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公开(公告)号：US20240140049A1
公开(公告)日：2024-05-02
申请号：US18407786
申请日：2024-01-09
Applicant: Industrial Dielectrics, Inc. , A & P Technology, Inc.
Inventor： Michael S. BRALEY , Kevin M. CAHILL , James D. JERN
CPC classification number: B29C70/081 , B29C70/0035 , B29C70/40 , B29C70/46 , B29K2307/04
Abstract: A composite article includes a first segment and a second segment spaced apart form the first segment. The composite article includes continuous fibers that extend from the first segment to the second segment. The composite article also includes discontinuous fiber distributed throughout the composite article.
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公开(公告)号：US09702069B2
公开(公告)日：2017-07-11
申请号：US14210874
申请日：2014-03-14
Applicant: A&P Technology, Inc.
Inventor： Andrew A. Head , Victor M. Ivers , Samuel P. Ivers
Abstract: A three dimensional braid includes a plurality of first plaits adjacent one another oriented in a first direction and a plurality of second plaits adjacent one another oriented in a transverse second direction intertwined forming a braid with each first plait intersecting each of the plurality of second plaits in succession. Each first plait includes a first group of tows and a second group of tows, each of the tows in the first group of tows corresponding to one of the tows in the second group of tows in pairs of first plait tows. Each second plait includes a plurality of tows. For each first plait, one of the first plait pairs crosses over a subset of second plait tows at each intersection of the first plait and successive second plaits forming a series of braid points along the first plait.
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公开(公告)号：US09327757B2
公开(公告)日：2016-05-03
申请号：US14210899
申请日：2014-03-14
Applicant: A&P Technology, Inc.
Inventor： David J. Kehrl
Abstract: An energy-absorbing deformable tube having a first end, a second end, and a reduced portion there between, a proximate tube portion between the reduced portion and the first end and a distal tube portion between the reduced portion and the second end, where a first cross section dimension in the reduced portion is smaller than a corresponding second cross section dimension in the proximal tube portion, distal tube portion, or both, and a cover spanning the reduced portion connected to the proximal tube portion and the distal tube portion, the cover provided over at least a portion of the reduced portion, the distal tube portion or the proximal tube portion or both moves relative to the cover after the deformable tube receives an axial force exceeding a predetermined threshold value.
Abstract translation: 一种能量吸收可变形管，其具有第一端，第二端和其间的减小部分，所述减压部分和所述第一端之间的近端管部分和所述减小部分与所述第二端部之间的远端管部分，其中 缩小部分的第一横截面尺寸小于近端管部分，远端管部分或两者中的对应的第二横截面尺寸，以及跨越连接到近端管部分和远端管部分的缩小部分的盖， 在可变形管接受超过预定阈值的轴向力之后，设置在减小部分的至少一部分上的远端管部分或近端管部分或两者相对于盖移动。
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公开(公告)号：US09169732B1
公开(公告)日：2015-10-27
申请号：US14270673
申请日：2014-05-06
Applicant: A&P Technology, Inc.
Inventor： Mike S. Braley , Andrew A. Head , Phillip M. Lariviere , Victor M. Ivers
CPC classification number: F01D5/147 , B29D99/0028 , F03D1/0675 , F03D1/0683 , F03D13/10 , Y02B10/30 , Y02E10/721 , Y02P70/523
Abstract: A wind turbine blade may include a plurality of longitudinal composite members each having a fiber and resin layer around a predetermined cross-sectional shape and each comprising at least one longitudinal outer surface and at least one longitudinal mounting surface, each of the outer surfaces of the plurality of longitudinal composite members corresponding to a different portion of a desired airfoil shape, the plurality of longitudinal composite members assembled such that the outer surfaces of the composite members form at least a majority of the airfoil shape. An outer skin may be provided. The composite members may be made up of transportable segments. A method of assembly may include transporting the segments to a desired location such as an installation site for assembly of the wind turbine blade at the installation site.
Abstract translation: 风力涡轮机叶片可以包括多个纵向复合构件，每个纵向复合构件具有围绕预定横截面形状的纤维和树脂层，并且每个包括至少一个纵向外表面和至少一个纵向安装表面，每个外表面 多个纵向复合构件对应于期望的翼型形状的不同部分，所述多个纵向复合构件组装成使得复合构件的外表面形成至少大部分翼型形状。 可以提供外皮。 复合构件可以由可移动段构成。 组装方法可以包括将段传送到期望的位置，例如在安装地点组装风力涡轮机叶片的安装地点。
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公开(公告)号：US08753091B1
公开(公告)日：2014-06-17
申请号：US12784320
申请日：2010-05-20
Applicant: Mike S. Braley , Andrew A. Head , Phillip M. Lariviere , Victor M. Ivers
Inventor： Mike S. Braley , Andrew A. Head , Phillip M. Lariviere , Victor M. Ivers
IPC: F03D11/00
CPC classification number: F01D5/147 , B29D99/0028 , F03D1/0675 , F03D1/0683 , F03D13/10 , Y02B10/30 , Y02E10/721 , Y02P70/523
Abstract: A wind turbine blade may include a plurality of longitudinal composite members each having a fiber and resin layer around a predetermined cross-sectional shape and each comprising at least one longitudinal outer surface and at least one longitudinal mounting surface, each of the outer surfaces of the plurality of longitudinal composite members corresponding to a different portion of a desired airfoil shape, the plurality of longitudinal composite members assembled such that the outer surfaces of the composite members form at least a majority of the airfoil shape. An outer skin may be provided. The composite members may be made up of transportable segments. A method of assembly may include transporting the segments to a desired location such as an installation site for assembly of the wind turbine blade at the installation site.
Abstract translation: 风力涡轮机叶片可以包括多个纵向复合构件，每个纵向复合构件具有围绕预定横截面形状的纤维和树脂层，并且每个包括至少一个纵向外表面和至少一个纵向安装表面，每个外表面 多个纵向复合构件对应于期望的翼型形状的不同部分，所述多个纵向复合构件组装成使得复合构件的外表面形成至少大部分翼型形状。 可以提供外皮。 复合构件可以由可移动段构成。 组装方法可以包括将段传送到期望的位置，例如在安装地点组装风力涡轮机叶片的安装地点。
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Patent Agency Ranking
6.发明授权Braided reinforcement for aircraft fuselage frames and method of producing the same 有权飞机机身框架的编织加固及其制造方法公开(公告)号：US08210086B2
公开(公告)日：2012-07-03
申请号：US12881895
申请日：2010-09-14
Applicant: Andrew Atkins Head , Brad Goetz , John Peter , Steven Charles Stenard , Thomas C. Story
Inventor： Andrew Atkins Head , Brad Goetz , John Peter , Steven Charles Stenard , Thomas C. Story
IPC: D04C3/40
CPC classification number: D04C3/48 , D04C1/02 , D04C3/36 , D10B2505/02
Abstract: A method for applying a braided fabric over a mandrel using a braiding apparatus having a central axis and providing braiding yarns drawn toward a braiding point where a braid is formed on the mandrel, the method comprising the steps of advancing the mandrel through the braiding point of the braiding apparatus, determining a current position of the mandrel; and controlling the position of the mandrel transversely to the central axis of the braiding apparatus responsive to the current position such that a center point of a mandrel cross-section passing through the braiding apparatus is coincident with the braiding point.
Abstract translation: 一种使用具有中心轴线的编织装置在芯轴上施加编织织物的方法，并且提供编织纱线，所述编织纱线被卷绕到芯轴上形成编织物的编织点，所述方法包括以下步骤：将心轴推进到编织点的编织点 编织装置，确定心轴的当前位置; 并且响应于当前位置横向于编织装置的中心轴线控制心轴的位置，使得通过编织装置的心轴横截面的中心点与编织点一致。
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7.发明申请BRAIDED REINFORCEMENT FOR AIRCRAFT FUSELAGE FRAMES AND METHOD OF PRODUCING THE SAME 有权用于飞机熔融框架的加固加固及其生产方法公开(公告)号：US20110283870A1
公开(公告)日：2011-11-24
申请号：US12881895
申请日：2010-09-14
Applicant: Andrew Atkins Head , Brad Goetz , John Peter , Steven Charles Stenard , Thomas C. Story
Inventor： Andrew Atkins Head , Brad Goetz , John Peter , Steven Charles Stenard , Thomas C. Story
CPC classification number: D04C3/48 , D04C1/02 , D04C3/36 , D10B2505/02
Abstract: A method for applying a braided fabric over a mandrel using a braiding apparatus having a central axis and providing braiding yarns drawn toward a braiding point where a braid is formed on the mandrel, the method comprising the steps of advancing the mandrel through the braiding point of the braiding apparatus, determining a current position of the mandrel; and controlling the position of the mandrel transversely to the central axis of the braiding apparatus responsive to the current position such that a center point of a mandrel cross-section passing through the braiding apparatus is coincident with the braiding point.
Abstract translation: 一种使用具有中心轴线的编织装置在芯轴上施加编织织物的方法，并且提供编织纱线，所述编织纱线被卷绕到芯轴上形成编织物的编织点，所述方法包括以下步骤：将心轴推进到编织点的编织点 编织装置，确定心轴的当前位置; 并且响应于当前位置横向于编织装置的中心轴线控制心轴的位置，使得通过编织装置的心轴横截面的中心点与编织点一致。
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8.发明授权Braided reinforcement for aircraft fuselage frames and method of producing the same 有权飞机机身框架的编织加固及其制造方法公开(公告)号：US07793576B2
公开(公告)日：2010-09-14
申请号：US12017964
申请日：2008-01-22
Applicant: Andrew Atkins Head , Brad Goetz , John Peter , Steven Charles Stenard , Thomas C. Story
Inventor： Andrew Atkins Head , Brad Goetz , John Peter , Steven Charles Stenard , Thomas C. Story
IPC: D04C3/40
CPC classification number: D04C3/48 , D04C1/02 , D04C3/36 , D10B2505/02
Abstract: A machine and method for applying braid by means of a braiding machine to a mandrel, where the mandrel has a shape that approximates a wheel but has an irregularly varying radius of curvature. The machine includes drive/positioning wheel assemblies that are used to continuously reposition a cross-section of the mandrel relative to the braiding machine such that a center point of cross-section of the mandrel is maintained to be coaxial with a braiding point of the braiding machine as the mandrel 18 is rotationally advanced by the drive/positioning wheel assemblies. Repositioning of the drive/positioning wheel assemblies is controlled by a computer numerical control (CNC) controller, based on information describing one or more radiuses of curvature for sections of the mandrel and a current position of the mandrel relative to the drive/positioning wheel assemblies.
Abstract translation: 一种通过编织机将编织物施加到心轴上的机器和方法，其中心轴具有近似于轮的形状但具有不规则变化的曲率半径的形状。 该机器包括驱动/定位轮组件，其用于连续地重新定位心轴相对于编织机的横截面，使得心轴的横截面的中心点保持与编织的编织点同轴 心轴18通过驱动/定位轮组件转动地推进。 驱动/定位轮组件的重新定位由计算机数控（CNC）控制器控制，该控制器基于描述心轴部分的一个或多个曲率半径的信息以及心轴相对于驱动/定位轮组件的当前位置 。
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公开(公告)号：US6112634A
公开(公告)日：2000-09-05
申请号：US4579
申请日：1998-01-08
Applicant: Andrew A. Head
Inventor： Andrew A. Head
IPC: B60R21/233 , B60R21/16 , B60R21/215 , B60R21/235 , D03D15/00 , D04C1/02 , D04C1/06 , D04C1/12 , D04C1/00
CPC classification number: B60R21/235 , D03D1/02 , D03D15/00 , D04C1/02 , D04C1/06 , B60R21/23184 , D10B2321/021 , D10B2321/022 , D10B2331/02 , D10B2331/04 , D10B2401/041 , D10B2505/124
Abstract: A braided structure produced by strands of a braiding material consisting of multiple yarn ends of multifilament fibers oriented side-by-side or in parallel to form a generally single layer band of yarn ends and treated with a suitable forming material in order to set such orientation. The braiding material can then be used to form strands for producing a braided structure. The braided structure resulting from the braiding material of our invention has a high coverage area and a high width to thickness ratio.
Abstract translation: 编织结构由编织材料的股线制成，编织材料由复丝纤维的多个纱线端组成，并排或并排定向，以形成纱线端部的大致单层带，并用合适的成形材料处理以设定这种取向 。 然后编织材料可用于形成用于产生编织结构的股线。 由本发明的编织材料产生的编织结构具有高覆盖面积和高宽比。
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公开(公告)号：US12152323B1
公开(公告)日：2024-11-26
申请号：US17548475
申请日：2021-12-10
Applicant: A&P Technology, Inc.
Inventor： Andrew Head , Victor M. Ivers , Samuel P. Ivers
Abstract: A three-dimensional braid includes a plurality of first plaits adjacent one another oriented in a first direction and a plurality of second plaits adjacent one another oriented in a transverse second direction intertwined forming a braid with each first plait intersecting each of the plurality of second plaits in succession. Each first plait includes a first group of tows and a second group of tows, each of the tows in the first group of tows corresponding to one of the tows in the second group of tows in pairs of first plait tows. Each second plait includes a plurality of tows. For each first plait, one of the first plait pairs crosses over a subset of second plait tows at each intersection of the first plait and successive second plaits forming a series of braid points along the first plait.
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