Inventor · disambiguated record
Jean-Claude Lacombe
Also filed as: LACOMBE JEAN-CLAUDE
13 granted patents·74 citations·filing 1996–2018
89Inventor score
Top patents by PatentIndex Score
13 records- 0167US8215584B2Aircraft structure including stiffener edge junctionsCAZENEUVE HELENE·Filed 2008·Granted Jul 10, 2012·11 cites·10 claims
- 0266US10150553B2Device and method for assembling two sections of aircraft fuselageCACCIAGUERRA BRUNO·Filed 2012·Granted Dec 11, 2018·3 cites·16 claims
- 0366US8484848B2Method for the orbital assembly of aircraft sections made of composite materialGALLANT GUILLAUME·Filed 2009·Granted Jul 16, 2013·8 cites·17 claims
- 0465US8967540B2Anti lateral-torsional buckling structural member of an aircraft fuselageAIRBUS OPERATIONS SAS·Filed 2012·Granted Mar 3, 2015·4 cites·14 claims
- 0561US5796370AOrientable antenna with conservation of polarization axesALCATEL ESPACE·Filed 1996·Granted Aug 18, 1998·37 cites·21 claims
- 0656US7503524B2Device for equipping a hole in a panel, and panel thus equippedAIRBUS FRANCE·Filed 2004·Granted Mar 17, 2009·4 cites·21 claims
- 0752US7814729B2Stiff panel having composite stiffeners with reduced shock sensitivityAIRBUS FRANCE·Filed 2007·Granted Oct 19, 2010·4 cites·13 claims
- 0851US11124285B2Aerodynamic/hydrodynamic profile with a composite reinforced oblong foam coreAIRBUS OPERATIONS SAS·Filed 2018·Granted Sep 21, 2021·1 cites·17 claims
- 0947US8286915B2Aircraft comprising a window panelDEPEIGE ALAIN·Filed 2009·Granted Oct 16, 2012·2 cites·11 claims
- 1042US8801885B2Method for making a structural part of a composite material having a calibrated thickness and structural part thus obtainedNORMAND MATHIEU·Filed 2008·Granted Aug 12, 2014·0 cites·7 claims
- 1137US8340594B2Thermally optimized microwave channel multiplexing device and signals repetition device comprising at least one such multiplexing deviceLAGORSSE JOEL·Filed 2010·Granted Dec 25, 2012·0 cites·24 claims
- 1234US8395497B2Radiofrequency circuit embedded onboard in a satellite comprising a thermal control system based on an alarm signal generated by the reflection of powerTONELLO EMILE·Filed 2011·Granted Mar 12, 2013·0 cites·12 claims
- 1328US9126671B2Stiff panel for aircraft, comprising stiffeners with notched coresDUBOST JÉÔME·Filed 2012·Granted Sep 8, 2015·0 cites·8 claims
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