Tokyo, Japan

Koji Ikeda

This inventor holds 1 USPTO granted patent and 1 published patent application. Top assignee: Subaru Corporation. Active years: 2026.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Koji Ikeda. Retrieved from https://idiyas.com/inventor/koji-ikeda-grnbry6a

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

USPTO Granted Patents = 1 

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: Koji Ikeda: Aircraft Maneuvering Innovation

Introduction

Koji Ikeda is an inventor based in Tokyo, Japan, and works at Subaru Corporation. His patent work includes an aircraft maneuvering system designed to improve the handling characteristics of single-propeller aircraft.

Latest Patents

Ikeda is associated with 1 patent: “Aircraft Maneuvering System for Single Propeller Aircraft and Single Propeller Aircraft.” The invention describes a system that simulates jet-aircraft maneuvering characteristics in a single-propeller aircraft. It uses a power lever, speed brakes on the aircraft’s right and left sides, and a controller.

When the power lever increases thrust, the controller deploys both speed brakes to moderate the aircraft’s acceleration. It can also deploy the brakes by different amounts to generate yaw and roll forces that counter the aircraft’s turning tendency.

Career Highlights

Ikeda’s patent reflects an engineering approach to managing the handling effects of increased thrust in single-propeller aircraft. The system coordinates thrust changes and speed-brake deployment to influence acceleration and directional stability.

Collaborations

Ikeda’s listed coworkers include Shunichiro Hara and Takeshi Fukurose. The available information does not specify their roles in the patent or their working relationship with him.

Conclusion

Koji Ikeda’s patent at Subaru Corporation addresses aircraft acceleration and stability through coordinated control of speed brakes, offering a specialized approach to single-propeller aircraft maneuvering.

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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