Indianapolis, IN, United States of America

Clark Snyder

This inventor holds 22 USPTO granted patents and 5 published patent applications, primarily in Turbine Shroud Assemblies. Top assignees: Rolls-Royce Corporation, Rolls-Royce High Temperature Composites Inc.. Active years: 2024-2026.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Clark Snyder. Retrieved from https://idiyas.com/inventor/clark-snyder-9w0yy1x8

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 = 95.5

Average Co-Inventor Count = 4.3

ph-index = 2

Forward Citations = 10(Granted Patents)


Company Filing History:


Years Active: 2024-2026

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Areas of Expertise:
Turbine Shroud
Ceramic Matrix Composite
Cooling Holes
Heat Shields
Anti-Migration Seals
Damping Strip Seals
Biasing Buffer
Thermal Management
Retention Plugs
Inter-Segment Seals
Locating Features
Strip Seals
22 patents (USPTO):Explore Patents

Title: Clark Snyder: Innovator in Turbine Technology

Introduction

Clark Snyder is a renowned inventor based in Indianapolis, IN, with an impressive portfolio of 11 patents. His innovative work primarily revolves around turbine shroud assemblies, contributing significantly to the field of gas turbine engine technology.

Latest Patents

His latest inventions include two noteworthy patents focusing on turbine shroud assemblies. The first patent, titled "Turbine shroud assemblies with channels for buffer cavity seal thermal management," presents a sophisticated assembly designed for gas turbine engines. This design boasts a carrier segment that encircles an axis, coupled with a blade track segment that defines part of the gas path. The innovative seal system integrates radially arranged seals between the carrier and blade track segments, effectively blocking gases from leaking.

The second patent, "Turbine shroud assemblies with rod seal and strip seals," also showcases an advanced turbine shroud assembly. This design includes a first and second shroud segment, along with multiple seals that extend circumferentially to prevent gas escape between the two segments. This groundbreaking work highlights Snyder’s commitment to enhancing efficiency within turbine systems.

Career Highlights

Throughout his career, Clark Snyder has lent his expertise to prominent organizations, notably Rolls-Royce Corporation and Rolls-Royce High Temperature Composites Inc. His contributions in these roles have been vital in advancing turbine technology, paving the way for innovations that improve the performance and reliability of gas turbines.

Collaborations

Snyder’s professional journey has been enriched by collaboration with talented peers, including David John Thomas and Ted Joseph Freeman. These partnerships have fostered a dynamic exchange of ideas, leading to collaborative innovations within the aerospace engineering field.

Conclusion

Clark Snyder’s impactful inventions and collaborations underscore his status as a significant contributor to turbine technology. With his ongoing commitment to innovation, Snyder continues to inspire the next generation of inventors in the field of gas turbine engineering.

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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