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:
Aug. 07, 2018

Filed:

Aug. 21, 2014
Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

John R. Otto, Middletown, CT (US);

James B. Coffin, Windsor, CT (US);

Jason Husband, South Glastonbury, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 3/06 (2006.01); F04D 25/04 (2006.01); F02C 3/107 (2006.01); F01D 5/02 (2006.01); F01D 15/12 (2006.01); F04D 25/02 (2006.01); F04D 27/00 (2006.01); F04D 29/32 (2006.01); F02C 7/36 (2006.01);
U.S. Cl.
CPC ...
F04D 25/045 (2013.01); F01D 5/02 (2013.01); F01D 15/12 (2013.01); F02C 3/107 (2013.01); F02C 7/36 (2013.01); F02K 3/06 (2013.01); F04D 25/028 (2013.01); F04D 27/004 (2013.01); F04D 29/321 (2013.01); F05D 2220/32 (2013.01); F05D 2260/40311 (2013.01); F05D 2270/02 (2013.01);
Abstract

A turbofan engine is disclosed that includes a fan rotatable about an axis, a compressor section including a high pressure compressor, a medium pressure compressor and a low pressure compressor and a turbine section including a high pressure turbine, an intermediate turbine and a fan drive turbine. A fan drive gear system is driven by the fan drive turbine for driving the fan. A compressor drive gear system is driven by the intermediate turbine for driving the low pressure compressor. A gear controller controls rotation of at least one of the fan drive gear system and the compressor drive gear system relative to a static structure to vary an effective speed reduction ratio of one of the fan drive gear system and the compressor drive gear system.


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