Derby, United Kingdom

Michael Paul Spooner

This inventor holds 14 USPTO granted patents and 1 EPO patent, primarily in Gas Turbine Technology. Top assignees: Rolls-Royce Corporation, Delavan Inc.. Active years: 2001-2014.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Michael Paul Spooner. Retrieved from https://idiyas.com/inventor/michael-paul-spooner

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

Calculating rank

% Patents Active = 92.9

 

Average Co-Inventor Count = 2.4

ph-index = 9

Forward Citations = 263(Granted Patents)


Location History:

  • Littleover, GB (2006)
  • Derby, GB (2001 - 2014)

Company Filing History:


Years Active: 2001-2014

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Areas of Expertise:
Combustor
Fuel Injector
Gas Turbine Engine
Lean Direct Injection
Atomizer
Combustion Apparatus
Wall Elements
Annular Prefilmers
14 patents (USPTO):Explore Patents

Title: Michael Paul Spooner: Innovator in Gas Turbine Technology

Introduction

Michael Paul Spooner is a distinguished inventor based in Derby, GB. He has made significant contributions to the field of gas turbine technology, holding a total of 14 patents. His innovative designs and engineering solutions have enhanced the efficiency and performance of gas turbine engines.

Latest Patents

Among his latest patents is a combustor for a gas turbine engine. This combustor features a wall that forms a gap with an outer nozzle guide vane platform. A closure mechanism is operable to open or close this gap. When the gap is opened, particularly during cruise conditions, it reduces the mass flow rate of air through the combustor's open end. This adjustment enriches the air-fuel ratio, thereby improving flame stability and combustion efficiency. Conversely, under high power conditions, closing the gap increases the air flow rate through the combustor's open end, achieving a lean burn air-fuel ratio when the fuel flow rate is increased.

Another notable patent is a fuel injector designed for gas turbine engines. This injector head comprises a pilot injector and a main injector, with the main injector located radially outward of the pilot injector. A concentric splitter separates the two injectors and bounds a duct through which fuel injected by the pilot injector flows. The splitter is hollow to enhance cooling and features a radially inner surface that tapers inwardly to a throat and outwardly from the throat. This design ensures that the flow of air remains attached over the length of the surface.

Career Highlights

Michael has worked with prominent companies in the aerospace industry, including Rolls-Royce Corporation and Delavan Inc. His experience in these organizations has allowed him to refine his skills and contribute to groundbreaking advancements in gas turbine technology.

Collaborations

Throughout his career, Michael has collaborated with notable professionals, including Anthony Pidcock and Desmond Close. These partnerships have fostered innovation and have been instrumental in the development of his patented technologies.

Conclusion

Michael Paul Spooner is a remarkable inventor whose work in gas turbine technology has led to significant advancements in efficiency and performance. His contributions continue to influence the industry and inspire future innovations.

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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