Tolland, CT, United States of America

Jeffrey L Ream

This inventor holds 3 USPTO granted patents. Top assignee: United Technologies Corporation. Active years: 1989-1992.


% Patents Active = 100.0

Average Co-Inventor Count = 2.0

ph-index = 3

Forward Citations = 145(Granted Patents)


Location History:

  • Tollano, CT (US) (1989)
  • Tolland, CT (US) (1991 - 1992)

Company Filing History:


Years Active: 1989-1992

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3 patents (USPTO):Explore Patents

Title: Jeffrey L. Ream: Innovator in Gas Turbine Technology

Introduction

Jeffrey L. Ream is a notable inventor based in Tolland, CT (US). He has made significant contributions to the field of gas turbine technology, holding a total of 3 patents. His work focuses on enhancing the efficiency and safety of gas turbine engines.

Latest Patents

One of his latest patents is titled "Buffer region for the nacelle of a gas turbine engine." This invention discloses a buffer system designed to cool a buffer region in the nacelle of a gas turbine engine after engine shutdown. Various construction details are developed to ensure the positive provision of cooling air to the buffer region, utilizing a blower system. Additionally, a coolable component is strategically placed within the region, and in one detailed embodiment, a shroud extends around the buffer region, incorporating a portion of the coolable component.

Career Highlights

Jeffrey L. Ream is currently employed at United Technologies Corporation, where he continues to innovate and develop advanced technologies in gas turbine systems. His expertise and dedication to improving engine performance have made him a valuable asset to the company.

Collaborations

Throughout his career, Jeffrey has collaborated with various professionals, including his coworker Robert Bubello. Their combined efforts have contributed to the advancement of gas turbine technology.

Conclusion

Jeffrey L. Ream's innovative work in gas turbine technology exemplifies his commitment to engineering excellence. His patents reflect a deep understanding of the complexities involved in turbine design and operation.

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