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公开(公告)号：US10800111B2
公开(公告)日：2020-10-13
申请号：US14740493
申请日：2015-06-16
申请人： The Boeing Company
发明人： Jose L. Encinosa , Samuel F. Zambrana , Daniel M. Rotter , Michael Robert Chapman , Stephen K. Halladin , Benjamin Bowen Lee , Joshua Dee Little , Douglas Alan McCarville , Jason A. Medenciy , Russell D. Chiupka , Marcin Artur Rabiega , Andrey F. Yurchik , Martin W. Hansen , Thomas P. Harper
摘要： Composite structure fabrication systems and methods. The systems include a plurality of ply carriers, each of which is configured to support at least one ply segment, and an elongate forming mandrel, which defines an elongate ply forming surface that is shaped to define a surface contour of the composite structure. The systems further include a carrier transfer device, which is configured to selectively convey a selected ply carrier from a ply kitting area to an intermediate location, and a forming machine, which is configured to deform the selected ply carrier and a respective ply segment over a selected portion of the elongate ply forming surface. The forming machine further is configured to separate the selected ply carrier from the respective ply segment and return the selected ply carrier to the carrier transfer device. The methods include methods of operating the systems.
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公开(公告)号：US10773787B2
公开(公告)日：2020-09-15
申请号：US15623277
申请日：2017-06-14
申请人： The Boeing Company
摘要： Wing-to-fuselage joints and aircraft including the same. An aircraft includes a fuselage with an outer fuselage skin that at least partially defines an outer surface of the fuselage and a wing assembly operably coupled to the fuselage via a wing-to-fuselage joint. The wing assembly includes a left wing region with a lower left-wing-region skin and an upper left-wing-region skin, a right wing region with a lower right-wing-region skin and an upper right-wing-region skin, and a center wing region with a lower center-wing-region skin and an upper center-wing-region skin. The upper center-wing-region skin is coextensive with at least one of the upper left-wing-region skin and the upper right-wing-region skin.
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公开(公告)号：US10766598B2
公开(公告)日：2020-09-08
申请号：US15623256
申请日：2017-06-14
申请人： The Boeing Company
摘要： Wing-to-fuselage joints and aircraft including the same. An aircraft includes a fuselage with an outer fuselage skin that at least partially defines an outer surface of the fuselage and a wing assembly operably coupled to the fuselage via a wing-to-fuselage joint. The wing assembly includes a left wing region with a lower left-wing-region skin and an upper left-wing-region skin, a right wing region with a lower right-wing-region skin and an upper right-wing-region skin, and a center wing region with a lower center-wing-region skin. The outer fuselage skin is coextensive with the lower center-wing-region skin.
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公开(公告)号：US10766241B2
公开(公告)日：2020-09-08
申请号：US15356420
申请日：2016-11-18
申请人： The Boeing Company
IPC分类号： B29C64/135 , B33Y10/00 , B29C64/264 , B29C64/106 , B29C64/20 , B33Y30/00 , B29C35/08
摘要： Systems for additive manufacturing comprise a delivery guide configured to dispense a curable material to additively manufacture a part in sequential layers of the curable material, and a source of curing energy configured to direct the curing energy to a discrete region of the curable material forward of or at a location where a subsequent layer of the curable material is dispensed from the delivery guide against a preceding layer of the curable material to cure together the subsequent layer and the preceding layer. Methods of additively manufacturing comprise dispensing a subsequent layer of a curable material against a preceding layer of the curable material, and concurrently with the dispensing, directing curing energy to a discrete region of the curable material to cure together the subsequent layer and the preceding layer.
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5.发明授权公开(公告)号：US10661417B2
公开(公告)日：2020-05-26
申请号：US15891236
申请日：2018-02-07
申请人： The Boeing Company
IPC分类号： B25B23/10 , B25B21/00 , B25B23/142 , B25G1/00 , B25B13/50
摘要： Tools for rotating fasteners, methods of utilizing the tools, and methods of manufacturing the tools. The tools include a gripping region, a fastener receptacle, and an interlock structure. The gripping region is configured to be gripped by a user of the tool. The fastener receptacle is shaped to receive the fasteners and includes a fastener-receiving opening on a fastener-facing side of the tool. The fastener-facing side faces in a fastener-facing direction. The fastener-receiving opening is sized to permit the fastener to enter the fastener receptacle from the fastener-facing side of the tool. The interlock structure is configured to interlock with the fastener while the fastener is received within the fastener receptacle. The interlock structure also is configured to prevent motion of the tool away from the fastener in a fastener-opposed direction, which is opposed to the fastener-facing side of the tool, while the interlock region is interlocked with the fastener.
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6.发明授权公开(公告)号：US10581105B2
公开(公告)日：2020-03-03
申请号：US15459436
申请日：2017-03-15
申请人： Paul E. DuFresne
发明人： Paul E. DuFresne
IPC分类号： H01M8/22 , H01M8/04082 , H01M8/0662 , H01M4/92
摘要： Fuel cells utilizing liquid sodium-potassium alloy (NaK) reducing agent and fuel cell systems including the same. The fuel cells include a housing defining a housing volume and a reducing agent-containment structure defining a reducing agent-containment volume. The fuel cells also include a volume of NaK reducing agent extending within the reducing agent-containment volume and an anode conductor extending in electrical contact with the NaK reducing agent such that the NaK reducing agent forms at least a portion of an anode electrode of the fuel cell. The fuel cells further include a cathode electrode that extends within the housing volume and is spaced-apart from the NaK reducing agent, an electrolyte present within the housing volume, and an oxidizing agent supply structure configured to provide an oxidizing agent to the housing volume.
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公开(公告)号：USD876113S1
公开(公告)日：2020-02-25
申请号：US29676083
申请日：2019-01-08
申请人： Ramod Chhetri
设计人： Ramod Chhetri
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公开(公告)号：USD871148S1
公开(公告)日：2019-12-31
申请号：US29607874
申请日：2017-06-16
设计人： William Gordon , Maria Bujalska
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公开(公告)号：US10517750B2
公开(公告)日：2019-12-31
申请号：US14949569
申请日：2015-11-23
发明人： Samuel Slishman
摘要： Portable traction splints and methods of use in applying traction to an injured patient's limb, or limbs, are disclosed. The disclosed traction splints may be extendable from a collapsed configuration adapted for transportation and storage towards an extended configuration adapted for applying traction to an injured patient, using telescoping members. One or more straps may be provided for securing the traction splint to the patient. One or more of such straps may include a tourniquet portion and/or may be selectively oriented in different directions relative to the telescoping members. The disclosed traction splints may include a traction mechanism that utilizes a mechanical advantage in applying traction to the patient's limb. Such traction mechanisms may have a traction cord path that utilizes the same hardware as an adjustment mechanism that selectively allows or prevents one of the telescoping members from moving with respect to another.
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公开(公告)号：US10512857B2
公开(公告)日：2019-12-24
申请号：US15356980
申请日：2016-11-21
申请人： The Boeing Company
发明人： Michael John Fleming
摘要： Presently disclosed systems and methods for depositing a compound into a void in a sandwich panel or other structure are configured to reduce the air pressure in and around the void as the compound flows into the void, thereby reducing the amount of air trapped between the compound and the sandwich panel skin (under the compound, within the void) during the repair. Additionally or alternatively, presently disclosed systems and methods for deaerating a compound are configured to remove trapped air from the compound prior to use of the compound (e.g., prior to depositing the compound within a void for repairing the void). In some examples, the same system is configured to both deaerate the compound and deposit the deaerated compound to the void, all while in a reduced air pressure environment inside a vacuum chamber.
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