Derby, United Kingdom

Michael O Hales

USPTO Granted Patents = 4 

Average Co-Inventor Count = 3.4

ph-index = 1


Location History:

  • Bristol, GB (2021 - 2022)
  • Derby, GB (2022 - 2023)

Company Filing History:


Years Active: 2021-2023

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4 patents (USPTO):Explore Patents

Title: Michael O Hales: Innovator in Gas Turbine Technology

Introduction

Michael O Hales is a distinguished inventor based in Derby, GB. He has made significant contributions to the field of gas turbine technology, holding a total of 4 patents. His innovative designs have advanced the efficiency and performance of gas turbine engines.

Latest Patents

One of his latest patents is a high pressure ratio gas turbine engine. This design includes a high pressure turbine, a low pressure turbine, and a high pressure compressor coupled to the high pressure turbine by a high pressure shaft. Additionally, it features a propulsor and a low pressure compressor coupled to the low pressure turbine via a low pressure shaft and a reduction gearbox. The high pressure compressor defines an average stage pressure ratio at cruise conditions of between 1.25 and 1.35 and consists of 10 or 11 stages. Furthermore, the high pressure compressor and low pressure compressor together define a core overall pressure ratio at cruise conditions of between 40:1 and 60:1.

Career Highlights

Michael O Hales is currently associated with Rolls-Royce Corporation, where he continues to innovate in the field of gas turbine technology. His work has been instrumental in enhancing the performance and reliability of turbine engines.

Collaborations

Throughout his career, Michael has collaborated with notable colleagues, including Ian J Bousfield and Craig W Bemment. These collaborations have fostered a creative environment that has led to groundbreaking advancements in turbine technology.

Conclusion

Michael O Hales is a prominent figure in the field of gas turbine innovation, with a proven track record of patents and collaborations. His contributions continue to shape the future of turbine technology.

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