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1.发明申请公开(公告)号：US20160076179A1
公开(公告)日：2016-03-17
申请号：US14852926
申请日：2015-09-14
Applicant: Airbus Operations GmbH
Inventor： Tassilo Witte , Georg Lonsdorfer
IPC: D04H1/4242 , B32B37/14 , B32B15/14 , B32B3/12 , B32B7/12
CPC classification number: D04H1/4242 , B29D24/005 , B29D99/0089 , B32B3/12 , B32B5/02 , B32B5/022 , B32B5/22 , B32B5/26 , B32B7/12 , B32B15/14 , B32B37/1292 , B32B37/146 , B32B2260/021 , B32B2260/046 , B32B2262/106 , B32B2305/024 , B32B2305/72 , B32B2307/50 , B32B2605/18
Abstract: A honeycomb structure comprising carbon-fiber non-woven, sandwich structure comprising the said honeycomb structure, and process for the production of the said honeycomb structure.
Abstract translation: 一种蜂窝结构体，其包含所述蜂窝结构体的碳纤维无纺布，夹层结构体，以及所述蜂窝结构体的制造方法。
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公开(公告)号：US09186842B2
公开(公告)日：2015-11-17
申请号：US14055162
申请日：2013-10-16
Applicant: AIRBUS OPERATIONS GMBH
Inventor： Tassilo Witte , Jan Huelnhagen
CPC classification number: B29C53/043 , B29B11/16 , B29D99/0007 , B29L2031/001 , B29L2031/7739 , Y10T156/1008
Abstract: Method for manufacturing a dry textile preform, including: pulling a textile fabric sheet; grabbing a first side portion of the sheet between rollers, the rollers forming a first flange of the first side portion of the sheet inclined at a predeterminable angle to the plane of extension of the sheet; grabbing a second side portion of the sheet opposite to the first side portion between other rollers, the other rollers forming a second flange of the second side portion of the sheet inclined at a predeterminable angle to the plane of extension of the sheet; adjusting a difference between the rolling speed of the pair of first rollers and the rolling speed of the pair of second rollers to form a curvature radius of the sheet; and adjusting distance between the rollers perpendicular to the movement direction of the sheet to form a web portion between the first flange.
Abstract translation: 干织物预制品的制造方法，包括：拉伸织物片; 在辊之间抓住片材的第一侧部分，所述辊形成片材的第一侧部的第一凸缘以与片材的延伸平面成可预定的角度倾斜; 抓住与其它辊子之间的第一侧部分相对的片材的第二侧部分，其他辊子形成片材的第二侧部分的第二凸缘，其以与片材的延伸平面成可预定的角度倾斜; 调整所述一对第一辊的轧制速度与所述一对第二辊的轧制速度之间的差以形成所述板的曲率半径; 以及调整垂直于片材的移动方向的辊之间的距离，以在第一凸缘之间形成腹板部分。
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公开(公告)号：US20150151498A1
公开(公告)日：2015-06-04
申请号：US14560671
申请日：2014-12-04
Applicant: Airbus Operations GmbH
Inventor： Tassilo Witte
CPC classification number: B29C73/02 , B29C35/045 , B29C35/16 , B29C73/34 , B29C2035/0838 , B29C2035/0855 , B29C2791/005 , B29K2101/10 , B29K2105/08 , B29L2031/3076 , B29L2031/3082 , B64C1/06 , B64C2001/0072
Abstract: A method of repairing an affected area of a component of a fiber-reinforced polymer composite, especially having elongate or continuous reinforcing fibers in a polymer matrix, is disclosed. The method includes: providing a controlled atmosphere around the affected area of the component; heating the component in the affected area within the controlled atmosphere to cause pyrolysis or depolymerization of the polymer matrix in the affected area and thereby to remove the polymer matrix from the affected area; introducing polymer resin into a space left by the pyrolyzed or depolymerized matrix to refill the affected area.
Abstract translation: 公开了一种修复纤维增强聚合物复合材料的部件的受影响区域的方法，特别是在聚合物基体中具有细长或连续的增强纤维。 该方法包括：在组件的受影响区域周围提供受控的气氛; 在受控气氛中加热受影响区域中的组分，使得受影响区域中的聚合物基质发生热解或解聚，从而从受影响的区域去除聚合物基质; 将聚合物树脂引入由热解或解聚的基质留下的空间中以再填充受影响的区域。
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公开(公告)号：US10661507B2
公开(公告)日：2020-05-26
申请号：US14879422
申请日：2015-10-09
Applicant: Airbus Operations GmbH
Inventor： Alexei Vichniakov , Mohamed-Mourad Sayeh , Tassilo Witte , Thomas Hoffmeister
Abstract: An assembly, configured in particular in the form of an aircraft assembly, comprises a plurality of individual components composed of a fibre-reinforced composite material. An edge section of at least one individual component is sealed by means of a sealing tape which contains reinforcing fibres and a curable plastics material.
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公开(公告)号：US10167583B2
公开(公告)日：2019-01-01
申请号：US14852926
申请日：2015-09-14
Applicant: Airbus Operations GmbH
Inventor： Tassilo Witte , Georg Lonsdorfer
IPC: D04H1/4242 , B32B15/14 , B29D24/00 , B29D99/00 , B32B37/12 , B32B5/02 , B32B5/22 , B32B5/26 , B32B3/12 , B32B7/12 , B32B37/14
Abstract: A honeycomb structure comprising carbon-fiber non-woven, sandwich structure comprising the honeycomb structure, and process for the production of the honeycomb structure.
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Patent Agency Ranking
公开(公告)号：US09856358B2
公开(公告)日：2018-01-02
申请号：US15381967
申请日：2016-12-16
Applicant: Airbus Operations GmbH
Inventor： Tassilo Witte
CPC classification number: C08J11/06 , B29B17/00 , B29B17/0026 , B29B17/0042 , B29B17/0412 , B29C43/02 , B29C47/0004 , B29C47/1027 , B29C47/1045 , B29C47/92 , B29C70/00 , B29C2947/92704 , B29C2947/92876 , B29K2101/10 , B29K2105/08 , B29K2105/0872 , B29K2105/246 , B29K2105/26 , B29K2707/04 , B29K2709/08 , C08J5/24 , C08J2300/30 , C08K3/22 , C08K7/06 , C08K7/14 , C08K2003/222 , C08K2003/2227 , Y02W30/62 , Y02W30/625
Abstract: A process for the recycling of wastes from webs or strands made of prepreg wastes comprising a first reactive resin, having the following steps: homogenization of prepreg wastes, dispersion of fillers and/or additives in a second reactive resin, mixing of the second resin, homogenized prepreg wastes and further processing of the mixture of resin, fillers and/or additives and prepreg wastes to produce molded workpieces.
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公开(公告)号：US20150151454A1
公开(公告)日：2015-06-04
申请号：US14551759
申请日：2014-11-24
Applicant: Airbus Operations GmbH
Inventor： Axel Herrmann , Jens Walla , Tassilo Witte
CPC classification number: B29B17/0042 , B29B7/002 , B29B7/38 , B29B17/0005 , B29C48/0011 , B29C48/277 , B29C48/287 , B29C48/30 , B29C55/00 , B29K2101/00 , B29K2105/0872 , B29K2105/12 , B29K2105/246 , B29K2105/26 , B29L2031/3076 , Y02P70/263 , Y02W30/62
Abstract: A method of recycling scraps or offcuts of uncured composite material, such as pre-impregnated or “prepreg” scraps or offcuts having reinforcing fibres and uncured polymer matrix material, includes introducing the scraps or offcuts into a mixing device directly; mixing the scraps or offcuts in the mixing device to blend uncured polymer matrix material and reinforcing fibres of the scraps or offcuts into a generally homogenous or consistent mixture; and feeding or conveying the mixture from the mixing device into a shaping mechanism to form a component or semi-finished product and preferably on a continuous basis.
