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:
Oct. 27, 2015

Filed:

Sep. 13, 2011
Applicants:

David H. Hunter, Cheshire, CT (US);

Ryan T. Casey, West Haven, CT (US);

Francis E. Byrnes, White Plains, NY (US);

Inventors:

David H. Hunter, Cheshire, CT (US);

Ryan T. Casey, West Haven, CT (US);

Francis E. Byrnes, White Plains, NY (US);

Assignee:

SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/473 (2006.01); B64C 27/32 (2006.01); B64C 27/33 (2006.01); B64C 27/58 (2006.01);
U.S. Cl.
CPC ...
B64C 27/473 (2013.01); B64C 27/32 (2013.01); B64C 27/33 (2013.01); B64C 27/58 (2013.01);
Abstract

A rotor for use in an aircraft includes an inner hub; and a plurality of blades arranged around the inner hub, each of the plurality of blades comprising an inner structural member; an outer blade shell surrounding the inner structural member; and a centering block located at a base of the inner structural member proximal to the inner hub, wherein the centering block is located between a first lateral portion of the inner structural member and a second lateral portion of the inner structural member, wherein the centering block is further connected to the outer blade shell, and wherein the centering block allows the outer blade shell to rotate about an axis approximately corresponding to the inner structural member.


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