36 | Expired |
| US5369954A | Turbofan engine bypass and exhaust system | Performing Operations; Transporting | 35 | Expired |
| US4052847A | Gas turbine engine gas flow ducts | Mechanical Engineering; Lighting; Heating | 24 | Expired |
| US8469309B2 | Monolithic structure for mounting aircraft engine | Emerging Cross-Sectional Technologies | 24 | Active |
| US4161318A | Sealing system for rotors | Mechanical Engineering; Lighting; Heating | 19 | Expired |
| US10823114B2 | Counter rotating turbine with reversing reduction gearbox | Emerging Cross-Sectional Technologies | 18 | Active |
| US8727269B2 | System and method for mounting an aircraft engine | Emerging Cross-Sectional Technologies | 17 | Active |
| US10801442B2 | Counter rotating turbine with reversing reduction gear assembly | Emerging Cross-Sectional Technologies | 17 | Active |
| US11085515B2 | Gearbox coupling in a turbomachine | Mechanical Engineering; Lighting; Heating | 8 | Active |
| US10006405B2 | Thrust reverser system with translating-rotating blocker doors and method of operation | Emerging Cross-Sectional Technologies | 8 | Active |
| US9016040B2 | Thrust reverser system with translating-rotating cascade and method of operation | Emerging Cross-Sectional Technologies | 6 | Active |
| US8713910B2 | Integrated thrust reverser/pylon assembly | Emerging Cross-Sectional Technologies | 6 | Active |
| USD286880S | Aircraft engine or similar article | General | 4 | Expired |
| US7673442B2 | Turbofan engine cowl assembly | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10465606B2 | Counter rotating turbine with reversing reduction gearbox | Emerging Cross-Sectional Technologies | 2 | Active |
| US10544734B2 | Three spool gas turbine engine with interdigitated turbine section | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10539020B2 | Two spool gas turbine engine with interdigitated turbine section | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10519860B2 | Turbine frame and bearing arrangement for three spool engine | Emerging Cross-Sectional Technologies | 2 | Active |
| US10113508B2 | Gas turbine engine and method of assembling the same | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10663036B2 | Gas turbine engine with rotating reversing compound gearbox | Emerging Cross-Sectional Technologies | 2 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.