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1. 发明授权

US5075166A Composite comprising a resin prepreg and a protective sheet containing ferromagnetic material and which is adhered to the resin prepreg by magnetic forces 失效
标题翻译：包含树脂预处理的复合材料和含有氟化物质的保护片，并通过磁力加入到树脂制品中
公开(公告)号：US5075166A
公开(公告)日：1991-12-24
申请号：US487741
申请日：1990-03-01
申请人： Siegfried Sikorski , Michael Schober , Reinhold Schoenacher
发明人： Siegfried Sikorski , Michael Schober , Reinhold Schoenacher
IPC分类号： B32B15/08 , B29C43/32 , B29C70/54 , B32B7/02 , B32B15/12 , B32B38/00 , C08J5/24 , H01F10/12
CPC分类号： C08J5/24 , B29C43/32 , B29C70/542 , B32B7/02 , Y10S425/033 , Y10S428/90 , Y10T428/249921 , Y10T428/26 , Y10T428/266 , Y10T428/28 , Y10T428/31504
摘要： A protective sheet for a resin pre-impregnated fiber board (prepreg) incorporates ferromagnetic material. This permits effective and safe manipulation of the fiber board during processing (trimming) and in the manufacture of fiber components.
摘要翻译：用于树脂预浸渍纤维板（预浸料）的保护片包含铁磁材料。这允许在处理（修整）和制造纤维部件期间有效且安全地操纵纤维板。

2. 发明授权

US06521331B1 Layer structure including metallic cover layer and fiber-reinforced composite substrate, and a method of making the same 失效
标题翻译：包括金属覆盖层和纤维增强复合基板的层结构及其制造方法
公开(公告)号：US06521331B1
公开(公告)日：2003-02-18
申请号：US09517346
申请日：2000-03-02
申请人： Siegfried Sikorski , Reinhold Schoenacher , Michael Schober
发明人： Siegfried Sikorski , Reinhold Schoenacher , Michael Schober
IPC分类号： D04H500
CPC分类号： B32B5/26 , B29C70/885 , B32B15/14 , B32B15/18 , B32B27/04 , B32B2260/021 , B32B2260/046 , B32B2262/103 , B32B2311/22 , B32B2311/30 , B32B2605/18 , Y02T50/43 , Y10T428/249923 , Y10T428/249924 , Y10T428/266
摘要： A composite laminate or layer structure includes a substrate (2) and a cover layer (4) bonded thereon. The substrate is made up of at least one layer (3) of fiber-reinforced synthetic material. The cover layer includes at least one layer (5) of metal fibers and/or threads (6), and a metal sheet (7) forming the outer surface skin (8) of the layer structure. The metal sheet is bonded by soldering or sintering onto the metal fibers and/or threads (6), while the layer of metal fibers and/or threads in turn is bonded to the underlying fiber-reinforced synthetic material (3) by being mutually and integrally permeated by a synthetic resin matrix and bonding material. Also, the metal fibers and/or threads (6) may be intermeshed with the fibers of the synthetic material (3). To provide improved bonding at both opposite sides thereof, the layer (5) of metal fibers and/or threads (6) has a lower porosity on the side adjoining the metal sheet, and a higher porosity on the side adjoining the fiber-reinforced synthetic material (3) of the substrate.
摘要翻译：复合层叠体或层结构体包括基材（2）和与其接合的覆盖层（4）。衬底由纤维增强合成材料的至少一层（3）组成。覆盖层包括金属纤维和/或丝线（6）的至少一层（5）和形成层结构的外表皮（8）的金属片（7）。金属片通过焊接或烧结粘合到金属纤维和/或螺纹（6）上，而金属纤维和/或螺纹层依次通过相互和相互接合在下面的纤维增强合成材料（3）上，并且由合成树脂基体和接合材料一体渗透。此外，金属纤维和/或线（6）可以与合成材料（3）的纤维相互啮合。为了在其相对两侧提供改进的粘合，金属纤维和/或螺纹（6）的层（5）在与金属片相邻的一侧具有较低的孔隙率，并且在与纤维增强合成物相邻的一侧上具有较高的孔隙率材料（3）。

