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公开(公告)号：US20110028061A1
公开(公告)日：2011-02-03
申请号：US12801826
申请日：2010-06-28
Applicant: Timothy Sanderson , Peter Burchell
Inventor： Timothy Sanderson , Peter Burchell
CPC classification number: B32B5/26 , B29C35/02 , B29C37/04 , B29C65/3436 , B29C65/344 , B29C65/3444 , B29C65/3636 , B29C65/364 , B29C65/3676 , B29C65/4815 , B29C65/4835 , B29C65/5014 , B29C65/5021 , B29C65/5057 , B29C66/112 , B29C66/131 , B29C66/43441 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/72141 , B29C66/73116 , B29C66/73752 , B29C66/7392 , B29C66/73921 , B29C66/7394 , B29C66/73941 , B29C66/8322 , B29C70/24 , B29C70/28 , B29L2031/3076 , B32B5/024 , B32B5/026 , B32B5/08 , B32B5/12 , B32B5/22 , B32B7/02 , B32B2260/021 , B32B2260/046 , B32B2262/0269 , B32B2262/101 , B32B2262/106 , B32B2262/14 , B32B2307/50 , B32B2307/58 , B32B2605/18 , Y10T428/249921 , Y10T442/3195 , Y10T442/45 , B29K2307/04 , B29K2077/00 , B29K2309/08 , B29K2277/10 , B29K2071/00 , B29K2079/085 , B29K2063/00
Abstract: An adjustable shim comprises a stack of plies comprising plastics material reinforced with a three-dimensional fibre layer, the plastics material being flowable under compressive force prior to cure for adjusting the thickness of the shim. The shim may be used to fill a void between two structural components joined together. Also, a method of filling a void between two structural components using the shim. The shim is easy to handle, can easily be laid up to a variety of thicknesses, and is quick to cure (depending on the plastics material used). The three-dimensional fibre layers make the shim highly compressible prior to cure, and provide significant reinforcement to the plastics material of the plies to support compressive stresses in the shim post cure.
Abstract translation: 可调节垫片包括一层叠层，包括用三维纤维层增强的塑料材料，塑料材料可在固化之前以压缩力流动，以调节垫片的厚度。 垫片可用于填充连接在一起的两个结构部件之间的空隙。 另外，使用垫片在两个结构部件之间填充空隙的方法。 垫片易于处理，可以容易地铺设成各种厚度，并且快速固化（取决于所使用的塑料材料）。 三维纤维层在固化之前使垫片高度可压缩，并且对层的塑料材料提供显着的加固以支持垫片后固化中的压应力。
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公开(公告)号：US09452588B2
公开(公告)日：2016-09-27
申请号：US12801826
申请日：2010-06-28
Applicant: Timothy Sanderson , Peter Burchell
Inventor： Timothy Sanderson , Peter Burchell
IPC: B29C43/00 , B32B5/26 , B29C65/34 , B29C65/36 , B29C65/50 , B29C65/00 , B29C70/24 , B29C70/28 , B29C65/48 , B32B5/02 , B32B5/08 , B32B5/12 , B32B5/22 , B32B7/02 , B29C35/02 , B29C37/04 , B29L31/30
CPC classification number: B32B5/26 , B29C35/02 , B29C37/04 , B29C65/3436 , B29C65/344 , B29C65/3444 , B29C65/3636 , B29C65/364 , B29C65/3676 , B29C65/4815 , B29C65/4835 , B29C65/5014 , B29C65/5021 , B29C65/5057 , B29C66/112 , B29C66/131 , B29C66/43441 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/72141 , B29C66/73116 , B29C66/73752 , B29C66/7392 , B29C66/73921 , B29C66/7394 , B29C66/73941 , B29C66/8322 , B29C70/24 , B29C70/28 , B29L2031/3076 , B32B5/024 , B32B5/026 , B32B5/08 , B32B5/12 , B32B5/22 , B32B7/02 , B32B2260/021 , B32B2260/046 , B32B2262/0269 , B32B2262/101 , B32B2262/106 , B32B2262/14 , B32B2307/50 , B32B2307/58 , B32B2605/18 , Y10T428/249921 , Y10T442/3195 , Y10T442/45 , B29K2307/04 , B29K2077/00 , B29K2309/08 , B29K2277/10 , B29K2071/00 , B29K2079/085 , B29K2063/00
Abstract: An adjustable shim comprises a stack of plies comprising plastics material reinforced with a three-dimensional fiber layer, the plastics material being flowable under compressive force prior to cure for adjusting the thickness of the shim. The shim may be used to fill a void between two structural components joined together. Also, a method of filling a void between two structural components using the shim. The shim is easy to handle, can easily be laid up to a variety of thicknesses, and is quick to cure (depending on the plastics material used). The three-dimensional fiber layers make the shim highly compressible prior to cure, and provide significant reinforcement to the plastics material of the plies to support compressive stresses in the shim post cure.
Abstract translation: 可调节垫片包括一层叠层，包括用三维纤维层增强的塑料材料，塑料材料可在固化之前以压缩力流动，以调节垫片的厚度。 垫片可用于填充连接在一起的两个结构部件之间的空隙。 另外，使用垫片在两个结构部件之间填充空隙的方法。 垫片易于处理，可以容易地铺设成各种厚度，并且快速固化（取决于所使用的塑料材料）。 三维纤维层在固化之前使垫片高度可压缩，并且对层的塑料材料提供显着的加固以支持垫片后固化中的压应力。
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公开(公告)号：US08899529B2
公开(公告)日：2014-12-02
申请号：US12801597
申请日：2010-06-16
Applicant: Timothy Sanderson
Inventor： Timothy Sanderson
Abstract: A telescopic strut comprises a plurality of hollow members arranged to slide one within another between a retracted and an extended position. Adjacent hollow members are arranged to be electrically connected by one or more electrical connector assemblies as the hollow members move between the retracted and extended positions. Each electrical connector assembly includes an electrically conductive pad on one of the hollow members which is in sliding contact with an electrically conductive strip on the other of the hollow members. The telescopic strut may be used to electrically connect a moveable control surface to a fixed aerofoil structure in an aircraft.
Abstract translation: 伸缩支柱包括多个中空构件，其布置成在缩回位置和伸出位置之间将另一个滑动。 相邻的中空构件被布置成通过一个或多个电连接器组件电连接，因为中空构件在缩回位置和伸出位置之间移动。 每个电连接器组件包括在一个中空构件上的导电垫，其与另一个中空构件上的导电带滑动接触。 可伸缩支柱可用于将可移动控制表面与飞行器中的固定机翼结构电连接。
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公开(公告)号：US08616499B2
公开(公告)日：2013-12-31
申请号：US13263215
申请日：2010-03-31
Applicant: Michael Tucker , Timothy Sanderson
Inventor： Michael Tucker , Timothy Sanderson
IPC: B64C3/00
Abstract: A wing structure is provided, wherein the wing structure comprises; an upper covering, a lower covering, and a spar, the spar comprising; a spar web, an upper spar cap attached to the upper covering, and a lower spar cap attached to the lower covering, the wing structure also comprising a face spaced apart from the spar web extending between the upper and lower spar caps. The wing structure is arranged to contain fuel in a fuel containment area between the upper and lower coverings on one side of the spar web. The upper and lower spar caps extend from the spar web only on the other side of the spar web to the fuel containment area.
Abstract translation: 提供翼结构，其中翼结构包括： 上盖，下覆盖物和翼梁，翼梁包括; 翼梁网，附接到上覆盖物的上翼梁帽和附接到下覆盖物的下翼梁帽，翼结构还包括与在上翼梁和下翼梁盖之间延伸的翼梁腹板间隔开的面。 翼结构被布置成在翼梁腹板的一侧上的上盖和下盖之间的燃料容纳区域中容纳燃料。 上部和下部翼梁盖仅在翼梁网的另一侧从翼梁网延伸到燃料密封区域。
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Patent Agency Ranking
公开(公告)号：US20120045613A1
公开(公告)日：2012-02-23
申请号：US13265267
申请日：2010-04-15
Applicant: Timothy Sanderson
Inventor： Timothy Sanderson
CPC classification number: B32B7/08 , B29C65/562 , B29C65/564 , B29C66/1122 , B29C66/30341 , B29C66/43 , B29C66/5346 , B29C66/53465 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/72141 , B29C66/73112 , B29C66/7392 , B29C66/7394 , B29C66/73941 , B29L2031/3076 , B29L2031/3085 , B29L2031/7172 , B32B3/26 , B32B3/30 , B32B5/022 , B32B5/024 , B32B5/026 , B32B5/14 , B32B5/22 , B32B5/26 , B32B2260/023 , B32B2260/046 , B32B2262/106 , B32B2307/50 , B32B2307/718 , B32B2605/18 , Y02T50/43 , Y10T156/1057 , Y10T428/24322 , B29K2307/04 , B29K2071/00 , B29K2063/00
Abstract: A structure comprising a cured composite part formed from a series of plies of fibre-reinforced composite material; a doubler plate attached to the composite part by an array of pointed prongs which partially penetrate the composite part; and a hole passing through the doubler plate and the composite part. An interface plate carries the array of prongs on a first side and is attached to the doubler plate on a second side.
Abstract translation: 一种结构，其包括由一系列纤维增强复合材料形成的固化复合部件; 通过一部分穿透复合部件的尖头尖头连接到复合部件的倍增板; 以及穿过倍加板和复合部件的孔。 接口板在第一侧承载尖头阵列，并且在第二侧上附接到倍频器板。
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公开(公告)号：US20120037755A1
公开(公告)日：2012-02-16
申请号：US13263215
申请日：2010-03-31
Applicant: Michael Tucker , Timothy Sanderson
Inventor： Michael Tucker , Timothy Sanderson
Abstract: A wing structure is provided, wherein the wing structure comprises; an upper covering, a lower covering, and a spar, the spar comprising; a spar web, an upper spar cap attached to the upper covering, and a lower spar cap attached to the lower covering, the wing structure also comprising a face spaced apart from the spar web extending between the upper and lower spar caps. The wing structure is arranged to contain fuel in a fuel containment area between the upper and lower coverings on one side of the spar web. The upper and lower spar caps extend from the spar web only on the other side of the spar web to the fuel containment area.
Abstract translation: 提供翼结构，其中翼结构包括： 上盖，下覆盖物和翼梁，翼梁包括; 翼梁网，附接到上覆盖物的上翼梁帽和附接到下覆盖物的下翼梁帽，翼结构还包括与在上翼梁和下翼梁盖之间延伸的翼梁腹板间隔开的面。 翼结构被布置成在翼梁腹板的一侧上的上盖和下盖之间的燃料容纳区域中容纳燃料。 上部和下部翼梁盖仅在翼梁网的另一侧从翼梁网延伸到燃料密封区域。
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公开(公告)号：US20100327111A1
公开(公告)日：2010-12-30
申请号：US12801597
申请日：2010-06-16
Applicant: Timothy Sanderson
Inventor： Timothy Sanderson
Abstract: A telescopic strut comprises a plurality of hollow members arranged to slide one within another between a retracted and an extended position. Adjacent hollow members are arranged to be electrically connected by one or more electrical connector assemblies as the hollow members move between the retracted and extended positions. Each electrical connector assembly includes an electrically conductive pad on one of the hollow members which is in sliding contact with an electrically conductive strip on the other of the hollow members. The telescopic strut may be used to electrically connect a moveable control surface to a fixed aerofoil structure in an aircraft.
Abstract translation: 伸缩支柱包括多个中空构件，其布置成在缩回位置和伸出位置之间将另一个滑动。 相邻的中空构件被布置成通过一个或多个电连接器组件电连接，因为中空构件在缩回位置和伸出位置之间移动。 每个电连接器组件包括在一个中空构件上的导电垫，其与另一个中空构件上的导电带滑动接触。 可伸缩支柱可用于将可移动控制表面与飞行器中的固定机翼结构电连接。
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公开(公告)号：US08506746B2
公开(公告)日：2013-08-13
申请号：US13064474
申请日：2011-03-28
Applicant: Chetan Korya , Timothy Sanderson
Inventor： Chetan Korya , Timothy Sanderson
CPC classification number: B29C66/43441 , B29C64/153 , B29C65/08 , B29C65/342 , B29C65/3432 , B29C65/3476 , B29C65/362 , B29C65/3632 , B29C65/3676 , B29C65/72 , B29C66/112 , B29C66/1122 , B29C66/116 , B29C66/131 , B29C66/30321 , B29C66/474 , B29C66/52441 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/72141 , B29C66/7392 , B29C66/7394 , B29C70/30 , B29L2031/3085 , B33Y10/00 , B33Y30/00 , B33Y80/00 , B64C2001/0072 , Y02T50/43 , Y10T156/10 , Y10T403/477 , B29K2071/00 , B29K2081/04 , B29K2307/04 , B29K2063/00
Abstract: A method of forming a joint between a first component and a second component, the first component comprising a plurality of layers of fibers impregnated with a thermosetting matrix. A welding interface element is provided with an array of pointed prongs. One or more of the layers of fibers are penetrated with the prongs, either before or after the fibers have been impregnated with the thermosetting matrix. The first component is cured by heating the thermosetting matrix after the prongs have been embedded. A thermoplastic weld is formed between the second component and the welding interface element.
Abstract translation: 一种在第一部件和第二部件之间形成接头的方法，所述第一部件包括浸渍有热固性基质的多层纤维。 一个焊接接口元件设有尖头尖头阵列。 在纤维被热固性基质浸渍之前或之后，一个或多个纤维层被尖头穿透。 第一种组分通过在插入嵌脚后加热热固性基质来固化。 在第二部件和焊接界面元件之间形成热塑性焊接。
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公开(公告)号：US20110240200A1
公开(公告)日：2011-10-06
申请号：US13064474
申请日：2011-03-28
Applicant: Chetan Korya , Timothy Sanderson
Inventor： Chetan Korya , Timothy Sanderson
CPC classification number: B29C66/43441 , B29C64/153 , B29C65/08 , B29C65/342 , B29C65/3432 , B29C65/3476 , B29C65/362 , B29C65/3632 , B29C65/3676 , B29C65/72 , B29C66/112 , B29C66/1122 , B29C66/116 , B29C66/131 , B29C66/30321 , B29C66/474 , B29C66/52441 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/72141 , B29C66/7392 , B29C66/7394 , B29C70/30 , B29L2031/3085 , B33Y10/00 , B33Y30/00 , B33Y80/00 , B64C2001/0072 , Y02T50/43 , Y10T156/10 , Y10T403/477 , B29K2071/00 , B29K2081/04 , B29K2307/04 , B29K2063/00
Abstract: A method of forming a joint between a first component and a second component, the first component comprising a plurality of layers of fibres impregnated with a thermosetting matrix. A welding interface element is provided with an array of pointed prongs. One or more of the layers of fibres are penetrated with the prongs, either before or after the fibres have been impregnated with the thermosetting matrix. The first component is cured by heating the thermosetting matrix after the prongs have been embedded. A thermoplastic weld is formed between the second component and the welding interface element.
Abstract translation: 一种在第一部件和第二部件之间形成接头的方法，所述第一部件包括浸渍有热固性基质的多层纤维。 一个焊接接口元件设有尖头尖头阵列。 在纤维被热固性基质浸渍之前或之后，一个或多个纤维层被尖头穿透。 第一种组分通过在插入嵌脚后加热热固性基质来固化。 在第二部件和焊接界面元件之间形成热塑性焊接。
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