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. 10, 2022

Filed:

Jul. 04, 2019
Applicant:

Doosan Heavy Industries & Construction Co., Ltd., Changwon-si, KR;

Inventors:

Chad Garner, Jupiter, FL (US);

Andres Jaramillo, Jupiter, FL (US);

Assignee:

Other;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); B33Y 10/00 (2015.01); B33Y 80/00 (2015.01); F04D 29/32 (2006.01); F01D 5/28 (2006.01); B29C 70/30 (2006.01); B29C 64/165 (2017.01); B29C 64/118 (2017.01); B33Y 70/00 (2020.01); B29L 31/08 (2006.01); B29K 77/00 (2006.01); B29K 307/04 (2006.01);
U.S. Cl.
CPC ...
F01D 5/147 (2013.01); B29C 64/118 (2017.08); B29C 64/165 (2017.08); B33Y 10/00 (2014.12); B33Y 70/00 (2014.12); B33Y 80/00 (2014.12); B29K 2077/00 (2013.01); B29K 2307/04 (2013.01); B29L 2031/08 (2013.01); F05D 2220/32 (2013.01); F05D 2230/31 (2013.01); F05D 2300/603 (2013.01);
Abstract

A compressor blade of a gas turbine includes a compressor blade portion including a plurality of layers; and a carbon fiber reinforcement embedded in the plurality of layers of the compressor blade portion and oriented in a direction of stress fields of the compressor blade when in operation. A method of manufacturing the compressor blade includes preparing a composite material including fiber-reinforced layers; forming a first layer of the composite material to extend in a radial direction of the compressor blade; and stacking a second layer of the composite material on the first layer in an axial direction of the compressor blade. The compressor blade is 3D-printed by forming each composite material layer in a radial direction, which layers are stacked in an axial direction. Fiber reinforcement in the composite compressor blade is oriented in line with the stress fields inherent in the operation of the compressor blade.


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