Brooks E. Snyder
27Patents
4h-index
12Co-inventors
52Inventor score
Filing activity: Jul 1, 2014 → May 30, 2019
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US9988923B2 | Seal for gas turbine engine | Mechanical Engineering; Lighting; Heating | 20 | Active |
| US9713843B2 | Method for additively constructing internal channels | Emerging Cross-Sectional Technologies | 13 | Active |
| US9932841B2 | Workpiece manufactured from an additive manufacturing system having a particle separator and method of operation | Emerging Cross-Sectional Technologies | 7 | Active |
| US10683768B2 | Circumferential axial segmented trough seal | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US10240464B2 | Gas turbine engine airfoil with leading edge trench and impingement cooling | Emerging Cross-Sectional Technologies | 3 | Active |
| US9932835B2 | Airfoil cooling device and method of manufacture | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10012088B2 | Additive manufacturing system utilizing an epitaxy process and method of operation | Emerging Cross-Sectional Technologies | 2 | Active |
| US10487667B2 | Airfoil, and method for manufacturing the same | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10960460B2 | Additive manufactured mold, a method of manufacturing the mold, and a workpiece casted from the mold | Emerging Cross-Sectional Technologies | 1 | Active |
| US10364683B2 | Gas turbine engine component cooling passage turbulator | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10094229B2 | Cooling system of a stator assembly for a gas turbine engine having a variable cooling flow mechanism and method of operation | Emerging Cross-Sectional Technologies | 1 | Active |
| US10012090B2 | Airfoil cooling apparatus | Emerging Cross-Sectional Technologies | 1 | Active |
| US9845524B2 | Fixture for application of coatings and method of using same | Emerging Cross-Sectional Technologies | 1 | Active |
| US10066549B2 | Variable vane segment | Emerging Cross-Sectional Technologies | 1 | Active |
| US10370981B2 | Gas turbine engine component cooling circuit with respirating pedestal | Emerging Cross-Sectional Technologies | 1 | Active |
| US10465530B2 | Gas turbine engine component cooling cavity with vortex promoting features | Emerging Cross-Sectional Technologies | 0 | Active |
| US10179948B2 | Method and system for controlling coating in non-line-of-sight locations | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11591914B2 | Cupped contour for gas turbine engine blade assembly | Emerging Cross-Sectional Technologies | 0 | Active |
| US10094240B2 | Anti-deflection feature for additively manufactured thin metal parts and method of additively manufacturing thin metal parts | Emerging Cross-Sectional Technologies | 0 | Active |
| US10935240B2 | Additive manufactured combustor heat shield | Emerging Cross-Sectional Technologies | 0 | Active |
| US10436039B2 | Gas turbine engine turbine blade tip cooling | Emerging Cross-Sectional Technologies | 0 | Active |
| US10494929B2 | Cooled airfoil structure | Emerging Cross-Sectional Technologies | 0 | Active |
| US10344597B2 | Cupped contour for gas turbine engine blade assembly | Emerging Cross-Sectional Technologies | 0 | Active |
| US10434545B2 | Particle separator for an additive manufacturing system and method of operation | Emerging Cross-Sectional Technologies | 0 | Active |
| US10563583B2 | Bore-cooled film dispensing pedestals | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.