Patents by Inventor Todd G. Wetzel

Todd G. Wetzel 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: 6933661
    Abstract: A piezoelectric actuator and a method of assembling and employing a piezoelectric actuator. This method comprises the steps of positioning an expandable piezoelectric material inside a case, and enclosing a vaporizable liquid in the case. The case is positioned in a high temperature environment; and the liquid vaporizes, in that high temperature environment, over a given period of time, to maintain the temperature of the piezoelectric material below a given value for said period of time. Preferably, the vaporizing liquid maintains the temperature of the piezoelectric material substantially constant over that period of time. Also, preferably the case is provided with a pressure responsive valve that opens and closes, in the high temperature environment, to expose the liquid to that environment and control the vaporization of the liquid to maintain the temperature of the piezoelectric material substantially constant over the period of time.
    Type: Grant
    Filed: October 16, 2002
    Date of Patent: August 23, 2005
    Assignee: Lockheed Martin Corporation
    Inventors: Charles E. Seeley, Todd G. Wetzel, Andrew J. Calver, Jeffrey B. Fortin, Keith B. Fosen
  • Patent number: 6883774
    Abstract: A microvalve and a method of forming a microvalve. The microvalve comprises first and second layers, a diaphragm member and a switching means. The first and second layers are secured together to form a valve body that forms an inlet opening for receiving fluid, an outlet opening for conducting fluid from the valve body, and a flow channel for conducting fluid from the inlet to the outlet. The diaphragm is disposed between the layers, and is movable between open and closed positions. In these position, the diaphragm, respectively, allows and blocks the flow of fluid from the inlet to the flow channel. The diaphragm is biased to the closed position, and moves from the closed position to the open position when the pressure of fluid in the inlet reaches a preset value. The switching means is connected to the valve body for moving the diaphragm to the closed position against the pressure of fluid in the inlet.
    Type: Grant
    Filed: October 21, 2002
    Date of Patent: April 26, 2005
    Assignee: Lockheed Martin Corporation
    Inventors: Matthew C. Nielsen, Laura J. Meyer, Todd G. Wetzel, Stanton E. Weaver, Jeffrey B. Fortin, Renato Guida
  • Publication number: 20040256585
    Abstract: A microvalve and a method of forming a microvalve. The microvalve comprises first and second layers, a diaphragm member and a switching means. The first and second layers are secured together to form a valve body that forms an inlet opening for receiving fluid, an outlet opening for conducting fluid from the valve body, and a flow channel for conducting fluid from the inlet to the outlet. The diaphragm is disposed between the layers, and is movable between open and closed positions. In these position, the diaphragm, respectively, allows and blocks the flow of fluid from the inlet to the flow channel. The diaphragm is biased to the closed position, and moves from the closed position to the open position when the pressure of fluid in the inlet reaches a preset value. The switching means is connected to the valve body for moving the diaphragm to the closed position against the pressure of fluid in the inlet.
    Type: Application
    Filed: October 21, 2002
    Publication date: December 23, 2004
    Applicant: Lockheed Martin Corporation
    Inventors: Matthew C. Nielsen, Laura J. Meyer, Todd G. Wetzel, Stanton E. Weaver, Jeffrey B. Fortin, Renato Guida
  • Publication number: 20040140738
    Abstract: A piezoelectric actuator and a method of assembling and employing a piezoelectric actuator. This method comprises the steps of positioning an expandable piezoelectric material inside a case, and enclosing a vaporizable liquid in the case. The case is positioned in a high temperature environment; and the liquid vaporizes, in that high temperature environment, over a given period of time, to maintain the temperature of the piezoelectric material below a given value for said period of time. Preferably, the vaporizing liquid maintains the temperature of the piezoelectric material substantially constant over that period of time. Also, preferably the case is provided with a pressure responsive valve that opens and closes, in the high temperature environment, to expose the liquid to that environment and control the vaporization of the liquid to maintain the temperature of the piezoelectric material substantially constant over the period of time.
    Type: Application
    Filed: October 16, 2002
    Publication date: July 22, 2004
    Applicant: Lockheed Martin Corporation
    Inventors: Charles E. Seeley, Todd G. Wetzel, Andrew J. Calver, Jeffrey B. Fortin
  • Patent number: 6636320
    Abstract: Flow separation detectors and, more particularly feedback sensor arrangements consisting of optical fiber tufts adapted to provide for the measurement of surface aerodynamic flow phenomena through the effects birefringence or transmitted light, and especially with regard to aerodynamic flow separation which is encountered over a surface. Also facilitated is the detection of aerodynamic flow separation with a concurrent detection of encountered mechanical strain and stresses on the surface structure being monitored.
    Type: Grant
    Filed: October 18, 2000
    Date of Patent: October 21, 2003
    Assignee: Lockheed Martin Corporation
    Inventors: Todd G. Wetzel, Edward R. Furlong
  • Publication number: 20020084703
    Abstract: A stator core assembly comprising adjacent packages of stacked lamination sheets that are separated by a plurality of radially extending spacer blocks, and each adjacent pair of spacer blocks define in cooperation with adjacent axially spaced laminations, a plurality of radial cooling ducts, each duct having a least one lamination surface having plurality of concavities.
    Type: Application
    Filed: January 4, 2001
    Publication date: July 4, 2002
    Inventors: Ronald S. Bunker, Todd G. Wetzel, Emil D. Jarczynski
  • Patent number: 6380535
    Abstract: Disclosed are flow separation detectors and, more particularly feedback sensor arrangements adapted to provide for the measurement of surface aerodynamic flow phenomena, and especially with regard to aerodynamic flow separation which is encountered over a surface. In order to obviate or ameliorate the electrical energy requirements in the provision of feedback sensor arrangements, particularly such which are employed for a closed-loop control of aerodynamic flow separation; for instance, that on the wing of an aircraft wherein there can be encountered a breakdown of a boundary-layer flow which may adversely affect the performance of the aircraft, provided is a novel system of flow separation sensors which are based on fiber optics and which may be employed for separation feedback control.
    Type: Grant
    Filed: August 6, 1999
    Date of Patent: April 30, 2002
    Assignee: Lockheed Martin Corporation
    Inventors: Todd G. Wetzel, Sandra F. Feldman