会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 4. 发明申请
    • Repair determination for heat damaged composite structures
    • 热损伤复合结构的修复测定
    • US20070276627A1
    • 2007-11-29
    • US11440742
    • 2006-05-25
    • Everett A. Westerman
    • Everett A. Westerman
    • G01N21/00
    • G06T7/001G06T2207/30164G07C5/006
    • A system and method for assessing the ability to rework a composite structure with a heat induced inconsistency is provided. The method includes acquiring information related to the composite structure with a heat induced inconsistency; comparing the information of the composite structures with a heat induced inconsistency with heat induced inconsistency assessment signatures stored in a look up table; correlating the output of the compared information with material master curves; analyzing the composite structures with a heat induced inconsistency to determine the remaining structural capability; determining if the composite structures with a heat induced inconsistency requires immediate rework or replacement; and displaying the results.
    • 提供了一种用于评估具有导热不一致性的复合结构返修能力的系统和方法。 该方法包括以热导致的不一致性获取与复合结构相关的信息; 将复合结构的信息与存储在查找表中的热引起的不一致性评估签名的热引起的不一致进行比较; 将比较信息的输出与材料主曲线相关联; 用热引起的不一致性分析复合结构以确定剩余的结构能力; 确定具有热引起的不一致性的复合结构是否需要立即返工或更换; 并显示结果。
    • 5. 发明授权
    • Apparatus and method for electroplating a workpiece
    • 用于电镀工件的设备和方法
    • US5279725A
    • 1994-01-18
    • US854350
    • 1992-03-18
    • Everett A. Westerman, Jr.
    • Everett A. Westerman, Jr.
    • C25D5/02C25D17/00
    • C25D5/02C25D17/004
    • An apparatus and method for electroplating a graphite-epoxy workpiece in-situ. An electroplating assembly includes a rigid base that is retained a fixed distance about the surface region by insulated standoff legs. A flexible vacuum bag is coupled to the graphite-epoxy workpiece with a fluid-tight seal. The vacuum bag surrounds the surface region and encloses the rigid base to form a plating chamber. A supply chamber, containing a plating fluid, is coupled to the plating chamber by a fluid-tight tubing. A storage chamber is coupled to the plating chamber by a fluid-tight tubing. A vacuum source is coupled by tubing to the supply chamber and to the storage chamber. Valves in each tubing permit the selective coupling of the vacuum source and plating chamber to either the supply chamber or the storage chamber. Electroplating is carried out while plating fluid is drawn by the vacuum, from the supply chamber into the plating chamber and into the storage chamber. When the plating fluid is nearly depleted from the supply chamber, the flow direction is reversed, to draw fluid from the storage chamber, into the plating chamber, and into the supply chamber.
    • 一种用于原位电镀石墨环氧工件的设备和方法。 电镀组件包括刚性基座,其通过绝缘的支脚保持在表面区域周围的固定距离。 柔性真空袋通过流体密封连接到石墨环氧树脂工件上。 真空袋围绕表面区域并包围刚性基底以形成电镀室。 包含电镀液的供应室通过流体密封的管连接到电镀室。 储存室通过流体密封的管连接到电镀室。 真空源通过管道耦合到供应室和储存室。 每个管道中的阀允许将真空源和电镀室选择性地耦合到供应室或储存室。 当电镀液体被抽真空,从供应室进入电镀室并进入储存室时进行电镀。 当电镀液体几乎从供应室中耗尽时,流动方向相反,以将流体从储存室中抽出到电镀室中并进入供应室。
    • 6. 发明授权
    • Bolted repair for curved surfaces
    • 弯曲表面螺栓修复
    • US4858853A
    • 1989-08-22
    • US157279
    • 1988-02-17
    • Everett A. WestermanMark S. Cohodas
    • Everett A. WestermanMark S. Cohodas
    • B32B43/00B64F5/00
    • B64F5/0081Y10T29/49732Y10T29/49739
    • A bolted repair for curved surfaces of an aircraft structure includes a plurality of relatively thin, flexible plates that are bent to conform to the surface, either individually or as a group. After the plates have been bent to conform to the surface, layers of adhesive are applied between adjacent plates to bond the plates to each other. The resulting stack of bonded plates is then secured to the structure with fasteners extending through attachment holes in the stack and structure. The plates may be bent by first securing a portion of a stack of plates to the structure and then bending the stack of plates so that the plates progressively conform to the surface of the structure. As areas of the stack of plates conform to the surface of said structure, the areas are temporarily secured to the structure with temporary fasteners until the entire surface of the stack of plates has been bent to conform to the surface of the structure. After layers of adhesive are applied between adjacent plates and all of the temporary fasteners have been installed so that the entire surface of the stack of plates conforms to the surface of the structure, the temporary fasteners are sequentially removed and permanent fasteners are installed in their places.
    • 飞机结构(10)的弯曲表面的螺栓修复包括多个相对薄的柔性板(14,16,18,20),其被单独地或作为一组弯曲成符合表面。 在板被弯曲以符合表面之后,将粘合剂层(15)施加在相邻板之间以将板彼此粘合。 然后将所得到的粘合板堆叠固定到具有延伸穿过堆叠和结构中的附接孔的紧固件的结构。 板可以通过首先将一堆板的一部分固定到结构上,然后弯曲板的堆叠而弯曲,使得板逐渐符合结构的表面。 由于板堆的区域符合所述结构的表面,所以这些区域被临时固定到结构上,其中临时紧固件(34,38,42,44)直到板堆的整个表面已被弯曲以符合 结构的表面。 在相邻的板之间施加一层粘合剂并且已经安装了所有的临时紧固件,使得堆叠的整个表面符合结构的表面,临时紧固件(34,38,42,44)是顺序地 拆卸和永久紧固件安装在他们的地方。
    • 9. 发明授权
    • Apparatus for repairing a hole in a structural wall of composite material
    • 用于修复复合材料结构壁中的孔的装置
    • US4916880A
    • 1990-04-17
    • US165938
    • 1988-02-18
    • Everett A. Westerman, Jr.
    • Everett A. Westerman, Jr.
    • B29C73/04B29C73/10
    • B29C73/10B29C73/04B29C2073/264Y10T29/49732Y10T428/20
    • A hole (12) in a panel (10) of composite material is cut by a router or the like to dress it into a rounded hole (12'). A cavity is routed or otherwise formed in the panel (10) to extend across the dressed hole (12') in the direction of maximum tension loads in the panel (10). An insert (16) is secured in the cavity (18). The insert (16) and the cavity (18) have matching plan forms and each has a relatively narrow central portion and enlarged end portions (42, 44). The end portions (42, 44) of the insert interlock with end portions of the cavity (18) such that tension loads will be carried by the insert (16) from a region of the wall (10) on one side of the hole (12') across the hole (12') to a region of the wall (10) on the opposite side of the hole (12').
    • 通过路由器等将复合材料的面板(10)中的孔(12)切割成圆形孔(12')。 空腔在面板(10)中被路由或以其他方式形成,以在面板(10)中沿最大张力负载的方向延伸穿过修整孔(12')。 插入件(16)固定在空腔(18)中。 插入件(16)和空腔(18)具有匹配的平面形式,并且每个具有相对窄的中心部分和扩大的端部部分(42,44)。 插入件的端部(42,44)与空腔(18)的端部互锁,使得拉伸载荷将由插入件(16)从孔的一侧的区域(10)承载( 12')穿过所述孔(12')的相对侧的所述壁(10)的区域。