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.
Patent No.:
Date of Patent:
Mar. 16, 2021
Filed:
May. 02, 2017
Applicant:
Unison Industries, Llc, Jacksonville, FL (US);
Inventors:
Yanzhe Yang, Waynesville, OH (US);
Daniel Dyer, Dayton, OH (US);
Armando Bringas, Querétaro, MX;
Jason Levi Burdette, Beavercreek, OH (US);
Gordon Tajiri, Allentown, PA (US);
Dattu GV Jonnalagadda, Ponnur, IN;
Michael Thomas Kenworthy, Gilbert, AZ (US);
Assignee:
Unison Industries, LLC, Jacksonville, FL (US);
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F16L 9/00 (2006.01); B22F 5/10 (2006.01); F28D 7/10 (2006.01); F02C 7/14 (2006.01); F16L 27/111 (2006.01); F02C 6/08 (2006.01); B23P 15/00 (2006.01); F28F 1/06 (2006.01); F02C 7/18 (2006.01); B22F 3/105 (2006.01); B22F 5/00 (2006.01); B64D 13/06 (2006.01); F16L 9/02 (2006.01); F16L 51/02 (2006.01); F28D 7/16 (2006.01);
U.S. Cl.
CPC ...
F16L 9/006 (2013.01); B22F 5/106 (2013.01); B23P 15/00 (2013.01); F02C 6/08 (2013.01); F02C 7/14 (2013.01); F02C 7/185 (2013.01); F16L 27/111 (2013.01); F28D 7/106 (2013.01); F28F 1/06 (2013.01); B22F 3/1055 (2013.01); B22F 5/009 (2013.01); B22F 2005/103 (2013.01); B22F 2998/10 (2013.01); B22F 2999/00 (2013.01); B64D 13/06 (2013.01); F05D 2220/32 (2013.01); F05D 2230/22 (2013.01); F05D 2230/31 (2013.01); F05D 2230/642 (2013.01); F05D 2250/12 (2013.01); F05D 2250/13 (2013.01); F05D 2250/131 (2013.01); F05D 2250/25 (2013.01); F05D 2250/75 (2013.01); F05D 2260/60 (2013.01); F16L 9/02 (2013.01); F16L 51/025 (2013.01); F28D 7/1615 (2013.01); F28F 2210/06 (2013.01);
Abstract
A duct for a turbine engine, such as a gas turbine engine, can be utilized to carry a fluid from one portion of the engine to another. The duct can include a metallic tubular element having one of a varying wall thickness, a varying cross section, or a tight bend. Such a duct can be formed utilizing additive manufacturing or metal deposition on an additively manufactured mandrel.