Inventor · disambiguated record
Francisco Javier Honorato Ruiz
Also filed as: HONORATO RUIZ FRANCISCO JAVIER
20 granted patents·6 pending applications·51 citations·filing 2007–2021
92Inventor score
Files withAIRBUS OPERATIONS SL20AIRBUS OPERATIONS SLU3CASADO ABARQUERO HUGO1CEBOLLA GARROFE PABLO1HONORATO RUIZ FRANCISCO JAVIER1
Top patents by PatentIndex Score
26 records- 0181US8573539B2Structure for joining torsion boxes in an aircraft using a triform fitting made from non-metallic composite materialsAIRBUS OPERATIONS SL·Filed 2012·Granted Nov 5, 2013·9 cites·9 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
- 0375US9216812B2Optimized torsion box for an aircraftAIRBUS OPERATIONS SL·Filed 2013·Granted Dec 22, 2015·7 cites·12 claims
- 0474US11225015B2Method for manufacturing an aeronautical structureAIRBUS OPERATIONS SLU·Filed 2019·Granted Jan 18, 2022·1 cites·11 claims
- 0574US9701393B2Highly integrated inner structure of a torsion box of an aircraft lifting surfaceAIRBUS OPERATIONS SL·Filed 2013·Granted Jul 11, 2017·2 cites·8 claims
- 0667US10532807B2Leading edge with laminar flow control and manufacturing method thereofAIRBUS OPERATIONS SL·Filed 2017·Granted Jan 14, 2020·2 cites·9 claims
- 0767US9322276B2Highly integrated leading edge of an aircraft lifting surfaceAIRBUS OPERATIONS SL·Filed 2013·Granted Apr 26, 2016·4 cites·15 claims
- 0864US9669581B2Method 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
- 0964US9463866B2Composite structure for an aircraft and manufacturing method thereofAIRBUS OPERATIONS SL·Filed 2014·Granted Oct 11, 2016·3 cites·14 claims
- 1062US9387922B2Main supporting structure of an aircraft lifting surfaceAIRBUS OPERATIONS SL·Filed 2013·Granted Jul 12, 2016·3 cites·7 claims
- 1162US8006932B2Pivoting coupling system for a large dihedral empennage to the tail fuselage of an aircraftAIRBUS OPERATIONS SL·Filed 2007·Granted Aug 30, 2011·9 cites·17 claims
- 1261US9381992B2Leading edge for an aircraft lifting surfaceAIRBUS OPERATIONS SL·Filed 2014·Granted Jul 5, 2016·3 cites·18 claims
- 1354US10830376B2Composite structure having an integrated supportAIRBUS OPERATIONS SL·Filed 2018·Granted Nov 10, 2020·0 cites·15 claims
- 1451US9381991B2Highly integrated structure including leading and trailing edge ribs for an aircraft lifting surfaceAIRBUS OPERATIONS SL·Filed 2013·Granted Jul 5, 2016·1 cites·12 claims
- 1547US11643222B2Method for manufacturing the trailing edge ribs and the bearing ribs of trailing edges of aircraft lifting surfacesAIRBUS OPERATIONS SL·Filed 2019·Granted May 9, 2023·0 cites·1 claims
- 1646US11987343B2Aircraft empennage with a horizontal stabilizer interfacing at the vertical stabilizer rootAIRBUS OPERATIONS SLU·Filed 2021·Granted May 21, 2024·0 cites·15 claims
- 1745US11858229B2Modular tooling for multi-spar torsion boxAIRBUS OPERATIONS SLU·Filed 2021·Granted Jan 2, 2024·0 cites·16 claims
- 1845US10745105B2Thermoplastic moulded injected tip structure for an aircraftAIRBUS OPERATIONS SL·Filed 2017·Granted Aug 18, 2020·0 cites·10 claims
- 1940US9868510B2Aircraft control surfaceAIRBUS OPERATIONS SL·Filed 2014·Granted Jan 16, 2018·0 cites·18 claims
- 2040US2017028652A1Monolithic primary structural part for aircraft and processes for manufacturing itAIRBUS OPERATIONS SL·Filed 2016·Application pending·0 cites
- 2138US10538308B2Aircraft empennageAIRBUS OPERATIONS SL·Filed 2017·Granted Jan 21, 2020·0 cites·12 claims
- 2238US2015183508A1Horizontal tail plane of an aircraftAIRBUS OPERATIONS SL·Filed 2014·Application pending·0 cites
- 2335US2017259902A1Aircraft Aerodynamic Surface With A Detachable Leading EdgeAIRBUS OPERATIONS SL·Filed 2017·Application pending·0 cites
- 2432US2013168009A1Method for manufacturing pieces of composite material having varied thicknessesCEBOLLA GARROFE PABLO·Filed 2012·Application pending·0 cites
- 2530US2013101801A1Optimized stringer run-out zones in aircraft componentsHONORATO RUIZ FRANCISCO JAVIER·Filed 2012·Application pending·0 cites
- 2628US2012193473A1Torsion box skin stiffened with non parallel stringersCASADO ABARQUERO HUGO·Filed 2011·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →