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.:

US 9494053 B1

PDF
Full Text
Expired
Date of Patent:
Nov. 15, 2016

Filed:

Sep. 23, 2013
Applicant:

John A. Orosa, Palm Beach Gardens, FL (US);

Inventor:

John A. Orosa, Palm Beach Gardens, FL (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/30 (2006.01); F01D 17/16 (2006.01); F01D 17/14 (2006.01);
U.S. Cl.
CPC ...
F01D 25/30 (2013.01); F01D 17/143 (2013.01); F01D 17/16 (2013.01); F05D 2220/32 (2013.01); F05D 2240/122 (2013.01); F05D 2240/127 (2013.01); F05D 2250/70 (2013.01);
Abstract

A gas turbine engine includes inner and outer shrouds forming an annular gas path, and a plurality of struts connecting the inner shroud to the outer shroud. Airfoil shaped shields surround the struts, and each of the shields include a main body having an upstream leading edge defining a chordal axis extending in a downstream axial direction from the leading edge toward a downstream end of the shield. A trailing edge flap is located at the downstream end of each shield, the trailing edge flap including first and second span-wise portions. The first span-wise portion is oriented to direct flow at an angle relative to the chordal axis of the main body and the second span-wise portion is oriented to direct flow in a direction that is at a different angle than the angle of first span-wise portion.


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