Patents by Inventor Kerrick Robert Dando
Kerrick Robert Dando 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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Publication number: 20230398748Abstract: A system and method for fusing at least two thermoplastic composite components together may include placing faying surfaces of the thermoplastic composite components in contact with each other, placing a separation layer over and against one of the thermoplastic composite components, and placing a multi-layer composite pressure pad over and in contact with the separation layer. The method may also include placing an activated inductor against the multi-layer composite pressure pad for induction welding the two thermoplastic composite components to each other. The thermoplastic composite components may comprise conductive fibers while the multi-layer composite pressure pad may comprise a first layer and a second layer with non-conductive fibers. The first layer may at least partially melt during induction welding of the two thermoplastic composite components while the second layer may remain rigid throughout this welding.Type: ApplicationFiled: June 8, 2022Publication date: December 14, 2023Applicant: Spirit AeroSystems, Inc.Inventor: Kerrick Robert Dando
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Publication number: 20230191528Abstract: A method of manufacturing metal matrix composite (MMC) parts, including the steps of applying a metallic sheath around a bundle of MMC laminates, heating the bundle of MMC laminates in the metallic sheath at a curing or fusing temperature to consolidate the bundle of MMC laminates into a single cured or fused part, and then cooling the cured or fused part. The bundle of MMC laminates may be formed by removing surface contamination from the dry reinforcement fibers, creating a plurality of individual MMC laminates by plating dry reinforcement fibers with electroless nickel, and/or electrodeposited nickel or cobalt, and stacking each of the plurality of individual MMC laminates into a bundle. Autocatalytic and/or electroplating may be used as the primary means to incorporate fiber reinforcement into the metal matrix composite by covering and bonding fiber reinforcement into MMC laminates/plies and/or 3-D woven parts.Type: ApplicationFiled: December 22, 2021Publication date: June 22, 2023Applicant: Spirit AeroSystems, Inc.Inventors: Rahbar Nasserrafi, Kerrick Robert Dando, Gerald Eugene Hicks, JR., Theodore Joseph Eilert, Shawn Douglas Vierthaler
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Publication number: 20230191712Abstract: Disclosed is a method of resistance welding between composite articles. A conductive element is provided between faying surfaces, having a plurality of lower resistivity electrode portions spaced apart along the length of the contact area between the composite articles. The electrode portions can be used to spot weld across the electrode portions, and along a longitudinal portion of the conductive element between the electrode portions by application of an electrical current. Also disclosed are apparatus for use in the resistance welding methods and composite articles and structures and elements incorporating the conductive element.Type: ApplicationFiled: February 15, 2023Publication date: June 22, 2023Applicants: Spirit AeroSystems, Inc., Stichting TPRCInventors: Kerrick Robert Dando, Andrea Christine Meyer, Ulrich Sachs, Thibault Hernandez
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Patent number: 11607852Abstract: Disclosed is a method of resistance welding between composite articles. A conductive element is provided between faying surfaces, having a plurality of lower resistivity electrode portions spaced apart along the length of the contact area between the composite articles. The electrode portions can be used to spot weld across the electrode portions, and along a longitudinal portion of the conductive element between the electrode portions by application of an electrical current. Also disclosed are apparatus for use in the resistance welding methods and composite articles and structures and elements incorporating the conductive element.Type: GrantFiled: January 20, 2022Date of Patent: March 21, 2023Assignees: Spirit AeroSystems, Inc., Stichting TPRCInventors: Kerrick Robert Dando, Andrea Christine Meyer, Ulrich Sachs, Thibault Hernandez
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Patent number: 11571861Abstract: A system and method for thermoplastic composite welding comprising a cooling means and a heat source. The cooling means cools a heat-side laminate so as to create a thermal gradient in the heat-side laminate. The heat source heats the heat-side laminate after the cooling step is initiated but before the thermal gradient dissipates so that a first side of the heat-side laminate closer to the heat source does not deform as faying surfaces of the heat-side laminate and another laminate farther away from the heat source are welded together.Type: GrantFiled: August 26, 2021Date of Patent: February 7, 2023Assignee: Spirit AeroSystems, Inc.Inventors: Mark Anthony Wadsworth, Kerrick Robert Dando
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Publication number: 20220227066Abstract: Disclosed is a method of resistance welding between composite articles. A conductive element is provided between faying surfaces, having a plurality of lower resistivity electrode portions spaced apart along the length of the contact area between the composite articles. The electrode portions can be used to spot weld across the electrode portions, and along a longitudinal portion of the conductive element between the electrode portions by application of an electrical current. Also disclosed are apparatus for use in the resistance welding methods and composite articles and structures and elements incorporating the conductive element.Type: ApplicationFiled: January 20, 2022Publication date: July 21, 2022Applicants: Spirit AeroSystems, Inc., Stichting TPRCInventors: Kerrick Robert Dando, Andrea Christine Meyer, Ulrich Sachs, Thibault Hernandez
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Publication number: 20220152939Abstract: A system and method for welding thermoplastic components by positioning and moving a heated plate between the components to melt their respective faying surfaces, and as the plate moves, pressing the components together so that the melted faying surfaces bond together as they cool and re-solidify, thereby creating a composite structure. The plate has a heated portion which is positioned between and heated to melt a portion of the first and second faying surfaces. A manipulator mechanism moves the plate along an interface from between the portion to between a series of subsequent portions of the first and second faying surfaces, thereby welding the thermoplastic components along the entire interface to create the composite structure. An injection device may also move behind the plate and reciprocally inject a polymer between the first and second faying surfaces to provide toughness and crack arresting properties.Type: ApplicationFiled: February 1, 2022Publication date: May 19, 2022Applicant: Spirit AeroSystems, Inc.Inventors: Mark Wadsworth, Kerrick Robert Dando, Rahbar Nasserrafi
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Publication number: 20210379840Abstract: A system and method for thermoplastic composite welding comprising a cooling means and a heat source. The cooling means cools a heat-side laminate so as to create a thermal gradient in the heat-side laminate. The heat source heats the heat-side laminate after the cooling step is initiated but before the thermal gradient dissipates so that a first side of the heat-side laminate closer to the heat source does not deform as faying surfaces of the heat-side laminate and another laminate farther away from the heat source are welded together.Type: ApplicationFiled: August 26, 2021Publication date: December 9, 2021Applicant: Spirit AeroSystems, Inc.Inventors: Mark Anthony Wadsworth, Kerrick Robert Dando
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Publication number: 20200269487Abstract: A system and method for forming a part using a moveable heater to heat a pre-aligned blank and an alignment mechanism to maintain the alignment of the heated blank during the forming process. A frame receives and holds the blank in the pre-aligned position within an open press. The heater advances into the press to heat the pre-aligned blank to a forming temperature, and withdraws to allow the press to close and form the heated blank into the part. The alignment mechanism maintains the blank in the alignment while the blank is heated and the press is closed, and includes a rail extending through the press and the frame and allowing the press to move between open and closed positions, and a collapsible member which pushes the frame as the press closes and collapses to allow the press to fully close and form the heated blank into the part.Type: ApplicationFiled: February 22, 2019Publication date: August 27, 2020Applicant: Spirit AeroSystems, Inc.Inventor: Kerrick Robert Dando