Middletown, CT, United States of America

Darryl Whitlow

This inventor holds 24 USPTO granted patents and 1 published patent application and 16 EPO patents, primarily in Gas Turbine Engine Design. Top assignees: United Technologies Corporation, Raytheon Technologies Corporation. Active years: 2015-2020.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Darryl Whitlow. Retrieved from https://idiyas.com/inventor/darryl-whitlow

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

USPTO Granted Patents = 24 

% Patents Active = 100.0

 

Average Co-Inventor Count = 6.1

ph-index = 7

Forward Citations = 121(Granted Patents)


Company Filing History:


Years Active: 2015-2020

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Areas of Expertise:
Gas Turbine
Engine Airfoil
Frequency Design
Chord Optimization
Aerodynamics
Performance Analysis
Fluid Dynamics
Thermal Efficiency
Mechanical Engineering
Structural Integrity
Turbomachinery
24 patents (USPTO):Explore Patents

Title: Darryl Whitlow: Innovator in Gas Turbine Engine Technology

Introduction

Darryl Whitlow is an accomplished inventor based in Middletown, Connecticut, USA, who has been granted 24 patents throughout his career. His innovative work primarily focuses on advancements in gas turbine engine technology, making significant contributions to the field that enhance efficiency and performance.

Latest Patents

Among his latest patents, Darryl has developed a groundbreaking gas turbine engine airfoil. This airfoil features a unique design where the pressure and suction sides extend radially from a 0% span position at an inner flow path location to a 100% span position at the airfoil tip. It incorporates a curve that represents the relationship between the trailing edge sweep angle and the span position, with the sweep angle varying from 0° to 10° within a 10-20% span position.

Another notable patent includes a design for gas turbine engine airfoil frequency. This turbomachine airfoil element comprises pressure and suction sides that span in thickness direction and connect at the leading and trailing edges. It extends radially between 27.5 inches and 28.5 inches, with a chord length of 13.0 inches to 14.0 inches at the 50% span. The frequency characteristics of the airfoil element pertain to multiple modes, including first, second, third, fourth, fifth, and sixth modes with specified frequencies.

Career Highlights

Darryl has had a distinguished career, having worked for prominent companies in the aerospace sector, such as United Technologies Corporation and Raytheon Technologies Corporation. His work in these organizations has allowed him to push the boundaries of turbine engine technology and innovate solutions that meet the demands of modern aviation.

Collaborations

Throughout his career, Darryl has collaborated with various talented professionals, including Edward J. Gallagher and Byron R. Monzon. These collaborations have enriched his work, enabling the sharing of ideas that lead to innovative designs and improvements in turbine engine components.

Conclusion

Darryl Whitlow's contributions to the field of gas turbine engine technology, exemplified by his multiple patents and collaborations, underscore his role as a significant innovator. His advancements in the design and functionality of airfoils not only reflect his expertise but also pave the way for future developments in aerospace technology.

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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