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. 22, 2019

Filed:

Jan. 23, 2017
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Matthew Robert Pearson, Hartford, CT (US);

Gabriel L. Suciu, Glastonbury, CT (US);

Justin R. Urban, Tolland, CT (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/12 (2006.01); F02C 7/04 (2006.01); F02C 7/12 (2006.01); F02C 7/14 (2006.01); F02C 3/04 (2006.01); F28D 15/02 (2006.01); F01D 5/08 (2006.01); F01D 21/00 (2006.01); F01D 25/10 (2006.01); F28D 15/04 (2006.01); F28D 21/00 (2006.01);
U.S. Cl.
CPC ...
F02C 7/12 (2013.01); F01D 5/08 (2013.01); F01D 21/00 (2013.01); F01D 25/10 (2013.01); F01D 25/12 (2013.01); F02C 3/04 (2013.01); F28D 15/0208 (2013.01); F28D 15/0233 (2013.01); F28D 15/0266 (2013.01); F28D 15/0275 (2013.01); F02C 7/14 (2013.01); F05D 2260/208 (2013.01); F28D 15/04 (2013.01); F28D 2021/0026 (2013.01); Y02T 50/676 (2013.01);
Abstract

A gas turbine engine includes a rotor section proximate to a combustor section, where the rotor section is subject to bowing effects due to thermal differences and heat transfer at engine shutdown. The gas turbine engine also includes a heat pipe system. The heat pipe system includes one or more heat pipes installed between an upper portion of the rotor section and a lower portion of the rotor section. The heat pipe system is operable to accept heat at a hot side of the heat pipe system at the upper portion, flow heat from the hot side to a cold side of the heat pipe system, and reject heat from the cold side of the heat pipe system at the lower portion to reduce a thermal differential between the upper portion and the lower portion at engine shutdown.


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