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:
Jul. 14, 2020

Filed:

Dec. 21, 2015
Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

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

Wesley K. Lord, South Glastonbury, CT (US);

Jayant Sabnis, Glastonbury, CT (US);

Jesse M. Chandler, South Windsor, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 1/02 (2006.01); F01D 17/10 (2006.01); F01D 7/00 (2006.01); F01D 5/02 (2006.01); F01D 9/04 (2006.01); F01D 25/24 (2006.01); F02C 3/107 (2006.01); F02C 3/14 (2006.01);
U.S. Cl.
CPC ...
F01D 17/105 (2013.01); F01D 1/02 (2013.01); F01D 1/023 (2013.01); F01D 5/02 (2013.01); F01D 7/00 (2013.01); F01D 9/041 (2013.01); F01D 25/24 (2013.01); F02C 3/107 (2013.01); F02C 3/14 (2013.01); F05D 2220/323 (2013.01); F05D 2240/128 (2013.01); F05D 2240/24 (2013.01); F05D 2240/60 (2013.01); F05D 2260/606 (2013.01);
Abstract

A turbine engine such as a pusher fan engine is provided. This turbine engine includes a nacelle with a bypass flowpath. A fan rotor is configured to propel air out of the bypass flowpath. A plurality of guide vanes are configured to direct the air to the fan rotor.


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