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For the Inventor, By the Inventor

Valley City, OH, United States of America

William S Blazek

USPTO Granted Patents = 16

Average Co-Inventor Count = 1.2

ph-index = 9

Forward Citations = 189(Granted Patents)


Company Filing History:

goldMedal12 out of 3,081 
 
Trw Limited
 patents
silverMedal4 out of 54 
 
Pcc Airfoils, Inc.
 patents

Years Active: 1977-1993

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16 patents (USPTO):Explore Patents
1. 5181550 - Method of making a turbine engine component (1993-01-26),
2. 5069265 - Method of making a turbine engine component (1991-12-03),
3. 4961459 - Method of making an improved turbine engine component (1990-10-09),
4. 4955423 - Method of making a turbine engine component (1990-09-11),
5. 4850419 - Method of casting a one-piece wheel (1989-07-25),
6. 4728258 - Turbine engine component and method of making the same (1988-03-01),
7. 4702298 - Method of assembling molds (1987-10-27),
8. 4572275 - Apparatus for use in casting an article (1986-02-25),
9. 4449567 - Method and apparatus for use in casting an article (1984-05-22),
10. 4315537 - Method of making a mold (1982-02-16),
11. 4224976 - Method of assembling molds (1980-09-30),
12. 4195683 - Method of forming metal article having plurality of airfoils extending (1980-04-01),
13. 4195396 - Method of forming an airfoil with inner and outer shroud sections (1980-04-01),
14. 4170256 - Mold assembly and method of making the same (1979-10-09),
15. 4066116 - Mold assembly and method of making the same (1978-01-03),

Title: The Innovative Contributions of William S. Blazek

Introduction

William S. Blazek is a notable inventor based in Valley City, OH, who has made significant contributions to the field of turbine engine components. With a total of 16 patents to his name, Blazek's work has advanced the technology used in modern turbine engines, showcasing his expertise and innovative spirit.

Latest Patents

Among his latest patents, Blazek has developed methods for making turbine engine components that enhance performance and durability. One of his notable inventions involves forming a heat-resistant layer on each airfoil of a plurality of airfoils. This layer has a higher melting temperature than the material forming the airfoil, allowing for improved thermal resistance. The process includes pouring molten metal into a mold formed around the airfoils, resulting in a shroud ring that is free of bonds at the slip joints. Another patent details a method for creating an annular array of airfoils that accommodate thermal expansion, ensuring the reliability of turbine engine components under varying conditions.

Career Highlights

Blazek has worked with prominent companies in the aerospace industry, including TRW Limited and PCC Airfoils, Inc. His experience in these organizations has allowed him to refine his skills and contribute to cutting-edge projects in turbine technology. His patents reflect a deep understanding of the complexities involved in turbine engine design and manufacturing.

Collaborations

Throughout his career, Blazek has collaborated with talented individuals such as Thomas S. Piwonka and James D. Jackson. These partnerships have fostered an environment of innovation and creativity, leading to advancements in turbine engine technology.

Conclusion

William S. Blazek's contributions to the field of turbine engine components are significant and impactful. His innovative patents and collaborations highlight his dedication to advancing technology in the aerospace industry. Blazek's work continues to influence the design and functionality of turbine engines, ensuring their efficiency and reliability for future applications.

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