Inventor
BLAIR MICHAEL F
US16 patents
⚠️ This page may combine multiple inventors who share the name “BLAIR MICHAEL F”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
10 patentsUS7984607B2Jul 26, 2011
Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity
UNITED TECHNOLOGIES CORP21 citations92
US7837441B2Nov 23, 2010
Impingement skin core cooling for gas turbine engine blade
UNITED TECHNOLOGIES CORP21 citations92
US5370831ADec 6, 1994
Method of molding polymeric skins for trim products
UNITED TECHNOLOGIES CORP44 citations92
US5090866AFeb 25, 1992
High temperature leading edge vane insert
UNITED TECHNOLOGIES CORP34 citations92
US7686068B2Mar 30, 2010
Blade outer air seal cores and manufacture methods
UNITED TECHNOLOGIES CORP25 citations90
US11085325B2Aug 10, 2021
Turbine engine cooling system with an open loop circuit
UNITED TECHNOLOGIES CORP1 citations73
US10156359B2Dec 18, 2018
Gas turbine engine component having vascular engineered lattice structure
UNITED TECHNOLOGIES CORP3 citations73
US9739171B2Aug 22, 2017
Turbine engine cooling system with an open loop circuit
UNITED TECHNOLOGIES CORP3 citations73
US10480326B2Nov 19, 2019
Vane for variable area turbine
UNITED TECHNOLOGIES CORP2 citations71
US10047631B2Aug 14, 2018
Turbine engine cooling system with an open loop circuit
UNITED TECHNOLOGIES CORP0 citations52
SHARMA OM P
3 patentsUS8973374B2Mar 10, 2015
Blades in a turbine section of a gas turbine engine
SHARMA OM P7 citations82
US8468797B2Jun 25, 2013
Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity
SHARMA OM P4 citations60
US8516793B2Aug 27, 2013
Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity
SHARMA OM P0 citations50