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:
Dec. 29, 2020

Filed:

Apr. 05, 2019
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Hien Duong, Mississauga, CA;

Vijay Kandasamy, T. Palur, IN;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/68 (2006.01); F01D 17/12 (2006.01); F04D 27/00 (2006.01); F01D 9/06 (2006.01);
U.S. Cl.
CPC ...
F04D 29/685 (2013.01); F01D 17/12 (2013.01); F04D 27/009 (2013.01); F01D 9/065 (2013.01); F05D 2220/3216 (2013.01); F05D 2260/60 (2013.01);
Abstract

A method of operating a compressor of a gas turbine engine is described which includes directing a main airflow through tandem stator rows in a gaspath of the compressor, extracting a first portion of the main airflow from a first location proximate radially inner roots of stators of the first or second stator rows, extracting a second portion of the main airflow from a second location proximate the radially inner roots of the stators of the first or second stator rows, the second location being downstream of the first location relative to the main airflow, and re-injecting the combined extracted flow back into the main airflow at a third location. The third location is located upstream of the first and second locations, and is upstream of a leading edge of stators of the first stator row.


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