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:
Apr. 12, 2016

Filed:

Feb. 22, 2013
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Ross Ashely Spoonire, Albany, NY (US);

Wendy Wen-Ling Lin, Niskayuna, NY (US);

Jan Christopher Schilling, Liberty Township, OH (US);

Dong Jin Shim, Niskayuna, NY (US);

Gregory Carl Gemeinhardt, Cincinnati, OH (US);

Prakash Kashiram Jadhav, Bangalore, IN;

Assignee:

General Electric Company, Niskayuna, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F01D 5/28 (2006.01); F04D 29/32 (2006.01); F04D 29/02 (2006.01);
U.S. Cl.
CPC ...
F01D 5/282 (2013.01); F04D 29/023 (2013.01); F04D 29/324 (2013.01); F01D 5/288 (2013.01); F05D 2220/36 (2013.01); Y02T 50/672 (2013.01); Y02T 50/673 (2013.01); Y10T 156/10 (2015.01); Y10T 156/1002 (2015.01);
Abstract

A hybrid turbine blade and method of fabrication, comprising a shank portion and an airfoil portion. The airfoil portion comprising a composite outer structure having a recess formed therein and an alternating stack of at least one composite section and at least two insert sections disposed in the recess. The outer composite structure and the at least one composite section having a first density. The at least two insert sections having a second mass density, which is less than the first mass density. The composite outer structure and the alternating stack of at least one composite section and at least two insert sections together define an airfoil portion that meets all mechanical load carrying requirements of said hybrid turbine blade such that no load transfer needs to occur through said at least two insert sections.


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