Busan, South Korea

Ji Hwan Bae

This inventor holds 1 USPTO granted patent and 1 published patent application and 1 EPO patent. Top assignee: Doosan Enerbility Co., Ltd.. Active years: 2026.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Ji Hwan Bae. Retrieved from https://idiyas.com/inventor/ji-hwan-bae-whmr86ab

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


Company Filing History:


Years Active: 2026

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1 patent (USPTO):Explore Patents

Title: Ji Hwan Bae and His Gas Turbine Combustor Invention.

Introduction

Ji Hwan Bae is an inventor associated with Busan, South Korea, and Doosan Enerbility Co., Ltd. His patent work concerns gas turbine combustion technology and components designed to guide airflow within a combustor.

Latest Patents

The provided information identifies one patent associated with Bae: Combustor, Gas Turbine Including Combustor, and Combustor Flow Guide Member Manufacturing Method. The invention describes a combustor with a tubular nozzle casing, a head plate, a burner with multiple fuel-and-air injection nozzles, and a duct assembly that carries combustion gases toward a turbine. A circular-annular flow guide member sits between the nozzles and the casing to direct air into the nozzles. It is divided into multiple guide segments, a design that is also relevant to the disclosed manufacturing method. Bae is credited with 1 patent in the information provided.

Career Highlights

Bae’s listed patent connects his inventive work with Doosan Enerbility’s gas turbine technology. Its focus on airflow guidance and a segmented flow guide member addresses the combustor’s internal arrangement and component manufacture.

Collaborations

Young Gun Go is identified as Bae’s coworker. The supplied information does not specify their roles in the patent or describe any particular collaboration.

Conclusion

Ji Hwan Bae’s listed patent reflects an engineering contribution to gas turbine combustor design, particularly the guidance of air into burner nozzles through a segmented flow guide member.

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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