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:
Feb. 13, 2018

Filed:

Aug. 31, 2015
Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

Michael G. McCaffrey, Windsor, CT (US);

Elizabeth F. Vinson, Wethersfield, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/08 (2006.01); F01D 5/18 (2006.01); F02C 3/04 (2006.01); F04D 29/32 (2006.01); F04D 29/053 (2006.01); F04D 29/58 (2006.01);
U.S. Cl.
CPC ...
F01D 5/187 (2013.01); F01D 5/082 (2013.01); F02C 3/04 (2013.01); F04D 29/053 (2013.01); F04D 29/321 (2013.01); F04D 29/584 (2013.01); F05D 2220/32 (2013.01); F05D 2240/60 (2013.01); F05D 2260/201 (2013.01); Y02T 50/676 (2013.01);
Abstract

A gas turbine engine includes a compressor section, a combustor fluidly connected to the compressor section, and a turbine section fluidly connected to the combustor and mechanically connected to the compressor section via a shaft. Multiple rotors are disposed in one of the compressor section and the turbine section. Each of the rotors includes a rotor disk portion having a radially inward bore, and is static relative to the shaft. Each rotor is axially adjacent at least one other rotor and a gap is defined between each rotor and an adjacent rotor. A cooling passage for a cooling flow is defined between the shaft and the rotors, and a cooling flow redirection component is disposed at the gap and is operable to redirect the cooling flow in the cooling passage into the gap.


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