Lidköping, Sweden

Jan Östlund

This inventor holds 1 USPTO granted patent. Top assignee: Volvo Aero Corporation. Active years: 2003.


Average Co-Inventor Count = 4.0

ph-index = 1

Forward Citations = 4(Granted Patents)


Company Filing History:


Years Active: 2003

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1 patent (USPTO):Explore Patents

Title: Innovations of Jan Östlund in Rocket Nozzle Design

Introduction

Jan Östlund is a notable inventor based in Lidköping, Sweden. He has made significant contributions to the field of aerospace engineering, particularly in the design of rocket nozzles. His innovative approach has led to the development of a unique patent that addresses critical challenges in rocket propulsion.

Latest Patents

Jan Östlund holds a patent for a "Rocket nozzle contour for flow separation control and side load reduction." This invention pertains to a full-flow rocket nozzle featuring a longitudinal contour that closely resembles a parabola. The design aims to enhance flow separation control and reduce side loads. The patent suggests that the parabola contour shape transitions into either a strictly conical shape with an angle between 15° and 25° to the center line, a slight outward curvature, or a slight inward curvature, all of which contribute to improved performance.

Career Highlights

Jan Östlund is associated with Volvo Aero Corporation, where he has applied his expertise in aerospace technology. His work has been instrumental in advancing rocket nozzle designs, which are crucial for efficient propulsion systems. With a focus on innovation, he has dedicated his career to enhancing the performance and reliability of aerospace components.

Collaborations

Throughout his career, Jan has collaborated with talented individuals such as Jan Häggander and Mats Olofsson. These partnerships have fostered a creative environment that encourages the exchange of ideas and the development of groundbreaking technologies.

Conclusion

Jan Östlund's contributions to rocket nozzle design exemplify the spirit of innovation in aerospace engineering. His patent reflects a deep understanding of fluid dynamics and engineering principles, paving the way for advancements in rocket propulsion systems. His work continues to inspire future innovations in the field.

Profile summary based on public USPTO records.
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