Inventor · disambiguated record
Jago Pridie
Also filed as: PRIDIE JAGO
8 granted patents·7 pending applications·18 citations·filing 2003–2024
78Inventor score
Top patents by PatentIndex Score
15 records- 0178US10016949B2Method of moulding a chargePRIDIE JAGO·Filed 2008·Granted Jul 10, 2018·9 cites·20 claims
- 0272US8419886B2Method of manufacturing composite partsASTWOOD SIMON·Filed 2010·Granted Apr 16, 2013·3 cites·11 claims
- 0362US2025135711A1Method for manufacturing a stiffened panel made of composite material comprising a step of laying a skin then a step of laying profiles, and tool for implementing said methodAIRBUS SAS·Filed 2024·Application pending·0 cites
- 0461US12005665B2Device for manufacturing a stiffened panel making it possible to control the geometry of said stiffened panel, and method for manufacturing a stiffened panel using said deviceAIRBUS OPERATIONS SAS·Filed 2022·Granted Jun 11, 2024·0 cites·7 claims
- 0558US12269576B2Method for manufacturing at least one portion of a box structure of an aircraft comprising a forming step, and a central wingbox thus obtainedAIRBUS OPERATIONS SAS·Filed 2023·Granted Apr 8, 2025·0 cites·14 claims
- 0654US11919259B2Method for fabricating a central caisson of an aircraft wing made from composite materialAIRBUS OPERATIONS SAS·Filed 2021·Granted Mar 5, 2024·0 cites·20 claims
- 0749US2009091052A1Method of monitoring the performance of a pressure intensifierAIRBUS UK LTD·Filed 2008·Application pending·0 cites
- 0846US2009197050A1Method of manufacturing composite partAIRBUS UK LTD·Filed 2007·Application pending·0 cites
- 0944US2021114318A1Method for manufacturing a part made of composite material comprising a first, then a second polymerizationAIRBUS OPERATIONS SAS·Filed 2020·Application pending·0 cites
- 1044US2015231835A1Fibre orientation optimisationAIRBUS OPERATIONS LTD·Filed 2013·Application pending·0 cites
- 1143US7883657B2Method for joining aircraft componentsAIRBUS UK LTD·Filed 2003·Granted Feb 8, 2011·6 cites·16 claims
- 1243US2018079154A1Method for manufacturing a component from composite materialAIRBUS OPERATIONS SAS·Filed 2017·Application pending·0 cites
- 1342US2019256185A1Method for manufacturing a central wing box from profile sections produced using high-pressure, low-temperature forming, and a central wing box obtained from implementing the methodAIRBUS OPERATIONS SAS·Filed 2019·Application pending·0 cites
- 1437US11465373B2Method for manufacturing an aircraft centre wing box including at least one stiffener having at least one through-hole and aircraft centre wing box obtained using said methodAIRBUS OPERATIONS SAS·Filed 2019·Granted Oct 11, 2022·0 cites·9 claims
- 1532US11872769B2Method for manufacturing connecting members for connecting an aircraft wing to a center wing box, using preformsAIRBUS OPERATIONS SAS·Filed 2020·Granted Jan 16, 2024·0 cites·12 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →