Glastonbury, CT, United States of America

David P Houston

This inventor holds 23 USPTO granted patents and 11 published patent applications, plus 2 CIPO patents and 11 EPO patents, primarily in Gas Turbine Engineering. Top assignees: United Technologies Corporation, Raytheon Technologies Corporation. Active years: 1994-2021.

IDiyas Innovation Intelligence. (2026). Inventor Profile: David P Houston. Retrieved from https://idiyas.com/inventor/david-p-houston

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

USPTO Granted Patents = 23 

% Patents Active = 100.0


 

Average Co-Inventor Count = 3.0

ph-index = 9

Forward Citations = 322(Granted Patents)


Company Filing History:


Years Active: 1994-2021

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Areas of Expertise:
Turbomachine Blade
Gas Turbine Engine
Geared Turbofan
Airfoil
Fatigue Strength
Rotor Stack Assembly
Damper
Seal Assembly
Blade Platform
Root Design
Lifing Calculations
23 patents (USPTO):Explore Patents

Title: David P. Houston: Innovator in Turbomachinery

Introduction

David P. Houston, an accomplished inventor based in Glastonbury, Connecticut, has made significant contributions to the field of turbomachinery. With a remarkable portfolio of 23 patents, Houston stands out for his innovative designs and engineering solutions that enhance the efficiency of gas turbine engines.

Latest Patents

Among his latest inventions, the "Turbomachine Blade" patent presents a cutting-edge design for a turbomachine airfoil element. This airfoil features specific dimensions with a span between the inboard and outboard ends measuring 1.4 to 1.6 inches, and a chord length at 50% span of 0.9 to 1.4 inches. The remanufactured element is critically defined by its resonance frequencies, which include first, second, third, fourth, and fifth modes at approximately 2591.5 Hz, 4675.2 Hz, 7892.9 Hz, 10098.2 Hz, and 14808.2 Hz, respectively.

Another noteworthy patent is the "Gas Turbine Engine with Lifting Calculations Based upon Actual Usage." This innovative method monitors gas turbine engine health by analyzing actual flight data, including ambient temperatures and internal engine pressures. The procedure assesses accumulated damage on engine components and refines recommendations for future usage based on the gathered data.

Career Highlights

David P. Houston has a noteworthy career with key positions at prestigious organizations such as United Technologies Corporation and Raytheon Technologies Corporation. His work in these companies has been instrumental in advancing turbomachinery technologies and solutions.

Collaborations

Throughout his career, Houston has collaborated with talented professionals, including Frederick M. Schwarz and Tracy A. Propheter-Hinckley. These partnerships have undoubtedly contributed to the innovative outcomes of his projects and patents.

Conclusion

David P. Houston exemplifies the spirit of innovation in the turbomachinery sector. With his extensive patent portfolio and collaborative work, he continues to influence the field significantly. His dedication to enhancing gas turbine engine technology ensures that he remains a prominent figure in engineering 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]
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