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公开(公告)号：US20050136256A1
公开(公告)日：2005-06-23
申请号：US11018583
申请日：2004-12-20
申请人： Alexei Vichniakov
发明人： Alexei Vichniakov
CPC分类号： C22C47/20 , C22C47/068 , C22C49/14 , Y10T428/12035 , Y10T428/12076 , Y10T428/12486 , Y10T428/12535 , Y10T428/249924 , Y10T428/2933
摘要： A fiber composite material which is particularly suitable for aircraft construction, includes anorganic mineral fibers embedded or enclosed in a metal matrix. The mineral fibers include a substantial or dominant proportion of SiO2, and/or Al2O3 and/or Fe2O3, the remainder being rock material. The fibers have a length of at least 10 mm and are oriented in parallel to one another in at least one direction. The metal matrix is made of aluminum or aluminum alloys, or of magnesium or magnesium alloys or of titanium or of titanium alloys. These matrix metal alloys contain a substantial or dominant proportion of the respective metal. The fibers are preferably coated with particles of the matrix metal and bonded to one another to form fiber films or fiber sheets which are then laminated between sheets of matrix metal.
摘要翻译： 特别适用于飞行器构造的纤维复合材料包括嵌入或封闭在金属基体中的无机矿物纤维。 矿物纤维包括大部分或占优势的SiO 2和/或Al 2 O 3 3和/或Fe 2 O 3， 其余为岩石材料。 纤维具有至少10mm的长度并且在至少一个方向上彼此平行取向。 金属基体由铝或铝合金或镁或镁合金或钛或钛合金制成。 这些基体金属合金含有相当或主要的相应金属比例。 纤维优选地涂覆有基质金属的颗粒并彼此粘合以形成纤维膜或纤维片，然后层压在基质金属片之间。
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2.发明申请Method for Connection At Least Two Pieces of Sheet Material, Particularly At Least Two Metal Sheets for a Lightweight Structure As Well a Joining and Lightweight Structure 有权用于连接至少两片片材的方法，特别是用于轻型结构的至少两个金属板以及连接和轻量结构公开(公告)号：US20090263676A1
公开(公告)日：2009-10-22
申请号：US11989188
申请日：2006-07-20
CPC分类号： B64C1/12 , B23K1/16 , B23K9/025 , B23K20/122 , B23K26/26 , B23K2101/18 , B64C2001/0081 , Y10T428/12493 , Y10T428/12569 , Y10T428/192
摘要： A method for connecting at least two sheet-like formations, in particular at least two metal sheets with a thin material thickness for aircraft, comprises establishing butt-joint connections between the sheet-like formations by forming a joining region; mechanical processing of the sheet-like formations and/or of the joining region; mechanical and/or chemical adhesive pre-treatment of the sheet-like formations and/or of the joining region; and pasting-on at least one reinforcement element in the region of the top and/or the bottom of the joining region, wherein for the purpose of forming a second load path the width of the at least one reinforcement element is wider than the width 16 of the joining region.A connection is provided and made according to the method. A lightweight structure is also provided that comprises at least one connection according to the invention.
摘要翻译： 用于连接至少两个片状结构，特别是至少两个用于飞行器的薄材料厚度的金属片的方法包括通过形成接合区域来在片状结构之间建立对接连接; 片状结构和/或接合区域的机械加工; 机械和/或化学粘合剂预处理片状结构和/或接合区域; 并且在所述接合区域的顶部和/或底部的区域中粘贴至少一个加强元件，其中为了形成第二负载路径，所述至少一个加强元件的宽度比宽度16宽 的加盟区域。 根据该方法提供和制造连接。 还提供了包括根据本发明的至少一个连接的轻质结构。
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3.发明申请Structural element, method for manufacturing a structural element and use of a structural element for an aircraft hull 有权结构元件，制造结构元件的方法和飞机机身的结构元件的使用公开(公告)号：US20060156662A1
公开(公告)日：2006-07-20
申请号：US11290042
申请日：2005-11-29
申请人： Alexei Vichniakov
发明人： Alexei Vichniakov
IPC分类号： E04C1/00
CPC分类号： B64C1/06 , B64C1/12 , B64C2001/0081 , Y02T50/42 , Y10T428/24174
摘要： A structural element includes the following elements: a carrier element, a reinforcing element, and a sheathing element. At least a portion of the reinforcing element is enveloped by the sheathing element and the reinforcing element is embedded in the carrier element. Materials of the elements are selected to inhibit crack initiation or propagation in the elements and/or from one element to another. An intermediate layer of a different material may be added between elements to further inhibit crack initiation and propagation and to inhibit corrosion, such as galvanic corrosion.
