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公开(公告)号：WO2013030536A1
公开(公告)日：2013-03-07
申请号：PCT/GB2012/052041
申请日：2012-08-21
Applicant: BAE SYSTEMS PLC , BAKER, David , REZAI, Amir
Inventor： BAKER, David , REZAI, Amir
CPC classification number: C08J3/20 , B29C70/025 , B29C70/465 , B29K2105/124 , B32B5/24 , B32B5/26 , B32B2255/02 , B32B2255/24 , C08J3/12 , C08J3/24 , C08J5/04 , C08J2363/00 , C08J2367/06 , C08J2375/04 , C08J2379/08 , C08K3/04 , C08K3/041 , C08K3/042 , C08K7/24 , C08K2201/011 , C08K2201/016
Abstract: The invention relates to methods and novel a powdered curable monomer which may be used to manufacture bulk polymers, adhesives and coatings composite materials with high percentage weight inclusions of particulate filler materials, more specifically to fibre reinforced polymer composite materials with high percentage weight inclusions of particulate filler materials. The preferred particulate filler materials are carbon nanotubes. The method according to the invention allows greater than 0.5wt% of carbon nanotubes, typically greater 10%wt of carbon nanotubes or other high aspect ratio fillers to be readily incorporated in the resin matrix, before being applied to the fibre reinforcing plys.
Abstract translation: 本发明涉及可用于制造散装聚合物，粘合剂和涂层复合材料的方法和新型粉末状可固化单体，其具有高百分比重量的颗粒填料材料夹杂物，更具体地说涉及具有高百分比重量的颗粒物夹杂物的纤维增强聚合物复合材料 填充材料。 优选的颗粒填料是碳纳米管。 根据本发明的方法，在施加到纤维增强层之前，允许大于0.5重量％的碳纳米管，通常较大的10重量％的碳纳米管或其它高纵横比的填料容易地结合到树脂基质中。
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公开(公告)号：WO2014064430A1
公开(公告)日：2014-05-01
申请号：PCT/GB2013/052744
申请日：2013-10-21
Applicant: BAE SYSTEMS PLC
Inventor： BAKER, David , REZAI, Amir , WESCOTT, Andrew, David , GRAHAM, Daniel Peter
CPC classification number: F16B5/045 , B21J15/00 , B21J15/02 , B21J15/147 , B21K25/00 , B29C65/567 , B29C65/606 , B29C65/607 , B29C65/64 , B29C66/1122 , B29C66/21 , B29C66/43 , B29C66/721 , B29C66/72141 , B29C66/742 , B29C66/81419 , B29C66/81423 , B29C66/81429 , B29C66/81431 , B29C66/8322 , B29C66/8432 , F16B17/008 , Y10T29/49938 , Y10T403/4966
Abstract: A method for forming a joint between a fibre reinforced composite component and a metallic component and a joint are provided. The metallic component and the composite component each define a joint surface for mating with the joint surface of the other to join the two components together and the composite component defines a free surface opposed to the joint surface thereof. The joint surface of the metallic component defines an array of pins extending therefrom with each pin defining a pin head at an end distal from the joint surface. The method includes the steps of pressing together the joint surfaces of the two components whereby to cause the array of pins to penetrate through the fibre reinforcing material, and modifying the effective cross sectional shape of the pin heads whereby to increase the constraint applied to the composite component against peeling of the composite component from the joint surface of the metallic component.
Abstract translation: 提供了一种在纤维增强复合部件与金属部件和接头之间形成接头的方法。 金属部件和复合部件各自限定用于与另一个的接头表面配合的接合表面，以将两个部件连接在一起，并且复合部件限定与其接头表面相对的自由表面。 金属部件的接合表面限定了从其延伸的销的阵列，每个销在远离接合表面的一端限定销头。 该方法包括以下步骤：将两个部件的接合表面压在一起，从而使销的阵列穿过纤维增强材料，并且改变销头的有效截面形状，从而增加对复合材料的约束 防止复合部件从金属部件的接合面剥离的部件。
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公开(公告)号：WO2010055338A1
公开(公告)日：2010-05-20
申请号：PCT/GB2009/051518
申请日：2009-11-12
Applicant: BAE SYSTEMS plc , HUCKER, Martyn John , JOHNSON, Graham, Andrew , BAKER, David , REZAI, Amir
Inventor： HUCKER, Martyn John , JOHNSON, Graham, Andrew , BAKER, David , REZAI, Amir
CPC classification number: G01P1/02 , F16B35/041 , G01F1/684 , G01P5/00
Abstract: A flow sensor and fastener assembly (101, 102, 103, 104), comprising at least the following modules: a sensor housing (4, 54, 74) and a fastener element(6, 62); wherein : the sensor housing (4, 54, 74) is adapted to receive a flow-based sensor (2), e.g. a MEMS airflow sensor; the sensor housing (4, 54, 74) comprises connection means (20, 50, 80) for transmitting sensing signals from a fitted flow-based sensor(2); the fastener element (6; 62) comprises a head (22) and a shank (24), at least part of the shank (24) being externally threaded (26); the fastener element (6, 62) comprises a bore (28) extending through the whole length of the fastener element (6, 62); and the bore (28) is shaped at the head (22) end of the fastener element (6, 62) to provide a sensor housing receiving part(30).
