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. 23, 2017

Filed:

Mar. 27, 2014
Applicant:

Honeywell International Inc., Morristown, NJ (US);

Inventors:

Shezan Kanjiyani, Glendale, AZ (US);

John Gintert, Tempe, AZ (US);

Rajiv Rana, Tempe, AZ (US);

Lorenzo Crosatti, Phoenix, AZ (US);

Bradley Reed Tucker, Chandler, AZ (US);

Ed Zurmehly, Phoenix, AZ (US);

Assignee:

HONEYWELL INTERNATIONAL INC., Morris Plains, NJ (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/18 (2006.01); F01D 25/12 (2006.01); F01D 25/14 (2006.01); F01D 5/18 (2006.01); F01D 11/08 (2006.01); F02C 3/10 (2006.01);
U.S. Cl.
CPC ...
F02C 7/18 (2013.01); F01D 5/187 (2013.01); F01D 11/08 (2013.01); F01D 25/12 (2013.01); F01D 25/14 (2013.01); F02C 3/10 (2013.01); F05D 2240/81 (2013.01); F05D 2260/201 (2013.01); F05D 2260/205 (2013.01); Y02T 50/673 (2013.01); Y02T 50/676 (2013.01);
Abstract

A turbine section includes a stator assembly having an inner diameter end wall, an outer diameter end wall, and a stator vane; a turbine rotor assembly including a rotor blade extending into the mainstream gas flow path; a housing including an annular shroud that circumscribes the rotor blade and at least partially defines the mainstream hot gas flow path; a first baffle arranged to define a first cavity with the outer diameter end wall of the stator assembly; a second baffle; and a third baffle arranged to define a second cavity with the second baffle and a third cavity with the shroud. The first cavity is fluidly coupled to the second cavity and the second cavity is fluidly coupled to the third cavity such that cooling air flows from the first cavity to the second cavity and from the second cavity to the third cavity.


Find Patent Forward Citations

Loading…