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:
Oct. 22, 2019

Filed:

Mar. 17, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Alan Scott Grissino, Amesbury, MA (US);

John Alan Manteiga, North Andover, MA (US);

Jonathan Harry Kerner, Brookline, MA (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/047 (2006.01); B64D 15/04 (2006.01); B64D 33/02 (2006.01); F02C 7/05 (2006.01); F04D 29/52 (2006.01); F02C 6/08 (2006.01); F02C 7/055 (2006.01);
U.S. Cl.
CPC ...
F02C 7/047 (2013.01); B64D 15/04 (2013.01); B64D 33/02 (2013.01); F02C 6/08 (2013.01); F02C 7/05 (2013.01); F02C 7/055 (2013.01); F04D 29/522 (2013.01); B64D 2033/022 (2013.01); B64D 2033/0233 (2013.01); B64D 2033/0246 (2013.01); B64D 2033/0293 (2013.01); F05D 2220/32 (2013.01); F05D 2240/129 (2013.01); F05D 2270/11 (2013.01); Y02T 50/671 (2013.01);
Abstract

An apparatus for providing foreign object debris protection and anti-icing capabilities to an air intake of an aircraft engine. The apparatus includes a frame having at least a portion configured to conduct fluids. A tube is positioned such that different portions of the frame are fluidly connected. There is a discharge outlet defined within the frame that is configured to discharge fluids from the frame into the air intake. An inlet is defined within the frame and is fluidly connected to a compressor section of the aircraft engine. In this manner, air from the compressor section of the aircraft engine can flow through the inlet, through the tube, and through the discharge outlet, to return to the compressor section of the aircraft engine.


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