3. 发明授权

US5951254A Blade for fluid flow engine having a metallic coating layer, and method of manufacturing and repairing the same 失效
标题翻译：具有金属涂层的流体流动发动机用叶片及其制造和修理方法
公开(公告)号：US5951254A
公开(公告)日：1999-09-14
申请号：US891853
申请日：1997-07-09
申请人： Siegfried Sikorski , Michael Schober , Reinhold Schoenacher
发明人： Siegfried Sikorski , Michael Schober , Reinhold Schoenacher
IPC分类号： F01D5/28 , B29C70/06 , B29C70/10 , B29C73/04 , B29K105/06 , B29L31/08 , B32B15/02 , F04D29/38
CPC分类号： B32B15/02
摘要： A blade for a fluid flow machine such as a jet turbine engine includes a blade body (2) that is to be exposed to the fluid flow and therefore is subject to damage by erosion due to abrasive particle entrained in the fluid flow and due to thermal loading. The blade body (2) is a layered body including base layers (6) of a fiber reinforced synthetic material and a metallic cover layer (7) applied as an erosion protective layer onto at least a portion or the entirety of the surface of the base layers (6). The cover layer (7) includes metallic fibers or threads (9A, 9B) which are bonded with the fiber reinforced synthetic material of the adjacent base layers (6) by the same synthetic resin binder material permeating through and forming a matrix for all the layers (6 and 7). The metallic fibers or threads (9A, 9B) embedded in a synthetic resin matrix are characterized by a high degree of erosion resistance and a good tolerance for defects in the case of local impact or erosion damage. The blade may be a blade of a fan or compressor stage of a jet turbine engine. A method for manufacturing and a method for repairing such blades involves exposing outer layers of fibers of a blade, and applying thereon a cover layer of metallic fibers or threads. An additional outer protective layer may be applied on the cover layer.
摘要翻译：用于诸如喷气涡轮发动机的流体流动机的叶片包括将被暴露于流体流动的叶片体（2），并且因此由于夹带在流体流中的磨料颗粒和由于热量而受到侵蚀而损坏加载。叶片体（2）是包括纤维增强合成材料的基层（6）和作为侵蚀保护层的金属覆盖层（7）的层叠体，其至少部分或全部的基底表面层（6）。覆盖层（7）包括金属纤维或线（9A，9B），其通过相同的合成树脂粘合剂材料与相邻基层（6）的纤维增强合成材料粘合，所述合成树脂粘合剂材料渗透并形成所有层的基质（6和7）。嵌入合成树脂基体中的金属纤维或线（9A，9B）的特征在于在局部冲击或侵蚀损伤的情况下具有高抗侵蚀性和良好的缺陷耐受性。叶片可以是喷气涡轮发动机的风扇或压缩机级的叶片。制造方法和修复这种刀片的方法包括暴露刀片的纤维外层，并在其上涂敷金属纤维或线的覆盖层。可以在覆盖层上施加另外的外部保护层。

4. 发明授权

US5429477A Vibration damper for rotor housings 失效
标题翻译：转子外壳的减振器
公开(公告)号：US5429477A
公开(公告)日：1995-07-04
申请号：US295265
申请日：1994-08-24
申请人： Siegfried Sikorski , Reinhold Schoenacher , Michael Schober , Wolfgang Diepolder
发明人： Siegfried Sikorski , Reinhold Schoenacher , Michael Schober , Wolfgang Diepolder
IPC分类号： F01D21/04 , F01D25/04 , F04D29/66
CPC分类号： F01D25/04 , F01D21/045 , Y02T50/672
摘要： A vibration damper for rotor housings includes a rubber-elastic damping band (6) that encircles the outer circumference of the rotor housing (4) in a contour fitting manner. A clamping band (7) encircles the damping band (6) and secures the damping band to the housing (4). The clamping band is made of a material having a different modulus of elasticity than the material of the rotor housing, which achieves a detuning of the vibrational system including the rotor housing and the vibration damper as components. Such a detuning reduces the vibrational tendency of the rotor housing. Frictional rubbing between the damping band and the housing surface, and between the damping band and the clamping band effectively damps or dissipates the energy of any vibration that does occur. The clamping band includes a tension adjustment element that is adjustable and releasable so that the clamping band and the entire vibration damper may easily be removed from the housing for carrying out maintenance and inspection procedures.
摘要翻译：用于转子壳体的减震器包括以轮廓拟合方式围绕转子壳体（4）的外圆周的橡胶弹性阻尼带（6）。夹紧带（7）围绕阻尼带（6）并将阻尼带固定到壳体（4）上。夹紧带由具有与转子壳体的材料不同的弹性模量的材料制成，其实现包括转子壳体和振动阻尼器作为部件的振动系统的失谐。这种失谐降低了转子壳体的振动趋势。在阻尼带和壳体表面之间以及阻尼带和夹紧带之间的摩擦摩擦可有效地抑制或消散确实发生的任何振动的能量。夹紧带包括可调节和可释放的张力调节元件，使得夹紧带和整个减震器可以容易地从壳体移除以进行维护和检查程序。

