Inventor
SINGER IRWIN D
US6 patents
Patents
6 patentsUS4151710AMay 1, 1979
Lubrication cooling system for aircraft engine accessory
UNITED TECHNOLOGIES CORP150 citations94
US5827043AOct 27, 1998
Coolable airfoil
UNITED TECHNOLOGIES CORP63 citations93
US7871245B2Jan 18, 2011
Method for forming turbine blade with angled internal ribs
UNITED TECHNOLOGIES CORP14 citations91
US7569172B2Aug 4, 2009
Method for forming turbine blade with angled internal ribs
UNITED TECHNOLOGIES CORP14 citations91
US7862325B2Jan 4, 2011
Apparatus for forming turbine blade with angled internal ribs
UNITED TECHNOLOGIES CORP7 citations83
US9476308B2Oct 25, 2016
Gas turbine engine serpentine cooling passage with chevrons
UNITED TECHNOLOGIES CORP3 citations67