Inventor
KANE DANIEL E
US16 patents
⚠️ This page may combine multiple inventors who share the name “KANE DANIEL E”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
15 patentsUS6487491B1Nov 26, 2002
System and method of controlling clearance between turbine engine blades and case based on engine components thermal growth model
UNITED TECHNOLOGIES CORP124 citations97
US5486090AJan 23, 1996
Turbine shroud segment with serpentine cooling channels
UNITED TECHNOLOGIES CORP114 citations97
US6241467B1Jun 5, 2001
Stator vane for a rotary machine
UNITED TECHNOLOGIES CORP101 citations96
US5538393AJul 23, 1996
Turbine shroud segment with serpentine cooling channels having a bend passage
UNITED TECHNOLOGIES CORP123 citations96
US5609469AMar 11, 1997
Rotor assembly shroud
UNITED TECHNOLOGIES CORP135 citations94
US7600967B2Oct 13, 2009
Stator assembly, module and method for forming a rotary machine
UNITED TECHNOLOGIES CORP73 citations92
US7465145B2Dec 16, 2008
Tip clearance control system
UNITED TECHNOLOGIES CORP21 citations92
US6393331B1May 21, 2002
Method of designing a turbine blade outer air seal
UNITED TECHNOLOGIES CORP96 citations92
US4826397AMay 2, 1989
Stator assembly for a gas turbine engine
UNITED TECHNOLOGIES CORP85 citations91
US5333992AAug 2, 1994
Coolable outer air seal assembly for a gas turbine engine
UNITED TECHNOLOGIES CORP34 citations90
US5927942AJul 27, 1999
Mounting and sealing arrangement for a turbine shroud segment
UNITED TECHNOLOGIES CORP50 citations89
US8016549B2Sep 13, 2011
Turbine engine alloys and crystalline orientations
UNITED TECHNOLOGIES CORP26 citations88
US7491029B2Feb 17, 2009
Active clearance control system for gas turbine engines
UNITED TECHNOLOGIES CORP24 citations85
US10107102B2Oct 23, 2018
Rotor disk assembly for a gas turbine engine
UNITED TECHNOLOGIES CORP2 citations73
US4859142AAug 22, 1989
Turbine clearance control duct arrangement
UNITED TECHNOLOGIES CORP18 citations72