Becky E. Rose
22Patents
7h-index
23Co-inventors
65Inventor score
Filing activity: Oct 31, 2006 → Jun 9, 2023
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US9932933B2 | Low pressure ratio fan engine having a dimensional relationship between inlet and fan size | Emerging Cross-Sectional Technologies | 24 | Active |
| US9920653B2 | Low pressure ratio fan engine having a dimensional relationship between inlet and fan size | Emerging Cross-Sectional Technologies | 14 | Active |
| US9121412B2 | Efficient, low pressure ratio propulsor for gas turbine engines | Emerging Cross-Sectional Technologies | 13 | Active |
| US9038366B2 | LPC flowpath shape with gas turbine engine shaft bearing configuration | Emerging Cross-Sectional Technologies | 13 | Active |
| US7963742B2 | Variable compressor stator vane having extended fillet | Mechanical Engineering; Lighting; Heating | 10 | Active |
| US10301971B2 | Low pressure ratio fan engine having a dimensional relationship between inlet and fan size | Emerging Cross-Sectional Technologies | 9 | Active |
| US8452516B1 | Variable vane scheduling based on flight conditions for inclement weather | Mechanical Engineering; Lighting; Heating | 8 | Active |
| US8438832B1 | High turning fan exit stator | Emerging Cross-Sectional Technologies | 6 | Active |
| US10526894B1 | Short inlet with low solidity fan exit guide vane arrangements | Emerging Cross-Sectional Technologies | 5 | Active |
| US9920708B2 | Nose cone assembly and method of circulating air in a gas turbine engine | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US11125168B2 | Dirt mitigation in a gas turbine engine | Emerging Cross-Sectional Technologies | 2 | Active |
| US10544802B2 | Compressor flowpath | Emerging Cross-Sectional Technologies | 2 | Active |
| US11015550B2 | Low pressure ratio fan engine having a dimensional relationship between inlet and fan size | Emerging Cross-Sectional Technologies | 1 | Active |
| US11286811B2 | Low pressure ratio fan engine having a dimensional relationship between inlet and fan size | Emerging Cross-Sectional Technologies | 1 | Active |
| US11680531B2 | Adaptive bleed schedule in a gas turbine engine | Emerging Cross-Sectional Technologies | 1 | Active |
| US11261800B2 | Adaptive bleed schedule in a gas turbine engine | Emerging Cross-Sectional Technologies | 1 | Active |
| US11725670B2 | Compressor flowpath | Emerging Cross-Sectional Technologies | 0 | Active |
| US9115649B2 | Fan stagger angle for dirt rejection | Emerging Cross-Sectional Technologies | 0 | Active |
| US11971051B2 | Compressor flowpath | Emerging Cross-Sectional Technologies | 0 | Active |
| US11428242B2 | Compressor flowpath | Emerging Cross-Sectional Technologies | 0 | Active |
| US11781505B2 | Low pressure ratio fan engine having a dimensional relationship between inlet and fan size | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11781447B2 | Low pressure ratio fan engine having a dimensional relationship between inlet and fan size | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.