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:
May. 05, 2020

Filed:

Mar. 26, 2014
Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

Anthony C. Jones, San Diego, CA (US);

Patrick M. Lydon, San Marcos, CA (US);

Nagamany Thayalakhandan, San Diego, CA (US);

Eric J. Alexander, San Diego, CA (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/04 (2006.01); F02C 7/06 (2006.01); B64D 33/02 (2006.01); F02C 3/04 (2006.01);
U.S. Cl.
CPC ...
F02C 7/04 (2013.01); B64D 33/02 (2013.01); F02C 3/04 (2013.01); F02C 7/06 (2013.01); B64D 2033/0273 (2013.01); F05D 2220/323 (2013.01); F05D 2250/51 (2013.01); F05D 2250/80 (2013.01); F05D 2250/82 (2013.01);
Abstract

A gas turbine engine has a nose cone with a nose cone upstream end and an inlet housing including a plurality of separate flow paths at a housing upstream end which is downstream of the nose cone upstream end. The inlet housing includes a mixing portion downstream of the housing upstream end which mixes airflow from the separate flow paths, such that the airflow is generally around 360 degrees of a rotational axis of the gas turbine engine. A rotor and a turbine drive a shaft to drive the rotor with the shaft including a bearing mounted at a location downstream of the nose cone upstream end.


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