Inventor
LANA KYLE C
US15 patents
Patents
15 patentsUS10677066B2Jun 9, 2020
Turbine blade with airfoil tip vortex control
UNITED TECHNOLOGIES CORP8 citations83
US9810075B2Nov 7, 2017
Faceted turbine blade damper-seal
UNITED TECHNOLOGIES CORP7 citations82
US10753210B2Aug 25, 2020
Airfoil having improved cooling scheme
UNITED TECHNOLOGIES CORP2 citations72
US10648353B2May 12, 2020
Low loss airfoil platform rim seal assembly
UNITED TECHNOLOGIES CORP5 citations72
US10557354B2Feb 11, 2020
Gas turbine engine airfoil crossover and pedestal rib cooling arrangement
UNITED TECHNOLOGIES CORP3 citations72
US10907482B2Feb 2, 2021
Turbine blade damper seal
UNITED TECHNOLOGIES CORP2 citations71
US10815788B2Oct 27, 2020
Turbine blade with slot film cooling
UNITED TECHNOLOGIES CORP1 citations62
US11286809B2Mar 29, 2022
Airfoil platform cooling channels
UNITED TECHNOLOGIES CORP0 citations51
US11021976B2Jun 1, 2021
Hardware geometry for increasing part overlap and maintaining clearance
UNITED TECHNOLOGIES CORP0 citations51
US10941663B2Mar 9, 2021
Airfoil having improved leading edge cooling scheme and damage resistance
UNITED TECHNOLOGIES CORP0 citations51
US10907479B2Feb 2, 2021
Airfoil having improved leading edge cooling scheme and damage resistance
UNITED TECHNOLOGIES CORP0 citations51
US10253635B2Apr 9, 2019
Blade tip cooling arrangement
UNITED TECHNOLOGIES CORP0 citations51
US9995147B2Jun 12, 2018
Blade tip cooling arrangement
UNITED TECHNOLOGIES CORP1 citations51
US10513931B2Dec 24, 2019
Cooling systems and internally-cooled engine parts having an impingement cavity with an undulating internal surface
UNITED TECHNOLOGIES CORP0 citations41
US10801331B2Oct 13, 2020
Gas turbine engine rotor including squealer tip pocket
UNITED TECHNOLOGIES CORP0 citations40