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:
Dec. 12, 2023

Filed:

Mar. 09, 2021
Applicant:

Mechanical Dynamics and Analysis Llc, Latham, NY (US);

Inventors:

Leissner F. Poth, III, San Antonio, TX (US);

Sanjay S. Hingorani, Johns Creek, GA (US);

Bensy Samuel, Alpharetta, GA (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); F01D 5/20 (2006.01); F01D 5/30 (2006.01);
U.S. Cl.
CPC ...
F01D 5/187 (2013.01); F01D 5/20 (2013.01); F01D 5/3007 (2013.01); F05D 2220/32 (2013.01); F05D 2230/80 (2013.01); F05D 2240/307 (2013.01); F05D 2260/20 (2013.01);
Abstract

A turbine blade includes a blade tip defining pressure side cooling apertures. The turbine blade defines a serpentine cooling passage having a first, second, and third legs, and first and second junction portions. The first leg extends radially and is connected to the second leg by the first junction portion proximate the blade tip. The second leg extends radially between the first and second junction portions. The second junction portion connects the second leg to the third leg which extends radially toward the blade tip and is connected to a trailing edge cooling aperture to exhaust the gas to an exterior of the turbine blade. The turbine blade defines a plenum connected to the first junction portion. At least one tip cooling aperture connects to the plenum and is radially outward of the third leg and axially aftward of at least a portion of the third leg.


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