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公开(公告)号：US20240208255A1
公开(公告)日：2024-06-27
申请号：US18087505
申请日：2022-12-22
申请人： The Boeing Company
发明人： Shane E. Arthur , John E. Miller , Matthew Mellin , Kjersta Larson-Smith , Anthony Baker , Luke Ingram , Steven Dorris , Jonathan Schwedhelm , Mark Bunker , Ryan Petz , Travis King , Matt Christner , Josiah Brubaker , Ryan Siok , Wendy Zaballos , Jesse Castleberry
摘要： An end effector for printing ink on a surface is disclosed. The end effector comprises a primary block comprises a primary-block body. A plurality of primary-printing modules are coupled to the primary-block body and translationally moveable, via a corresponding first actuator. Each one of the primary-printing modules includes at least one printhead which is adjustable, relative to the primary-block body. The printhead may be adjusted by at least one of a second actuator, configured to rotate the printhead about a first axis, or a third actuator, configured to rotate the printhead about a second axis. In some examples, a fourth actuator is configured to rotate at least one printhead, relative to at least one other printhead, about a third axis. Additionally, at least one trailing block can be coupled to the primary block so that the at least one trailing block is movable relative to the primary block.
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公开(公告)号：US20240253339A1
公开(公告)日：2024-08-01
申请号：US18160057
申请日：2023-01-26
申请人： The Boeing Company
发明人： Kjersta Larson-Smith , Terrell D. Riley , Christopher Garnier , Alexandra E. Corona , Jessica O. Fry , Kevin D. Gordon , Mark R. Brei
IPC分类号： B32B27/40 , B32B7/10 , B32B27/08 , B32B27/12 , B32B27/18 , B32B27/38 , B32B37/10 , B32B38/08
CPC分类号： B32B27/40 , B32B7/10 , B32B27/08 , B32B27/12 , B32B27/18 , B32B27/38 , B32B37/1018 , B32B38/08 , B32B2038/0076 , B32B2260/021 , B32B2260/046 , B32B2307/71 , B32B2363/00 , B32B2375/00
摘要： A method of manufacturing a resin-infused part, may include: preparing a laminate by layering a curable protective film onto a fibrous preform; infusing resin into the laminate under a vacuum, such that the resin impregnates the fibrous preform and the protective film adheres to the fibrous preform; and curing the laminate at a curing temperature.
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公开(公告)号：US20240109349A1
公开(公告)日：2024-04-04
申请号：US17937227
申请日：2022-09-30
申请人： The Boeing Company
IPC分类号： B41J25/304 , B41J3/407
CPC分类号： B41J25/304 , B41J3/4073
摘要： The present disclosure includes a method and apparatus for ink jet printing an exterior surface of a vehicle including a reversibly moveable crossbeam mounted above an open pit; a first track located above the reversibly moveable crossbeam, a first reversibly moveable monument including a first serial robotic manipulator including a first end effector defining a first end effector range of motion based on fully extended reversible movement of the first serial robotic manipulator; a second track located in the open pit beneath the reversibly moveable crossbeam; a second reversibly moveable monument coupled to the second pair of rails, the second reversibly moveable monument including a second end effector defining a second end effector range of motion based on fully extended reversible movement of the second serial robotic manipulator. The first end effector range of motion overlaps the second end effector range of motion.
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公开(公告)号：US20240149299A1
公开(公告)日：2024-05-09
申请号：US17983162
申请日：2022-11-08
申请人： The Boeing Company
CPC分类号： B05D7/576 , B41J2/04586 , B41J3/413 , B41M5/0011 , B41M7/0027
摘要： Disclosed herein is a surface preparation and livery printing system and a method of preparing a surface and printing a livery. The method includes preparing a surface of an aircraft part in a first processing booth to form a prepared surface of the aircraft part. The method also includes transporting the aircraft part to a second processing booth being adjacent to the first processing booth upon completion of preparing the surface. The method further includes applying a livery to the prepared surface of the aircraft part in a second processing booth and upon completion of applying the livery, transporting the aircraft part to a third processing booth being adjacent to the second processing booth. The method still further includes applying a clearcoat over at least the livery applied to the prepared surface of the aircraft part in a third processing booth.
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公开(公告)号：US20240109095A1
公开(公告)日：2024-04-04
申请号：US17937237
申请日：2022-09-30
申请人： The Boeing Company
摘要： The present disclosure includes a method and apparatus for changing livery on a vehicle. A method of inkjet printing an exterior surface of a vehicle, includes preparing at least a portion of the exterior surface of the vehicle in a first bay using crossflow or downflow air handling and using explosion protected equipment. That method includes inkjet printing at least the portion of the exterior surface of the vehicle in a second bay. This method includes clear-coating at least the portion of the exterior surface of the vehicle in a third bay using downflow or crossflow air handling, using air filtration and using explosion protected equipment.
