Patents by Inventor Wilhelmus J. Lam

Wilhelmus J. Lam 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: 7252644
    Abstract: The present invention relates to a system for use in rehabilitation and/or physical therapy for the treatment of injury or disease. The system can overcome gravity-induced dysfunction in extremity paresis following stroke or other neurological disorders.
    Type: Grant
    Filed: September 29, 2005
    Date of Patent: August 7, 2007
    Assignees: Northwestern University, The Rehabilitation Institute, Lam Design Management LLC
    Inventors: Julius P. A. Dewald, Wilhelmus J. Lam
  • Patent number: 4398889
    Abstract: A flight simulating system is provided with a manually operated control member connected to a servomechanism which responds to manual input by the control member and reacts to provide realistic feedback to the control member in accord with simulated flight conditions. For this purpose, a combining circuit, a dividing circuit and two integrator circuits are provided in series. The combining circuit has an input which represents manual input force to the control member and another input from the flight-simulating computer which represents simulated internal forces acting on the controlled member and the dividing circuit divides the output of the combining circuit by a value representing the mass of the control member to produce a control member acceleration-related signal. This acceleration-related signal is integrated twice to produce, respectively, a control member velocity-related signal and a control member position-related signal.
    Type: Grant
    Filed: June 8, 1981
    Date of Patent: August 16, 1983
    Assignee: Fokker B.V.
    Inventors: Wilhelmus J. Lam, Luitzen de Vries
  • Patent number: 4358959
    Abstract: A method of measuring the rigidity, the damping coefficient and the inertia of a system consisting of a damped, spring-supported mass, particularly, the manually operable member of the control-system of an aircraft or a flight simulator, in which method the measurement of the rigidity takes place by determining the relationship between the force exerted on the mass and the deviation of the mass from the state of equilibrium at a speed and an acceleration of substantially zero value and storing the relationship. The method is characterized by the initial step of forming three electric signals--namely, a force signal having a value directly proportional to the force exerted on the mass, an acceleration signal having a value directly proportional to the acceleration of the mass, and a velocity signal having a value directly proportional to the speed of the mass.
    Type: Grant
    Filed: April 14, 1980
    Date of Patent: November 16, 1982
    Assignee: Fokker-VFW B.V.
    Inventors: Wilhelmus J. Lam, Luitzen De Vries