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:
Jul. 18, 2023

Filed:

Jun. 10, 2022
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Christopher Gover, Longueuil, CA;

Remy Synnott, St-Jean-sur-Richelieu, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/14 (2006.01); F01D 11/24 (2006.01); F01D 25/14 (2006.01); F02C 7/18 (2006.01); F01D 11/16 (2006.01);
U.S. Cl.
CPC ...
F01D 11/24 (2013.01); F01D 11/16 (2013.01); F01D 25/14 (2013.01); F02C 7/18 (2013.01); F05D 2220/323 (2013.01); F05D 2240/14 (2013.01); F05D 2260/201 (2013.01);
Abstract

A turbine assembly in a turbine section of an aircraft engine includes a rotor with blades having blade tips, and a turbine housing radially surrounding the blades. A distance between an inner surface of the housing and the blade tips defines a tip clearance gap. A passive cooling system for optimizing the tip clearance gap includes a cooling airflow passage located radially outward from, and in heat-transfer with, the turbine housing. The cooling airflow passage has an inlet opening located upstream of the rotor and an exit opening located downstream of the rotor. The inlet opening provides air flow into the cooling airflow passage. The exit opening provides air flow communication between the cooling airflow passage and a main gaspath of the turbine section. A flow of cooling air through the cooling airflow passage is induced, to cool the housing.


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