5. 发明申请

US20070248780A1 FIBROUS LAMINATE AND METHOD FOR THE PRODUCTION THEREOF 审中-公开
标题翻译：纤维层压板及其生产方法
公开(公告)号：US20070248780A1
公开(公告)日：2007-10-25
申请号：US10566317
申请日：2004-07-22
申请人： Michael Schober , Reinhold Schoenacher , Siegfried Sikorski
发明人： Michael Schober , Reinhold Schoenacher , Siegfried Sikorski
IPC分类号： B29C70/54
CPC分类号： B29C70/543 , B29B11/16 , B29C70/24 , B29C70/48 , Y10T428/19
摘要： A fiber laminate is provided, as well as a method for producing the fiber laminate and a method for making a component from the fiber laminate. The fiber laminate includes several fiber layers having reinforcement fibers extending in a preferential direction, and/or several multiaxial nonwoven fabrics consisting of reinforcement fibers, of various contours, wherein the fiber layers are fixed one under the other and/or placed in the multiaxial nonwoven one on top of the other along at least one area before contouring.
摘要翻译：提供纤维层压材料，以及纤维层压体的制造方法以及从纤维层压体制造成分的方法。纤维层压板包括几根纤维层，其中纤维层具有沿优先方向延伸的增强纤维，和/或由多种不同轮廓的增强纤维组成的多根多轴无纺织物，其中纤维层一个固定在另一个上，和/或放置在多轴非织造布中一个在另一个之上沿至少一个区域在轮廓之前。

6. 发明授权

US5380152A Adjustable guide vane for turbines, compressors, or the like 失效
标题翻译：用于涡轮机，压缩机等的可调导向叶片
公开(公告)号：US5380152A
公开(公告)日：1995-01-10
申请号：US144575
申请日：1993-10-28
申请人： Siegfried Sikorski , Michael Schober , Reinhold Schoenacher
发明人： Siegfried Sikorski , Michael Schober , Reinhold Schoenacher
IPC分类号： B29D99/00 , F01D5/28 , F01D9/02
CPC分类号： F01D17/162 , B29D99/0025 , F01D5/282 , Y02T50/672 , Y02T50/673
摘要： A guide vane for an axial guide baffle of an axial flow engine, such as a jet engine, is adjustable in its position about a guide vane adjustment axis extending radially to a rotational engine axis. The guide vane has a vane body and an adjustment lever extending at an angle of about 90.degree. away from the adjustment axis. The vane body, the adjustment lever, and at least one bearing journal form an integral one piece construction either of molded fiber composite material or of forged, e.g. drop forged, metal.
摘要翻译：用于诸如喷气发动机的轴流引擎的轴向引导挡板的引导叶片可围绕径向延伸到旋转发动机轴线的导向叶片调节轴线的位置进行调节。导向叶片具有叶片体和调节杆，该调节杆与调节轴线成大约90°的角度延伸。叶片主体，调节杆和至少一个轴承轴颈形成模制的纤维复合材料或锻造的一体的一体构造。下降锻造，金属。

7. 发明授权

US06221795B1 Composite material and process for manufacturing same 失效
标题翻译：复合材料及其制造方法相同
公开(公告)号：US06221795B1
公开(公告)日：2001-04-24
申请号：US08954199
申请日：1997-10-20
申请人： Siegfried Sikorski , Michael Schober , Reinhold Schönacher
发明人： Siegfried Sikorski , Michael Schober , Reinhold Schönacher
IPC分类号： B32B1502
CPC分类号： B32B5/26 , B29C70/025 , B29C70/64 , B32B5/024 , B32B5/22 , B32B2260/021 , B32B2262/103 , Y10T442/112 , Y10T442/131 , Y10T442/3382 , Y10T442/339 , Y10T442/3463 , Y10T442/655 , Y10T442/658
摘要： The invention relates to a composite material having a substrate, which contains at least one fiber layer, and a cover layer, which adjoins the substrate and which, at least adjacent to the at least one fiber layer, contains metallic fibers and/or threads. The at least one fiber layer of the substrate and the metallic fibers and/or threads of the cover layer being saturated with binder and, as a result, the substrate and the cover layer are formed together or connected. Metallic, ceramic or glass-type particles are embedded in the cover layer in the area of the metallic fibers and/or threads. Preferably, the particles may be one or more or a combination of TiC, TiN, TiAl, Fe, steel, Ni, Si, metal alloys, diamond, or glass. In addition, the invention provides a process for manufacturing a composite material and articles of manufacture comprising the composite material, especially for rotor blades or propellers. The composite material and products comprising it display improved abrasion and erosion resistance and are protected from electrical damages.
摘要翻译：本发明涉及一种复合材料，其具有包含至少一个纤维层的基底和覆盖层，所述覆盖层邻接所述基底，并且至少邻近所述至少一个纤维层包含金属纤维和/或线。衬底的至少一个纤维层和覆盖层的金属纤维和/或螺纹被粘合剂饱和，结果，基底和覆盖层形成在一起或连接。金属，陶瓷或玻璃型颗粒被嵌入在金属纤维和/或螺纹区域的覆盖层中。优选地，颗粒可以是TiC，TiN，TiAl，Fe，钢，Ni，Si，金属合金，金刚石或玻璃中的一种或多种或组合。此外，本发明提供了一种制造复合材料和制品的方法，其包括复合材料，特别是用于转子叶片或螺旋桨。包含它的复合材料和产品显示出改进的耐磨损和抗腐蚀性，并且防止电损坏。

