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公开(公告)号：US09365283B2
公开(公告)日：2016-06-14
申请号：US13883398
申请日：2011-11-07
摘要： A foldable seal comprising an elastomeric seal substrate and at least one molded-in stiffener plate embedded within the seal substrate. Also, a method of manufacturing the seal.
摘要翻译： 一种可折叠密封件，其包括弹性体密封基底和嵌入密封基底内的至少一个模制加强板。 另外，制造密封件的方法。
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公开(公告)号：US09038789B2
公开(公告)日：2015-05-26
申请号：US13010063
申请日：2011-01-20
CPC分类号： F16F1/3615 , B64D27/26 , F16F1/379
摘要： A method of controlling an elastomeric damper. The damper is heated by passing an electric current through the damper or through a heating element in contact with the damper said heating causing a decrease in stiffness of the damper. The elastomeric damper may comprise an elastomeric material filled with electrically conductive particles, and the damper may be heated by passing an electric current through the elastomeric material. Alternatively the damper may be heated using a discrete resistive heating element, such as a coil embedded within the elastomeric damper or wound around it.
摘要翻译： 一种控制弹性阻尼器的方法。 通过使电流通过阻尼器或通过与阻尼器接触的加热元件来加热阻尼器，所述加热导致阻尼器刚度的降低。 弹性阻尼器可以包括填充有导电颗粒的弹性体材料，并且可以通过使电流通过弹性体材料来加热阻尼器。 或者，可以使用分立的电阻加热元件来加热阻尼器，例如嵌入弹性阻尼器内的线圈或缠绕在其周围的线圈。
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公开(公告)号：US08881924B2
公开(公告)日：2014-11-11
申请号：US12761938
申请日：2010-04-16
申请人： Colin John West , James Alves , Robert Piper
发明人： Colin John West , James Alves , Robert Piper
IPC分类号： B65D6/10 , B65D6/34 , B65D88/12 , B65D8/08 , B64D37/02 , B64D37/12 , B64D37/08 , F16B5/02 , B60K15/03
CPC分类号： B64D37/08 , B60K15/03 , B60K2015/03118 , B60K2015/03144 , B60K2015/03151 , F16B5/02 , Y02T50/44 , Y10S220/905
摘要： A tank for containing a fluid, such as fuel, oil or gas within a chamber. The walls of the chamber are partially defined by a rigid structure having an opening; and partially defined by an elastomeric diaphragm which is attached around its periphery to the rigid structure and covers the opening in the rigid structure. An attachment frame engages the diaphragm and the rigid structure, and extends around the periphery of the diaphragm. The attachment frame has a first portion which engages the diaphragm, and a second portion which is positioned outside an outer edge of the diaphragm and attached to the rigid structure.
摘要翻译： 用于在腔室内容纳诸如燃料，油或气体之类的流体的罐。 室的壁部分地由具有开口的刚性结构限定; 并且部分地由弹性体膜片限定，弹性体膜片围绕其周边附接到刚性结构并且覆盖刚性结构中的开口。 附接框架接合隔膜和刚性结构，并且围绕隔膜的周边延伸。 附接框架具有接合隔膜的第一部分和位于隔膜的外边缘外部并附接到刚性结构的第二部分。
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公开(公告)号：US08864141B2
公开(公告)日：2014-10-21
申请号：US12349116
申请日：2009-01-06
IPC分类号： F16J15/08 , F16J15/10 , B29C43/14 , B29C43/20 , B29C43/00 , B29C43/52 , B29K307/00 , B29K105/00 , B29C65/00 , B29C43/36 , B29K21/00 , B29K83/00 , B29C35/02 , B29K105/24 , B29K27/12
CPC分类号： F16J15/104 , B29C35/02 , B29C43/003 , B29C43/146 , B29C43/203 , B29C43/52 , B29C66/7375 , B29C2043/148 , B29C2043/3634 , B29K2021/00 , B29K2027/12 , B29K2083/00 , B29K2105/0023 , B29K2105/246 , B29K2305/14 , B29K2307/00 , B29K2995/0005 , F05C2201/0421 , F05C2203/0808 , F05C2225/02 , B29C65/00
摘要： A blade seal comprising: a base; a tip; a first part formed from an elastomeric material which extends continuously from the base to the tip; and a second part formed from an elastomeric material mixed with conductive filler which extends continuously from the base to the tip. The blade seal is manufactured by compressing the first and second parts together; and curing one or both of the parts as they are compressed together.
