Patents by Inventor Patrick G. Jarvis-Shean
Patrick G. Jarvis-Shean 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: 11833798Abstract: In a preferred embodiment, a composite panel with a smooth outer surface, ready for painting with or without addition of primer, may be created by constructing a panel layup assembly upon a mold, the panel layup assembly including a composite panel having a core and a resin formulation, and a release film between the mold and the composite panel, where a smooth release surface of the release film is in contact with the composite panel upon construction; initiating curing of the composite panel at a first temperature within a lowermost ten percent of a curing temperature range of the resin formulation; continuing curing of the composite panel at a second temperature above the lowermost ten percent of the curing temperature range; and completing curing of the composite panel at a third temperature below the second temperature.Type: GrantFiled: July 12, 2021Date of Patent: December 5, 2023Assignee: B/E Aerospace, Inc.Inventors: George T. Franck, III, Alvin S. Bartolome, Patrick G. Jarvis-Shean
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Patent number: 11766856Abstract: In a preferred embodiment, a composite panel with a smooth outer surface, ready for painting with or without addition of primer, may be created by constructing a panel layup assembly upon a mold, the panel layup assembly including a composite panel having a core and a resin formulation, and a release film between the mold and the composite panel, where a smooth release surface of the release film is in contact with the composite panel upon construction; initiating curing of the composite panel at a first temperature within a lowermost ten percent of a curing temperature range of the resin formulation; continuing curing of the composite panel at a second temperature above the lowermost ten percent of the curing temperature range; and completing curing of the composite panel at a third temperature below the second temperature.Type: GrantFiled: January 5, 2022Date of Patent: September 26, 2023Assignee: B/E Aerospace, Inc.Inventors: George T. Franck, III, Alvin S. Bartolome, Patrick G. Jarvis-Shean
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Publication number: 20220126556Abstract: In a preferred embodiment, a composite panel with a smooth outer surface, ready for painting with or without addition of primer, may be created by constructing a panel layup assembly upon a mold, the panel layup assembly including a composite panel having a core and a resin formulation, and a release film between the mold and the composite panel, where a smooth release surface of the release film is in contact with the composite panel upon construction; initiating curing of the composite panel at a first temperature within a lowermost ten percent of a curing temperature range of the resin formulation; continuing curing of the composite panel at a second temperature above the lowermost ten percent of the curing temperature range; and completing curing of the composite panel at a third temperature below the second temperature.Type: ApplicationFiled: January 5, 2022Publication date: April 28, 2022Applicant: B/E Aerospace, Inc.Inventors: George T. Franck, III, Alvin S. Bartolome, Patrick G. Jarvis-Shean
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Patent number: 11247448Abstract: In a preferred embodiment, a composite panel with a smooth outer surface, ready for painting with or without addition of primer, may be created by constructing a panel layup assembly upon a mold, the panel layup assembly including a composite panel having a core and a resin formulation, and a release film between the mold and the composite panel, where a smooth release surface of the release film is in contact with the composite panel upon construction; initiating curing of the composite panel at a first temperature within a lowermost ten percent of a curing temperature range of the resin formulation; continuing curing of the composite panel at a second temperature above the lowermost ten percent of the curing temperature range; and completing curing of the composite panel at a third temperature below the second temperature.Type: GrantFiled: August 27, 2016Date of Patent: February 15, 2022Assignee: B/E Aerospace, Inc.Inventors: George T. Franck, III, Alvin S. Bartolome, Patrick G. Jarvis-Shean
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Publication number: 20210394501Abstract: In a preferred embodiment, a composite panel with a smooth outer surface, ready for painting with or without addition of primer, may be created by constructing a panel layup assembly upon a mold, the panel layup assembly including a composite panel having a core and a resin formulation, and a release film between the mold and the composite panel, where a smooth release surface of the release film is in contact with the composite panel upon construction; initiating curing of the composite panel at a first temperature within a lowermost ten percent of a curing temperature range of the resin formulation; continuing curing of the composite panel at a second temperature above the lowermost ten percent of the curing temperature range; and completing curing of the composite panel at a third temperature below the second temperature.Type: ApplicationFiled: July 12, 2021Publication date: December 23, 2021Applicant: B/E Aerospace, Inc.Inventors: George T. Franck, Alvin S. Bartolome, Patrick G. Jarvis-Shean
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Patent number: 9987832Abstract: A method for curing a composite panel, including the steps of inserting a Biaxially Oriented Polypropylene release film into a mold, and curing the panel using a cold-in/cold-out process at a lowermost temperature within the panel's temperature curing range. The process further includes the use of a twice smoothed caul sheet, where the smoothing includes a coarse sanding and a fine sanding.Type: GrantFiled: February 25, 2015Date of Patent: June 5, 2018Assignee: B/E Aerospace, Inc.Inventors: George T. Franck, Alvin S. Bartolome, Patrick G. Jarvis-Shean
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Publication number: 20160361910Abstract: In a preferred embodiment, a composite panel with a smooth outer surface, ready for painting with or without addition of primer, may be created by constructing a panel layup assembly upon a mold, the panel layup assembly including a composite panel having a core and a resin formulation, and a release film between the mold and the composite panel, where a smooth release surface of the release film is in contact with the composite panel upon construction; initiating curing of the composite panel at a first temperature within a lowermost ten percent of a curing temperature range of the resin formulation; continuing curing of the composite panel at a second temperature above the lowermost ten percent of the curing temperature range; and completing curing of the composite panel at a third temperature below the second temperature.Type: ApplicationFiled: August 27, 2016Publication date: December 15, 2016Applicant: B/E AEROSPACE, INC.Inventors: George T. FRANCK, III, Alvin S. BARTOLOME, Patrick G. JARVIS-SHEAN
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Publication number: 20150239226Abstract: A method for curing a composite panel, including the steps of inserting a Biaxially Oriented Polypropylene release film into a mold, and curing the panel using a cold-in/cold-out process at a lowermost temperature within the panel's temperature curing range. The process further includes the use of a twice smoothed caul sheet, where the smoothing includes a coarse sanding and a fine sanding.Type: ApplicationFiled: February 25, 2015Publication date: August 27, 2015Inventors: George T. Franck, III, Alvin S. Bartolome, Patrick G. Jarvis-Shean