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).
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Patent number: 11738836Abstract: 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: GrantFiled: December 13, 2021Date of Patent: August 29, 2023Assignee: Veeline Marine Equipment, LLCInventor: Marshall Glenn Dildy
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Patent number: 7209814Abstract: 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: GrantFiled: March 12, 2004Date of Patent: April 24, 2007Assignee: The Boeing CompanyInventors: Oscar Kipersztok, Glenn A. Dildy
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Patent number: 6868319Abstract: 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: GrantFiled: February 26, 2003Date of Patent: March 15, 2005Assignee: The Boeing CompanyInventors: Oscar Kipersztok, Karl J. Rein-Weston, Scott L. Nelson, Glenn A. Dildy, Susan Chan Chew
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Publication number: 20040199307Abstract: 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: ApplicationFiled: March 12, 2004Publication date: October 7, 2004Inventors: Oscar Kipersztok, Glenn A. Dildy
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Patent number: 6751536Abstract: 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: GrantFiled: December 4, 2002Date of Patent: June 15, 2004Assignee: The Boeing CompanyInventors: Oscar Kipersztok, Glenn A. Dildy
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Publication number: 20040111197Abstract: 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: ApplicationFiled: December 4, 2002Publication date: June 10, 2004Inventors: Oscar Kipersztok, Glenn A. Dildy
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Publication number: 20030167111Abstract: 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: ApplicationFiled: February 26, 2003Publication date: September 4, 2003Applicant: The Boeing CompanyInventors: Oscar Kipersztok, Karl J. Rein-Weston, Scott L. Nelson, Glenn A. Dildy, Susan Chan Chew
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Patent number: 6574537Abstract: 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: GrantFiled: February 5, 2001Date of Patent: June 3, 2003Assignee: The Boeing CompanyInventors: Oscar Kipersztok, Karl J. Rein-Weston, Scott L. Nelson, Glenn A. Dildy, Nicholas James Walker, Susan Chan Chew
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Patent number: D1002494Type: GrantFiled: October 18, 2021Date of Patent: October 24, 2023Assignee: Veeline Marine Equipment, LLCInventor: Marshall Glenn Dildy