Thurman Carlo Dabbs

This inventor holds 13 USPTO granted patents and 1 published patent application and 8 EPO patents. Top assignee: United Technologies Corporation. Active years: 2010-2020.

USPTO Granted Patents = 13 (Patent Applications = 1)

% Patents Active = 84.6

EPO Patents = 8 (Patent Applications = 9)

Average Co-Inventor Count = 3.8

ph-index = 6

Forward Citations = 163(Granted Patents)

Company Filing History:

13 out of 10,655

United Technologies Corporation

patents

Years Active: 2010-2020

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13 patents (USPTO):Sort by Forward CitationsExplore Patents

1. 10619504 - Gas turbine engine blade outer air seal cooling hole configuration (2020-04-14),

2. 10557366 - Boas having radially extended protrusions (2020-02-11),

3. 10378371 - Anti-rotation vane (2019-08-13),

4. 10196917 - Blade outer air seal with cored passages (2019-02-05),

5. 10077680 - Blade outer air seal assembly and support (2018-09-18),

6. 10018068 - Blade outer air seal with cooling holes (2018-07-10),

7. 9869202 - Blade outer air seal for a gas turbine engine (2018-01-16),

8. 9810088 - Floating blade outer air seal assembly for gas turbine engine (2017-11-07),

9. 9103225 - Blade outer air seal with cored passages (2015-08-11),

10. 8998572 - Blade outer air seal for a gas turbine engine (2015-04-07),

11. 8961108 - Cooling system for a turbine vane (2015-02-24),

12. 8876458 - Blade outer air seal assembly and support (2014-11-04),

13. 7770375 - Particle collector for gas turbine engine (2010-08-10),

Title: The Innovative Contributions of Thurman Carlo Dabbs

Introduction

Thurman Carlo Dabbs is a notable inventor based in Dover, NH (US), recognized for his significant contributions to engineering and technology. With a total of 13 patents to his name, Dabbs has made remarkable advancements in the field of gas turbine engine design.

Latest Patents

One of his latest patents is focused on a gas turbine engine blade outer air seal cooling hole configuration. This innovative design features a blade outer air seal that includes a body extending axially between forward and aft rails, with an inner arcuate surface that effectively seals relative to a blade tip. The body is equipped with multiple cooling holes that penetrate through its exterior surface, strategically placed according to specific geometric coordinates. Another notable patent involves a blade outer air seal comprising an arcuate segment with an aft wall that has a radially extending protrusion. This design enhances the functionality and efficiency of gas turbine engines.

Career Highlights

Throughout his career, Dabbs has worked with prominent companies such as United Technologies Corporation and Raytheon Technologies Corporation. His experience in these leading organizations has allowed him to refine his skills and contribute to groundbreaking projects in the aerospace and defense sectors.

Collaborations

Dabbs has collaborated with esteemed colleagues, including Paul M Lutjen and Bruce E Chick, further enriching his work and expanding the impact of his inventions.

Conclusion

Thurman Carlo Dabbs stands out as a significant figure in the realm of innovation, with his patents reflecting a deep understanding of engineering principles and a commitment to advancing technology. His contributions continue to influence the industry and inspire future inventors.