Patents by Inventor Robert J. Durwin

Robert J. Durwin 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).

  • Publication number: 20040168876
    Abstract: A spring clutch has a housing containing first and second sleeves surrounding first and second longitudinal spans of a coil spring. A carrier mounting at least one of the sleeves relative to the housing flexes to maintain alignment of axes of the sleeves to control forces on the portion of the spring spanning the gap between the sleeves.
    Type: Application
    Filed: February 28, 2003
    Publication date: September 2, 2004
    Inventors: Thomas L. Tully, Ruth H. Durwin, Charles J. Isabelle, Robert T. Bohm, Robert J. Durwin
  • Patent number: 5813292
    Abstract: A method for fabricating a split path transmission system that achieves equal torque splitting between the forward and aft split load paths of each gear train thereof at a predefined operating point by providing an intentional timing difference between gears and pinions of the forward and aft split load paths of each gear train of the split path transmission system is disclosed. The method includes the steps of identifying the torque distribution curves of the forward and aft split load paths of one gear train of the split path transmission system. The method further includes a step of selecting a predefined operating point for the split path transmission system wherein equal torque splitting between the forward and aft split load paths of the one gear train is desired. Next, the forward and aft torque distribution curves are analytically modified as required to pass through the predefined operating point.
    Type: Grant
    Filed: December 15, 1995
    Date of Patent: September 29, 1998
    Assignee: Sikorsky Aircraft Corporation
    Inventors: Jules G. Kish, Robert J. Durwin, Timothy L. Krantz
  • Patent number: 5149013
    Abstract: A retractable helicopter rotor in which the rotor and its blades, the swashplate and the pitch change rods are retracted and extended as a unit during the helicopter rotor retraction/extension mode of operation, wherein the connection between the rotor support system and the fuselage constitutes a single interface between overlapping circumferentially extending flanges of each, and with the bolts joining those flanges being loaded in compression.
    Type: Grant
    Filed: May 16, 1991
    Date of Patent: September 22, 1992
    Assignee: United Technologies Corporation
    Inventors: Ralph D. Costanzo, Robert J. Durwin, Lee N. Hager, William L. Noehren
  • Patent number: 4012154
    Abstract: A shaft bearing retention means comprises a segmented ring having a conical inner surface which is placed about a large diameter shaft having a corresponding conical indentation about its periphery to receive the ring. The segments are retained in assembled position on the shaft by joining pins extended through interengaging lapped tongues on the ends of each segment and by attaching one or more flanged retaining rings thereto by screws or bolts. Additional clamping screws or bolts pass through the retaining ring and are threaded into the segments, projecting beyond the latter so as to bear against a thrust ring through which the shaft passes. The axially adjustable thrust ring engages a bearing assembly which is fixed against axial movement by a shoulder on the shaft. Axial force is produced against the bearing assembly by the clamping bolts due to wedging action of the mating conical surfaces on the shaft and the segmented ring.
    Type: Grant
    Filed: September 28, 1973
    Date of Patent: March 15, 1977
    Assignee: United Technologies Corporation
    Inventors: Robert J. Durwin, Joseph H. Mancini