Inventor
KESTNER BRIAN K
US5 patents
Patents
5 patentsUS11073090B2Jul 27, 2021
Valved airflow passage assembly for adjusting airflow distortion in gas turbine engine
GEN ELECTRIC11 citations84
US10794281B2Oct 6, 2020
Gas turbine engine having instrumented airflow path components
GEN ELECTRIC14 citations84
US9777633B1Oct 3, 2017
Secondary airflow passage for adjusting airflow distortion in gas turbine engine
GEN ELECTRIC8 citations82
US11448127B2Sep 20, 2022
Translating inlet for adjusting airflow distortion in gas turbine engine
GEN ELECTRIC3 citations71
US10753278B2Aug 25, 2020
Translating inlet for adjusting airflow distortion in gas turbine engine
GEN ELECTRIC3 citations71