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:
Jun. 06, 2006

Filed:

Apr. 30, 2003
Applicants:

Anthony Jones, San Diego, CA (US);

Mark Harris, San Diego, CA (US);

Patrick Lydon, San Marcos, CA (US);

Eric Alexander, San Diego, CA (US);

Inventors:

Anthony Jones, San Diego, CA (US);

Mark Harris, San Diego, CA (US);

Patrick Lydon, San Marcos, CA (US);

Eric Alexander, San Diego, CA (US);

Assignee:

Hamilton Sundstrand Corporation, Rockford, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 3/02 (2006.01);
U.S. Cl.
CPC ...
Abstract

A turbofan engine includes a combined stage rotor mounted for common rotation with a shaft, a compressor stage, and a turbine stage. Each of the plurality of fan blades of the combined stage rotor are contiguous with a respective compressor blade. The combined stage rotor is located at a junction between a fan bypass duct and a core duct. The fan bypass stage portion includes a plurality of the fan blades which communicate incoming airflow into fan bypass airflow through the fan bypass duct. The compressor stage portion includes a plurality of the compressor blades which communicated airflow into core airflow through the core duct. The plurality of fan blades extend substantially perpendicular to the plurality of compressor blades such that the plurality of compressor blade portions extend at least partially into the core duct and preferably will include splitters for enhanced efficiency.


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