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:
May. 02, 2006

Filed:

Aug. 10, 2002
Applicants:

A. Dean Jacot, Kent, WA (US);

Robert T. Ruggeri, Kirkland, WA (US);

Dan J. Clingman, Auburn, WA (US);

Inventors:

A. Dean Jacot, Kent, WA (US);

Robert T. Ruggeri, Kirkland, WA (US);

Dan J. Clingman, Auburn, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/36 (2006.01);
U.S. Cl.
CPC ...
Abstract

A preferred rotary actuator includes an actuator assembly having a torque tube formed of a shape memory alloy (SMA), a superelastic NiTinol return spring associated with the torque tube and adapted to bias the torque tube toward an initial position, and a torque tube heating element, especially a thermoelectric device, for switching the SMA to cause rotation to an object connected to the actuator or to generate a torque upon that object. The torque tube () includes a proximal end () and a distal end (). The return spring and torque tube are connected at their ends, with the torque tube being pretwisted while in a martensitic state relative to the spring. Activation of the heating element causes the torque tube to enter an austenitic state in which it returns to its previous untwisted configuration. Removal of heat allows the torque tube to return to a martensitic state, when the return spring retwists the torque tube. A unique locking assemblyis used with the preferred actuator assembly. A helicopter blade twist rotation system for a rotorcraft bladehaving a blade rootand a tipincludes a SMA rotary actuatorlocated within the blade near the blade root, and a passive torque tube () located within the blade and having a proximal end connected to the rotary actuator and a distal end connected to the blade near to the blade tip.


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