Inventor · disambiguated record
Ricardo Burdisso
Also filed as: BURDISSO RICARDO · BURDISSO RICARDO A · BURDISSO RICARDO ANIBAL
8 granted patents·1 pending application·359 citations·filing 1992–2008
90Inventor score
Files withVIRGINIA TECH INTELL PROP2BOULDIN BRUCE DAN1DEFENSE RESEARCH TECHNOLOGIES1FORD GLOBAL TECH INC1HONEYWELL INT INC1
Top patents by PatentIndex Score
9 records- 0189US7047725B2Assembly and method for aircraft engine noise reductionROHR INC·Filed 2003·Granted May 23, 2006·41 cites·20 claims
- 0288US5515444AActive control of aircraft engine inlet noise using compact sound sources and distributed error sensorsVIRGINIA POLYTECHNIC INST·Filed 1994·Granted May 7, 1996·98 cites·6 claims
- 0384US5355417AActive control of aircraft engine inlet noise using compact sound sources and distributed error sensorsINNOVATIVE TECH CENTER·Filed 1992·Granted Oct 11, 1994·78 cites·14 claims
- 0483US5884736AActive dual reaction mass absorber for vibration controlVIRGINIA TECH INTELL PROP·Filed 1997·Granted Mar 23, 1999·56 cites·11 claims
- 0573US6112514AFan noise reduction from turbofan engines using adaptive Herschel-Quincke tubesVIRGINIA TECH INTELL PROP·Filed 1998·Granted Sep 5, 2000·43 cites·25 claims
- 0669US8070092B2Noise-suppressing strut support system for an unmanned aerial vehicleBOULDIN BRUCE DAN·Filed 2008·Granted Dec 6, 2011·10 cites·20 claims
- 0757US5662136AAcousto-fluidic driver for active control of turbofan engine noiseDEFENSE RESEARCH TECHNOLOGIES·Filed 1995·Granted Sep 2, 1997·22 cites·26 claims
- 0845US2011001017A1Uav ducted fan swept and lean stator designHONEYWELL INT INC·Filed 2008·Application pending·0 cites
- 0938US6275591B1Method and apparatus for extracting a component signal from a composite signalFORD GLOBAL TECH INC·Filed 1996·Granted Aug 14, 2001·11 cites·6 claims
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