Mark Cunningham
33Patents
4h-index
35Co-inventors
59Inventor score
Filing activity: Jul 9, 2013 → Mar 1, 2024
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US9879591B2 | Engine intake assembly with selector valve | Emerging Cross-Sectional Technologies | 9 | Active |
| US9797297B2 | Compound engine assembly with common inlet | Emerging Cross-Sectional Technologies | 8 | Active |
| US9896998B2 | Compound engine assembly with modulated flow | Emerging Cross-Sectional Technologies | 6 | Active |
| US10030581B2 | Air intake with scroll portion and strutted portion for gas turbine engine | Emerging Cross-Sectional Technologies | 5 | Active |
| US10245540B2 | Inertial particle separator for engine inlet | Emerging Cross-Sectional Technologies | 3 | Active |
| US10197009B2 | Gas turbine engine ejector | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10018150B2 | Integrated TEC/mixer strut axial position | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10087839B2 | Air intake for turboprop engine | Emerging Cross-Sectional Technologies | 2 | Active |
| US10765980B2 | Inertial particle separator for engine inlet | Emerging Cross-Sectional Technologies | 1 | Active |
| US10794280B2 | Air intake for gas turbine engine | Emerging Cross-Sectional Technologies | 1 | Active |
| US11535386B2 | System and method for operating a multi-engine rotorcraft for ice accretion shedding | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10865711B2 | Air inlet system for auxiliary power units | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11898452B1 | Gas turbine engine sensor system with static pressure sensors | General | 0 | Revoked |
| US11952962B1 | Exhaust duct for gas turbine engine | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10533487B2 | Engine intake assembly with selector valve | Emerging Cross-Sectional Technologies | 0 | Active |
| US11339716B2 | Inertial particle separator for aircraft engine | Emerging Cross-Sectional Technologies | 0 | Active |
| US12000358B1 | Gas turbine engine nozzle loft for thrust reverser | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12163486B2 | Exhaust mixer with protrusions | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11867070B1 | Gas turbine engine sensor system with static pressure sensors | General | 0 | Revoked |
| US10899464B2 | Moveable aircraft cowl and bypass section | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11939876B2 | Gas turbine engine sensor system with static pressure sensors | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10533489B2 | Compound engine assembly with common inlet | Emerging Cross-Sectional Technologies | 0 | Active |
| US12018615B2 | Systems and methods for controlling an air flow rate for a propulsion system air intake | Performing Operations; Transporting | 0 | Active |
| US11965460B1 | Systems and methods for controlling an air flow path for a propulsion system air intake | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11933220B1 | Systems and methods for controlling an air flow path for a propulsion system air intake | General | 0 | Revoked |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.