Superior, CO, United States of America

Kate Hudon

This inventor holds 29 USPTO granted patents and 4 published patent applications and 10 EPO patents, primarily in Gas Turbine Design. Top assignees: Raytheon Technologies Corporation, United Technologies Corporation, Rtx Corporation. Active years: 2017-2024.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Kate Hudon. Retrieved from https://idiyas.com/inventor/kate-hudon

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

USPTO Granted Patents = 29 

% Patents Active = 100.0

 

Average Co-Inventor Count = 5.4

ph-index = 3

Forward Citations = 25(Granted Patents)


Company Filing History:


Years Active: 2017-2024

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Areas of Expertise:
Gas Turbine
Airfoil
Frequency Design
Aerodynamic Efficiency
Engine Performance
Turbine Blade
Flow Dynamics
Thermal Management
Mechanical Structure
Fluid Mechanics
Aerospace Engineering
Performance Optimization
29 patents (USPTO):Explore Patents

Title: Insights into the Innovations of Kate Hudon

Introduction

Kate Hudon, an accomplished inventor based in Superior, Colorado, has made significant contributions to the field of gas turbine engine technology. With an impressive portfolio of 29 patents, Hudon's work reflects a deep commitment to innovation and engineering excellence.

Latest Patents

Among her latest patents is a groundbreaking design for a gas turbine engine airfoil. This design features a combustor section strategically positioned between a compressor section and a turbine section. The compressor includes both a low-pressure and a high-pressure component, with the latter located upstream of the combustor. The invention emphasizes an airfoil structure that integrates pressure and suction sides extending radially from a 0% span position to a 100% span position. It includes a notable axial stacking offset at the 10% span position, which is not only positive but also greater than or equal to the offset at the 100% span position. Additionally, another patent details an airfoil with a stagger angle significantly greater than 35° from the 0% to at least the 50% span, ensuring optimal functionality in gas turbine engines.

Career Highlights

Hudon's career has been distinguished by her tenure at leading aerospace companies, including Raytheon Technologies Corporation and United Technologies Corporation. Her work has contributed to advancements in turbine technology, showcasing her expertise in optimizing engine efficiency and performance.

Collaborations

Throughout her career, Hudon has collaborated with esteemed professionals such as Edward J. Gallagher and Lisa I. Brilliant. These partnerships have undoubtedly enriched her work, leading to innovative solutions and successful patent applications in the aerospace domain.

Conclusion

Kate Hudon stands out as a leading innovator in the field of gas turbine engine technology. Her extensive patent portfolio and collaborative spirit highlight her dedication to advancing engineering solutions. As the aviation industry continues to evolve, Hudon's contributions will likely play a vital role in pushing the boundaries of performance and efficiency in aerospace engineering.

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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