Patents by Inventor Sidney G. Allison

Sidney G. Allison has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 7732998
    Abstract: A telescoping actuator assembly includes a plurality of cylindrical actuators in a concentric arrangement. Each cylindrical actuator is at least one piezoelectric fiber composite actuator having a plurality of piezoelectric fibers extending parallel to one another and to the concentric arrangement's longitudinal axis. Each cylindrical actuator is coupled to concentrically-adjacent ones of the cylindrical actuators such that the plurality of cylindrical actuators can experience telescopic movement. An electrical energy source coupled to the cylindrical actuators applies actuation energy thereto to generate the telescopic movement.
    Type: Grant
    Filed: August 3, 2006
    Date of Patent: June 8, 2010
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Sidney G. Allison, Qamar A. Shams, Robert L. Fox, Christopher L. Fox, legal representative, Melanie L. Fox Chattin, legal representative
  • Publication number: 20100118405
    Abstract: Actuator assemblies are formed by at least one cylinder where each cylinder is formed by at least one piezoelectric fiber composite actuator adapted to have actuation energy applied thereto.
    Type: Application
    Filed: August 3, 2006
    Publication date: May 13, 2010
    Applicant: United States of America as represented by the Admins of the Ntl Aeronautics and Space Admins
    Inventors: Sidney G. Allison, Qamar A. Shams, Robert L. Fox, Christopher L. Fox, Melanie L. Fox Chattin
  • Patent number: 7580323
    Abstract: An optical assembly is formed by one or more piezoelectric fiber composite actuators having one or more optical fibers coupled thereto. The optical fiber(s) experiences strain when actuation voltage is applied to the actuator(s). Light passing through the optical fiber(s) is wavelength tuned by adjusting the actuation voltage.
    Type: Grant
    Filed: May 23, 2006
    Date of Patent: August 25, 2009
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Adninistration
    Inventors: Sidney G. Allison, Qamar A. Shams, Robert L. Fox, Christopher L. Fox, legal representative, Melanie L. Fox Chattin, legal representative
  • Patent number: 5150620
    Abstract: The present invention is a method of recertifying a loaded bearing member using ultrasound testing to compensate for different equipment configurations and temperature conditions. The standard frequency F1 of a reference block is determined via an ultrasound tone burst generated by a first pulsed phase locked loop (P2L2) equipment configuration. Once a lock point number s is determined for F1, the reference frequency F1a of the reference block is determined at this lock point number via a second P2L2 equipment configuration to permit an equipment offset compensation factor Fo1=((F1-F1a)/F1)(1000000) to be determined. Next, a reference frequency F2 of the unloaded bearing member is determined using the second P2L2 equipment configuration and is then compensated for equipment offset errors via the relationship F2c=F2+F2(Fo1)/1000000. A lock point number b is also determined for F2.
    Type: Grant
    Filed: June 19, 1991
    Date of Patent: September 29, 1992
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Sidney G. Allison
  • Patent number: 5121058
    Abstract: A method and apparatus for testing steel components for temperature embrittlement uses magneto-acoustic emission to nondestructively evaluate the component. Acoustic emission signals occur more frequently at higher levels in embrittled components. A pair of electromagnets are used to create magnetic induction in the test component. Magneto-acoustic emission signals may be generated by applying an AC current to the electromagnets. The acoustic emission signals are analyzed to provide a comparison between a component known to be umembrittled and a test component. Magnetic remanence is determined by applying a DC current to the electromagnets, then turning the magnets off and observing the residual magnetic induction.
    Type: Grant
    Filed: April 15, 1991
    Date of Patent: June 9, 1992
    Assignee: Administrator, National Aeronautics and Space Administration
    Inventors: Sidney G. Allison, Min Namkung, William T. Yost, John H. Cantrell
  • Patent number: 5117184
    Abstract: A method and apparatus for testing steel components for temper embrittlement uses magneto-acoustic emission to nondestructively evaluate the component. Acoustic emission signals occur more frequently at higher levels in embrittled components. A pair of electromagnets are used to create magnetic induction in the test component. Magneto-acoustic emission signals may be generated by applying an AC current to the electromagnets. The acoustic emission signals are analyzed to provide a comparison between a component known to be unembrittled and a test component. Magnetic remanence is determined by applying a DC current to the electromagnets, then turning the magnets off and observing the residual magnetic induction.
    Type: Grant
    Filed: November 2, 1990
    Date of Patent: May 26, 1992
    Inventors: Sidney G. Allison, Min Namkung, William T. Yost, John H. Cantrell
  • Patent number: 5109195
    Abstract: A method and apparatus for testing steel components for temper embrittlement uses magneto-acoustic emission to nondestructively evaluate the component. Acoustic emission signals occur more frequently at higher levels in embrittled components. A pair of electromagnets are used to create magnetic induction in the test component. Magneto-acoustic emission signals may be generated by applying an AC current to the electromagnets. The acoustic emission signals are analyzed to provide a comparison between a component known to be umembrittled and a test component. Magnetic remanence is determined by applying a DC current to the electromagnets, then turning the magnets off and observing the residual magnetic induction.
    Type: Grant
    Filed: December 12, 1989
    Date of Patent: April 28, 1992
    Inventors: Sidney G. Allison, Min Namkung, William T. Yost, John H. Cantrell
  • Patent number: 4912411
    Abstract: A method and apparatus for testing steel components for temper embrittlement uses magneto-acoustic emission to nondestructively evaluate the component. Acoustic emission signals occur more frequently at higher levels in embrittled components. A pair of electromagnets are used to create magnetic induction in the test component. Magneto-acoustic emission signals may be generated by applying an AC current to the electromagnets. The acoustic emission signals are analyzed to provide a comparison between a component known to be unembrittled and a test component. Magnetic remanence is determined by applying a DC current to the electromagnets, then turning the magnets off and observing the residual magnetic induction.
    Type: Grant
    Filed: June 23, 1988
    Date of Patent: March 27, 1990
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Sidney G. Allison, Min Namkung, William T. Yost, John H. Cantrell