Trollhättan, Sweden

Jan H{umlaut Over (a)}ggander

This inventor holds 1 USPTO granted patent. Top assignee: Volvo Aero Corporation. Active years: 2001.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Jan H{umlaut Over (a)}ggander. Retrieved from https://idiyas.com/inventor/jan-humlaut-over-aggander

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

Calculating rank

% Patents Active = 100.0

Average Co-Inventor Count = 2.0

ph-index = 1

Forward Citations = 2(Granted Patents)


Company Filing History:


Years Active: 2001

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1 patent (USPTO):Explore Patents

Title: Jan Häggander: Innovator in Rocket Engine Technology

Introduction

Jan Häggander is a notable inventor based in Trollhättan, Sweden. He has made significant contributions to the field of rocket engine technology. His innovative designs focus on enhancing the efficiency and performance of rocket systems.

Latest Patents

Jan Häggander holds a patent for a rocket engine nozzle. This patent describes a rocket engine system that comprises a single nozzle with a curved profile in axial section. The design allows for better control of flow separation occurring within the nozzle outlet. The outlet portion features a radius in transverse section, which varies in length to ensure a smooth transition from a circular nozzle throat to a polygonal outlet section. This innovation is crucial for improving the performance of rocket engines.

Career Highlights

Jan Häggander is associated with Volvo Aero Corporation, where he applies his expertise in aerospace engineering. His work at Volvo Aero Corporation has positioned him as a key player in the development of advanced rocket technologies.

Collaborations

Jan collaborates with Lars-Olof Pekkari, who is also involved in the aerospace sector. Their partnership enhances the innovative capabilities within their projects.

Conclusion

Jan Häggander's contributions to rocket engine technology exemplify the spirit of innovation in the aerospace industry. His patent for a novel rocket engine nozzle showcases his commitment to advancing engineering solutions.

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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