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:
Mar. 24, 2026

Filed:

Mar. 21, 2024
Applicant:

General Electric Company, Evendale, OH (US);

Inventors:

Syed J. Khalid, Palm Beach Gardens, FL (US);

David Marion Ostdiek, Liberty Township, OH (US);

Randy M. Vondrell, Newport, KY (US);

Brandon Wayne Miller, Liberty Township, OH (US);

Craig William Higgins, Liberty Township, OH (US);

Alexander Kimberley Simpson, Cincinnati, OH (US);

Assignee:

General Electric Company, Evendale, OH (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 3/077 (2006.01); F02K 1/38 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F02K 3/077 (2013.01); F02K 1/386 (2013.01); F02K 3/06 (2013.01);
Abstract

A gas turbine engine is provided having a turbomachine; a primary fan driven by the turbomachine; a secondary fan located downstream of the primary fan within the inlet duct, the gas turbine engine defining a thrust to power airflow ratio between 3.5 and 100 and a core bypass ratio between 0.1 and 10; and an airflow mixer assembly comprising: a low pressure duct positioned within the core cowl; a plenum extending along the circumferential direction located downstream of the low pressure duct and in fluid communication with the low pressure duct; an inner shroud located downstream of the plenum and downstream of the exhaust and in fluid communication with both the plenum and the exhaust; and an outer shroud located outward of the plenum along the radial direction and extending along the circumferential direction and along the axial direction over and downstream of the inner shroud.


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