Jonathan M. Rivers
39Patents
4h-index
32Co-inventors
59Inventor score
Filing activity: Jun 15, 2010 → Jun 28, 2024
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US9932840B2 | Rotor for a gas turbine engine | Emerging Cross-Sectional Technologies | 7 | Active |
| US9481448B2 | Aerodynamic fairings secondarily attached to nosecone | Emerging Cross-Sectional Technologies | 6 | Active |
| US10612564B2 | Acoustic panel of turbine engine and method of arranging the acoustic panel | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US10024191B2 | Fan track liner designed to yield next to fan case hook | Emerging Cross-Sectional Technologies | 4 | Active |
| US10260522B2 | Liner system | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US9470097B2 | Airfoil with leading edge reinforcement | Emerging Cross-Sectional Technologies | 3 | Active |
| US11321296B1 | Dynamically selecting among learned and non-learned indexes for data access | Physics | 3 | Active |
| US9739158B2 | Attachment feature of a gas turbine engine blade having a curved profile | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US9896948B2 | Gas turbine engine blade and disk | Emerging Cross-Sectional Technologies | 2 | Active |
| US11635026B1 | Fan case assembly for a gas turbine engine | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10473030B2 | Acoustic panel of turbine engine | Emerging Cross-Sectional Technologies | 1 | Active |
| US12286936B1 | Adjustable fan track liner with groove array active fan tip treatment for distortion tolerance | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10605257B2 | Thrust-ring and rotor fan system | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12209502B1 | Active fan tip treatment using rotating drum array with axial channels in fan track liner for distortion tolerance | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12253994B2 | Dynamically selecting among learned and non-learned indexes for data access | Physics | 0 | Active |
| US12085021B1 | Adjustable air flow plenum with movable closure for a fan of a gas turbine engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12286930B1 | Turbine engine fan case with bleed air for tip injection and heat exchanger cooling | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12258870B1 | Adjustable fan track liner with slotted array active fan tip treatment for distortion tolerance | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10344675B2 | Fastener and method of restricting fluid flow using same | Emerging Cross-Sectional Technologies | 0 | Active |
| US11965528B1 | Adjustable air flow plenum with circumferential movable closure for a fan of a gas turbine engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12215712B1 | Adjustable fan track liner with dual grooved array active fan tip treatment for distortion tolerance | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11726974B2 | Dynamically selecting among learned and non-learned indexes for data access | Physics | 0 | Active |
| US12331660B1 | Vane assemblies with overlapping band couplings in gas turbine engines | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11797514B2 | System and methods for data model detection and surveillance | Physics | 0 | Active |
| US12209541B1 | Adjustable fan track liner with dual slotted array active fan tip treatment for distortion tolerance | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.