Cranfield, United Kingdom

Ioannis Roumeliotis

This inventor holds 1 USPTO granted patent. Top assignee: Rolls-Royce Corporation. Active years: 2026.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Ioannis Roumeliotis. Retrieved from https://idiyas.com/inventor/ioannis-roumeliotis-ca89py4d

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

Calculating rank

Average Co-Inventor Count = 1.0

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Company Filing History:


Years Active: 2026

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1 patent (USPTO):Explore Patents

Title: Ioannis Roumeliotis and Aircraft Propulsion Innovation.

Introduction

Ioannis Roumeliotis is an inventor associated with Cranfield, Great Britain, and Rolls-Royce Corporation. His patent work concerns aircraft propulsion systems and the management of heat and airflow in gas turbine engines.

Latest Patents

Roumeliotis is associated with one patent, titled “Aircraft Propulsion System.” The invention describes a core gas turbine engine with a core compressor, combustor, and turbine arranged in sequence. It also includes a separate auxiliary compressor that supplies air to an auxiliary air system. A heat exchanger transfers heat from the auxiliary-compressor air to fuel in the main fuel conduit before the fuel reaches the core combustor. This arrangement integrates auxiliary airflow and fuel heating into an aircraft propulsion system.

Career Highlights

Roumeliotis’s recorded patent contribution focuses on aircraft propulsion technology. The patent describes an approach to transferring heat within the engine system while supplying air to auxiliary equipment. He is associated with Rolls-Royce Corporation, a company active in aerospace and propulsion engineering.

Collaborations

Vasileios Kyritsis and Vasileios Pachidis are identified as Roumeliotis’s coworkers. Their shared professional context connects them to the engineering environment surrounding his propulsion-system work.

Conclusion

Ioannis Roumeliotis’s patent presents an aircraft propulsion concept that combines a core gas turbine, auxiliary air supply, and fuel heating through heat exchange.

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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