Patents by Inventor Arne H. Wiedermann

Arne H. Wiedermann 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: 4562036
    Abstract: The shock or energy absorber disclosed herein utilizes an apertured plate maintained under the normal level of liquid flowing in a piping system and disposed between the normal liquid flow path and a cavity pressurized with a compressible gas. The degree of openness (or porosity) of the plate is between 0.01 and 0.60. The energy level of a shock wave travelling down the piping system thus is dissipated by some of the liquid being jetted through the apertured plate toward the cavity. The cavity is large compared to the quantity of liquid jetted through the apertured plate, so there is little change in its volume. The porosity of the apertured plate influences the percentage of energy absorbed.
    Type: Grant
    Filed: August 26, 1983
    Date of Patent: December 31, 1985
    Assignee: The United States of America as represented by the United States Department of Energy
    Inventors: Yong W. Shin, Arne H. Wiedermann, Carl E. Ockert
  • Patent number: 4149447
    Abstract: A multi-effect passive detonation trap utilizes a manifold having a rectalarly shaped cross sectional area with oppositely disposed off-set pipeline fixedly connected thereto to attenuate an upstream detonation wave. The detonation wave is arrested by providing for maximum containment and self relief of the energy produced, directional control of the reaction, and a manifold configuration which assures extinction of the detonation wave.
    Type: Grant
    Filed: April 29, 1977
    Date of Patent: April 17, 1979
    Assignee: The United States of America as represented by the Secretary of the Army
    Inventor: Arne H. Wiedermann
  • Patent number: 3992995
    Abstract: A variable position launcher including a launch tube in which the second event (SE) package is placed. A positioning spring on the explosive side of the SE package urges it toward the muzzle end of the tube which is sealed with a frangible cover. A gas inlet operates to pressurize the muzzle end of the tube and apply a velocity dependent force on the SE package opposite the spring force so that the SE package is accurately positioned within the tube thereby controlling the retrolaunch velocity.
    Type: Grant
    Filed: September 4, 1975
    Date of Patent: November 23, 1976
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventor: Arne H. Wiedermann