Patents by Inventor Joel H. Cohen

Joel H. Cohen 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: 5466905
    Abstract: Direct electric current arc welding between an electrode and a workpiece surface is accomplished in the electric current range of about 0.5-45 amps while reversing the polarities between the electrode and the workpiece surface at a low frequency rate in the range of about 1-1000 cycles per second, in a series of polarity cycles. The workpiece surface, in at least some of the cycles, is positive for a time less than that surface is negative to result in anodic cleaning of the workpiece surface. If the arc is extinguished during a polarity reversal, the arc is maintained, for example, by restriking.
    Type: Grant
    Filed: April 5, 1994
    Date of Patent: November 14, 1995
    Assignee: General Electric Company
    Inventors: Gilbert E. Flowers, Joel H. Cohen, Earl L. Kelly, Jr., Levi Williams, Gray W. Grubbs
  • Patent number: 5464958
    Abstract: A variable polarity device reverses the polarity of an electrically conductive workpiece and an electrode, having opposite polarities, between positive and negative in a low D.C. range of about 0.5-45 amps. Combined with the device is a control means which schedules a frequency of time rate of the reversing in the low time frequency of about 1-1000 cycles per second as well as the electric current at each polarity to provide a series of time and current defined polarity cycles for D.C. arc welding apparatus.
    Type: Grant
    Filed: April 5, 1994
    Date of Patent: November 7, 1995
    Assignee: General Electric Company
    Inventors: Gilbert E. Flowers, Joel H. Cohen, Earl L. Kelly, Jr., Levi Williams, Gray W. Grubbs, Stefan P. Kyselica
  • Patent number: 4305697
    Abstract: A gas turbine engine air cooled vane assembly which includes inner and outer platform members and an airfoil member therebetween is repaired by removing from the vane assembly a vane assembly segment comprising at least a portion of the leading edge wall, a portion of the airfoil body wall and a portion of at least one platform member connected with the leading edge wall. The vane assembly segment is removed along a preselected path which, during operation of the vane assembly in a gas turbine engine, experiences relatively low mechanical stresses. A replacement member of substantially the same type of material and of a size and shape which matches the removed vane assembly segment is placed into registry with the vane assembly and then metallurgically bonded to the vane assembly.
    Type: Grant
    Filed: March 19, 1980
    Date of Patent: December 15, 1981
    Assignee: General Electric Company
    Inventors: Joel H. Cohen, Henry E. Lynch