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:
Mar. 08, 2016

Filed:

Feb. 11, 2011
Applicants:

Claude G. Matalanis, Longmeadow, CT (US);

Andrzej Ernest Kuczek, Bristol, CT (US);

Zaffir A. Chaudhry, Rockford, IL (US);

Brian E. Wake, South Glastonbury, CT (US);

Vijaya Ramaraju Lakamraju, Longmeadow, MA (US);

Alan Matthew Finn, Hebron, CT (US);

Fanping Sun, Glastonbury, CT (US);

Ulf J. Jonsson, South Windsor, CT (US);

Inventors:

Claude G. Matalanis, Longmeadow, CT (US);

Andrzej Ernest Kuczek, Bristol, CT (US);

Zaffir A. Chaudhry, Rockford, IL (US);

Brian E. Wake, South Glastonbury, CT (US);

Vijaya Ramaraju Lakamraju, Longmeadow, MA (US);

Alan Matthew Finn, Hebron, CT (US);

Fanping Sun, Glastonbury, CT (US);

Ulf J. Jonsson, South Windsor, CT (US);

Assignee:

SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/615 (2006.01);
U.S. Cl.
CPC ...
B64C 27/615 (2013.01);
Abstract

A rotor blade assembly includes a rotor blade including one or more pockets and a housing located on the rotor blade within one or more pockets. The housing is secured to the rotor blade via one or more dovetail joints. A drive mechanism for a control surface of a rotor blade includes an actuator and a rocker operably connected to the actuator. At least one hinge rod is operably connected to the rocker and operably connected to a control surface at a control surface pivot. The drive mechanism translates substantially linear motion of the actuator into rotational motion of the control surface about the control surface pivot.


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