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:
Nov. 19, 2024

Filed:

Jan. 11, 2023
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Kudum Shinde, Bengaluru, IN;

Yashpal Patel, Bengaluru, IN;

Sesha Subramanian, Bengaluru, IN;

Brandon C. Clarke, Milford, OH (US);

Assignee:

GENERAL ELECTRIC COMPANY, Evendale, OH (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/06 (2006.01); F01D 9/04 (2006.01); F02C 6/08 (2006.01);
U.S. Cl.
CPC ...
F01D 9/065 (2013.01); F01D 9/041 (2013.01); F02C 6/08 (2013.01); F05D 2220/3218 (2013.01); F05D 2240/121 (2013.01); F05D 2240/122 (2013.01); F05D 2260/606 (2013.01);
Abstract

A gas turbine engine includes a compressor section having rotor shaft assembly and a stator shroud assembly including a stator shroud casing surrounding the compressor rotor shaft assembly, a compressor flow passage being defined between the compressor rotor shaft assembly and the stator shroud casing. A compressor bleed air system includes a compressor bleed air duct that includes a sloped inlet portion, such as a NACA submerged inlet portion, in the stator shroud casing. Alternatively, stator vanes at a compressor bleed air passage may have a NACA inlet scoop and an airflow passage through the stator vane providing a bleed airflow to a cavity, which has airflow passages providing bleed air to an upstream side of the bleed air passage.


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