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:
Jun. 12, 2018

Filed:

Apr. 26, 2013
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Mustafa Dindar, Cincinnati, OH (US);

Vaughn Ray Kunze, Cincinnati, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 1/38 (2006.01); F02K 1/46 (2006.01); F02K 1/34 (2006.01); F02K 1/48 (2006.01); B64D 33/04 (2006.01); F02K 1/82 (2006.01);
U.S. Cl.
CPC ...
F02K 1/386 (2013.01); B64D 33/06 (2013.01); F02K 1/46 (2013.01); F02K 1/48 (2013.01); B64D 2033/045 (2013.01); F02K 1/38 (2013.01); F02K 1/827 (2013.01); F05D 2230/20 (2013.01); F05D 2230/60 (2013.01); F05D 2250/184 (2013.01); F05D 2250/61 (2013.01); F05D 2250/611 (2013.01); F05D 2250/70 (2013.01); F05D 2250/71 (2013.01); F05D 2260/96 (2013.01); F05D 2300/6033 (2013.01); Y02T 50/672 (2013.01); Y10T 29/49234 (2015.01);
Abstract

A method of fabricating a mixer for a gas turbine engine is provided. The method includes forming a forward end and an aft end of the mixer, and forming an annularly undulating contour that defines a plurality of core immersion lobes and a plurality of bypass immersion lobes between the forward end and the aft end. The plurality of bypass immersion lobes includes a first bypass immersion lobe and a second bypass immersion lobe. The first bypass immersion lobe has a first crown contour line extending from the forward end to the aft end of the mixer, and the second bypass immersion lobe has a second crown contour line extending from the forward end to the aft end of the mixer. The first crown contour line is different than the second crown contour line.


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