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For the Inventor, By the Inventor

Mason, OH, United States of America

Judd Dodge Tressler

This inventor holds 13 USPTO granted patents. Top assignee: General Electric Company. Active years: 2000-2009.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Judd Dodge Tressler. Retrieved from https://idiyas.com/inventor/judd-dodge-tressler

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

USPTO Granted Patents = 13

% Patents Active = 92.3

Average Co-Inventor Count = 2.4

ph-index = 10

Forward Citations = 381(Granted Patents)


Company Filing History:

goldMedal13 out of 52,387 
 
General Electric Company
 patents

Years Active: 2000-2009

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13 patents (USPTO):Explore Patents
1. RE40658 - Methods and apparatus for cooling gas turbine nozzles (2009-03-09),
2. RE39479 - Durable turbine nozzle (2007-01-22),
3. RE39320 - Thermal barrier coating wrap for turbine airfoil (2006-10-02),
4. 6910868 - Airfoil shape for a turbine bucket (2005-06-28),
5. 6652235 - Method and apparatus for reducing turbine blade tip region temperatures (2003-11-25),
6. 6652220 - Methods and apparatus for cooling gas turbine nozzles (2003-11-25),
7. 6609880 - Methods and apparatus for cooling gas turbine nozzles (2003-08-26),
8. 6602047 - Methods and apparatus for cooling gas turbine nozzles (2003-08-05),
9. 6382914 - Cooling medium transfer passageways in radial cooled turbine blades (2002-05-07),
10. 6382908 - Nozzle fillet backside cooling (2002-05-07),
11. 6382906 - Floating spoolie cup impingement baffle (2002-05-07),
12. 6183192 - Durable turbine nozzle (2001-02-06),
13. 6126400 - Thermal barrier coating wrap for turbine airfoil (2000-10-03),

Title: Innovations of Judd Dodge Tressler

Introduction

Judd Dodge Tressler is a notable inventor based in Mason, OH (US). He has made significant contributions to the field of gas turbine technology, holding a total of 13 patents. His work focuses on improving the efficiency and durability of turbine nozzles, which are critical components in gas turbine engines.

Latest Patents

Among his latest patents is a method for assembling a turbine nozzle for a gas turbine engine. This innovative method enhances the cooling efficiency of the turbine nozzle. It involves providing a hollow doublet that includes a leading airfoil and a trailing airfoil, coupled by at least one platform. Each airfoil features a first sidewall and a second sidewall extending between respective leading and trailing edges. The method also includes inserting an insert into at least one of the airfoils, which contains a first sidewall with a first plurality of cooling openings and a second sidewall with a second plurality of cooling openings. This design facilitates improved cooling of the airfoil. Another significant patent is for a durable turbine nozzle that consists of a plurality of vanes joined at opposite ends to outer and inner bands. The inner band features a forward hook that is segmented to reduce thermal mismatch, and the vane includes an impingement baffle for preferential cooling.

Career Highlights

Judd Tressler is currently employed at General Electric Company, where he continues to innovate in the field of turbine technology. His work has been instrumental in advancing the efficiency and reliability of gas turbine engines.

Collaborations

Throughout his career, Tressler has collaborated with notable colleagues, including Glenn Herbert Nichols and Andrew Charles Powis. Their combined expertise has contributed to the development of cutting-edge technologies in the industry.

Conclusion

Judd Dodge Tressler's contributions to gas turbine technology through his innovative patents and collaborations highlight his significant role in the field. His work continues to influence advancements in turbine efficiency and durability.

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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