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. 14, 2016

Filed:

Feb. 14, 2013
Applicants:

Rajesh Rajaram, Oviedo, FL (US);

Juan Enrique Portillo Bilbao, Oviedo, FL (US);

Danning You, Shanghai, CN;

Inventors:

Rajesh Rajaram, Oviedo, FL (US);

Juan Enrique Portillo Bilbao, Oviedo, FL (US);

Danning You, Shanghai, CN;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/26 (2006.01); F23R 3/10 (2006.01); F23R 3/46 (2006.01); F23R 3/54 (2006.01);
U.S. Cl.
CPC ...
F23R 3/26 (2013.01); F23R 3/10 (2013.01); F23R 3/46 (2013.01); F23R 3/54 (2013.01); F23R 2900/00014 (2013.01); F23R 2900/03043 (2013.01);
Abstract

A combustor assembly in a gas turbine engine includes a liner defining a combustion zone, at least one fuel injector for providing fuel, and a flow sleeve. An inner surface of the flow sleeve defines an outer boundary for an air flow passageway. Upon the air reaching a head end of the combustor assembly at an end of the air flow passageway the air turns 180 degrees to flow into the combustion zone where it is burned with the fuel. The combustor assembly further includes an inlet assembly positioned radially between the liner and the flow sleeve. The inlet assembly defines an inlet to the air flow passageway and includes a plurality of overlapping conduits that are arranged such that the air entering the air flow passageway passes through radial spaces between adjacent conduits.


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