Patents by Inventor Harold J. Palin

Harold J. Palin 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: 8091862
    Abstract: A butterfly valve having a valve body, a butterfly shaft, a butterfly plate, and a sleeve insert is provided. The valve body is made of a first material and the sleeve insert is made of a second material. The butterfly shaft is in the valve body for rotation about a first axis. The butterfly plate is in the valve body and secured to the butterfly shaft so that rotation of the butterfly shaft causes the butterfly plate to rotate about a second axis through a travel path between a closed position and an open position. The sleeve insert is in the valve body at least in a region of the travel path between the valve body and the butterfly plate.
    Type: Grant
    Filed: September 29, 2006
    Date of Patent: January 10, 2012
    Assignee: Sikorsky Aircraft Corporation
    Inventors: Harold J. Palin, Lawrence N. Secchiaroli, John C. Luckachina, Alexander Vygoder
  • Publication number: 20080078972
    Abstract: A butterfly valve having a valve body, a butterfly shaft, a butterfly plate, and a sleeve insert is provided. The valve body is made of a first material and the sleeve insert is made of a second material. The butterfly shaft is in the valve body for rotation about a first axis. The butterfly plate is in the valve body and secured to the butterfly shaft so that rotation of the butterfly shaft causes the butterfly plate to rotate about a second axis through a travel path between a closed position and an open position. The sleeve insert is in the valve body at least in a region of the travel path between the valve body and the butterfly plate.
    Type: Application
    Filed: September 29, 2006
    Publication date: April 3, 2008
    Inventors: Harold J. Palin, Lawrence N. Secchiaroli, John C. Luckachina, Alexander Vygoder
  • Patent number: 6848652
    Abstract: An aircraft heating system taps into a bleed air flowpath between a turbine engine and an external bleed air port on the aircraft. A system may be installed as a retrofit for heating the cabin of an aircraft already having a heating system for heating the cockpit.
    Type: Grant
    Filed: February 28, 2003
    Date of Patent: February 1, 2005
    Assignee: Sikorsky Aircraft Corporation
    Inventors: Harold J. Palin, Roger V. Backert, Curtis S. James, Anthony Schultz
  • Publication number: 20040195444
    Abstract: An aircraft heating system taps into a bleed air flowpath between a turbine engine and an external bleed air port on the aircraft. A system may be installed as a retrofit for heating the cabin of an aircraft already having a heating system for heating the cockpit.
    Type: Application
    Filed: February 28, 2003
    Publication date: October 7, 2004
    Inventors: Harold J. Palin, Roger V. Backert, Curtis S. James, Anthony Schultz