Patents by Inventor Peter Babilo
Peter Babilo 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: 11292943Abstract: Provided are methods of forming thermally conductive flexible bonds for use in electronic boards of unmanned spacecraft and other types of aircraft. Also provided are methods of preparing adhesive materials to form these bonds including methods of preparing treated filler particles. In some aspects, an adhesive material includes filler particles having organofunctional groups, such as boron nitride particles treated in silane. These particles may be combined with a urethane modified epoxy to form the adhesive material. The weight ratio of the particles in the adhesive material may be about 40-60%. The adhesive material may be thermally cured using a temperature of less than 110° C. to prevent damage to bonded electronic components. The cured adhesive may have a thermal conductivity of at least about 2 W/m K measured in vacuum and may have a glass transition temperature if less than ?40° C.Type: GrantFiled: May 13, 2019Date of Patent: April 5, 2022Assignee: The Boeing CompanyInventors: Peter Babilo, Randall Jay Moss
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Patent number: 10844230Abstract: The present disclosure relates to highly reflective coating formulations that produce coatings having an average infrared reflectivity ranging from about 75% to about 90% at wavelengths ranging from about 0.5 ?m to about 1000 ?m, methods for making the coatings and coating mixtures, and substrates comprising such coatings.Type: GrantFiled: February 7, 2017Date of Patent: November 24, 2020Assignee: The Boeing CompanyInventors: Peter Babilo, Giuseppe A. Russo
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Publication number: 20190264073Abstract: Provided are methods of forming thermally conductive flexible bonds for use in electronic boards of unmanned spacecraft and other types of aircraft. Also provided are methods of preparing adhesive materials to form these bonds including methods of preparing treated filler particles. In some aspects, an adhesive material includes filler particles having organofunctional groups, such as boron nitride particles treated in silane. These particles may be combined with a urethane modified epoxy to form the adhesive material. The weight ratio of the particles in the adhesive material may be about 40-60%. The adhesive material may be thermally cured using a temperature of less than 110° C. to prevent damage to bonded electronic components. The cured adhesive may have a thermal conductivity of at least about 2 W/m K measured in vacuum and may have a glass transition temperature if less than ?40° C.Type: ApplicationFiled: May 13, 2019Publication date: August 29, 2019Applicant: The Boeing CompanyInventors: Peter Babilo, Randall Jay Moss
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Patent number: 10336916Abstract: Provided are methods of forming thermally conductive flexible bonds for use in electronic boards of unmanned spacecraft and other types of aircraft. Also provided are methods of preparing adhesive materials to form these bonds including methods of preparing treated filler particles. In some aspects, an adhesive material includes filler particles having organofunctional groups, such as boron nitride particles treated in silane. These particles may be combined with a urethane modified epoxy to form the adhesive material. The weight ratio of the particles in the adhesive material may be about 40-60%. The adhesive material may be thermally cured using a temperature of less than 110° C. to prevent damage to bonded electronic components. The cured adhesive may have a thermal conductivity of at least about 2 W/m K measured in vacuum and may have a glass transition temperature if less than ?40° C.Type: GrantFiled: May 23, 2018Date of Patent: July 2, 2019Assignee: The Boeing CompanyInventors: Peter Babilo, Randall Jay Moss
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Publication number: 20190152626Abstract: A thermal control tape for providing thermal control of a spacecraft structure, to which the thermal control tape is applied is provided. The thermal control tape has a filled silicone resin layer having a first side and a second side. The filled silicone resin layer has a silicone resin material filled with a white inorganic filler material. The tape further has a silicone pressure sensitive adhesive (PSA) layer having a first side and a second side, the first side of the silicone PSA layer attached to the second side of the filled silicone resin layer. The filled silicone resin layer and the silicone PSA layer form the thermal control tape, with the second side of the silicone PSA layer configured for attachment to at least one surface of the spacecraft structure of a spacecraft, to provide thermal control of the spacecraft structure, by radiating heat away from the spacecraft structure.Type: ApplicationFiled: November 22, 2017Publication date: May 23, 2019Inventor: Peter Babilo
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Publication number: 20180265751Abstract: Provided are methods of forming thermally conductive flexible bonds for use in electronic boards of unmanned spacecraft and other types of aircraft. Also provided are methods of preparing adhesive materials to form these bonds including methods of preparing treated filler particles. In some aspects, an adhesive material includes filler particles having organofunctional groups, such as boron nitride particles treated in silane. These particles may be combined with a urethane modified epoxy to form the adhesive material. The weight ratio of the particles in the adhesive material may be about 40-60%. The adhesive material may be thermally cured using a temperature of less than 110° C. to prevent damage to bonded electronic components. The cured adhesive may have a thermal conductivity of at least about 2 W/m K measured in vacuum and may have a glass transition temperature if less than ?40° C.Type: ApplicationFiled: May 23, 2018Publication date: September 20, 2018Applicant: The Boeing CompanyInventors: Peter Babilo, Randall Jay Moss