Abstract translation: 至少包括以下模块的流量传感器和紧固件组件（101,102,103,104）：传感器壳体（4,54,74）和紧固元件（6,62）; 其中：所述传感器壳体（4,54,74）适于接收基于流体的传感器（2），例如， 一个MEMS气流传感器; 所述传感器外壳（4,54,74）包括用于传送来自安装的基于流体的传感器（2）的传感信号的连接装置（20,50,80）。 所述紧固元件（6; 62）包括头部（22）和柄部（24），所述柄部（24）的至少一部分是外螺纹（26）; 紧固元件（6,62）包括延伸穿过紧固件元件（6,62）整个长度的孔（28）; 并且孔（28）在紧固元件（6,62）的头部（22）端部成形，以提供传感器壳体接收部分（30）。
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公开(公告)号：WO2015049509A1
公开(公告)日：2015-04-09
申请号：PCT/GB2014/052961
申请日：2014-10-01
Applicant: BAE SYSTEMS PLC
Inventor： BAKER, David , REZAI, Amir
CPC classification number: B29C43/12 , B29C33/20 , B29C33/308 , B29C43/18 , B29C43/52 , B29C43/56 , B29C2043/562 , B29K2025/06 , B29K2105/20 , B29K2705/02 , B29L2007/002 , B29L2009/00
Abstract: A flexible manufacturing tool is provided. The tool includes a multi-layer generally planar sheet of material defining a tool surface thereon, means such as spaced jacks to controllably deform the sheet by applying out-of-plane deforming forces to the sheet and means selectively to increase and decrease interlayer shear or frictional forces whereby to vary the flexural stiffness of the sheet. Such means may comprise applying a vacuum between the layers to increase interlayer friction or the use of softenable polymers between the layers.
Abstract translation: 提供了灵活的制造工具。 该工具包括多层大体平坦的材料片材，其在其上限定工具表面，诸如间隔开的插孔的装置，以通过向片材施加面外变形力来控制地使片材变形，并且选择性地增加和减少层间剪切或 从而改变片材的弯曲刚度的摩擦力。 这种方法可以包括在层之间施加真空以增加层间摩擦或在层之间使用可软化聚合物。
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公开(公告)号：WO2014080195A1
公开(公告)日：2014-05-30
申请号：PCT/GB2013/053051
申请日：2013-11-19
Applicant: BAE SYSTEMS PLC
Inventor： GRAHAM, Daniel Peter , BAKER, David , REZAI, Amir , WESCOTT, Andrew, David
CPC classification number: B23K9/20 , B23K9/201 , B29C65/56 , B29C66/02 , B29C66/1122 , B29C66/43 , B29C66/721 , B29C66/73751 , B29C66/742 , B29C66/8322 , B29C70/86
Abstract: The invention relates to the manufacture of hybrid joints more particularly to the manufacture of joints between parts made of differing materials and most particularly to the manufacture of a metallic component comprising a plurality of preformed projections which penetrate composite fabric within a composite part. Particularly there is a method of forming an array of projections on a surface of a metallic component, the method including the steps of bringing at least one preformed projection into at least close proximity to the surface of the component and causing a portion of the projection and a portion of the component in the region of an intersection thereof to at least partially melt, and causing them to be joined together.
Abstract translation: 本发明涉及混合接头的制造，更具体地涉及由不同材料制成的部件之间的接头的制造，最特别涉及制造金属部件，该金属部件包括多个穿透复合材料部件内的复合织物的预制凸起。 特别地，存在在金属部件的表面上形成突起阵列的方法，该方法包括以下步骤：使至少一个预成形突起至少靠近部件的表面，并使突起的一部分和 在其交叉部分的区域中的部分部分至少部分熔化，并使它们接合在一起。
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Patent Agency Ranking
公开(公告)号：WO2011051724A2
公开(公告)日：2011-05-05
申请号：PCT/GB2010/051816
申请日：2010-10-29
Applicant: BAE SYSTEMS PLC , MCDONALD, Jennifer, Laura , BAKER, David , REZAI, Amir
Inventor： MCDONALD, Jennifer, Laura , BAKER, David , REZAI, Amir
CPC classification number: F41H5/023 , F41H5/0457 , Y10T156/10
Abstract: There is disclosed armour comprising an outer metallic layer, an inner fibre composite layer, and a supporting framework between the inner and outer layers. The supporting framework can comprise projections from the outer layer arranged to mechanically interlock with the fibres of the fibre composite, and can be arranged to provide an open region between the inner and outer layers that can be filled with a functional filler material.
