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:
Apr. 18, 2017

Filed:

Mar. 27, 2011
Applicants:

Robert A. Ress, Jr., Carmel, IN (US);

Steve Stratton, Indianapolis, IN (US);

Matthew J. Starr, Indianapolis, IN (US);

Inventors:

Robert A. Ress, Jr., Carmel, IN (US);

Steve Stratton, Indianapolis, IN (US);

Matthew J. Starr, Indianapolis, IN (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 3/075 (2006.01); F02K 3/077 (2006.01); F02C 7/36 (2006.01); F02C 3/113 (2006.01); F02K 3/06 (2006.01); F02C 7/32 (2006.01); F16D 47/04 (2006.01); F16D 21/06 (2006.01);
U.S. Cl.
CPC ...
F02K 3/075 (2013.01); F02C 3/113 (2013.01); F02C 7/32 (2013.01); F02C 7/36 (2013.01); F02K 3/06 (2013.01); F02K 3/077 (2013.01); F16D 47/04 (2013.01); F05D 2260/40 (2013.01); F05D 2260/4023 (2013.01); F05D 2260/40311 (2013.01); F16D 21/06 (2013.01); Y02T 50/671 (2013.01);
Abstract

An adaptive fan system for a variable cycle turbofan engine having at least one turbine, includes a shaft structured to receive mechanical power from a turbine in the variable cycle turbofan engine and a first fan stage that is coupled directly to the shaft and is driven directly by the shaft. A transmission system is coupled to the shaft and a second fan stage is coupled to the shaft via the transmission system and is driven by the shaft via the transmission system. The transmission system is structured to selectively vary a speed between high and low speeds at which power is supplied from the shaft to the second fan stage relative to at least one of the shaft and the first fan stage, wherein the first fan stage and the second fan stage are configured to rotate in the same direction and at the same high speed to increase the mechanical power of the turbine.


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