Delft, Netherlands

Bart Diane Walter Remes

This inventor holds 1 USPTO granted patent and 1 EPO patent. Top assignee: Technische Universiteit Delft. Active years: 2026.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Bart Diane Walter Remes. Retrieved from https://idiyas.com/inventor/bart-diane-walter-remes

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


% Patents Active = 100.0


Average Co-Inventor Count = 1.0

ph-index = 1


Company Filing History:


Years Active: 2026

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1 patent (USPTO):Explore Patents

Title: Bart Diane Walter Remes and Aeronautical Vehicle Innovation.

Introduction

Bart Diane Walter Remes is an inventor associated with Technische Universiteit Delft in Delft, the Netherlands. His patent work addresses aircraft capable of transitioning between horizontal and vertical flight.

Latest Patents

The supplied information lists one patent for Remes: “Aeronautical Vehicle and Method of Transitioning Between Flight Modes for an Aeronautical Vehicle.” The invention describes a vehicle with a fuselage, a wing assembly, vertical-thrust rotors, a horizontal thruster, and an attitude control system. The wing assembly rotates between stowed and active positions, while the rotor assembly also moves between those positions. For horizontal flight, the wings are active and the rotors are stowed; for vertical flight, the wings are stowed and the rotors are active. Remes is credited with 1 patent.

Career Highlights

The available details connect Remes’s inventive work with Technische Universiteit Delft. His patent focuses on coordinating movable wings and rotors to support different flight modes in a single aeronautical vehicle.

Collaborations

Technische Universiteit Delft is identified as the organization where Remes works. The supplied information does not specify additional collaborators or institutional roles related to the patent.

Conclusion

Bart Diane Walter Remes’s listed patent presents a flight-mode transition concept that combines repositionable wings and rotors, reflecting an engineering approach to aircraft capable of both horizontal and vertical flight.

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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