Nottingham, United Kingdom

Michael J Sheath

USPTO Granted Patents = 4 

 

Average Co-Inventor Count = 2.4

ph-index = 3

Forward Citations = 13(Granted Patents)


Location History:

  • Nottingham, GB (2010 - 2015)
  • Derby, GB (2021)

Company Filing History:


Years Active: 2010-2021

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4 patents (USPTO):Explore Patents

Title: Innovative Contributions of Inventor Michael J. Sheath

Introduction: Michael J. Sheath is a distinguished inventor based in Nottingham, GB, recognized for his significant contributions to the field of gas turbine technology. With a total of four patents to his name, Sheath has demonstrated a commitment to innovation in engineering, particularly in optimizing the performance and efficiency of gas turbine engines.

Latest Patents: Among his latest patents are two remarkable inventions related to gas turbine engines. The first, titled "Gas turbine engine," involves a design that features an inner core nacelle, an outer fan nacelle, and a sophisticated cooling system. This innovative system utilizes pipes that convey cooling fluid through bifurcations to enhance thermal efficiency. The second patent, "Gas turbine engine with turbine cooling arrangement," presents a comprehensive cooling methodology that includes multiple compressed air bleed arrangements. This advanced setup is designed to provide effective sealing and cooling for the turbine section, significantly improving the overall performance of gas turbine engines.

Career Highlights: Michael J. Sheath has built a commendable career at Rolls-Royce Corporation, where he has played a vital role in the advancement of aerospace technology. His expertise in gas turbine systems has been pivotal in the development of cutting-edge engine designs that aim to meet rigorous performance and environmental standards.

Collaborations: Throughout his career, Sheath has collaborated with fellow engineers and inventors, including Crispin David Bolgar and Jonathan M. King. These partnerships have fostered an environment of innovation and creativity, resulting in the successful development of critical technologies that benefit the aerospace industry.

Conclusion: Michael J. Sheath stands as an influential figure in the realm of gas turbine technology. His innovative patents reflect a deep understanding of engineering principles and a dedication to improving engine efficiency. As he continues to push the boundaries of aerospace technology, Sheath's contributions will undoubtedly impact future advancements in the field.

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