摘要翻译： 结构元件包括以下元件：载体元件，加强元件和护套元件。 增强元件的至少一部分被护套元件包围，并且加强元件嵌入载体元件中。 选择元件的材料以抑制元件和/或从一个元件到另一个元件的裂纹开始或传播。 可以在元件之间添加不同材料的中间层，以进一步抑制裂纹的产生和扩展，并抑制诸如电偶腐蚀的腐蚀。
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公开(公告)号：US20050156095A1
公开(公告)日：2005-07-21
申请号：US11018588
申请日：2004-12-20
申请人： Alexei Vichniakov , Herwig Assler
发明人： Alexei Vichniakov , Herwig Assler
CPC分类号： B23K20/16 , B23K20/00 , B23K20/2333 , B60N2/01558 , B60P7/0815 , B64D11/0696 , Y02T50/46
摘要： A seat mounting rail suitable for mounting passenger seats to a floor, for example an aircraft cabin floor, is divided into an upper section for securing a seat and a lower section for mounting the rail to the floor. The upper section is preferably made of a titanium alloy. The lower section is preferably made of an aluminum alloy. Both sections are connected to each other by an interconnection preferably in the form of a metallurgical bond formed under heat and pressure. A bonding metal foil compatible with the metals of which the rail sections are made is used for enhancing the bonding strength of the interconnection.
摘要翻译： 适合于将乘客座椅安装到地板（例如飞机机舱地板）上的座椅安装轨道被分成用于固定座椅的上部和用于将轨道安装到地板的下部。 上部优选由钛合金制成。 下部优选由铝合金制成。 两个部分通过互连优选地以热和压力形成的冶金结合的形式彼此连接。 使用与制造轨道部分的金属相容的接合金属箔来增强互连的接合强度。
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公开(公告)号：US09347221B2
公开(公告)日：2016-05-24
申请号：US13345182
申请日：2012-01-06
申请人： Alexei Vichniakov
发明人： Alexei Vichniakov
CPC分类号： B64C1/12 , B64C1/064 , B64C2001/0072 , E04C2/08 , E04C2/20 , E04C2/28 , E04C2/38 , Y02T50/43 , Y10T428/24174
摘要： A lightweight structural panel which comprises a planarly extended outer skin having a thickness and stiffening elements which are connected to the outer skin and arranged at a distance from one another. The outer skin is formed by component layers which are each extended in the planar direction of the lightweight structural panel and complement one another to form the thickness of the outer skin and are interconnected, the stiffening elements being formed in one piece with one of the component layers.
摘要翻译： 一种轻质结构面板，其包括具有厚度和加强元件的平面延伸外皮，其连接到外皮并且彼此间隔一定距离设置。 外皮是由轻质结构板的平面方向延伸的构件层构成，并且互相补充以形成外皮的厚度，并且互连，加强件与该部件中的一个形成为一体 层。
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公开(公告)号：US08096092B2
公开(公告)日：2012-01-17
申请号：US11810549
申请日：2007-06-06
申请人： Alexei Vichniakov
发明人： Alexei Vichniakov
CPC分类号： B64C1/12 , B64C1/064 , B64C2001/0072 , E04C2/08 , E04C2/20 , E04C2/28 , E04C2/38 , Y02T50/43 , Y10T428/24174
摘要： What is described is a lightweight structural panel which comprises a planarly extended outer skin of given thickness and stiffening elements which are connected to this outer skin and are arranged at a given distance from one another. According to the invention, the outer skin is formed by component layers which are each extended in the planar direction of the lightweight structural panel and complement one another in the direction of thickness to form the thickness of the outer skin and are interconnected, the stiffening elements being formed in one piece with one of the component layers.
摘要翻译： 所描述的是轻质结构面板，其包括具有给定厚度的平面延伸的外皮和加强元件，其连接到该外皮并且彼此以给定的距离布置。 根据本发明，外皮由各层在轻质结构面板的平面方向上延伸并且在厚度方向互相补充而形成，以形成外皮的厚度并互连，加强件 与其中一个部件层形成一体。
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7.发明授权Metallic layer material, reinforced with basalt fibers, as well as products made thereof 失效用玄武岩纤维增强的金属层材料，以及由其制成的产品公开(公告)号：US07255916B2
公开(公告)日：2007-08-14
申请号：US11029047
申请日：2005-01-04
CPC分类号： B29C70/885 , B32B15/08 , B32B15/20 , B32B27/18 , B32B2250/40 , B32B2262/108 , B32B2274/00 , B32B2307/51 , B32B2307/714 , B32B2605/18 , Y02T50/43 , Y10T428/249924 , Y10T428/249951 , Y10T428/249952
摘要： A metallic layer material includes at least two metal sheets. Each sheet has a thickness of less than 1.5 mm. Between the sheets, a plastic layer is disposed, which is bonded to the metal sheets. The plastic layer comprises a plastic material and basalt fibers, and the basalt fibers have a modulus of elasticity exceeding 50 GPa. The basalt fibers may constitute 35-75% of the volume of the plastic layer. and may be comprised of 35-55 weight % of SiO2, 10-25 weight % of Al2O3, and 3-10 weight % of MgO. In aerospace applications and other applications requiring good specific strength, stiffness and damage tolerance, the metal sheets may be made of a metal having a tensile strength exceeding 0.20 GPa.
