Assignee
SPANGLER BRANDON W
US·16 granted patents·3 pending applications·114 citations·filing 2007–2012
Top patents by PatentIndex Score
19 records- 0195US8707712B2Gas turbine engine turbine vane airfoil profileSPANGLER BRANDON W·Filed 2012·Granted Apr 29, 2014·18 cites·17 claims
- 0292US8807945B2Cooling system for turbine airfoil including ice-cream-cone-shaped pedestalsSPANGLER BRANDON W·Filed 2011·Granted Aug 19, 2014·15 cites·30 claims
- 0388US9322279B2Airfoil cooling arrangementSPANGLER BRANDON W·Filed 2012·Granted Apr 26, 2016·10 cites·15 claims
- 0485US9109453B2Airfoil cooling arrangementSPANGLER BRANDON W·Filed 2012·Granted Aug 18, 2015·9 cites·11 claims
- 0582US9138804B2Core for a casting processSPANGLER BRANDON W·Filed 2012·Granted Sep 22, 2015·2 cites·17 claims
- 0682US9115597B2Gas turbine engine turbine vane airfoil profileSPANGLER BRANDON W·Filed 2012·Granted Aug 25, 2015·6 cites·15 claims
- 0771US9500099B2Cover plate for a component of a gas turbine engineSPANGLER BRANDON W·Filed 2012·Granted Nov 22, 2016·3 cites·1 claims
- 0870US8240981B2Turbine airfoil with platform coolingSPANGLER BRANDON W·Filed 2007·Granted Aug 14, 2012·13 cites·24 claims
- 0969US8240987B2Gas turbine engine systems involving baffle assembliesSPANGLER BRANDON W·Filed 2008·Granted Aug 14, 2012·11 cites·14 claims
- 1069US8206114B2Gas turbine engine systems involving turbine blade platforms with cooling holesSPANGLER BRANDON W·Filed 2008·Granted Jun 26, 2012·12 cites·16 claims
- 1164US9790801B2Gas turbine engine component having suction side cutback openingSPANGLER BRANDON W·Filed 2012·Granted Oct 17, 2017·2 cites·8 claims
- 1263US9273566B2Turbine engine variable area vaneSPANGLER BRANDON W·Filed 2012·Granted Mar 1, 2016·2 cites·20 claims
- 1362US9353631B2Gas turbine engine airfoil baffleSPANGLER BRANDON W·Filed 2011·Granted May 31, 2016·2 cites·13 claims
- 1456US9422816B2Airfoil with hybrid drilled and cutback trailing edgeSPANGLER BRANDON W·Filed 2009·Granted Aug 23, 2016·5 cites·19 claims
- 1554US8282354B2Reduced weight blade for a gas turbine engineSPANGLER BRANDON W·Filed 2008·Granted Oct 9, 2012·4 cites·19 claims
- 1648US2010143132A1Turbine blade with reverse cooling air film hole directionSPANGLER BRANDON W·Filed 2010·Application pending·0 cites
- 1741US2012171045A1Turbine component fixture and coating systemSPANGLER BRANDON W·Filed 2011·Application pending·0 cites
- 1841US2012076660A1Conduction pedestals for a gas turbine engine airfoilSPANGLER BRANDON W·Filed 2010·Application pending·0 cites
- 1940US8257045B2Platforms with curved side edges and gas turbine engine systems involving such platformsSPANGLER BRANDON W·Filed 2008·Granted Sep 4, 2012·0 cites·21 claims
Counts cover granted patents and pending applications in the PatentIndex corpus. How scoring works →