Middletown, CT, United States of America

Joseph C Straccia

This inventor holds 31 USPTO granted patents and 4 published patent applications and 12 EPO patents, primarily in Gas Turbine Engineering. Top assignees: United Technologies Corporation, Raytheon Technologies Corporation, Rtx Corporation. Active years: 2015-2024.

USPTO Granted Patents = 31 

% Patents Active = 100.0

 

Average Co-Inventor Count = 4.4

ph-index = 3

Forward Citations = 41(Granted Patents)


Location History:

  • Erie, CO (US) (2020)
  • Middletown, CT (US) (2015 - 2024)

Company Filing History:


Years Active: 2015-2024

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Areas of Expertise:
Gas Turbine Engine
Airfoil Design
Frequency Design
High-Turning Fan
Curved Airfoil
Incidence-Tolerant
High Order Shaped Curve
Stator Technology
Aerodynamic Performance
Engine Efficiency
Turbine Components
31 patents (USPTO):Explore Patents

Title: **Joseph C. Straccia: Innovator in Gas Turbine Technology**

Introduction

Joseph C. Straccia, based in Middletown, CT, has made significant contributions to the field of gas turbine engines with an impressive portfolio of 31 patents. His work exemplifies innovation in aerospace technology, particularly in improving the performance and efficiency of gas turbine engines.

Latest Patents

Among his latest patents is a groundbreaking design for a gas turbine engine airfoil. This innovative airfoil structure includes a combustor section strategically placed between a low-pressure compressor and a high-pressure compressor. The design features a fan section, where the low-pressure compressor is located downstream from the fan. The airfoil is designed to achieve optimal airflow with its pressure and suction sides extending radially from a 0% span position to a 100% span position. Notably, the airfoil showcases an axial stacking offset at a 10% span position, which is positive and exceeds the axial stacking offset at the 100% span position. This design contributes to the efficiency of the turbine system.

Another notable patent relates to an airfoil that demonstrates a relationship between the stagger angle and span position. This airfoil's geometry is defined by a stagger angle greater than 35° from 0% span to at least a 50% span, with the stagger angle at 100% span surpassing that at 50% span. These advancements underline Straccia's commitment to enhancing gas turbine engine performance.

Career Highlights

Joseph C. Straccia has built a robust career through his affiliations with prominent corporations in the aerospace industry. He has worked for United Technologies Corporation and Raytheon Technologies Corporation, where his innovative ideas contributed to their cutting-edge engineering projects.

Collaborations

Throughout his career, Straccia has collaborated with industry experts, including his notable coworkers Mark A. Stephens and Edward J. Gallagher. Their collective expertise has further advanced the innovation of gas turbine technologies.

Conclusion

Joseph C. Straccia's dedication to innovation and excellence in the field of gas turbine engines is reflected in his impressive patent portfolio and collaborations with leading companies. His contributions continue to influence the future of aerospace engineering, setting benchmarks for efficiency and performance in gas turbine technology.

Profile summary based on public USPTO records.
Please report any incorrect information to [email protected]
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