Inventor
BLANEY KEN F
US51 patents
⚠️ This page may combine multiple inventors who share the name “BLANEY KEN F”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
40 patentsUS10697303B2Jun 30, 2020
Internally damped airfoiled component and method
UNITED TECHNOLOGIES CORP7 citations84
US10247028B2Apr 2, 2019
Gas turbine engine blade outer air seal thermal control system
UNITED TECHNOLOGIES CORP7 citations84
US9879551B2Jan 30, 2018
Fluid damper and method of making
UNITED TECHNOLOGIES CORP9 citations84
US10370999B2Aug 6, 2019
Gas turbine engine rapid response clearance control system with air seal segment interface
UNITED TECHNOLOGIES CORP8 citations83
US10196917B2Feb 5, 2019
Blade outer air seal with cored passages
UNITED TECHNOLOGIES CORP6 citations83
US9745898B2Aug 29, 2017
Planetary gear system for turbomachine
UNITED TECHNOLOGIES CORP6 citations83
US10041369B2Aug 7, 2018
BOAS with radial load feature
UNITED TECHNOLOGIES CORP15 citations82
US11073038B2Jul 27, 2021
CMC BOAS arrangement
UNITED TECHNOLOGIES CORP2 citations73
US11022002B2Jun 1, 2021
Attachment body for blade outer air seal
UNITED TECHNOLOGIES CORP1 citations73
US10920600B2Feb 16, 2021
Integrated seal and wear liner
UNITED TECHNOLOGIES CORP2 citations73
US10794206B2Oct 6, 2020
CMC BOAS intersegment seal
UNITED TECHNOLOGIES CORP2 citations73
US10648407B2May 12, 2020
CMC boas cooling air flow guide
UNITED TECHNOLOGIES CORP2 citations73
US10634010B2Apr 28, 2020
CMC BOAS axial retaining clip
UNITED TECHNOLOGIES CORP3 citations73
US10443425B2Oct 15, 2019
Blade outer air seal fin cooling assembly and method
UNITED TECHNOLOGIES CORP5 citations73
US10815827B2Oct 27, 2020
Variable thickness core for gas turbine engine component
UNITED TECHNOLOGIES CORP2 citations72
US10519872B2Dec 31, 2019
Planetary gear system for turbomachine
UNITED TECHNOLOGIES CORP2 citations72
US10036271B2Jul 31, 2018
Gas turbine engine blade outer air seal profile
UNITED TECHNOLOGIES CORP5 citations72
US9874111B2Jan 23, 2018
Low thermal mass joint
UNITED TECHNOLOGIES CORP2 citations72
US10557367B2Feb 11, 2020
Accessible rapid response clearance control system
UNITED TECHNOLOGIES CORP2 citations71
US10329934B2Jun 25, 2019
Reversible flow blade outer air seal
UNITED TECHNOLOGIES CORP3 citations71
US11248482B2Feb 15, 2022
CMC BOAS arrangement
UNITED TECHNOLOGIES CORP1 citations63
US11105214B2Aug 31, 2021
CMC BOAS arrangement
UNITED TECHNOLOGIES CORP0 citations63
US11073037B2Jul 27, 2021
CMC BOAS arrangement
UNITED TECHNOLOGIES CORP0 citations63
US11466857B2Oct 11, 2022
Self-pumping fuel injector for a gas turbine engine and method of operation
UNITED TECHNOLOGIES CORP0 citations62
US10920601B2Feb 16, 2021
Blade outer air seal fin cooling assembly and method
UNITED TECHNOLOGIES CORP0 citations62
US9366149B2Jun 14, 2016
Multi-stage high pressure compressor case
UNITED TECHNOLOGIES CORP2 citations62
US11073036B2Jul 27, 2021
Boas flow directing arrangement
UNITED TECHNOLOGIES CORP0 citations56
US10968772B2Apr 6, 2021
Attachment block for blade outer air seal providing convection cooling
UNITED TECHNOLOGIES CORP0 citations52
US10961866B2Mar 30, 2021
Attachment block for blade outer air seal providing impingement cooling
UNITED TECHNOLOGIES CORP0 citations52
US10927710B2Feb 23, 2021
Blade outer air seal laminate T-joint
UNITED TECHNOLOGIES CORP0 citations52
US10443851B2Oct 15, 2019
Self-pumping fuel injector for a gas turbine engine and method of operation
UNITED TECHNOLOGIES CORP0 citations52
US9752451B2Sep 5, 2017
Active clearance control system with zone controls
UNITED TECHNOLOGIES CORP1 citations52
US10309253B2Jun 4, 2019
Gas turbine engine blade outer air seal profile
UNITED TECHNOLOGIES CORP0 citations51
US10100667B2Oct 16, 2018
Axial flowing cooling passages for gas turbine engine components
UNITED TECHNOLOGIES CORP0 citations51
US10138748B2Nov 27, 2018
Gas turbine engine components with optimized leading edge geometry
UNITED TECHNOLOGIES CORP1 citations50
US10815813B2Oct 27, 2020
Gas turbine rapid response clearance control system with annular piston
UNITED TECHNOLOGIES CORP0 citations48
US10018068B2Jul 10, 2018
Blade outer air seal with cooling holes
UNITED TECHNOLOGIES CORP0 citations48
US10145257B2Dec 4, 2018
Blade outer air seal
UNITED TECHNOLOGIES CORP0 citations42
US10132193B2Nov 20, 2018
Gas turbine engine duct assembly
UNITED TECHNOLOGIES CORP0 citations41
US10557368B2Feb 11, 2020
Gas turbine engine rapid response clearance control system with variable volume turbine case
UNITED TECHNOLOGIES CORP0 citations40
RAYTHEON TECH CORP
6 patentsUS11421558B2Aug 23, 2022
Gas turbine engine component
RAYTHEON TECH CORP1 citations73
US11400624B2Aug 2, 2022
Constant cross section mandrel for CMC components
RAYTHEON TECH CORP2 citations73
US11661865B2May 30, 2023
Gas turbine engine component
RAYTHEON TECH CORP0 citations63
US11215119B2Jan 4, 2022
CMC BOAS cooling air flow guide
RAYTHEON TECH CORP1 citations63
US11668197B2Jun 6, 2023
Internally damped airfoiled component
RAYTHEON TECH CORP0 citations62
US10883426B2Jan 5, 2021
Planetary gear system for turbomachine
RAYTHEON TECH CORP0 citations62
RAYTHEONTECHNOLOGIES CORP
1 patentLUTJEN PAUL M
1 patentBLANEY KEN F
1 patentRTX CORP
1 patentShowing the top 50 of 51 patents by PatentIndex Score.