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:
Oct. 08, 2024

Filed:

Jun. 30, 2023
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Ryan A. Mitchell, Jupiter, FL (US);

Robert B. Fowler, West Palm Beach, FL (US);

Assignee:

RTX Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 13/06 (2006.01); B64D 13/08 (2006.01); B64D 27/10 (2006.01); F02C 3/13 (2006.01); F02C 6/08 (2006.01); F02C 6/18 (2006.01); F02C 7/08 (2006.01); F02C 9/42 (2006.01); F02K 3/12 (2006.01);
U.S. Cl.
CPC ...
B64D 13/06 (2013.01); B64D 13/08 (2013.01); B64D 27/10 (2013.01); F02C 3/13 (2013.01); F02C 6/08 (2013.01); F02C 6/18 (2013.01); F02C 7/08 (2013.01); F02C 9/42 (2013.01); F02K 3/12 (2013.01);
Abstract

A method of operation is provided during which a heating fluid is directed through a first passage into a combustor section to heat a component within the combustor section when an aircraft engine is in a first standby mode. The aircraft engine includes a flowpath, a compressor section, the combustor section, a turbine section and an exhaust section. The flowpath extends through the compressor section, the combustor section, the turbine section and the exhaust section from an inlet into the flowpath to an exhaust from the flowpath. The heating fluid is directed through a second passage into the exhaust section when the aircraft engine is in a second mode. The heating fluid is directed through the second passage bypasses the turbine section.


Find Patent Forward Citations

Mitchell, Ryan. (2024). Pre-heating aircraft engine in standby mode (U.S. Patent No. 12110116). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12110116

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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