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公开(公告)号：US11066859B2
公开(公告)日：2021-07-20
申请号：US16398414
申请日：2019-04-30
Applicant: Lockheed Martin Corporation
Inventor： Michael J. Malia , Brian Kaplun , Dominick Consalvi
IPC: B29C45/14 , E05D1/00 , A63H27/00 , B29C65/02 , B29C65/48 , B29C65/50 , B29C65/00 , B29C70/34 , B29C45/16 , B29C65/70 , B64C9/02 , B29K21/00 , B29K101/12 , B29K105/08 , B29L9/00 , B29L31/22
Abstract: A hinged component fabrication method in which, in a layup stage of fabrication, the component includes a live hinge joining uncured material portions together at a hinge region and comprising a layer of tensile fabric at least partially infiltrated by an uncured elastomer layer at least partially interposed between the tensile fabric and the uncured material portions such that the uncured elastomer blocks the uncured material portions from infiltrating the hinge region. The method may include locating overlapped tensile fabric and elastomer layers in a tool and introducing polymer-based material into the tool such that polymer-based material portions overlap respective opposite ends of the fabric and elastomer layers. The polymer-based material portions are formed to a desired shape using the forming tool so that the fabric and elastomer layers form a live hinge between the polymer-based material portions.
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公开(公告)号：US10544610B2
公开(公告)日：2020-01-28
申请号：US13960009
申请日：2013-08-06
Applicant: Lockheed Martin Corporation
Inventor： Michael J. Malia , Brian Kaplun , Dominick Consalvi
IPC: E05D1/00 , B29C45/00 , A63H27/00 , B29C65/02 , B29C65/48 , B29C65/50 , B29C65/00 , B29C70/34 , B29C45/14 , B29C45/16 , B29C65/70 , B64C9/02 , B29K21/00 , B29K101/12 , B29K105/08 , B29L9/00 , B29L31/22
Abstract: A hinged component includes first and second portions of material coupled together by a composite live hinge. The live hinge includes a layer of tensile fabric and a layer of elastomer interposed between the tensile fabric and the material of one or both of the coupled first and second portions. The composite live hinge is capable of joining structural composite materials without the need for scoring, and thereby weakening, the structural composite material along the desired hinge line. The live hinge can be embedded in the materials it joins in a method that is compatible with traditional structural composite layup processes and in a manner which prevents resin from the structural composite materials from infiltrating the tensile fabric and compromising its flexibility.
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公开(公告)号：US09389103B1
公开(公告)日：2016-07-12
申请号：US14573496
申请日：2014-12-17
Applicant: LOCKHEED MARTIN CORPORATION
Inventor： James E. Bishop , Allan Johnson , Brian Kaplun , Steven E. McElwain, Jr. , David L. Vos
CPC classification number: G01D11/245 , G02B6/04 , G02B6/4298
Abstract: A gigahertz sensor array packaging solution for harsh operating environments is disclosed. The sensor array packaging system includes a structural core body comprising sensor mounting features on a surface thereof and an alignment through hole extending from the surface to a backside thereof which incorporates finned features providing cooling and stiffness. The sensor array packaging system further includes one or more electro-optical components mounted to the backside of the structural core body. The sensor array packaging system further includes a wiring board comprising a plurality of sensor array elements contacting walls of the spiral ribbon configuration, each having a cable extending through the through hole to at least one of the one or more electro-optical components.
Abstract translation: 公开了用于恶劣操作环境的千兆赫传感器阵列封装解决方案。 传感器阵列封装系统包括结构芯体，其包括在其表面上的传感器安装特征和从表面延伸到其背面的对准通孔，其包括提供冷却和刚度的翅片特征。 传感器阵列封装系统还包括安装在结构芯体的背面的一个或多个电光部件。 传感器阵列封装系统还包括布线板，该布线板包括接触螺旋带构造的壁的多个传感器阵列元件，每个传感器阵列元件具有穿过通孔延伸至至少一个或多个电光部件之一的电缆。
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公开(公告)号：US20150040349A1
公开(公告)日：2015-02-12
申请号：US13960009
申请日：2013-08-06
Applicant: Lockheed Martin Corporation
Inventor： Mike Malia , Brian Kaplun , Dominick Consalvi
Abstract: A hinged component includes first and second portions of material coupled together by a composite live hinge. The live hinge includes a layer of tensile fabric and a layer of elastomer interposed between the tensile fabric and the material of one or both of the coupled first and second portions. The composite live hinge is capable of joining structural composite materials without the need for scoring, and thereby weakening, the structural composite material along the desired hinge line. The live hinge can be embedded in the materials it joins in a method that is compatible with traditional structural composite layup processes and in a manner which prevents resin from the structural composite materials from infiltrating the tensile fabric and compromising its flexibility.
Abstract translation: 铰链部件包括通过复合活动铰链连接在一起的材料的第一和第二部分。 活动铰链包括一层拉伸织物和介于拉伸织物和耦合的第一和第二部分之一或两者的材料之间的弹性层。 复合活动铰链能够连接结构复合材料，而不需要对沿着所需铰链线的结构复合材料进行刻痕，从而削弱结构复合材料。 活动铰链可以以与传统的结构复合铺层工艺相兼容的方法嵌入其连接的材料中，并且以防止结构复合材料的树脂渗透拉伸织物并损害其柔性的方式。
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