Abstract translation: 一种再循环未固化复合材料的废料或切口的方法，例如具有增强纤维和未固化的聚合物基质材料的预浸渍或“预浸料”废料或切口，包括将废料或切口直接引入混合装置; 在混合装置中混合废料或切块，将未固化的聚合物基质材料和碎片或切片的增强纤维混合成一般均匀或一致的混合物; 以及将混合物从混合装置进料或输送到成形机构中，以形成组分或半成品，优选连续地进行。
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公开(公告)号：US11701839B2
公开(公告)日：2023-07-18
申请号：US16439167
申请日：2019-06-12
Applicant: Airbus Operations GmbH
Inventor： Tassilo Witte
IPC: B29C65/16 , B23K26/06 , B23K26/067 , B23K26/08 , B23K26/244 , B23K26/324 , B29C65/00 , B29C65/78 , B23K26/70 , B29L31/30 , B23K101/00 , B23K103/00 , B29K701/12
CPC classification number: B29C65/1645 , B23K26/0604 , B23K26/0643 , B23K26/0652 , B23K26/0676 , B23K26/08 , B23K26/244 , B23K26/324 , B23K26/702 , B29C65/7802 , B29C66/1122 , B23K2101/006 , B23K2103/42 , B29K2701/12 , B29L2031/3005
Abstract: A method for joining two components of a meltable material comprises the steps of providing a first component having a first border region and a second component having a second border region, placing the second component relative to the first component so as to form an overlap between the first border region and the second border region under a gap between the first border region and the second border region, continuously heating opposed sections of the first border region and the second border region at the same time through at least one energy source arranged in the gap at least partially, continuously providing a relative motion of the at least one energy source along the first border region and the second border region in the gap, and continuously pressing already heated sections of the first border region and the second border region onto each other.
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公开(公告)号：US10184035B2
公开(公告)日：2019-01-22
申请号：US14526051
申请日：2014-10-28
Applicant: AIRBUS Operations GmbH
Inventor： Hauke Seegel , Tassilo Witte
IPC: B05D3/12 , B32B37/24 , B32B38/00 , C08J5/24 , B29B15/12 , B29C70/06 , B29C70/32 , B29C70/50 , B29C70/54 , B64C1/00 , B64F5/00 , B29C70/44 , B29L31/00
Abstract: A system and method for producing a composite component, especially for continuous production of such composite components, includes a feeding device for feeding one or more layers of reinforcing material from a material supply along a process path, a resin application device for applying a resin matrix to the reinforcing material fed along the process path, and a forming device configured to shape or mould a profile of the reinforcing material and the resin matrix applied thereto to form a composite component as the reinforcing material is fed or conveyed along the process path.
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公开(公告)号：US09221212B2
公开(公告)日：2015-12-29
申请号：US14133018
申请日：2013-12-18
Applicant: Airbus Operations GmbH
Inventor： Jons Velten , Adam Andrae , Niels Deschauer , Tassilo Witte
CPC classification number: B29B11/16 , B29C53/04 , B29C70/085 , B29K2105/0881 , B29K2307/04 , Y10T156/1028 , Y10T156/1044
Abstract: A method of producing a composite preform having a profile with variable profile height or width is provided. The method includes: providing a plurality of first fiber layers overlapping or upon one another in or substantially parallel to a primary plane; inserting a second fiber layer via a guide member between two of the first fiber layers at an edge region of the preform profile, such that the second fiber layer extends substantially parallel to the first fiber layers; and positioning the edge region of the preform profile, and thus respective edge regions of the first fiber layers, out of the primary plane to set or determine a dimension of the preform profile in the primary plane.
Abstract translation: 提供了具有可变轮廓高度或宽度的轮廓的复合预制件的制造方法。 该方法包括：提供在主平面上或基本上平行于主平面彼此重叠或相互重叠的多个第一光纤层; 在所述预制件轮廓的边缘区域处经由引导构件在所述第一纤维层的两个之间插入第二纤维层，使得所述第二纤维层基本上平行于所述第一纤维层延伸; 并且将预成型件轮廓的边缘区域以及因此将第一纤维层的相应边缘区域定位在主平面之外，以设置或确定初级平面中的预成型件轮廓的尺寸。
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