公开(公告)号：EP3495686A1

公开(公告)日：2019-06-12

申请号：EP18210892.8

申请日：2018-12-06

申请人： The Boeing Company

发明人： GRIFFIN, Steven F. ,  ASTON, Richard W. ,  MARTINEZ, Jazzmin P. ,  LANGMACK, Michael John ,  SHURILLA, Christopher R.

IPC分类号： F16F15/03

摘要： Systems and methods for dampening dynamic loading between two bodies are described. An example dampening system includes a non-ferrous metal body attached to a second body and a stack of magnets attached to a third body. The stack of magnets is movably disposed within or around the non-ferrous metal body, and adjacent magnets are arranged in an opposed polar relationship, whereby relative movement of said second and third bodies is damped. An example method of dampening dynamic loading includes arranging a plurality of magnets along an axis to form at least one pair of magnets having an opposed polar relationship along the axis. The method further includes axially moving the at least one pair of magnets relative to a non-ferrous metal body, so as to dampen dynamic loading of a payload attached to a vehicle.

公开(公告)号：EP3239054A1

公开(公告)日：2017-11-01

申请号：EP17155364.7

申请日：2017-02-09

申请人： The Boeing Company

发明人： ASTON, Richard W. ,  TOMZYNSKA, Anna M. ,  LANGMACK, Michael J. ,  MARTINEZ, Jazzmin P.

IPC分类号： B64D45/02 ,  B64F5/10 ,  B29C39/10

CPC分类号： F16B33/004 ,  B29C39/10 ,  B64C3/26 ,  B64D45/02 ,  B64F5/10

摘要： A sealant containment assembly for enclosing fasteners disposed within a confined space. The sealant containment assembly includes a first containment member and a second containment member that extend between two surfaces. The first and second containment members each include structure-engaging ends for engaging a structural member and the first and second containment members each include enclosure ends that connect the first and second containment members together to enclose the fasteners within a confined space defined by the first and second containment members, the first and second surfaces, the structural member and the connected enclosure ends. The assembly also includes at least one injection port disposed outside of the confined space but is in communication with at least one distribution port disposed inside the confined space for filling the confined space with sealant, thereby embedding the fasteners in sealant.

摘要翻译： 用于封闭设置在有限空间内的紧固件的密封剂密封组件。 密封剂容纳组件包括在两个表面之间延伸的第一容器构件和第二容器构件。 第一和第二容纳部件每个包括用于接合结构部件的结构接合端部，并且第一和第二容纳部件每个均包括将第一和第二容纳部件连接在一起以将紧固件包围在由第一和第二容纳部件限定的有限空间内的封闭端部， 第二容纳构件，第一和第二表面，结构构件和连接的外壳端部。 所述组件还包括至少一个注入口，所述至少一个注入口布置在所述密闭空间的外部，但与布置在所述密闭空间内的至少一个分配端口连通，以用密封剂填充所述密闭空间，从而将所述紧固件嵌入密封剂中。

公开(公告)号：EP3232071A1

公开(公告)日：2017-10-18

申请号：EP17153195.7

申请日：2017-01-26

申请人： The Boeing Company

发明人： ASTON, Richard W. ,  TOMZYNSKA, Anna M. ,  LANGMACK, Michael J. ,  MARTINEZ, Jazzmin P.

IPC分类号： F16B37/14 ,  B64D45/02 ,  F16B33/00

CPC分类号： F16B37/14 ,  B64D45/02 ,  F16B33/004

摘要： This disclosure provides a cap assembly (32) for encapsulating a fastener (27) or portion of a fastener (27) that protrudes from a surface (33) and into a confined space. The cap assembly (32) includes a plurality of nested sections (36, 51, 52, 38) that telescope from a collapsed configuration to an extended configuration. The plurality of nested sections (36, 51, 52, 38) includes a base section (36) that includes a base rim (37) that engages the surface (33) in the extended configuration. The plurality of nested sections (36, 51, 52, 38) also includes an end section (38) that has an end wall (41). The end wall (41) and the base rim (37) define a length of the cap assembly (32) in the extended configuration that is sufficient to encapsulate the fastener (27) within the cap assembly (32) with the base rim (37) engaging the surface (33) and the end wall (41) spaced apart from a distal end (34) of the fastener (27).

摘要翻译： 本公开提供了一种用于封装从表面（33）突出并进入有限空间的紧固件（27）或紧固件（27）的一部分的盖组件（32）。 盖组件（32）包括多个嵌套部分（36,51,52,38），所述多个嵌套部分从收缩构型伸缩到伸展构型。 多个嵌套部分（36,51,52,38）包括基部部分（36），该基部部分包括在延伸构型中接合表面（33）的基部边缘（37）。 多个嵌套部分（36,51,52,38）还包括具有端壁（41）的端部部分（38）。 端壁（41）和基部边缘（37）限定处于延伸构型中的帽组件（32）的长度，该长度足以将紧固件（27）与基部边缘（37）包封在帽组件 ）与紧固件（27）的远端（34）间隔开的表面（33）和端壁（41）接合。