Inventor · disambiguated record
Gianni Iagulli
Also filed as: IAGULLI GIANNI
12 granted patents·3 pending applications·36 citations·filing 2008–2021
87Inventor score
Top patents by PatentIndex Score
15 records- 0179US8114241B2Method for applying a vacuum bag around a fuselage barrel made of composite material to be polymerizedIAGULLI GIANNI·Filed 2008·Granted Feb 14, 2012·11 cites·14 claims
- 0278US10384401B2Method for manufacturing stiffened panels of composite material by means of co-curingLEONARDO SPA·Filed 2016·Granted Aug 20, 2019·4 cites·2 claims
- 0377US8419875B2Method of manufacturing a curved structural element made of composite material and having a complex, open cross-sectionINSERRA IMPARATO SABATO·Filed 2008·Granted Apr 16, 2013·4 cites·7 claims
- 0473US11597192B2Multilayer radar-absorbing laminate for aircraft made of polymer matrix composite material with graphene nanoplatelets, and method of manufacturing sameLEONARDO SPA·Filed 2019·Granted Mar 7, 2023·2 cites·16 claims
- 0572US10449733B2Methods of manufacturing single piece multi-spar boxes of composite material in a closed mouldALENIA AERMACCHI SPA·Filed 2013·Granted Oct 22, 2019·3 cites·5 claims
- 0671US10449734B2Methods for manufacturing elongated structural elements of composite materialALENIA AERMACCHI SPA·Filed 2015·Granted Oct 22, 2019·1 cites·1 claims
- 0767US9168646B2Calibrated clamping deviceGALOTA VINCENZO·Filed 2012·Granted Oct 27, 2015·7 cites·9 claims
- 0866US11097522B2Method for manufacturing a multi-ribbed wing-box of composite material with integrated stiffened panels and communicating baysLEONARDO SPA·Filed 2019·Granted Aug 24, 2021·2 cites·18 claims
- 0965US2020001553A1Methods for manufacturing elongated structural elements of composite materialALENIA AERMACCHI SPA·Filed 2019·Application pending·0 cites
- 1055US12337548B2Method and equipment for the integration of continuous J shaped spars in extended panels of composite materialLEONARDO SPA·Filed 2021·Granted Jun 24, 2025·0 cites·10 claims
- 1149US8815044B2Method of manufacturing spars, longerons and fuselage beams having a variable H cross-sectionINSERRA IMPARATO SABATO·Filed 2011·Granted Aug 26, 2014·2 cites·4 claims
- 1242US2023382561A1Manufacturing method of a stiffened panel with open-section stringers for aeronautical applicationLEONARDO SPA·Filed 2021·Application pending·0 cites
- 1340US11292577B2Method for manufacturing a multi-ribbed wing box of composite material with integrated stiffened panelsLEONARDO SPA·Filed 2019·Granted Apr 5, 2022·0 cites·16 claims
- 1438US9878505B2Tool and a method for forming and assembling beams of composite materialALENIA AERMACCHI SPA·Filed 2014·Granted Jan 30, 2018·0 cites·5 claims
- 1527US2012288666A1Structural member with flange having a clean cut edge, and process for the manufacture thereofRAFFONE MARCO·Filed 2012·Application pending·0 cites
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