Assignee
CUNHA FRANK J
US·12 granted patents·146 citations·filing 2010–2012
Top patents by PatentIndex Score
12 records- 0198US9057523B2Microcircuit cooling for gas turbine engine combustorCUNHA FRANK J·Filed 2011·Granted Jun 16, 2015·31 cites·9 claims
- 0297US9335050B2Gas turbine engine combustorCUNHA FRANK J·Filed 2012·Granted May 10, 2016·31 cites·19 claims
- 0397US8978385B2Distributed cooling for gas turbine engine combustorCUNHA FRANK J·Filed 2011·Granted Mar 17, 2015·24 cites·18 claims
- 0493US9243801B2Combustor liner with improved film coolingCUNHA FRANK J·Filed 2012·Granted Jan 26, 2016·15 cites·16 claims
- 0587US9217568B2Combustor liner with decreased liner coolingCUNHA FRANK J·Filed 2012·Granted Dec 22, 2015·9 cites·20 claims
- 0686US9482432B2Gas turbine engine combustor with integrated combustor vane having swirlerCUNHA FRANK J·Filed 2012·Granted Nov 1, 2016·9 cites·17 claims
- 0785US9222674B2Multi-stage amplification vortex mixture for gas turbine engine combustorCUNHA FRANK J·Filed 2011·Granted Dec 29, 2015·8 cites·20 claims
- 0883US9404654B2Gas turbine engine combustor with integrated combustor vaneCUNHA FRANK J·Filed 2012·Granted Aug 2, 2016·7 cites·19 claims
- 0980US9335049B2Combustor liner with reduced cooling dilution openingsCUNHA FRANK J·Filed 2012·Granted May 10, 2016·6 cites·15 claims
- 1074US9239165B2Combustor liner with convergent cooling channelCUNHA FRANK J·Filed 2012·Granted Jan 19, 2016·4 cites·19 claims
- 1171US8220522B2Peripheral microcircuit serpentine cooling for turbine airfoilsCUNHA FRANK J·Filed 2011·Granted Jul 17, 2012·2 cites·10 claims
- 1257US8215374B2Peripheral microcircuit serpentine cooling for turbine airfoilsCUNHA FRANK J·Filed 2010·Granted Jul 10, 2012·0 cites·8 claims
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