摘要翻译： 一种叶片密封件，包括：基部; 一个提示; 由弹性体材料形成的第一部分，其从基部连续延伸到尖端; 以及由与从底部连续延伸到尖端的导电填料混合的弹性体材料形成的第二部分。 叶片密封件通过将第一和第二部件压缩在一起来制造; 并且当它们被压缩在一起时固化部件中的一个或两个。
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公开(公告)号：US08844881B2
公开(公告)日：2014-09-30
申请号：US12743870
申请日：2008-12-01
IPC分类号： F16L3/08 , B65D63/00 , H02G3/00 , F16L3/10 , F16L55/035
CPC分类号： F16L3/1041 , F16L55/035 , H02G3/263 , Y10T24/14 , Y10T24/1498
摘要： A routing clip for securing a line to a structure comprising: a base for attaching the clip to a structure; and a clamp comprising: a first flexible strap which extends from the base and has one or more projections extending from its side; and a second flexible strap which extends from the base and has a passageway for receiving the first flexible strap and a locking surface which is arranged to engage one of the projections on the first flexible strap to prevent the first flexible strap from being withdrawn from the passageway. At least part of the clip is made from an elastomeric material.
摘要翻译： 一种用于将线固定到结构的布线夹，包括：用于将夹子附接到结构的基座; 以及夹具，其包括：第一柔性带，其从所述基部延伸并且具有从其侧面延伸的一个或多个突起; 以及第二柔性带，其从所述基部延伸并且具有用于接收所述第一柔性带的通道和锁定表面，所述锁定表面布置成接合所述第一柔性带上的所述突起之一，以防止所述第一柔性带从所述通道 。 夹子的至少一部分由弹性材料制成。
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公开(公告)号：US08400749B2
公开(公告)日：2013-03-19
申请号：US12719243
申请日：2010-03-08
IPC分类号： H05F3/00
CPC分类号： H01R4/64 , B64D37/005 , F16L25/01 , H01R11/11 , Y10T29/49117
摘要： A joint on an aircraft, the joint comprising: a first component; a second component; and a bonding lead which provides an electrical pathway between the first and second components. The bonding lead comprises a conductive core and a sheath which covers a substantial length of the core and has a lower electrical conductivity than the core. The path of least electrical resistance between the first component and the core of the bonding lead comprises the sheath, typically with an electrical resistance between 50 kΩ and 50 MΩ. By making the electrical resistance of the core much smaller than that of the sheath, the total resistance of the bonding lead remains substantially the same regardless of its length.
摘要翻译： 一种飞机上的接头，该接头包括：第一部件; 第二个组成部分 以及在第一和第二部件之间提供电路径的接合引线。 接合引线包括导电芯和护套，其覆盖芯的相当长度并且具有比芯更低的导电性。 焊接引线的第一部件和芯部之间的最小电阻的路径包括护套，通常具有在50kΩ和OHgr之间的电阻; 和50 M＆OHgr。 通过使芯的电阻远小于护套的电阻，焊接引线的总电阻保持与其长度无关的基本相同。
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公开(公告)号：US20120043419A1
公开(公告)日：2012-02-23
申请号：US13035436
申请日：2011-02-25
CPC分类号： B64C25/32 , B64C25/60 , Y10T29/49815 , Y10T29/49947
摘要： An aircraft landing gear assembly comprising an impact protection boot mounted to a landing gear component, the impact protection boot comprising: a resilient inner impact energy absorption layer which engages the component; and an outer protective layer which substantially covers the impact energy absorption layer, wherein the inner layer is more compressible than the outer layer. The boot has first and second ends which are tied to each other by a connector which exerts oppositely directed forces on the first and second ends respectively, the forces being directed around the circumference of the boot so as to tighten the boot against the landing gear component.
