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. 16, 2018

Filed:

Nov. 24, 2014
Applicant:

Rolls-royce Deutschland Ltd & CO KG, Blankenfelde-Mahlow, Dahlewitz, DE;

Inventors:

Ioana Negulescu, Berlin, DE;

Peter Davison, Zossen, DE;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/10 (2006.01); F01D 5/08 (2006.01); F01D 5/26 (2006.01); F01D 11/00 (2006.01); F16F 15/10 (2006.01);
U.S. Cl.
CPC ...
F01D 5/08 (2013.01); F01D 5/082 (2013.01); F01D 5/26 (2013.01); F01D 11/008 (2013.01); F16F 15/10 (2013.01); F05D 2260/95 (2013.01); F05D 2260/96 (2013.01);
Abstract

A gas turbine engine including a rotor and a cooling fluid delivery system is presented. The rotor includes a disc and a plurality of blades extending radially therefrom. Each blade has a suction side and a pressure side and includes a shank, a platform and a main portion, the main portion being radially outward of the shank and separated therefrom by the platform. At least one cavity is defined, each radially inward of the platforms and between a suction side of the shank of one blade and a pressure side of the shank of an adjacent blade. The rotor includes at least one damper, the damper including a main body in contact with at least one blade and a deflector nose. The deflector nose extends from the main body into the cavity.


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