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6.发明授权公开(公告)号：US12070770B2
公开(公告)日：2024-08-27
申请号：US16515121
申请日：2019-07-18
申请人： The Boeing Company
IPC分类号： B05D7/00 , C09J163/00
CPC分类号： B05D7/584 , C09J163/00 , B05D2201/02 , B05D2420/00 , B05D2503/00 , B05D2504/00 , C09J2463/006
摘要： A composite structure having a co-curable or co-cured coated epoxy-based composite material coated with a co-curable epoxy-based adhesive surfacing material layer and a polyurethane-based coating material layer, along with components and large objects including the co-curable or co-cured coated epoxy-based composite structures.
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公开(公告)号：US20240198703A1
公开(公告)日：2024-06-20
申请号：US18082334
申请日：2022-12-15
申请人： The Boeing Company
发明人： Shane E. Arthur , John E. Miller , Matthew Mellin , Kjersta Larson-Smith , Anthony Baker , Luke Ingram , Steven Dorris , Jonathan Schwedhelm , Mark Bunker , Ryan Petz , Travis King , Jesse Castleberry , Matt Christner
CPC分类号： B41J25/001 , B41J3/4073
摘要： An end effector and associated systems and methods for printing ink on a surface is disclosed. The end effector comprises a main block including a back plate. The end effector also includes a plurality of slice assemblies slidably coupled to the back plate. Each one of the plurality of slice assemblies includes a printhead and a y-actuator. The y-actuator is selectively operable to extend and retract the printhead, parallel to a y-axis in first directions, and relative to the back plate. The end effector further includes a plurality of z-actuators coupled to the back plate. Each one of the plurality of z-actuators is selectively operable to extend and retract a corresponding one of the plurality of slice assemblies, parallel to a z-axis in second directions, which is perpendicular to the y-axis and relative to the back plate.
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公开(公告)号：US20240149300A1
公开(公告)日：2024-05-09
申请号：US17983166
申请日：2022-11-08
申请人： The Boeing Company
发明人： Kjersta Larson-Smith , Shane Arthur , Edward Greene , Matthew Mellin , Alexandra Corona , Terrell Riley
CPC分类号： B05D7/576 , B41J2/04586 , B41J3/413 , B41M5/0011 , B41M7/0027
摘要： Disclosed herein is a surface repair and livery printing system and method. The method includes receiving an aircraft part having an altered surface image and selecting a repair process from one of a paint repair process, a decal repair process, or an inkjet repair process, based on characteristics of the altered surface image. The method also includes applying paint to the surface over the altered surface image. In response to selecting the decal repair process, the method includes printing a first image on a decal based on the characteristics of the altered surface image and a second image associated with the altered surface image and a step of applying the decal to the surface at least partially over the altered surface image. In response to selecting the inkjet repair process, the method includes performing the inkjet repair process to at least a portion of the surface based on the characteristics of the altered surface image.
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公开(公告)号：US11590746B2
公开(公告)日：2023-02-28
申请号：US16515225
申请日：2019-07-18
申请人： The Boeing Company
IPC分类号： B32B17/04 , B32B27/38 , B32B5/02 , B32B27/08 , B32B27/12 , B32B27/20 , B32B27/26 , B32B27/40 , C08J5/04 , C08J9/00 , C08J7/04
摘要： Co-curable epoxy-based composite materials coated with co-curable polyurethane-based coating materials to form co-curable and co-cured polyurethane coated epoxy-based composite materials, with the polyurethane-based coating materials comprising UV-stabilizer agents and cure control agents are disclosed, along with components and large structures comprising the co-cured materials.
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公开(公告)号：US20170152949A1
公开(公告)日：2017-06-01
申请号：US14954270
申请日：2015-11-30
申请人： THE BOEING COMPANY
发明人： Jesse Randal Wiseman , Shane S. Park , Donald K. Crenshaw , Kjersta Larson-Smith , Geoffrey Eric Towle , Hugh Christopher VanValkenburgh , Karen A. Schultz , Solomon T. Atsebha
CPC分类号： F16J15/002 , B64C3/00 , B64F5/10 , F16J15/14
摘要： A sealant containment assembly is configured to bound at least a portion of a fastener pattern between at least two components, such as components used to form at least a portion of an aircraft. The sealant containment assembly includes at least one sealant containment member that is configured to sealingly engage peripheral portions of components. The sealant containment member(s) is configured to form a sealing chamber around at least a portion of the fastener pattern. Fluid sealant is configured to flow into the sealing chamber and cure to seal fasteners within the fastener pattern that connect the components together.
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