Bristol, United Kingdom

James M Pointon

This inventor holds 2 USPTO granted patents and 2 published patent applications and 1 EPO patent. Top assignee: Rolls-Royce Corporation. Active years: 2020-2021.

IDiyas Innovation Intelligence. (2026). Inventor Profile: James M Pointon. Retrieved from https://idiyas.com/inventor/james-m-pointon

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

USPTO Granted Patents = 2 

% Patents Active = 100.0

 

Average Co-Inventor Count = 2.0

ph-index = 2

Forward Citations = 4(Granted Patents)


Company Filing History:


Years Active: 2020-2021

Loading Chart...
Loading Chart...
2 patents (USPTO):Explore Patents

Title: Innovations of James M Pointon in Gas Turbine Engine Technology

Introduction

James M Pointon is a notable inventor based in Bristol, GB, recognized for his contributions to gas turbine engine technology. He holds 2 patents that showcase his innovative approach to optimizing engine performance. His work primarily focuses on enhancing the efficiency and functionality of aircraft gas turbine engines.

Latest Patents

One of his latest patents is titled "Gas turbine engine with optimized fan, core passage inlet, and compressor forward stage diameter ratios." This invention involves an aircraft gas turbine engine that includes a fan coupled to a fan drive turbine. The fan is designed to provide a bypass flow and a core flow during operation. The engine features a reduction gearbox that connects the fan to the fan drive turbine, along with a core compressor arrangement. The core compressor arrangement has a core inlet at the upstream end of a core gas flow passage, defined by radially inner and outer walls. A first ratio of the first diameter to the second diameter is established to be greater than or equal to 1.4.

Another significant patent is "Gas turbine engine and core casing arrangement." This invention includes a compressor system comprising both low and high-pressure compressors coupled to their respective shafts. It features an inner core casing provided radially inwardly of the compressor blades and an outer core casing that defines a core working gas flow path. The design ensures that at an axial plane of the inlet to the high-pressure compressor, the second outer core casing has an inner radius at least 1.4 times that of the first outer core casing.

Career Highlights

James M Pointon is currently employed at Rolls-Royce Corporation, where he continues to develop innovative solutions in the field of gas turbine engines. His work has significantly contributed to advancements in engine design and efficiency.

Collaborations

He collaborates with Stephen John Bradbrook, working together to push the boundaries of gas turbine technology.

Conclusion

James M Pointon's innovative patents and contributions to gas turbine engine technology reflect his expertise and commitment to advancing aerospace engineering. His work continues to influence the industry and improve aircraft performance.

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]
Loading…