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. 06, 2018

Filed:

Feb. 20, 2013
Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

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

Alan H. Epstein, Lexington, MA (US);

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

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

Assignee:

United Technologies Corporation, Hartford, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/052 (2006.01); F02C 7/36 (2006.01); B64D 33/02 (2006.01); B64D 33/10 (2006.01);
U.S. Cl.
CPC ...
F02C 7/36 (2013.01); B64D 33/02 (2013.01); B64D 33/10 (2013.01); F02C 7/052 (2013.01); B64D 2033/022 (2013.01); F05D 2220/324 (2013.01); F05D 2220/325 (2013.01); F05D 2250/44 (2013.01); F05D 2260/20 (2013.01); Y02T 50/675 (2013.01);
Abstract

A gas turbine engine comprises an outer nacelle. A nose cone is spaced radially inward of the outer nacelle. The nose cone defines a particle separator for directing an outer air flow and an inner airflow. The inner airflow is directed through a core inlet to a compressor. The engine further comprises a drive gear system for driving at least one propeller. A variable pitch control system may alter a pitch angle of the at least one propeller. Some of the outer air flow is directed to at least one of the drive gear system and the pitch control system.


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