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:
Dec. 23, 2014

Filed:

Mar. 21, 2014
Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

Thomas J. Praisner, Colchester, CT (US);

Shankar S. Magge, South Windsor, CT (US);

Matthew B. Estes, South Windsor, CT (US);

Assignee:

United Technologies Corporation, Hartford, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02D 1/00 (2006.01); F01D 9/04 (2006.01); F01D 25/28 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F01D 9/041 (2013.01); F01D 9/04 (2013.01); F01D 25/28 (2013.01); F02K 3/06 (2013.01);
Abstract

A gas turbine engine includes first and second stages having a rotational axis. A circumferential array of airfoils is arranged axially between the first stage and the second stage. At least one of the airfoils have a curvature provided equidistantly between pressure and suction sides. The airfoils extend from a leading edge to a trailing edge at a midspan plane along the airfoil. An angle is defined between first and second lines respectively tangent to the intersection of the midspan plane and the curvature at airfoil leading and trailing edges. The angle is equal to or greater than about 10°.


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