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:
May. 01, 2018

Filed:

Dec. 18, 2013
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventor:

Daniel F. Palmer, East Hampton, CT (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16N 3/02 (2006.01); F01D 5/00 (2006.01); F01D 5/30 (2006.01); B05B 7/24 (2006.01); F01D 25/18 (2006.01); F16N 3/00 (2006.01);
U.S. Cl.
CPC ...
F16N 3/02 (2013.01); B05B 7/2402 (2013.01); F01D 5/005 (2013.01); F01D 5/3092 (2013.01); F01D 25/18 (2013.01); F05D 2220/32 (2013.01); F05D 2220/36 (2013.01); F05D 2240/30 (2013.01); F05D 2260/98 (2013.01); F16N 3/00 (2013.01);
Abstract

In accordance with one aspect of the disclosure, a lubricant application device for providing lubricant to an airfoil of a gas turbine engine is disclosed. The device may include a container for holding a lubricant, a fluid outlet in fluid communication with the container, a discharge mechanism controlling a flow of the lubricant from the container to the fluid outlet, and an extension tube in fluid communication with the fluid outlet. When the discharge mechanism is activated the lubricant may flow out of the container and through the extension tube. The extension tube may be dimensioned to fit between an airfoil root and rotor cavity of a gas turbine engine.


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