Coventry, CT, United States of America

Ricardo Trindade

This inventor holds 29 USPTO granted patents and 1 published patent application, plus 4 CIPO patents and 21 EPO patents, primarily in Gas Turbine Cooling. Top assignees: Raytheon Technologies Corporation, United Technologies Corporation, Pratt-Whitney Canada Corp. Active years: 2002-2024.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Ricardo Trindade. Retrieved from https://idiyas.com/inventor/ricardo-trindade

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 = 96.6


 

Average Co-Inventor Count = 3.7

ph-index = 10

Forward Citations = 243(Granted Patents)


Location History:

  • Montreal, CA (2002)
  • Conventry, CT (US) (2006)
  • Saint Lambert, CA (2006)
  • Coventry, CT (US) (2007 - 2019)
  • Mansfield, CT (US) (2019 - 2024)

Company Filing History:


Years Active: 2002-2024

Loading Chart...
Loading Chart...
Loading Chart...
Areas of Expertise:
Airfoil Design
Gas Turbine Engine
Cooling Configurations
Heat Transfer
Turbine Blade
Combustor Assembly
Impingement Cooling
Cooling Passage
Wavy Cooling Channels
Hybrid Cooling Schemes
Cooling Air Feed
Investment Casting
29 patents (USPTO):Explore Patents

Title: Innovations and Contributions of Ricardo Trindade

Introduction

Ricardo Trindade is a prolific inventor based in Coventry, Connecticut, who holds an impressive portfolio of 27 patents. His work predominantly focuses on advancements in gas turbine technology, showcasing his expertise in the aerospace and engineering sectors.

Latest Patents

Two of his latest patents exemplify his innovative approach to solving complex engineering challenges. The first patent involves a tip cooling design for an airfoil. In this design, the airfoil features a pressure side wall and a suction side wall that are circumferentially spaced apart. These walls extend radially between a root region and a tip region while also axially extending between a leading edge and trailing edge. This advanced design includes a gusset, a squealer pocket, and a tip pocket, enhancing the efficiency and cooling capabilities of the airfoil.

The second patent, titled "Redundant Entry Cooling Air Feed Hole Blockage Preventer for a Gas Turbine Engine," addresses critical aspects of cooling airflow in gas turbines. This innovative vane ring comprises multiple vanes extending between the inner and outer vane platforms. Each vane contains an airfoil cooling circuit that utilizes a series of feed passages, metering passages, and secondary passages to ensure optimal cooling performance and reliability in gas turbine operations.

Career Highlights

Throughout his career, Trindade has made significant contributions while working with renowned companies such as United Technologies Corporation and Raytheon Technologies Corporation. His expertise has allowed him to impact various projects that require innovative solutions in the aerospace and defense industries.

Collaborations

Trindade has worked alongside notable colleagues such as Steven Bruce Gautschi and Mark F. Zelesky. Together, they have collaborated on projects that push the boundaries of technology and foster advancements in the field.

Conclusion

Ricardo Trindade's contributions to the field of engineering and gas turbine technology through his 27 patents underline his status as a leading inventor. His innovative designs and collaborative efforts continue to influence the aerospace industry, paving the way for future advancements.

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]
Loading…