Cincinnati, OH, United States of America

Brandon ALlanson Reynolds

This inventor holds 21 USPTO granted patents and 1 published patent application and 3 EPO patents, primarily in Gas Turbine Engineering. Top assignee: General Electric Company. Active years: 2019-2025.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Brandon ALlanson Reynolds. Retrieved from https://idiyas.com/inventor/brandon-allanson-reynolds

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

USPTO Granted Patents = 21 

% Patents Active = 95.2

 

Average Co-Inventor Count = 3.4

ph-index = 7

Forward Citations = 110(Granted Patents)


Company Filing History:


Years Active: 2019-2025

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Areas of Expertise:
Gas Turbine Engines
CMC Structures
Flow Path Assemblies
Airfoil Designs
Combustor Deflector
Fluid Curtain
Nozzle Airfoils
CTE Matching
Unitary Flow Path
Assembly Methods
Positioning Features
Flow Path Leakage
21 patents (USPTO):Explore Patents

Title: Innovations of Brandon Allanson Reynolds in Gas Turbine Technology

Introduction

Brandon Allanson Reynolds, a prolific inventor based in Cincinnati, OH, has made significant contributions to the field of gas turbine technology. With a total of 20 patents to his name, his work reflects a deep understanding of combustion systems and high-performance materials.

Latest Patents

Among his latest innovations, two noteworthy patents stand out:

1. **CMC Combustor Deflector** - This invention involves combustor dome assemblies equipped with combustor deflectors. The design features a combustor dome with an opening and a ceramic matrix composite (CMC) deflector strategically positioned on the aft side. It incorporates a fuel-air mixer with a groove around its outer perimeter and a seal plate that includes a key. The innovative design allows bayonets on the CMC deflector to engage with the fuel-air mixer groove, ensuring a secure and efficient assembly.

2. **CTE Matching Hanger Support for CMC Structures** - This patent presents a flow path assembly intended for gas turbine engines, comprising a metal outer casing and a ceramic structure. The mounting component connecting these components is crafted from materials that transition to create varying coefficients of thermal expansion. This thoughtful engineering enhances the assembly's performance and durability under varying operational conditions.

Career Highlights

Brandon Reynolds has built his career at General Electric Company, where his expertise in engineering and innovation has been pivotal. His focus on advancing gas turbine technology will continue to enhance the reliability and efficiency of turbine systems worldwide.

Collaborations

Throughout his career, Brandon has collaborated with talented individuals such as Daniel Patrick Kerns and Jonathan David Baldiga. Together, they have driven forward various projects and innovations, contributing to the technological advancements at General Electric Company.

Conclusion

Brandon Allanson Reynolds exemplifies the spirit of innovation in the field of gas turbine technology. His 20 patents, including advancements in combustor deflectors and thermal expansion supports, demonstrate his commitment to improving performance and efficiency in engineering. With a background in collaboration and creativity, Brandon continues to push the boundaries of what is possible in his field.

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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