Rexford, NY, United States of America

Michal Osusky

This inventor holds 2 USPTO granted patents and 4 published patent applications. Top assignee: General Electric Company. Active years: 2026.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Michal Osusky. Retrieved from https://idiyas.com/inventor/michal-osusky

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

Calculating rank
USPTO Granted Patents = 2 

% Patents Active = 50.0

Average Co-Inventor Count = 3.0

ph-index = 1


Company Filing History:


Years Active: 2026

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2 patents (USPTO):Explore Patents

Title: Michal Osusky: Gas Turbine Patent Inventor.

Introduction

Michal Osusky is an inventor associated with Rexford, New York, and General Electric Company. His patent work addresses the alignment of turbine nozzles with the combustor in gas turbine engines. The available information lists 1 patent for him.

Latest Patents

Osusky’s listed patent, “Turbine Nozzle Alignment with Combustor of Gas Turbine Engines,” describes a gas turbine engine with compressor, combustion, and turbine sections arranged along a central axis. The combustion section has multiple fuel nozzles communicating with the combustion chamber, while the turbine section includes vanes and rotor blades. The invention defines a clocking pitch fraction between a peak-temperature region and the midpoint of a vane pitch, relating the turbine vane arrangement to the fuel-nozzle layout.

Career Highlights

Osusky’s listed patent connects his inventive work with gas turbine engineering at General Electric Company. Its subject matter focuses on coordinating combustor fuel-nozzle positioning with turbine vane placement.

Collaborations

The provided information names Jonathan A. Filipa and Paul Hadley Vitt as Osusky’s coworkers. Their shared association points to a professional environment involving gas turbine technology and patent development.

Conclusion

Michal Osusky’s listed patent concerns the alignment of turbine nozzles and combustor components, reflecting a focused contribution to gas turbine engine design.

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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