Patents by Inventor Ronald W. Boscaljon

Ronald W. Boscaljon 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: 6073973
    Abstract: In the first embodiment, a coupling assembly is provided wherein the inner peripheral diameter of an annular spring is sized to be threadably received over the threads of a coupler and is held in a recess formed by the ends of threads and the edge of a shoulder. This structure minimizes the diameter of the annular spring and lock ring to minimize both the size and weight of coupling assembly. Additionally, it provides a quick connect, quick disconnect coupling and has a peripheral stripe to provide a visual indication of its connected or disconnected status. In the second embodiment, a wavy spring is split which allows its diameter to be temporarily enlarged so that it can be received over the threads of the coupler and then spring back to its original smaller diameter so that it is held in a recess formed by the ends of the threads and a coupler flange. This structure also minimizes the diameter of the annular spring and lock ring to minimize both the size and weight of coupling assembly.
    Type: Grant
    Filed: April 30, 1998
    Date of Patent: June 13, 2000
    Assignee: Stanley Aviation Corporation
    Inventors: Ronald W. Boscaljon, Ronald A. Rossway, David E. Jewell, Eric Hazelwood
  • Patent number: 6050609
    Abstract: A first coupling member has a peripheral facing surface with a pair of annular slots, each of a different length and width. A second coupling member has a lock ring longitudinally slidable thereon with a facing surface having a pair of annular raised locking tabs sized to correspond to the respective annular slots. A resilient annular spring mounted within the lock ring urges it toward the first coupling member so that the locking tabs engage their respective slots when the coupling is tightened to a predetermined extent during rotation in the locking direction to releasably and positively lock the coupling. An indicator stripe on the peripheral edge of the first coupling member is exposed before the locking tabs and slots are engaged. Alignment between the respective locking tabs and slots allows longitudinal movement of the lock ring so that it covers the indicator stripe.
    Type: Grant
    Filed: April 30, 1998
    Date of Patent: April 18, 2000
    Assignee: Stanley Aviation Corporation
    Inventors: Ronald W. Boscaljon, Ronald A. Rossway, David E. Jewell
  • Patent number: 5871239
    Abstract: A threaded coupling assembly is provided for interconnecting the ends of first and second fluid-carrying conduit members in fixed releasably locking relationship. First and second coupling members are circumferentially engageable with the ends of the conduit members to hold them in fluid communication. The coupling members are rotatable in a locking direction and in an opposite unlocking direction. The first coupling member has a peripheral facing surface with a pair of annular slots, each of a different length and width. The second coupling member has a lock ring longitudinally slidable thereon with a facing surface having a pair of annular raised locking tabs. Each locking tab is of a predetermined height but of a different length and width which corresponds to the respective length and width of the annular slots.
    Type: Grant
    Filed: October 31, 1996
    Date of Patent: February 16, 1999
    Assignee: Stanley Aviation Corporation
    Inventors: Ronald W. Boscaljon, Ronald A. Rossway, David E. Jewell