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. 10, 2019

Filed:

May. 02, 2016
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Dominic J. Mongillo, West Hartford, CT (US);

Parth Jariwala, Iselin, NJ (US);

Bret M. Teller, Meriden, CT (US);

Mark F. Zelesky, Bolton, CT (US);

James Tilsley Auxier, Bloomfield, CT (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); F01D 25/12 (2006.01); F04D 29/32 (2006.01); F04D 29/58 (2006.01); F01D 9/02 (2006.01); F04D 29/54 (2006.01);
U.S. Cl.
CPC ...
F01D 5/187 (2013.01); F01D 9/02 (2013.01); F01D 25/12 (2013.01); F04D 29/324 (2013.01); F04D 29/542 (2013.01); F04D 29/582 (2013.01); F05D 2220/32 (2013.01); F05D 2250/185 (2013.01); F05D 2260/202 (2013.01); F05D 2260/22141 (2013.01); F05D 2260/606 (2013.01);
Abstract

An airfoil of a gas turbine engine is provided including a leading edge extending in a radial direction, a tip extending in an axial direction from the leading edge, a first rib extending radially within the airfoil, the leading edge and the first rib defining a leading edge cavity within the airfoil, a second rib, the second rib and the first rib defining a serpentine cavity therein, a third rib extending axially within the tip, a flag tip cavity defined by the third rib, the leading edge, and the tip, the leading edge cavity fluidly connected to the flag tip cavity, and a bypass aperture formed between the first rib and the third rib, the bypass aperture configured to fluidly connect the serpentine cavity with the flag tip cavity.


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