Patents by Inventor Allen L. Arndt

Allen L. Arndt 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: 7152842
    Abstract: A shock-isolation system having a platform for supporting an operator station and a console which can both be fixedly secured to the platform in a relative non-displacement mode with the platform supported by a shock mount that simultaneously isolates the platform including an operator, the operator station and the console as a unitary component from high ā€œgā€ shock to thereby minimize injury to an operator due to impact with either the operator station, the console or the platform.
    Type: Grant
    Filed: January 24, 2000
    Date of Patent: December 26, 2006
    Assignee: Lockheed Martin Corporation
    Inventors: Robert J. Monson, Allen L. Arndt, Samuel A. Runge
  • Patent number: 6848631
    Abstract: A fluid flow device in one embodiment comprising a housing having an aperture or a plurality of apertures therein and in another embodiment a single chamber with a piston such as a flexible member forming a chamber and a vibratory member for vibrating the flexible member to simultaneously eject an array of laminar flow fluid vortices that coalesce with each other to form a larger fluid vortex that can be used for direct cooling or for inducing circulation of a cooling fluid within an enclosure to cool the components within the system. When used within a closed system the inventor provides a zero net flux device as the fluid contained within a sealed chamber can be stirred, or mixed, without the introduction of fresh fluid from the outside the system.
    Type: Grant
    Filed: January 23, 2002
    Date of Patent: February 1, 2005
    Inventors: Robert James Monson, Allen L. Arndt
  • Publication number: 20030177899
    Abstract: A fluid flow device in one embodiment comprising a housing having an aperture or a plurality of apertures therein and in another embodiment a single chamber with a piston such as a flexible member forming a chamber and a vibratory member for vibrating the flexible member to simultaneously eject an array of laminar flow fluid vortices that coalesce with each other to form a larger fluid vortex that can be used for direct cooling or for inducing circulation of a cooling fluid within an enclosure to cool the components within the system. When used within a closed system the inventor provides a zero net flux device as the fluid contained within a sealed chamber can be stirred, or mixed, without the introduction of fresh fluid from the outside the system.
    Type: Application
    Filed: January 23, 2002
    Publication date: September 25, 2003
    Inventors: Robert James Monson, Allen L. Arndt
  • Publication number: 20020153467
    Abstract: Shock and vibration eliminating elements are constructed of an elastomeric material, which is formed into shapes that have an elongated, generally trapezoidal cross-sectional area. Upper and lower mounting surfaces extend from the ends of the cross-sectional area. The upper and lower end mounting surfaces of the damping elements have integral, parallel surfaces that are used to mount the element to the two structures. The cross-sectional area of the damping elements locates the mounting surfaces so that a straight line normal to one of parallel mounting surfaces at one end of the cross-sectional area of a block, will not intersect the other mounting surface at the other end of the cross-sectional area. Thus, a force applied in a normal direction to one of the mounting surfaces will be translated into shear forces instead of comprehensive forces.
    Type: Application
    Filed: June 20, 2002
    Publication date: October 24, 2002
    Inventors: Noel Allen, Allen L. Arndt, Robert James Monson
  • Patent number: 6412616
    Abstract: An energy dissipation system for limiting forces applied to object; includes a piston rod that extends out of a pneumatic cylinder which contacts the object, the piston rod is forced from its initial position against a return spring and air is forced into an air line. The force transmitted to the object is consumed by an energy transformation device that responds to the air in the air line. [One such energy transformation device as an air accumulator, which is coupled to the air line trough a check valve. An orifice or release valve, releases air up a predetermined flow rate so that the linear motion of the protected object is transformed into work, which is dissipated.] [Another] The energy transformation device consists of an air-driven motor coupled to a heavy flywheel [through] that is driven by the motor.
    Type: Grant
    Filed: February 22, 2000
    Date of Patent: July 2, 2002
    Assignee: Lockheed Martin Corporation
    Inventors: Noel L. Allen, Allen L. Arndt, Robert J. Monson
  • Patent number: 6386134
    Abstract: A shock isolator having a housing securable to a support structure with the housing containing a bell shaped elastomer having a base secured to the housing and an axially offset apex surface secured to a connector to cantileverly support equipment to be isolated from shock with the cantileverly support of apex surface from the base insuring that any displacement of the connector produces a substantial shearing action in the elastomer to effectively damp the effect of a shock on the shock isolator.
    Type: Grant
    Filed: March 13, 2000
    Date of Patent: May 14, 2002
    Assignee: Lockheed Martin Corporation
    Inventors: Robert James Monson, Wesley Eugene Revely, Trevor J. McCollough, Allen L. Arndt
  • Patent number: 6299150
    Abstract: A spring element is made of a spring material and is formed into a generally elliptical shape. Two mounting pins extend in a normal direction through parallel relatively short segments of said elliptically-shaped spring element. The mounting pins are substantially aligned with the shorter of the two axis of the elliptically-shaped spring element so as to extend both inwardly and outwardly of said elliptically-shaped spring element. An elastomeric coating is applied around substantially all of the spring elements and a pair of blocks, each of which surrounds one of the mounting pins receives one of the mounting pins. A number of spring elements are joined together by two parallel, spaced-apart coupling links which contain cavities therein to receive one of the blocks of each of the spring elements.
    Type: Grant
    Filed: February 1, 2000
    Date of Patent: October 9, 2001
    Assignee: Lockheed Martin Corporation
    Inventors: Noel L. Allen, Allen L. Arndt, Scott M. Ralston