Inventor · disambiguated record
Pablo Cebolla Garrofe
Also filed as: CEBOLLA GARROFE PABLO
8 granted patents·7 pending applications·17 citations·filing 2011–2020
80Inventor score
Files withAIRBUS OPERATIONS SL12CEBOLLA GARROFE PABLO1HONORATO RUIZ FRANCISCO JAVIER1SANTOS GOMEZ JOSE MANUEL1
Top patents by PatentIndex Score
15 records- 0179US9669919B2Highly integrated infused box made of composite material and method of manufacturingAIRBUS OPERATIONS SL·Filed 2014·Granted Jun 6, 2017·4 cites·19 claims
- 0275US10377464B2Method, injection moulding tool for manufacturing a leading edge section with hybrid laminar flow control for an aircraft, and leading edge section with hybrid laminar flow control obtained thereofAIRBUS OPERATIONS SL·Filed 2017·Granted Aug 13, 2019·3 cites·15 claims
- 0375US10071507B2Method and device for manufacturing a composite part of an aircraftAIRBUS OPERATIONS SL·Filed 2015·Granted Sep 11, 2018·2 cites·14 claims
- 0467US10532807B2Leading edge with laminar flow control and manufacturing method thereofAIRBUS OPERATIONS SL·Filed 2017·Granted Jan 14, 2020·2 cites·9 claims
- 0564US9669581B2Method for manufacturing an aeronautical torsion box, torsion box and tool for manufacturing an aeronautical torsion boxAIRBUS OPERATIONS SL·Filed 2014·Granted Jun 6, 2017·4 cites·10 claims
- 0663US10576723B2Hybrid tool for curing pieces of composite materialAIRBUS OPERATIONS SL·Filed 2014·Granted Mar 3, 2020·2 cites·13 claims
- 0757US11518067B2Method for forming fiber composite preformsAIRBUS OPERATIONS SL·Filed 2020·Granted Dec 6, 2022·0 cites·15 claims
- 0850US2015064393A1Laminate for joining parts, and method and system for joining partsAIRBUS OPERATIONS SL·Filed 2014·Application pending·0 cites
- 0945US10745105B2Thermoplastic moulded injected tip structure for an aircraftAIRBUS OPERATIONS SL·Filed 2017·Granted Aug 18, 2020·0 cites·10 claims
- 1039US2016167318A1Method and system for manufacturing of a moulded cfrp partAIRBUS OPERATIONS SL·Filed 2015·Application pending·0 cites
- 1137US2018155006A1Aircraft stabilizer leading edge integration with torsion box and fuselageAIRBUS OPERATIONS SL·Filed 2017·Application pending·0 cites
- 1235US2017259902A1Aircraft Aerodynamic Surface With A Detachable Leading EdgeAIRBUS OPERATIONS SL·Filed 2017·Application pending·0 cites
- 1332US2013168009A1Method for manufacturing pieces of composite material having varied thicknessesCEBOLLA GARROFE PABLO·Filed 2012·Application pending·0 cites
- 1430US2013101801A1Optimized stringer run-out zones in aircraft componentsHONORATO RUIZ FRANCISCO JAVIER·Filed 2012·Application pending·0 cites
- 1525US2011290421A1Automatic system for quality control and position correction of taped partsSANTOS GOMEZ JOSE MANUEL·Filed 2011·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →