Inventor
DIPIETRO JR ANTHONY LOUIS
US7 patents
Patents
7 patentsUS10883515B2Jan 5, 2021
Method and system for leading edge auxiliary vanes
GEN ELECTRIC9 citations82
US9874221B2Jan 23, 2018
Axial compressor rotor incorporating splitter blades
GEN ELECTRIC14 citations81
US11149552B2Oct 19, 2021
Shroud for splitter and rotor airfoils of a fan for a gas turbine engine
GEN ELECTRIC8 citations80
US10385871B2Aug 20, 2019
Method and system for compressor vane leading edge auxiliary vanes
GEN ELECTRIC10 citations79
US9938984B2Apr 10, 2018
Axial compressor rotor incorporating non-axisymmetric hub flowpath and splittered blades
GEN ELECTRIC6 citations70
US11002141B2May 11, 2021
Method and system for leading edge auxiliary turbine vanes
GEN ELECTRIC1 citations55
US12540551B1Feb 3, 2026
Gas turbine engines including splittered airfoils
GEN ELECTRIC0 citations43