Abstract translation: 公开了一种包括外金属层，内纤维复合层和在内层和外层之间的支撑框架的装甲。 支撑框架可以包括从外层布置成与纤维复合材料的纤维机械互锁的突起，并且可以布置成在可以填充功能填充材料的内层和外层之间提供开放区域。
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公开(公告)号：EP2751173B1
公开(公告)日：2020-02-05
申请号：EP12759805.0
申请日：2012-08-21
Applicant: BAE Systems PLC
Inventor： BAKER, David , REZAI, Amir
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公开(公告)号：EP2922656A1
公开(公告)日：2015-09-30
申请号：EP13796131.4
申请日：2013-11-19
Applicant: BAE Systems PLC
Inventor： GRAHAM, Daniel Peter , BAKER, David , REZAI, Amir , WESCOTT, Andrew, David
CPC classification number: B23K9/20 , B23K9/201 , B29C65/56 , B29C66/02 , B29C66/1122 , B29C66/43 , B29C66/721 , B29C66/73751 , B29C66/742 , B29C66/8322 , B29C70/86
Abstract: The invention relates to the manufacture of hybrid joints more particularly to the manufacture of joints between parts made of differing materials and most particularly to the manufacture of a metallic component comprising a plurality of preformed projections which penetrate composite fabric within a composite part. Particularly there is a method of forming an array of projections on a surface of a metallic component, the method including the steps of bringing at least one preformed projection into at least close proximity to the surface of the component and causing a portion of the projection and a portion of the component in the region of an intersection thereof to at least partially melt, and causing them to be joined together.
Abstract translation: 本发明涉及混合接头的制造，更具体地涉及制造由不同材料制成的部件之间的接头，并且更具体地涉及制造包括多个预成型凸起的金属部件，所述预成型凸起穿透复合部件内的复合织物。 特别是存在一种在金属部件的表面上形成突起阵列的方法，所述方法包括以下步骤：使至少一个预成形的突起至少接近部件的表面并且使突起的一部分和 部件的一部分在其相交区域内至少部分地熔化，并使它们连接在一起。
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公开(公告)号：EP2751173A1
公开(公告)日：2014-07-09
申请号：EP12759805.0
申请日：2012-08-21
Applicant: BAE Systems PLC
Inventor： BAKER, David , REZAI, Amir
CPC classification number: C08J3/20 , B29C70/025 , B29C70/465 , B29K2105/124 , B32B5/24 , B32B5/26 , B32B2255/02 , B32B2255/24 , C08J3/12 , C08J3/24 , C08J5/04 , C08J2363/00 , C08J2367/06 , C08J2375/04 , C08J2379/08 , C08K3/04 , C08K3/041 , C08K3/042 , C08K7/24 , C08K2201/011 , C08K2201/016
Abstract: The invention relates to methods and a novel powdered curable monomer which may be used to manufacture bulk polymers, adhesives and coatings composite materials with high percentage weight inclusions of particulate filler materials, more specifically to fibre reinforced polymer composite materials with high percentage weight inclusions of particulate filler materials. The preferred particulate filler materials are carbon nanotubes. The method according to the invention allows greater than 0.5 wt % of carbon nanotubes, typically greater 10% wt of carbon nanotubes or other high aspect ratio fillers to be readily incorporated in the resin matrix, before being applied to the fibre reinforcing plys.
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公开(公告)号：EP2909486B1
公开(公告)日：2018-12-12
申请号：EP13783370.3
申请日：2013-10-21
Applicant: BAE SYSTEMS plc
Inventor： BAKER, David , REZAI, Amir , WESCOTT, Andrew, David , GRAHAM, Daniel Peter
CPC classification number: F16B5/045 , B21J15/00 , B21J15/02 , B21J15/147 , B21K25/00 , B29C65/567 , B29C65/606 , B29C65/607 , B29C65/64 , B29C66/1122 , B29C66/21 , B29C66/43 , B29C66/721 , B29C66/72141 , B29C66/742 , B29C66/81419 , B29C66/81423 , B29C66/81429 , B29C66/81431 , B29C66/8322 , B29C66/8432 , F16B17/008 , Y10T29/49938 , Y10T403/4966
Abstract: A method for forming a joint between a fiber reinforced composite component and a metallic component and a joint are provided. The metallic component and the composite component each define a joint surface for mating with the joint surface of the other to join the two components together and the composite component defines a free surface opposed to the joint surface thereof. The joint surface of the metallic component defines an array of pins extending therefrom with each pin defining a pin head at an end distal from the joint surface. The method includes the steps of pressing together the joint surfaces of the two components whereby to cause the array of pins to penetrate through the fiber reinforcing material, and modifying the effective cross sectional shape of the pin heads whereby to increase the constraint applied to the composite component against peeling of the composite component from the joint surface of the metallic component.
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