摘要翻译： 金属层材料包括至少两个金属片。 每张薄片的厚度小于1.5毫米。 在片材之间，设置塑料层，其粘合到金属片材上。 塑料层包括塑料材料和玄武岩纤维，玄武岩纤维的弹性模量超过50GPa。 玄武岩纤维可以占塑料层体积的35-75％。 并且可以包含35-55重量％的SiO 2，10-25重量％的Al 2 O 3 3和3-10 MgO的重量％。 在航空航天应用和其它需要较高比强度，刚度和损伤公差的应用中，金属片可以由拉伸强度超过0.20GPa的金属制成。
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8.发明申请Lightweight structure especially for an aircraft and method for making such a structure 有权轻型结构，特别适用于飞机和制造这种结构的方法公开(公告)号：US20050112347A1
公开(公告)日：2005-05-26
申请号：US10888565
申请日：2004-07-08
CPC分类号： B32B15/08 , B32B3/14 , B32B7/12 , B32B15/02 , B32B15/20 , B32B2260/021 , B32B2262/0269 , B32B2262/10 , B32B2262/101 , B32B2262/106 , B32B2305/08 , B32B2311/18 , Y10T428/249924
摘要： An additional fiber reinforced layer reduces crack propagation in a lightweight structure of an outer skin adhesively bonded to a reinforcing frame. For this purpose the additional fiber reinforced layer is interposed between the outer skin and the frame and adhesively bonded to the outer skin and to the frame. The additional layer has reinforcing fibers extending in parallel to each other or the reinforcing fibers are woven into a fabric embedded in a synthetic adhesive bonding material. The embedding of the parallel fibers or of the fiber fabric in the bonding material is performed either prior to the bonding or during the bonding of the additional layer to the outer skin and to the reinforcing frame.
摘要翻译： 附加的纤维增强层减少了粘附到加强框架的外皮的轻质结构中的裂纹扩展。 为此，另外的纤维增强层介于外皮和框架之间，并且粘合到外皮和框架上。 附加层具有彼此平行延伸的增强纤维或将增强纤维编织成嵌入合成粘合剂粘合材料中的织物。 平行纤维或纤维织物在接合材料中的嵌入是在粘合之前或在附加层与外皮和加强框之间的粘合期间进行的。
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公开(公告)号：US20120102869A1
公开(公告)日：2012-05-03
申请号：US13345182
申请日：2012-01-06
申请人： Alexei Vichniakov
发明人： Alexei Vichniakov
CPC分类号： B64C1/12 , B64C1/064 , B64C2001/0072 , E04C2/08 , E04C2/20 , E04C2/28 , E04C2/38 , Y02T50/43 , Y10T428/24174
摘要： What is described is a lightweight structural panel which comprises a planarly extended outer skin of given thickness and stiffening elements which are connected to this outer skin and are arranged at a given distance from one another. According to the invention, the outer skin is formed by component layers which are each extended in the planar direction of the lightweight structural panel and complement one another in the direction of thickness to form the thickness of the outer skin and are interconnected, the stiffening elements being formed in one piece with one of the component layers.
摘要翻译： 所描述的是轻质结构面板，其包括具有给定厚度的平面延伸的外皮和加强元件，其连接到该外皮并且彼此以给定的距离布置。 根据本发明，外皮由各层在轻质结构面板的平面方向上延伸并且在厚度方向互相补充而形成，以形成外皮的厚度并互连，加强件 与其中一个部件层形成一体。
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10.发明授权Structural element, method for manufacturing a structural element and use of a structural element for an aircraft hull 有权结构元件，制造结构元件的方法和飞机机身的结构元件的使用公开(公告)号：US07850118B2
公开(公告)日：2010-12-14
申请号：US11290042
申请日：2005-11-29
申请人： Alexei Vichniakov
发明人： Alexei Vichniakov
IPC分类号： B64C1/00
CPC分类号： B64C1/06 , B64C1/12 , B64C2001/0081 , Y02T50/42 , Y10T428/24174
摘要： A structural element includes the following elements: a carrier element, a reinforcing element, and a sheathing element. At least a portion of the reinforcing element is enveloped by the sheathing element and the reinforcing element is embedded in the carrier element. Materials of the elements are selected to inhibit crack initiation or propagation in the elements and/or from one element to another. An intermediate layer of a different material may be added between elements to further inhibit crack initiation and propagation and to inhibit corrosion, such as galvanic corrosion.
摘要翻译： 结构元件包括以下元件：载体元件，加强元件和护套元件。 增强元件的至少一部分被护套元件包围，并且加强元件嵌入载体元件中。 选择元件的材料以抑制元件和/或从一个元件到另一个元件的裂纹开始或传播。 可以在元件之间添加不同材料的中间层，以进一步抑制裂纹的产生和扩展，并抑制诸如电偶腐蚀的腐蚀。
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