Inventor · disambiguated record
Alberto Arana Hidalgo
Also filed as: ARANA HIDALGO ALBERTO
11 granted patents·6 pending applications·8 citations·filing 2012–2022
81Inventor score
Top patents by PatentIndex Score
17 records- 0181US10906628B2Box structural arrangement for an aircraft and manufacturing method thereofAIRBUS OPERATIONS SL·Filed 2018·Granted Feb 2, 2021·5 cites·14 claims
- 0274US11225015B2Method for manufacturing an aeronautical structureAIRBUS OPERATIONS SLU·Filed 2019·Granted Jan 18, 2022·1 cites·11 claims
- 0373US11845531B2Fireproof and thermal insulator productAIRBUS OPERATIONS SL·Filed 2020·Granted Dec 19, 2023·1 cites·18 claims
- 0457US11377204B2Retractable vortex generator system for an aircraftAIRBUS OPERATIONS SL·Filed 2020·Granted Jul 5, 2022·0 cites·17 claims
- 0556US12103252B2Device and method for manufacturing composite parts for an aircraft bulkheadAIRBUS OPERATIONS SL·Filed 2022·Granted Oct 1, 2024·0 cites·23 claims
- 0656US11220354B2Composite fuselage assembly and methods to form the assemblyAIRBUS OPERATIONS SL·Filed 2019·Granted Jan 11, 2022·0 cites·17 claims
- 0753US10890971B2Real time virtual reality (VR) system and related methodsAIRBUS OPERATIONS SL·Filed 2019·Granted Jan 12, 2021·0 cites·8 claims
- 0850US9919785B2Stringer made of composite material with an elastic run-out and method of manufacturing sameAIRBUS OPERATIONS SL·Filed 2013·Granted Mar 20, 2018·1 cites·9 claims
- 0947US11541983B2Method for manufacturing a multi-spar box with a continuous skin upper shell of a tail cone section for a rear end of an aircraft and a composite assemblyAIRBUS OPERATIONS SL·Filed 2019·Granted Jan 3, 2023·0 cites·8 claims
- 1046US11377190B2Method for manufacturing a rear section of an aircraft and aircraft rear section manufactured by said methodAIRBUS OPERATIONS SL·Filed 2019·Granted Jul 5, 2022·0 cites·16 claims
- 1142US11267584B2Method for manufacturing a rear section of an aircraft and aircraft rear sectionAIRBUS OPERATIONS SL·Filed 2019·Granted Mar 8, 2022·0 cites·4 claims
- 1238US2018201362A1Aircraft with a variable fuselage surface for boundary layer optimizationAIRBUS OPERATIONS SL·Filed 2017·Application pending·0 cites
- 1337US2018155006A1Aircraft stabilizer leading edge integration with torsion box and fuselageAIRBUS OPERATIONS SL·Filed 2017·Application pending·0 cites
- 1436US2018022436A1Magnetic union of access panels and fairings of aircraft to its resistant structureAIRBUS OPERATIONS SL·Filed 2017·Application pending·0 cites
- 1535US2019161211A1Aircraft with a system for rearward mounting and dismounting an engine and method for rearward dismounting an engineAIRBUS OPERATIONS SL·Filed 2018·Application pending·0 cites
- 1635US2021147063A1Fireproof and thermal insulator productAIRBUS OPERATIONS SL·Filed 2020·Application pending·0 cites
- 1730US2013101801A1Optimized stringer run-out zones in aircraft componentsHONORATO RUIZ FRANCISCO JAVIER·Filed 2012·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →