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1. 发明授权

US08854787B2 Bond lead 有权
标题翻译：债券领先
公开(公告)号：US08854787B2
公开(公告)日：2014-10-07
申请号：US13212473
申请日：2011-08-18
申请人： Andrew Paul Limmack , David Alistair Sutton , Colin John West
发明人： Andrew Paul Limmack , David Alistair Sutton , Colin John West
IPC分类号： H05F3/00 , B64D37/32 , H01B1/24 , F16L27/12 , F16L25/01 , F16L27/02
CPC分类号： F16L27/12 , B64D37/32 , F16L25/01 , F16L27/026 , H01B1/24 , Y10T29/49174
摘要： A bonding lead comprising a core; and a sheath bonded to the core. The core comprises a substrate of fibers coated with nano-objects with at least one dimension between 1 nm and 200 nm. The nano-objects form a continuous electrically conductive network from one end of the bonding lead to the other with some of the nano-objects coating the fibers and others forming bridges between adjacent fibers. The nano-objects may be carbon nanotubes and the core may be woven or knitted. A conductive connector is provided at each end of the bonding lead, for instance a tab formed from an electrically conductive polymer. The lead can be used to dissipate static charge and/or lightning current between components, typically within an aircraft fuel tank.
摘要翻译：一种包括芯的接合引线; 和与芯结合的护套。芯包括涂覆有至少一个尺寸在1nm和200nm之间的纳米物体的纤维基底。纳米物体从接合引线的一端到另一端形成连续的导电网络，其中一些纳米物体涂覆纤维，而其它纳米物体在相邻的纤维之间形成桥。纳米物体可以是碳纳米管，并且芯可以被编织或编织。导电连接器设置在接合引线的每个端部处，例如由导电聚合物形成的突片。引线可用于消除部件之间的静电荷和/或雷电流，通常在飞机燃料箱内。

2. 发明授权

US08424807B2 Track container 有权
标题翻译：跟踪容器
公开(公告)号：US08424807B2
公开(公告)日：2013-04-23
申请号：US12750990
申请日：2010-03-31
申请人： David Alistair Sutton , Colin John West
发明人： David Alistair Sutton , Colin John West
IPC分类号： B64C9/14
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。

3. 发明授权

US08254078B2 Bonding lead 有权
标题翻译：粘接铅
公开(公告)号：US08254078B2
公开(公告)日：2012-08-28
申请号：US12719206
申请日：2010-03-08
申请人： David Alistair Sutton , Colin John West
发明人： David Alistair Sutton , Colin John West
IPC分类号： H05F3/00
CPC分类号： H01R4/64 , B64D37/32 , F16L25/01 , H01R11/12 , Y10T29/49117
摘要： A joint on an aircraft, a bonding lead for use in such a joint, and a method of manufacturing such a joint. The bonding lead comprises an elongate conductive core with a pair of end faces at the extremities of its length. The conductive core is encapsulated along at least a majority of its length and at both end faces in a barrier layer typically formed from an elastomer. The lead is encapsulated along its length in the barrier layer apart from at a first contact region towards a first end of the bonding lead and a second contact region towards a second end of the bonding lead. A first electrical connector passes through a first hole in the barrier layer to engage the first contact region of the conductive core and provide an electrical connection between the conductive core and the first component; and a second electrical connector passes through a second hole in the barrier layer to engage the second contact region of the conductive core and provide an electrical connection between the conductive core and the second component.
摘要翻译：飞机上的接头，用于这种接头的接合引线以及这种接头的制造方法。接合引线包括细长的导电芯，在其长度的末端具有一对端面。导电芯沿其长度的至少大部分被封装，并且通常由弹性体形成的阻挡层的两个端面被封装。引线沿阻挡层的长度被封装在远离接合引线的第一接触区域朝向第一端，并且朝向接合引线的第二端的第二接触区域。第一电连接器穿过阻挡层中的第一孔以接合导电芯的第一接触区，并在导电芯和第一部件之间提供电连接; 并且第二电连接器穿过阻挡层中的第二孔以接合导电芯的第二接触区，并在导电芯和第二组件之间提供电连接。

4. 发明申请

US20100243826A1 LINE ROUTING CLIP 有权
标题翻译：线路线夹
公开(公告)号：US20100243826A1
公开(公告)日：2010-09-30
申请号：US12743870
申请日：2008-12-01
申请人： Colin John West , David Alistair Sutton
发明人： Colin John West , David Alistair Sutton
IPC分类号： F16L3/22 , F16L3/12
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。

5. 发明授权

US09365283B2 Seal 有权
标题翻译：密封
公开(公告)号：US09365283B2
公开(公告)日：2016-06-14
申请号：US13883398
申请日：2011-11-07
申请人： James Wilson , Colin John West , David Alistair Sutton , Paul Hadley
发明人： James Wilson , Colin John West , David Alistair Sutton , Paul Hadley
IPC分类号： B64C7/00 , B64C9/02 , B64C9/22 , B64C3/50 , B29C70/26
CPC分类号： B64C7/00 , B29C70/26 , B64C3/50 , B64C9/02 , B64C9/22 , Y02T50/43
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。

6. 发明授权

US09038789B2 Method and apparatus for controlling an elastomeric damper 有权
标题翻译：用于控制弹性阻尼器的方法和装置
公开(公告)号：US09038789B2
公开(公告)日：2015-05-26
申请号：US13010063
申请日：2011-01-20
申请人： Colin John West , David Alistair Sutton
发明人： Colin John West , David Alistair Sutton
IPC分类号： F16F15/03 , F16F1/36 , F16F1/379 , B64D27/26
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。

7. 发明授权

US08864141B2 Blade seal 有权
标题翻译：刀片密封
公开(公告)号：US08864141B2
公开(公告)日：2014-10-21
申请号：US12349116
申请日：2009-01-06
申请人： Colin John West , David Alistair Sutton
发明人： Colin John West , David Alistair Sutton
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。

8. 发明授权

US08844881B2 Line routing clip 有权
标题翻译：线路路由剪辑
公开(公告)号：US08844881B2
公开(公告)日：2014-09-30
申请号：US12743870
申请日：2008-12-01
申请人： Colin John West , David Alistair Sutton
发明人： Colin John West , David Alistair Sutton
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。

9. 发明授权

US08400749B2 Aircraft joint and bonding lead 有权
标题翻译：飞机接头和接头导线
公开(公告)号：US08400749B2
公开(公告)日：2013-03-19
申请号：US12719243
申请日：2010-03-08
申请人： Colin John West , David Alistair Sutton
发明人： Colin John West , David Alistair Sutton
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。

10. 发明申请

US20120043419A1 AIRCRAFT LANDING GEAR ASSEMBLY 审中-公开
标题翻译：飞机接地齿轮总成
公开(公告)号：US20120043419A1
公开(公告)日：2012-02-23
申请号：US13035436
申请日：2011-02-25
申请人： Leslie John CLARK , Colin John West , David Alistair Sutton
发明人： Leslie John CLARK , Colin John West , David Alistair Sutton
IPC分类号： B64C25/58 , B23P11/00
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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