Bryan Olver
33Patents
10h-index
25Co-inventors
71Inventor score
Filing activity: Dec 17, 2002 → Jan 28, 2020
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7861512B2 | Turbofan bypass duct air cooled fluid cooler installation | Emerging Cross-Sectional Technologies | 72 | Active |
| US7377100B2 | Bypass duct fluid cooler | Emerging Cross-Sectional Technologies | 39 | Expired |
| US7861981B2 | Protective saddle mount for cable tie | Emerging Cross-Sectional Technologies | 34 | Active |
| US6851267B2 | Compact quick attach starter-generator installation | Mechanical Engineering; Lighting; Heating | 27 | Expired |
| US7862293B2 | Low profile bleed air cooler | Emerging Cross-Sectional Technologies | 17 | Active |
| US8171738B2 | Gas turbine internal manifold mounting arrangement | Emerging Cross-Sectional Technologies | 16 | Active |
| US7013651B2 | Compact quick attach starter-generator installation | Mechanical Engineering; Lighting; Heating | 16 | Expired |
| US6942452B2 | Grommeted bypass duct penetration | Emerging Cross-Sectional Technologies | 14 | Expired |
| US8979491B2 | Turbofan mounting arrangement | Emerging Cross-Sectional Technologies | 13 | Active |
| US8621839B2 | Gas turbine engine breather exhaust oil collector | Mechanical Engineering; Lighting; Heating | 13 | Active |
| US9784129B2 | Rear mount assembly for gas turbine engine | Mechanical Engineering; Lighting; Heating | 9 | Active |
| US8231142B2 | Fluid conduit coupling with leakage detection | Emerging Cross-Sectional Technologies | 8 | Active |
| US7854120B2 | Fuel manifold with reduced losses | Emerging Cross-Sectional Technologies | 7 | Active |
| US7703286B2 | Internal fuel manifold and fuel fairing interface | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US8222165B2 | Composite fire shield | Emerging Cross-Sectional Technologies | 5 | Active |
| US8313293B2 | Turbofan mounting system | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US9068476B2 | Hybrid metal/composite link rod for turbofan gas turbine engine | Emerging Cross-Sectional Technologies | 3 | Active |
| US8757540B2 | Nacelle inlet lip | Emerging Cross-Sectional Technologies | 3 | Active |
| US8567202B2 | Support links with lockable adjustment feature | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10364700B2 | Method for forming a composite part of a gas turbine engine | Emerging Cross-Sectional Technologies | 3 | Active |
| US9068508B2 | Gas turbine internal manifold mounting arrangement | Emerging Cross-Sectional Technologies | 3 | Active |
| US7320212B2 | Side-fed shielded internal fuel manifold inlet tube | Mechanical Engineering; Lighting; Heating | 3 | Expired |
| US10753229B2 | Mounting arrangement for mounting a fluid cooler to a gas turbine engine case | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US9909501B2 | Acoustic structure for a gas turbine engine | Emerging Cross-Sectional Technologies | 2 | Active |
| US9879606B2 | Method of supplying fuel to an internal fuel manifold | Mechanical Engineering; Lighting; Heating | 1 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.