Patents by Inventor Richard J. Ulman

Richard J. Ulman 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: 6564626
    Abstract: A simultaneous measurement of small displacements, from which forces, moments, pressures, and other physical quantities can be determined, with a high degree of precision and accuracy. A computer may be used to resolve the displacement into the applied loads. More specifically, a class of precision instruments is provided whose chief task is to resolve the applied loads acting on a body into their component forces and moments relative to a fixed coordinated axis system. This class of instruments includes the measurement of forces and moments acting on models tested in aerodynamic wind tunnel facilities.
    Type: Grant
    Filed: November 26, 1999
    Date of Patent: May 20, 2003
    Assignee: The Boeing Company
    Inventors: Richard J. Ulman, William R. Teman, David A. Rohrig
  • Publication number: 20020092348
    Abstract: A simultaneous measurement of small displacements, from which forces, moments, pressures, and other physical quantities can be determined, with a high degree of precision and accuracy. A computer may be used to resolve the displacement into the applied loads. More specifically, a class of precision instruments is provided whose chief task is to resolve the applied loads acting on a body into their component forces and moments relative to a fixed coordinated axis system. This class of instruments includes the measurement of forces and moments acting on models tested in aerodynamic wind tunnel facilities.
    Type: Application
    Filed: November 26, 1999
    Publication date: July 18, 2002
    Inventors: RICHARD J. ULMAN, WILLIAM R. TEMAN, DAVID A. ROHRIG
  • Patent number: 5156359
    Abstract: A handle assembly for controlling an aircraft door latch mechanism so that the door can be opened or closed from either inside or outside the aircraft. The assembly includes an inner shaft that is connected to the latch mechanism so as to control the opening and closing of the door, and an outer shaft that overlaps the inner shaft and that can be telescopically extended away from inner shaft. An inside handle is attached to the inner shaft so as to rotate the shaft. Rotation of the outer shaft is controlled by an outside handle attached thereto. An inner clutch half is attached, by splines, to the inboard end of the outer shaft. An outer clutch half is attached, by splines, to the outboard end of the inner shaft. The clutch halves are normally spaced away from each other. When the outside handle and the outer shaft are extended, the clutch halves interlock so that the shafts will rotate in unison. An actuator disarming assembly with a translating pivoting crank is attached to the outer shaft.
    Type: Grant
    Filed: June 13, 1991
    Date of Patent: October 20, 1992
    Assignee: The Boeing Company
    Inventors: Donald R. Noble, Kurt Poechlauer, Richard J. Ulman