The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
May. 27, 2025

Filed:

May. 04, 2022
Applicants:

Agency for Defense Development, Daejeon, KR;

Industry-academic Cooperation Foundation, Yonsei University, Seoul, KR;

Inventors:

Jeong-Woo Kim, Daejeon, KR;

Hyung-Hee Cho, Seoul, KR;

Joo-Hyoung Lee, Seoul, KR;

Min-Ho Bang, Seoul, KR;

Jeong-Ju Kim, Seoul, KR;

Seung-Yeong Choi, Seoul, KR;

Tae-Hyun Kim, Seoul, KR;

Hee-Seung Park, Seoul, KR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/20 (2006.01); F01D 5/14 (2006.01); F01D 5/18 (2006.01);
U.S. Cl.
CPC ...
F01D 5/20 (2013.01); F01D 5/14 (2013.01); F01D 5/141 (2013.01); F01D 5/18 (2013.01); F05D 2220/32 (2013.01); F05D 2240/307 (2013.01); F05D 2240/55 (2013.01); F05D 2260/20 (2013.01);
Abstract

The present invention relates to a gas turbine blade having a shelf squealer tip, the gas turbine blade including an airfoil-shaped blade housing, and a squealer tip extending from an edge portion of a tip surface that is an end surface of the blade housing, in which the squealer tip is formed only on a part of the edge portion of the tip surface. According to the present invention, it is possible to maximize film-cooling performance on the tip surface and additionally reduce an aerodynamic loss by suppressing high-temperature main flow reattachment and swirl flow generation on the tip surface.


Find Patent Forward Citations

Loading…