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    LAMINATED METALLIC STRUCTURE AND METHOD OF MAKING THE SAME
    2.
    发明申请
    LAMINATED METALLIC STRUCTURE AND METHOD OF MAKING THE SAME 审中-公开

    公开(公告)号：US20200316899A1

    公开(公告)日：2020-10-08

    申请号：US16377664

    申请日：2019-04-08

    申请人： The Boeing Company

    发明人： Kenneth H. Griess ,  Gary E. Georgeson

    IPC分类号： B32B1/00 ,  B32B7/12 ,  B32B15/01

    摘要： A method of forming a laminated metallic structure includes steps of: (1) providing a first preformed-metallic sheet having a three-dimensional shape of a first graduated three-dimensional size; (2) providing a second preformed-metallic sheet having the three-dimensional shape of a second graduated three-dimensional size; (3) nesting the second preformed-metallic sheet in the first preformed-metallic sheet; and (4) bonding the first preformed-metallic sheet and the second preformed-metallic sheet together.

    Systems, methods, and apparatus for high-traffic density personalized transportation
    6.
    发明授权
    Systems, methods, and apparatus for high-traffic density personalized transportation 有权

    公开(公告)号：US11989033B2

    公开(公告)日：2024-05-21

    申请号：US16582870

    申请日：2019-09-25

    申请人： The Boeing Company

    发明人： Gary E. Georgeson ,  Kenneth H. Griess ,  Joseph Lawrence Hafenrichter

    IPC分类号： G05D1/00 ,  B60D1/01 ,  B62D63/02

    CPC分类号： G05D1/0287 ,  B60D1/01 ,  B62D63/025

    摘要： Methods, apparatus, systems, and articles of manufacture are disclosed for high-traffic density personalized transportation. An example system includes a transit carrier having a first movement system, first stacking couplers, first and second magnetic couplers, and a first location, a transit pod having a second movement system, second stacking couplers, and a second location, the second stacking couplers configured to couple to the first stacking couplers, and a controller to in response to obtaining a request to direct the transit carrier to move from the first location to the second location, invoke the transit pod to couple to the transit carrier by directing the transit pod to move on top of the transit carrier using the second movement system, and when the transit carrier is coupled to the transit pod, invoke the transit carrier to move the transit pod to a third location using the first movement system.

    COMPOSITE REPAIR KIT
    7.
    发明申请
    COMPOSITE REPAIR KIT 审中-公开

    公开(公告)号：US20190177007A1

    公开(公告)日：2019-06-13

    申请号：US15838346

    申请日：2017-12-11

    申请人： THE BOEING COMPANY

    发明人： Kenneth H. Griess ,  Gary E. Georgeson

    IPC分类号： B64F5/40 ,  B29C73/10

    摘要： Disclosed is a method for repairing a damaged portion of a composite fuselage or wing on an aircraft. The method includes performing a non-destructive inspection (“NDI”) of the damage portion to determine a size and a location of the damaged portion, determining a repair for the damaged portion based on the size and location of the damaged portion, and repairing the damaged portion with a composite repair kit.

    WING-TO-FUSELAGE JOINTS AND AIRCRAFT INCLUDING THE SAME
    8.
    发明申请
    WING-TO-FUSELAGE JOINTS AND AIRCRAFT INCLUDING THE SAME 审中-公开

    公开(公告)号：US20180362140A1

    公开(公告)日：2018-12-20

    申请号：US15623256

    申请日：2017-06-14

    申请人： The Boeing Company

    发明人： Kenneth H. Griess ,  Gary E. Georgeson

    IPC分类号： B64C1/26 ,  B64C3/18 ,  B64C1/06

    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.

    GRAPHENE FIBER FOR AEROSPACE COMPOSITES
    10.
    发明申请
    GRAPHENE FIBER FOR AEROSPACE COMPOSITES 审中-公开
    用于航空复合材料的石墨纤维

    公开(公告)号：US20160194482A1

    公开(公告)日：2016-07-07

    申请号：US14589036

    申请日：2015-01-05

    申请人： The Boeing Company

    发明人： Keith Daniel Humfeld ,  Kenneth H. Griess

    IPC分类号： C08K9/04 ,  C08J5/24 ,  D01H1/14 ,  D02G3/06 ,  D02G3/02 ,  C07D303/02 ,  C08K7/06

    CPC分类号： C08K9/04 ,  C01B32/194 ,  C07D303/02 ,  C08J5/005 ,  C08J5/06 ,  C08J5/24 ,  C08J2300/00 ,  C08J2300/24 ,  C08K7/06 ,  D01H1/14 ,  D02G3/02 ,  D02G3/06

    摘要： Graphene fibers made from a graphene film formed into an elongated fiber-like shape and composite materials made from the graphene fibers. The graphene film has amine groups formed on at least an outer surface of the graphene film and epoxide groups formed on at least one edge of the graphene film. The amine groups are formed in a functionalized area on the outer surface of the graphene film that is within about 10 microns from the at least one edge of the graphene film, or the functionalized area may extend the entire width of the graphene film. The graphene film may also have holes formed through the graphene film. The elongated fiber-like shapes may be the graphene film in a rolled spiral orientation or the graphene film in a twisted formation.

    摘要翻译： 由石墨烯膜制成的石墨烯纤维形成细长的纤维状形状和由石墨烯纤维制成的复合材料。 石墨烯膜具有在石墨烯膜的至少外表面上形成的胺基和在石墨烯膜的至少一个边缘上形成的环氧基。 在石墨烯膜的外表面上的功能化区域中形成胺基，其距离石墨烯膜的至少一个边缘在约10微米内，或者官能化区域可以延伸石墨烯膜的整个宽度。 石墨烯膜也可以具有通过石墨烯膜形成的孔。 细长的纤维状形状可以是卷绕的螺旋取向的石墨烯膜或扭曲形式的石墨烯膜。