Avon, CT, United States of America

Francisco J Cunha

This inventor holds 22 USPTO granted patents and 2 published patent applications and 22 EPO patents, primarily in Turbine Blade Cooling. Top assignee: United Technologies Corporation. Active years: 2008-2014.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Francisco J Cunha. Retrieved from https://idiyas.com/inventor/francisco-j-cunha

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

USPTO Granted Patents = 22 

% Patents Active = 68.2

 

Average Co-Inventor Count = 1.5

ph-index = 10

Forward Citations = 321(Granted Patents)


Company Filing History:


Years Active: 2008-2014

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Areas of Expertise:
Turbofan Exhaust Assembly
Microcircuit Cooling
High Aspect Ratio Blades
Thermal Management
Airfoil Cooling
Gas Turbine Engine
Serpentine Microcircuits
Blade Cooling Techniques
Refractory Metal Core
Tip Blowing
Outflow Margin Protection
Vortex Turbulatons
22 patents (USPTO):Explore Patents

Title: **Innovative Contributions of Francisco J Cunha in Gas Turbine Technology**

Introduction

Francisco J Cunha, based in Avon, Connecticut, is a notable inventor with a remarkable portfolio of 22 patents primarily focused on advancements in gas turbine technology. His extensive work reflects a commitment to improving efficiency and performance in engineering applications.

Latest Patents

Among his latest inventions, Cunha introduced two significant patents:

1. **Elimination of Unfavorable Outflow Margin** - This innovation encompasses a panel designed for use in a gas turbine engine exhaust case. The panel features an airfoil section coupled with a flow-diverting structure near its leading edge, enabling efficient fluid flow into areas of the airfoil that may otherwise lack adequate internal pressure for effective cooling fluid circulation.

2. **Impingement Cooling for Turbofan Exhaust Assembly** - In this system, essential components such as a bypass duct, turbine case, turbine exhaust ring, and splash plate work in harmony. The design includes cooling fluid apertures within the turbine case to facilitate fluid flow from the bypass duct onto the splash plate, while impingement holes in the splash plate deliver cooling flow onto the turbine exhaust ring, enhancing overall cooling efficacy.

Career Highlights

Cunha has played a pivotal role at United Technologies Corporation, where he leverages his expertise to drive innovation in gas turbine technologies. His contributions not only demonstrate technical acumen but also a keen understanding of practical applications in the aerospace field.

Collaborations

Throughout his career, Francesco J Cunha has collaborated with eminent colleagues, including Timothy S Snyder and Matthew T Dahmer. These partnerships have led to further advancements in their collective projects and innovations.

Conclusion

Francisco J Cunha’s contributions to the field of gas turbine technology through his inventive patents signify him as a valuable asset to United Technologies Corporation. His work not only represents individual achievement but also the collaborative spirit inherent in engineering innovation. As he continues to develop new ideas, the impact of his inventions is sure to resonate within the industry for years to come.

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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