Nathan Snape
64Patents
8h-index
33Co-inventors
74Inventor score
Filing activity: May 25, 2010 → Aug 15, 2024
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US8347637B2 | Accessory gearbox with internal layshaft | Emerging Cross-Sectional Technologies | 24 | Active |
| US8490410B2 | Axial accessory gearbox | Mechanical Engineering; Lighting; Heating | 18 | Active |
| US8490411B2 | Axial accessory gearbox | Mechanical Engineering; Lighting; Heating | 13 | Active |
| US9127566B2 | Turbomachine thermal management | Emerging Cross-Sectional Technologies | 12 | Active |
| US9194294B2 | Gas turbine engine oil tank | Mechanical Engineering; Lighting; Heating | 12 | Active |
| US9714610B2 | Low profile compressor bleed air-oil coolers | Emerging Cross-Sectional Technologies | 11 | Active |
| US10352241B2 | Gas turbine engine thermal management system | Mechanical Engineering; Lighting; Heating | 9 | Active |
| US9062566B2 | Turbomachine thermal management | Emerging Cross-Sectional Technologies | 8 | Active |
| US9109464B2 | Distributed lubrication system | Emerging Cross-Sectional Technologies | 7 | Active |
| US10669940B2 | Gas turbine engine with intercooled cooling air and turbine drive | Emerging Cross-Sectional Technologies | 7 | Active |
| US9115593B2 | Turbomachine thermal management | Emerging Cross-Sectional Technologies | 7 | Active |
| US9845735B2 | System and apparatus for diversified gearbox | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US8978351B2 | Integrated thermal management system and environmental control system for a gas turbine engine | Emerging Cross-Sectional Technologies | 6 | Active |
| US10082078B2 | Aircraft thermal management system | Emerging Cross-Sectional Technologies | 6 | Active |
| US11920526B1 | Inter-cooled preheat of steam injected turbine engine | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US9797311B2 | Integrated thermal system for a gas turbine engine | Emerging Cross-Sectional Technologies | 5 | Active |
| US11542016B2 | Cryogenic cooling system for an aircraft | Emerging Cross-Sectional Technologies | 4 | Active |
| US9080511B2 | Integrated thermal system for a gas turbine engine | Emerging Cross-Sectional Technologies | 4 | Active |
| US10006370B2 | Intercooled cooling air with heat exchanger packaging | Emerging Cross-Sectional Technologies | 3 | Active |
| US10371055B2 | Intercooled cooling air using cooling compressor as starter | Emerging Cross-Sectional Technologies | 3 | Active |
| US10378374B2 | Active clearance control for gas turbine engine | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US9920708B2 | Nose cone assembly and method of circulating air in a gas turbine engine | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10563585B2 | Heat exchanger for gas turbine engine | Emerging Cross-Sectional Technologies | 2 | Active |
| US9945252B2 | Gas turbine engine oil tank with integrated packaging configuration | Emerging Cross-Sectional Technologies | 2 | Active |
| US10823462B2 | Gas turbine engine with transcritical vapor cycle cooling | Mechanical Engineering; Lighting; Heating | 2 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.