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Publication number: 20180223106Abstract: The present disclosure relates to highly reflective coating formulations that produce coatings having an average infrared reflectivity ranging from about 75% to about 90% at wavelengths ranging from about 0.5 ?m to about 1000 ?m, methods for making the coatings and coating mixtures, and substrates comprising such coatings.Type: ApplicationFiled: February 7, 2017Publication date: August 9, 2018Inventors: PETER BABILO, GIUSEPPE A. RUSSO
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Patent number: 10005927Abstract: Provided are methods of forming thermally conductive flexible bonds for use in electronic boards of unmanned spacecrafts and other types of aircraft. Also provided are methods of preparing adhesive materials to form these bonds including methods of preparing treated filler particles. In some aspects, an adhesive material includes filler particles having organofunctional groups, such as boron nitride particles treated in silane. These particles may be combined with a urethane modified epoxy to form the adhesive material. The weight ratio of the particles in the adhesive material may be about 40-60%. The adhesive material may be thermally cured using a temperature of less than 110° C. to prevent damage to bonded electronic components. The cured adhesive may have a thermal conductivity of at least about 2 W/m K measured in vacuum and may have a glass transition temperature if less than ?40° C.Type: GrantFiled: September 7, 2016Date of Patent: June 26, 2018Assignee: The Boeing CompanyInventors: Peter Babilo, Randall Jay Moss
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Publication number: 20160376477Abstract: Provided are methods of forming thermally conductive flexible bonds for use in electronic boards of unmanned spacecrafts and other types of aircraft. Also provided are methods of preparing adhesive materials to form these bonds including methods of preparing treated filler particles. In some aspects, an adhesive material includes filler particles having organofunctional groups, such as boron nitride particles treated in silane. These particles may be combined with a urethane modified epoxy to form the adhesive material. The weight ratio of the particles in the adhesive material may be about 40-60%. The adhesive material may be thermally cured using a temperature of less than 110° C. to prevent damage to bonded electronic components. The cured adhesive may have a thermal conductivity of at least about 2 W/m K measured in vacuum and may have a glass transition temperature if less than ?40° C.Type: ApplicationFiled: September 7, 2016Publication date: December 29, 2016Applicant: The Boeing CompanyInventors: Peter Babilo, Randall Jay Moss
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Patent number: 9464214Abstract: Provided are methods of forming thermally conductive flexible bonds for use in electronic boards of unmanned spacecrafts and other types of aircraft. Also provided are methods of preparing adhesive materials to form these bonds including methods of preparing treated filler particles. In some aspects, an adhesive material includes filler particles having organofunctional groups, such as boron nitride particles treated in silane. These particles may be combined with a urethane modified epoxy to form the adhesive material. The weight ratio of the particles in the adhesive material may be about 40-60%. The adhesive material may be thermally cured using a temperature of less than 110° C. to prevent damage to bonded electronic components. The cured adhesive may have a thermal conductivity of at least about 2 W/m K measured in vacuum and may have a glass transition temperature if less than ?40° C.Type: GrantFiled: February 25, 2014Date of Patent: October 11, 2016Assignee: The Boeing CompanyInventors: Peter Babilo, Randall Jay Moss
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Publication number: 20150240132Abstract: Provided are methods of forming thermally conductive flexible bonds for use in electronic boards of unmanned spacecrafts and other types of aircraft. Also provided are methods of preparing adhesive materials to form these bonds including methods of preparing treated filler particles. In some aspects, an adhesive material includes filler particles having organofunctional groups, such as boron nitride particles treated in silane. These particles may be combined with a urethane modified epoxy to form the adhesive material. The weight ratio of the particles in the adhesive material may be about 40-60%. The adhesive material may be thermally cured using a temperature of less than 110° C. to prevent damage to bonded electronic components. The cured adhesive may have a thermal conductivity of at least about 2 W/m K measured in vacuum and may have a glass transition temperature if less than ?40° C.Type: ApplicationFiled: February 25, 2014Publication date: August 27, 2015Applicant: The Boeing CompanyInventors: Peter Babilo, Randall Jay Moss