Inventor · disambiguated record
Bruno Cacciaguerra
Also filed as: CACCIAGUERRA BRUNO
12 granted patents·268 citations·filing 1998–2013
92Inventor score
Files withCACCIAGUERRA BRUNO4CAZENEUVE HELENE2AIRBUS FRANCE1AIRBUS HELICOPTERS1AIRBUS OPERATIONS SAS1
Top patents by PatentIndex Score
12 records- 0191US7874516B2Structural frame for an aircraft fuselageAIRBUS FRANCE·Filed 2005·Granted Jan 25, 2011·30 cites·9 claims
- 0289US5971443AThreaded joint for pipesVALLOUREC MANNESMANN OIL & GAS·Filed 1998·Granted Oct 26, 1999·121 cites·22 claims
- 0388US8302909B2Splicing of omega-shaped stiffeners at a circumferential joint in an aircraft fuselageCAZENEUVE HELENE·Filed 2008·Granted Nov 6, 2012·35 cites·10 claims
- 0485US9315263B2Method of automatically triggering an emergency buoyancy system for a hybrid helicopterAIRBUS HELICOPTERS·Filed 2013·Granted Apr 19, 2016·11 cites·17 claims
- 0582US8820673B2Rotary-wing and fixed-wing aircraftCACCIAGUERRA BRUNO·Filed 2012·Granted Sep 2, 2014·10 cites·17 claims
- 0677US8083182B2Monolithic self-stiffened panelsCACCIAGUERRA BRUNO·Filed 2006·Granted Dec 27, 2011·13 cites·14 claims
- 0773US7942369B2Windscreen frame and a method of production for a windscreen frameSOURIAU·Filed 2007·Granted May 17, 2011·13 cites·11 claims
- 0871US7963477B2Aircraft that comprises a structure that ensures the structural and electrical functionsAIRBUS OPERATIONS SAS·Filed 2008·Granted Jun 21, 2011·14 cites·3 claims
- 0967US8215584B2Aircraft structure including stiffener edge junctionsCAZENEUVE HELENE·Filed 2008·Granted Jul 10, 2012·11 cites·10 claims
- 1066US10150553B2Device and method for assembling two sections of aircraft fuselageCACCIAGUERRA BRUNO·Filed 2012·Granted Dec 11, 2018·3 cites·16 claims
- 1154US9033275B2Aircraft undercarriageBARBIERI ANDRÉ·Filed 2011·Granted May 19, 2015·3 cites·20 claims
- 1253US8220154B2Method for fabricating an aircraft fuselage in composite materialCACCIAGUERRA BRUNO·Filed 2006·Granted Jul 17, 2012·4 cites·8 claims
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