Patents by Inventor Glenn A. Dildy

Glenn A. Dildy 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: 11738836
    Abstract: A boat cradle assembly is adapted for dry storage of a pontoon boat having a deck and a hull. The hull includes a tubular midline pontoon. The boat cradle assembly comprises first and second spaced apart longitudinal side beam. A plurality of crossbeams extends between the first and second side beams. Each crossbeam has a substantially V-shaped bottom structure and a top structure. The V-shaped bottom structure is configured to reside between and engage spaced apart frame members of a dry storage rack. The top structure defines an intermediate arcuate formation configured to accommodate a rounded underside of the midline pontoon.
    Type: Grant
    Filed: December 13, 2021
    Date of Patent: August 29, 2023
    Assignee: Veeline Marine Equipment, LLC
    Inventor: Marshall Glenn Dildy
  • Patent number: 7209814
    Abstract: A diagnostic system and method for enabling multistage decision optimization in aircraft preflight dispatch. The diagnostic system includes an interface for receiving one or more inputs relating to one or more observed symptoms indicative of a failed component in an aircraft. The diagnostic system extends an entropy-based value of information (VOI) diagnostic model by adding an explicit value function into the VOI diagnostic model to accommodate various variables associated with the aircraft preflight dispatch problem. The construction of the entropy-based VOI diagnostic model and thus the extended VOI diagnostic model are both based upon at least one of systemic information relating to aircraft components and input-output relationships of the aircraft components, experience-based information relating to direct relationships between aircraft component failures and observed symptoms, and factual information relating to aircraft component reliability.
    Type: Grant
    Filed: March 12, 2004
    Date of Patent: April 24, 2007
    Assignee: The Boeing Company
    Inventors: Oscar Kipersztok, Glenn A. Dildy
  • Patent number: 6868319
    Abstract: A diagnostic system and method are provided that include an interface for receiving input relating to observed symptoms indicative of one or more failed components, a processing element for correlating the input relating to the observed symptoms with at least one suspect component that is capable of causing the observed symptoms upon failure, and a display for presenting information relating to the suspect components. The processing element correlates the input relating to the observed symptoms with the suspect components in accordance with a diagnostic model constructed based upon systemic information, experiential information and factual information. The processing element generally presents the suspect components in a listing prioritized based upon the relative likelihood that the respective suspect components caused the observed symptoms.
    Type: Grant
    Filed: February 26, 2003
    Date of Patent: March 15, 2005
    Assignee: The Boeing Company
    Inventors: Oscar Kipersztok, Karl J. Rein-Weston, Scott L. Nelson, Glenn A. Dildy, Susan Chan Chew
  • Publication number: 20040199307
    Abstract: A diagnostic system and method for enabling multistage decision optimization in aircraft preflight dispatch. The diagnostic system includes an interface for receiving one or more inputs relating to one or more observed symptoms indicative of a failed component in an aircraft. The diagnostic system extends an entropy-based value of information (VOI) diagnostic model by adding an explicit value function into the VOI diagnostic model to accommodate various variables associated with the aircraft preflight dispatch problem. The construction of the entropy-based VOI diagnostic model and thus the extended VOI diagnostic model are both based upon at least one of systemic information relating to aircraft components and input-output relationships of the aircraft components, experience-based information relating to direct relationships between aircraft component failures and observed symptoms, and factual information relating to aircraft component reliability.
    Type: Application
    Filed: March 12, 2004
    Publication date: October 7, 2004
    Inventors: Oscar Kipersztok, Glenn A. Dildy
  • Patent number: 6751536
    Abstract: A diagnostic system and method for enabling multistage decision optimization in aircraft preflight dispatch. The diagnostic system includes an interface for receiving one or more inputs relating to one or more observed symptoms indicative of a failed component in an aircraft. The diagnostic system extends an entropy-based value of information (VOI) diagnostic model by adding an explicit value function into the VOI diagnostic model to accommodate various variables associated with the aircraft preflight dispatch problem. The construction of the entropy-based VOI diagnostic model and thus the extended VOI diagnostic model are both based upon at least one of systemic information relating to aircraft components and input-output relationships of the aircraft components, experience-based information relating to direct relationships between aircraft component failures and observed symptoms, and factual information relating to aircraft component reliability.
    Type: Grant
    Filed: December 4, 2002
    Date of Patent: June 15, 2004
    Assignee: The Boeing Company
    Inventors: Oscar Kipersztok, Glenn A. Dildy
  • Publication number: 20040111197
    Abstract: A diagnostic system and method for enabling multistage decision optimization in aircraft preflight dispatch. The diagnostic system includes an interface for receiving one or more inputs relating to one or more observed symptoms indicative of a failed component in an aircraft. The diagnostic system extends an entropy-based value of information (VOI) diagnostic model by adding an explicit value function into the VOI diagnostic model to accommodate various variables associated with the aircraft preflight dispatch problem. The construction of the entropy-based VOI diagnostic model and thus the extended VOI diagnostic model are both based upon at least one of systemic information relating to aircraft components and input-output relationships of the aircraft components, experience-based information relating to direct relationships between aircraft component failures and observed symptoms, and factual information relating to aircraft component reliability.
    Type: Application
    Filed: December 4, 2002
    Publication date: June 10, 2004
    Inventors: Oscar Kipersztok, Glenn A. Dildy
  • Publication number: 20030167111
    Abstract: A diagnostic system and method are provided that include an interface for receiving input relating to observed symptoms indicative of one or more failed components, a processing element for correlating the input relating to the observed symptoms with at least one suspect component that is capable of causing the observed symptoms upon failure, and a display for presenting information relating to the suspect components. The processing element that correlates the input relating to the observed symptoms with the suspect components in accordance with a diagnostic model constructed based upon systemic information, experiential information and factual information. The processing element generally presents the suspect components in a listing prioritized based upon the relative likelihood that the respective suspect components caused the observed symptoms.
    Type: Application
    Filed: February 26, 2003
    Publication date: September 4, 2003
    Applicant: The Boeing Company
    Inventors: Oscar Kipersztok, Karl J. Rein-Weston, Scott L. Nelson, Glenn A. Dildy, Susan Chan Chew
  • Patent number: 6574537
    Abstract: A diagnostic system and method are provided that include an interface for receiving input relating to observed symptoms indicative of one or more failed components, a processing element for correlating the input relating to the observed symptoms with at least one suspect component that is capable of causing the observed symptoms upon failure, and a display for presenting information relating to the suspect components. The processing element correlates the input relating to the observed symptoms with the suspect components in accordance with a diagnostic model constructed based upon systemic information, experiential information and factual information. The processing element generally presents the suspect components in a listing prioritized based upon the relative likelihood that the respective suspect components caused the observed symptoms.
    Type: Grant
    Filed: February 5, 2001
    Date of Patent: June 3, 2003
    Assignee: The Boeing Company
    Inventors: Oscar Kipersztok, Karl J. Rein-Weston, Scott L. Nelson, Glenn A. Dildy, Nicholas James Walker, Susan Chan Chew
  • Patent number: D1002494
    Type: Grant
    Filed: October 18, 2021
    Date of Patent: October 24, 2023
    Assignee: Veeline Marine Equipment, LLC
    Inventor: Marshall Glenn Dildy