摘要翻译： 一种飞机起落架组件，包括安装到起落架部件的冲击保护靴，所述冲击保护靴包括：与所述部件接合的弹性内冲击能量吸收层; 以及基本上覆盖冲击能量吸收层的外部保护层，其中内层比外层更可压缩。 靴子具有通过分别在第一和第二端部上施加相反方向的力的连接器彼此连接的第一端和第二端，所述力分别围绕护罩的圆周指向，以将护罩紧固在起落架部件 。
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公开(公告)号：US20100264274A1
公开(公告)日：2010-10-21
申请号：US12762743
申请日：2010-04-19
CPC分类号： B64D37/02 , B32B3/26 , B32B7/12 , B64D45/02 , Y10T156/10 , Y10T156/1052 , Y10T428/249995 , Y10T428/31504
摘要： A fibre-reinforced composite structure includes a cut edge; an elastomeric cap covering the cut edge; and an adhesive sealant bonding the elastomeric cap to the cut edge. The fibre-reinforced composite structure is joined to a component and the elastomeric cap includes a generally Z or L-shaped cap with a web bonded to the cut edge of the fibre-reinforced structure and a flange bonded to the component and extending away from the fibre-reinforced structure.
摘要翻译： 纤维增强复合结构包括切边; 覆盖切割边缘的弹性帽; 以及将弹性体盖粘合到切割边缘上的粘合密封剂。 纤维增强复合结构被连接到部件上，并且弹性体盖包括一般为Z或L形的盖，其具有接合到纤维增强结构的切割边缘的腹板和与该部件接合并远离 纤维增强结构。
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公开(公告)号：US20100258674A1
公开(公告)日：2010-10-14
申请号：US12750990
申请日：2010-03-31
CPC分类号： B64C3/34 , B29C43/12 , B29C43/3642 , B29C2043/3649 , B29K2105/0854 , B29L2031/3085 , B29L2031/712 , B29L2031/7172 , B64C9/02 , Y02T50/44
摘要： An aircraft wing assembly comprising: a spar; a fuel tank; a track container which is attached to the spar and extends into the fuel tank; a track which extends through the spar and into the track container; and a high-lift device, such as a slat or flap, carried by the track. The track container comprises a stiffening element encased in an elastomeric sheath. The track container is manufactured by placing a stiffening element and elastomeric material together in a mould; and compressing and heating them to cure and shape the elastomeric material.
摘要翻译： 一种飞机机翼组件，包括：翼梁; 燃油箱 轨道容器，其附接到翼梁并延伸到燃料箱中; 轨道，其延伸穿过翼梁并进入轨道容器; 以及由轨道承载的高升力装置，例如板条或翼片。 轨道容器包括被包裹在弹性体护套中的加强元件。 轨道容器通过将加强元件和弹性体材料放置在模具中而制成; 并压缩和加热它们以固化和成形弹性体材料。
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公开(公告)号：US20100253014A1
公开(公告)日：2010-10-07
申请号：US12752667
申请日：2010-04-01
申请人： Colin John West
发明人： Colin John West
CPC分类号： F16J15/14
摘要： A method of sealing a joint between components especially in an aircraft comprises the steps of identifying the sealing gap to be sealed; selecting a suitable sealing material having a fractional maximum sealing thickness and a fractional fully-compressed thickness and selecting a suitable thickness of that sealing material, based on a consideration of the fractional maximum sealing thickness and the fractional fully-compressed thickness of the sealing material and on the sealing gap; locating, between the mating surfaces of the components to be sealed, the suitable thickness of the suitable sealing material; and fastening the components together.
摘要翻译： 特别是在飞行器中密封部件之间的接头的方法包括以下步骤：识别待密封的密封间隙; 基于密封材料的分数最大密封厚度和分数全压缩厚度的考虑，选择具有分数最大密封厚度和分数完全压缩厚度的合适的密封材料并选择该密封材料的合适厚度，以及 密封间隙; 在要密封的部件的配合表面之间定位合适的密封材料的合适厚度; 并将部件固定在一起。
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