Inventor
VANTASSEL BRAD WILSON
US31 patents
⚠️ This page may combine multiple inventors who share the name “VANTASSEL BRAD WILSON”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
GEN ELECTRIC
25 patentsUS10989068B2Apr 27, 2021
Turbine shroud including plurality of cooling passages
GEN ELECTRIC9 citations85
US10640849B1May 5, 2020
Nickel-based superalloy and articles
GEN ELECTRIC7 citations83
US10815807B2Oct 27, 2020
Shroud and seal for gas turbine engine
GEN ELECTRIC17 citations81
US11976565B2May 7, 2024
Nested damper pin and vibration dampening system for turbine nozzle or blade
GEN ELECTRIC5 citations74
US11162432B2Nov 2, 2021
Integrated nozzle and diaphragm with optimized internal vane thickness
GEN ELECTRIC3 citations72
US9771819B2Sep 26, 2017
Anti-corner-leakage seal in gas turbine
GEN ELECTRIC4 citations72
US10738651B2Aug 11, 2020
Shroud for gas turbine engine
GEN ELECTRIC2 citations71
US10458342B2Oct 29, 2019
System and method for controlling operation of a gas turbine based power plant
GEN ELECTRIC5 citations70
US10001013B2Jun 19, 2018
Turbine rotor blades with platform cooling arrangements
GEN ELECTRIC5 citations70
US10047613B2Aug 14, 2018
Gas turbine components having non-uniformly applied coating and methods of assembling the same
GEN ELECTRIC4 citations69
US11572803B1Feb 7, 2023
Turbine airfoil with leading edge cooling passage(s) coupled via plenum to film cooling holes, and related method
GEN ELECTRIC1 citations62
US11454133B2Sep 27, 2022
Coolant delivery via an independent cooling circuit
GEN ELECTRIC1 citations62
US11313237B2Apr 26, 2022
Conforming coating mask for a component and system background
GEN ELECTRIC0 citations62
US11434767B2Sep 6, 2022
Coolant delivery via an independent cooling circuit
GEN ELECTRIC0 citations61
US10378383B2Aug 13, 2019
Alignment apparatus for coupling diaphragms of turbines
GEN ELECTRIC1 citations59
US11480070B2Oct 25, 2022
Coolant delivery via an independent cooling circuit
GEN ELECTRIC0 citations52
US12091982B2Sep 17, 2024
Turbine component with heated structure to reduce thermal stress
GEN ELECTRIC0 citations51
US11358335B2Jun 14, 2022
Cantilevered mask for openings in additively manufactured part
GEN ELECTRIC0 citations51
US11242760B2Feb 8, 2022
Turbine rotor blade with integral impingement sleeve by additive manufacture
GEN ELECTRIC0 citations51
US11085374B2Aug 10, 2021
Impingement insert with spring element for hot gas path component
GEN ELECTRIC0 citations50
US11077527B2Aug 3, 2021
Modified components and methods for modifying components
GEN ELECTRIC0 citations49
US10989070B2Apr 27, 2021
Shroud for gas turbine engine
GEN ELECTRIC0 citations47
US10550710B2Feb 4, 2020
Shroud for gas turbine engine
GEN ELECTRIC0 citations39
US10519873B2Dec 31, 2019
Air bypass system for rotor shaft cooling
GEN ELECTRIC0 citations38
US10760451B2Sep 1, 2020
Manufacture and installation of diffuser flow mixing lobes
GEN ELECTRIC0 citations36
GE INFRASTRUCTURE TECHNOLOGY LLC
5 patentsUS12188373B1Jan 7, 2025
Cooling circuit for a platform of a stator vane assembly
GE INFRASTRUCTURE TECHNOLOGY LLC0 citations62
US12129771B1Oct 29, 2024
Stator vane assembly having mechanical retention device
GE INFRASTRUCTURE TECHNOLOGY LLC0 citations62
US11965429B1Apr 23, 2024
Turbomachine component with film-cooling hole with hood extending from wall outer surface
GE INFRASTRUCTURE TECHNOLOGY LLC1 citations62
US12497920B2Dec 16, 2025
Gas turbine aerodynamic component cyclonic particle separator with multiple particle traps
GE INFRASTRUCTURE TECHNOLOGY LLC0 citations52
US12497897B1Dec 16, 2025
Airfoil component for turbomachine component with platform cooling using airfoil coolant
GE INFRASTRUCTURE TECHNOLOGY LLC0 citations51