Inventor · disambiguated record
Daniel P. Guinan
Also filed as: GUINAN DANIEL · GUINAN DANIEL P
11 granted patents·118 citations·filing 1993–2014
90Inventor score
Top patents by PatentIndex Score
11 records- 0174US8806747B2Method of manufacturing heat exchanger cooling passages in aero propulsion structureGUINAN DANIEL P·Filed 2009·Granted Aug 19, 2014·6 cites·12 claims
- 0269US9108282B2Method of manufacturing heat exchanger cooling passages in aero propulsion structureORBITAL ATK INC·Filed 2014·Granted Aug 18, 2015·3 cites·20 claims
- 0369US6102329AFlow diverter system for multiple streams for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 1998·Granted Aug 15, 2000·27 cites·11 claims
- 0462US6715293B2Scram jet engine designUNITED TECHNOLOGIES CORP·Filed 2002·Granted Apr 6, 2004·20 cites·25 claims
- 0551US7328571B2Semi-axisymmetric scramjet flowpath with conformal nozzleUNITED TECHNOLOGIES CORP·Filed 2004·Granted Feb 12, 2008·8 cites·18 claims
- 0651US5305609ASeal assemblyUNITED TECHNOLOGIES CORP·Filed 1993·Granted Apr 26, 1994·18 cites·6 claims
- 0749US9726080B2Helical cross flow (HCF) pulse detonation engineORBITAL ATK INC·Filed 2013·Granted Aug 8, 2017·0 cites·13 claims
- 0849US5816042AFlow diverter system for multiple streams for gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 1996·Granted Oct 6, 1998·14 cites·8 claims
- 0948US6883330B2Variable geometry inlet design for scram jet engineUNITED TECHNOLOGIES CORP·Filed 2002·Granted Apr 26, 2005·9 cites·20 claims
- 1040US6351940B1Inverter ducting for dual fan conceptUNITED TECHNOLOGIES CORP·Filed 1999·Granted Mar 5, 2002·13 cites·5 claims
- 1139US8438834B2Helical cross flow (HCF) pulse detonation engineGUINAN DANIEL P·Filed 2009·Granted May 14, 2013·0 cites·14 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →