Inventor · disambiguated record
Sabato Inserra Imparato
Also filed as: INSERRA IMPARATO SABATO
13 granted patents·244 citations·filing 1994–2013
89Inventor score
Files withINSERRA IMPARATO SABATO7ALENIA AERMACCHI SPA2ALENIA AERONAUTICA SPA1DE VITA VINCENZO1FINMECCANICA SPA1
Top patents by PatentIndex Score
13 records- 0196US5493390AIntegrated optical instrumentation for the diagnostics of parts by embedded or surface attached optical sensorsFINMECCANICA SPA·Filed 1994·Granted Feb 20, 1996·202 cites·9 claims
- 0280US7503273B2Method for the manufacture of a dry reinforcing preform for a composite structural member of an aircraftALENIA AERONAUTICA SPA·Filed 2005·Granted Mar 17, 2009·8 cites·12 claims
- 0379US8303761B2Method of manufacturing a curved element made of composite materialINSERRA IMPARATO SABATO·Filed 2008·Granted Nov 6, 2012·7 cites·8 claims
- 0477US8419875B2Method of manufacturing a curved structural element made of composite material and having a complex, open cross-sectionINSERRA IMPARATO SABATO·Filed 2008·Granted Apr 16, 2013·4 cites·7 claims
- 0576US8298359B2Method for recycling scraps of prepreg materialsINSERRA IMPARATO SABATO·Filed 2008·Granted Oct 30, 2012·8 cites·8 claims
- 0667US9168646B2Calibrated clamping deviceGALOTA VINCENZO·Filed 2012·Granted Oct 27, 2015·7 cites·9 claims
- 0763US9399329B2Method for producing a closed-section portion of an aircraft provided with deformation sensorsALENIA AERMACCHI SPA·Filed 2013·Granted Jul 26, 2016·2 cites·18 claims
- 0861US9962917B2Method of manufacturing single piece fuselage barrels in composite materialALENIA AERMACCHI SPA·Filed 2013·Granted May 8, 2018·3 cites·15 claims
- 0955US8980152B2Method of manufacturing an integral profile monolithic wing structureDE VITA VINCENZO·Filed 2008·Granted Mar 17, 2015·1 cites·4 claims
- 1053US8323446B2Curing method and apparatus for manufacturing beams of composite material with a J-shaped cross-sectionINSERRA IMPARATO SABATO·Filed 2008·Granted Dec 4, 2012·0 cites·5 claims
- 1149US8815044B2Method of manufacturing spars, longerons and fuselage beams having a variable H cross-sectionINSERRA IMPARATO SABATO·Filed 2011·Granted Aug 26, 2014·2 cites·4 claims
- 1233US8388789B2Method of manufacturing a fuselage frame of composite materialINSERRA IMPARATO SABATO·Filed 2010·Granted Mar 5, 2013·0 cites·7 claims
- 1325US8869631B2Method for detecting the thickness of the walls of hollow manufactured bodies made from non-ferromagnetic materialINSERRA IMPARATO SABATO·Filed 2011·Granted Oct 28, 2014·0 cites·13 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →