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. 09, 2018

Filed:

Jan. 22, 2013
Applicants:

Mrinal Munshi, Orlando, FL (US);

John W. Finneran, Palm Beach Gardens, FL (US);

Yevgeniy Shteyman, West Palm Beach, FL (US);

Daryl J. Graber, Palm Beach Gardens, FL (US);

Matthew R. Porter, West Palm Beach, FL (US);

Jonathan M. Leagon, Cassatt, SC (US);

Inventors:

Mrinal Munshi, Orlando, FL (US);

John W. Finneran, Palm Beach Gardens, FL (US);

Yevgeniy Shteyman, West Palm Beach, FL (US);

Daryl J. Graber, Palm Beach Gardens, FL (US);

Matthew R. Porter, West Palm Beach, FL (US);

Jonathan M. Leagon, Cassatt, SC (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 9/06 (2006.01); F01D 25/14 (2006.01); F01D 25/16 (2006.01); F02C 7/12 (2006.01); F01D 25/12 (2006.01); F01D 25/30 (2006.01);
U.S. Cl.
CPC ...
F02C 7/12 (2013.01); F01D 9/065 (2013.01); F01D 25/12 (2013.01); F01D 25/145 (2013.01); F01D 25/162 (2013.01); F01D 25/30 (2013.01); F05D 2240/128 (2013.01); F05D 2240/15 (2013.01);
Abstract

A gas turbine engine including an outer case and an exhaust gas passage defined within the outer case for conducting an exhaust gas flow from a turbine section of the gas turbine engine. A cooling channel is associated with an outer surface of the outer case, the cooling channel having a channel inlet and a channel outlet. An air duct structure is provided and includes an inlet end in fluid communication with the channel outlet and includes an outlet end in fluid communication with an area of reduced pressure relative to the air duct structure inlet end. An exit cavity is located at the air duct structure outlet end, wherein the exit cavity effects a reduced pressure at the outlet end to draw air from the cooling channel into the air duct.


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