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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.

Patent No.:

US 11661906 B1

PDFFull Text
Date of Patent:
May. 30, 2023

Filed:

Jul. 09, 2021

Propulsion system arrangement for turbofan gas turbine engine

Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Christopher A. Eckett, West Hartford, CT (US);

Gabriel L. Suciu, Glastonbury, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:

Carlson, Gaskey & Olds, P.C.

Primary Examiner:

Craig Kim

Int. Cl.
CPC ...
F02K 3/075 (2006.01); F02K 1/72 (2006.01); F02K 3/06 (2006.01); F02K 1/76 (2006.01); F02K 1/09 (2006.01); B64D 27/26 (2006.01); B64D 29/06 (2006.01); B64D 33/04 (2006.01); F01D 25/24 (2006.01); F02C 3/04 (2006.01); F02K 1/70 (2006.01);
U.S. Cl.
CPC ...
F02K 3/075 (2013.01); B64D 27/26 (2013.01); B64D 29/06 (2013.01); B64D 33/04 (2013.01); F01D 25/24 (2013.01); F02C 3/04 (2013.01); F02K 1/09 (2013.01); F02K 1/72 (2013.01); F02K 1/763 (2013.01); F02K 3/06 (2013.01); B64D 2027/266 (2013.01); B64D 2027/268 (2013.01); F02K 1/70 (2013.01); F05D 2240/14 (2013.01); F05D 2270/051 (2013.01); Y02T 50/60 (2013.01);
Abstract

An integrated propulsion system according to an example of the present disclosure includes, among other things, a fan section, a gas turbine engine, a geared architecture, a nacelle assembly and a mounting assembly. The nacelle assembly includes a fan nacelle and an aft nacelle, the fan nacelle arranged at least partially about a fan and the engine, and the fan nacelle arranged at least partially about a core cowling to define a bypass flow path.

Find Patent Forward Citations

Quick Actions:

Eckett, Christopher. (2023). Propulsion system arrangement for turbofan gas turbine engine (U.S. Patent No. 11661906). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/11661906

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

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