GETAFE, Spain

Raúl GÓMEZ VIZCAÍNO

This inventor holds 1 USPTO granted patent and 2 published patent applications. Top assignee: Airbus Operations, S.L.U.. Active years: 2026.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Raúl GÓMEZ VIZCAÍNO. Retrieved from https://idiyas.com/inventor/raul-gomez-vizcaino

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

USPTO Granted Patents = 1 

% Patents Active = 100.0

Average Co-Inventor Count = 6.0

ph-index = 1


Company Filing History:


Years Active: 2026

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1 patent (USPTO):Explore Patents

Title: Raúl Gómez Vizcaíno and Aircraft Structural Innovation.

Introduction

Raúl Gómez Vizcaíno is an inventor associated with Getafe, Spain, and Airbus Operations, S.L.U. His patent work addresses the design and assembly of structural components for aircraft. The available information lists 1 patent for him.

Latest Patents

His listed patent is titled “Assembly Comprising a Continuous Structural Element for Aircraft and a Fitting.” It describes an aircraft structural element with outer and inner flanges connected by a web. A portion of the inner flange has a wavy shape, which changes the web’s height. A fitting is designed to fit against the web in this area, while keeping at least one of its through holes uncovered by the web in the assembled structure. This arrangement supports the joining of the fitting and structural element while preserving access to the hole.

Career Highlights

The patent identifies Gómez Vizcaíno’s work in aircraft structural design and assembly. His listed company affiliation is Airbus Operations, S.L.U., an organization involved in aircraft operations and manufacturing.

Collaborations

The provided information names Ana Fernández Ramírez and Jorge Ballestero Méndez as coworkers. Their inclusion indicates professional connections, though the available details do not specify their roles in the patent.

Conclusion

Raúl Gómez Vizcaíno’s listed patent focuses on fitting an aircraft component to a shaped structural web while leaving a through hole unobstructed. It reflects a practical approach to aircraft assembly and structural design.

Profile summary based on public USPTO records.
Data Sources: USPTO Patent Grant XML, Patent Center, EPO & CIPO • Normalized by IDiyas Innovation Graph. Methodology & provenance architecturePlease report any incorrect information to [email protected]
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