Patents by Inventor William G. Hoop

William G. Hoop 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: 7975488
    Abstract: An exhaust duct assembly includes a cooling liner spaced apart from an exhaust duct case that articulate for use in a short take off vertical landing (STOVL) type of aircraft. The cooling liner assembly is attached to the exhaust duct case through a foldable attachment hanger system. The foldable attachment hanger system provides a low profile (foldable up/down) for a limited access installation envelope typical of a three bearing swivel duct (3BSD) which rotates about three bearing planes to permit transition between a cruise configuration and a hover configuration. In this way, each cooling liner segment may be formed as a complete cylindrical member requiring joints only between the swivelable duct sections.
    Type: Grant
    Filed: July 28, 2006
    Date of Patent: July 12, 2011
    Assignee: United Technologies Corporation
    Inventors: Jorge L. Farah, William G. Hoop, Jose M. Cintron
  • Publication number: 20110016879
    Abstract: An exhaust duct assembly includes a cooling liner spaced apart from an exhaust duct case that articulate for use in a short take off vertical landing (STOVL) type of aircraft. The cooling liner assembly is attached to the exhaust duct case through a foldable attachment hanger system. The foldable attachment hanger system provides a low profile (foldable up/down) for a limited access installation envelope typical of a three bearing swivel duct (3BSD) which rotates about three bearing planes to permit transition between a cruise configuration and a hover configuration. In this way, each cooling liner segment may be formed as a complete cylindrical member requiring joints only between the swivelable duct sections.
    Type: Application
    Filed: July 28, 2006
    Publication date: January 27, 2011
    Inventors: Jorge L. Farah, William G. Hoop, Jose M. Cintron
  • Patent number: 7814753
    Abstract: An exhaust duct assembly includes a cooling liner spaced apart from an exhaust duct case that articulate for use in a short take off vertical landing (STOVL) type of aircraft. The cooling liner assembly is attached to the exhaust duct case through a foldable attachment hanger system. The foldable attachment hanger system provides a low profile (foldable up/down) for a limited access installation envelope typical of a three bearing swivel duct (3BSD) which rotates about three bearing planes to permit transition between a cruise configuration and a hover configuration. In this way, each cooling liner segment may be formed as a complete cylindrical member requiring joints only between the swivelable duct sections.
    Type: Grant
    Filed: July 25, 2006
    Date of Patent: October 19, 2010
    Assignee: United Technologies Corporation
    Inventors: Jorge I. Farah, William G. Hoop
  • Publication number: 20080022689
    Abstract: An exhaust duct assembly includes a cooling liner spaced apart from an exhaust duct case that articulate for use in a short take off vertical landing (STOVL) type of aircraft. The cooling liner assembly is attached to the exhaust duct case through a foldable attachment hanger system. The foldable attachment hanger system provides a low profile (foldable up/down) for a limited access installation envelope typical of a three bearing swivel duct (3BSD) which rotates about three bearing planes to permit transition between a cruise configuration and a hover configuration. In this way, each cooling liner segment may be formed as a complete cylindrical member requiring joints only between the swivelable duct sections.
    Type: Application
    Filed: July 25, 2006
    Publication date: January 31, 2008
    Inventors: Jorge L. Farah, William G. Hoop
  • Patent number: 5667140
    Abstract: A seal for a gas turbine engine exhaust nozzle is provided, comprising a body, a spine member attached to one side of the body, and a plurality of face segments attached to the side of the body opposite that to which the spine member is attached. The body includes a length and a width, a plurality of corrugations formed in the body extending across the width, and a first and a second channel. One of the channels is positioned on one side of the body width and the other channel is positioned on the other side of the body width. Each face segment includes a first end and a second end. The ends of the face segments are freely received within the first and second channels such that the ends may translate within the channels.
    Type: Grant
    Filed: December 2, 1994
    Date of Patent: September 16, 1997
    Assignee: United Technologies Corporation
    Inventors: Steven B. Johnson, Curtis W. Berger, Miguel A. Garrido, William G. Hoop
  • Patent number: 5005991
    Abstract: A truncated spherical ball enters a cavity in a link using an entry slot in the link away from the end of the link and axially extending toward the link arm. Passage of the rotated ball through the entry slot is prevented by excess thickness of the ball relative to slot width until the link is expanded by heating. Full bearing surface exists at the end and sides of the link cavity and bearing surfaces are not contacted while forcing a fit. The ball is secure from inadvertent removal.
    Type: Grant
    Filed: December 4, 1987
    Date of Patent: April 9, 1991
    Assignee: United Technologies Corporation
    Inventors: David E. Heumann, William G. Hoop