8. 发明申请

US20100074740A1 VANE RING, AND METHOD FOR THE PRODUCTION THEREOF 审中-公开
标题翻译：帆板及其制造方法
公开(公告)号：US20100074740A1
公开(公告)日：2010-03-25
申请号：US12517252
申请日：2007-12-01
申请人： Siegfried Sikorski , Max Kraus , Karl Hoffmann , Alois Niedersüss
发明人： Siegfried Sikorski , Max Kraus , Karl Hoffmann , Alois Niedersüss
IPC分类号： F01D9/04 , B23P11/00
CPC分类号： F01D5/28 , F01D9/044 , F05D2230/22 , F05D2230/238 , F05D2230/25 , F05D2300/50212 , Y10T29/49323
摘要： The invention relates to a vane ring of a turbo engine, particularly a gas turbine, comprising a vane support ring and several guide vanes that are mounted on the vane support ring. According to the invention, the vane support ring and the guide vanes are made of different materials, the materials of which the guide vanes are made being of a higher quality than the material of which the vane support ring is made.
摘要翻译：本发明涉及涡轮发动机，特别是燃气轮机的叶环，其包括叶片支撑环和安装在叶片支撑环上的几个导向叶片。根据本发明，叶片支撑环和导向叶片由不同的材料制成，其导叶的材料制造质量高于制造叶片支撑环的材料。

9. 发明授权

US4884948A Deflectable blade assembly for a prop-jet engine and associated method 失效
标题翻译：用于喷气式发动机的可偏转叶片组件及相关方法
公开(公告)号：US4884948A
公开(公告)日：1989-12-05
申请号：US174781
申请日：1988-03-29
申请人： Siegfried Sikorski
发明人： Siegfried Sikorski
IPC分类号： B64C11/20 , B64C11/26 , F01D5/28 , F04D29/36 , F04D29/38
CPC分类号： B64C11/26 , F01D5/282 , F04D29/362 , F04D29/382 , Y02T50/66 , Y02T50/672 , Y02T50/673
摘要： A propeller for a prop-jet engine having a propellor blade formed as a hollow shell member whose outer surface has an aerodynamic blade profile, the propellor blade being secured to a rotor via an adjustment pin. The hollow shell member is internally braced partly along its radial length by a flexible spar secured to the pin and made of thermoplastic material. The flexible spar is hollow and receives a metal spar hich is fixed to the pin and is given flexibility in bending by the provision of a slot therein.
摘要翻译：用于具有形成为外表面具有空气动力学叶片轮廓的中空壳构件的推进器叶片的推进式发动机的螺旋桨，所述推进器叶片经由调节销固定到转子。中空的外壳构件通过固定到销上并由热塑性材料制成的柔性翼梁沿其径向长度部分地内部支撑。柔性翼梁是中空的并且接收固定到销的金属翼梁，并且通过在其中设置狭槽而赋予弯曲挠性。

10. 发明授权

US09952236B2 Method and device for process monitoring 有权
公开(公告)号：US09952236B2
公开(公告)日：2018-04-24
申请号：US13981186
申请日：2012-01-11
申请人： Wilhelm Satzger , Siegfried Sikorski , Karl-Heinz Dusel , Wilhelm Meir , Bertram Kopperger , Josef Waermann , Andreas Jakimov , Manuel Hertter , Hans-Christian Melzer , Thomas Hess
发明人： Wilhelm Satzger , Siegfried Sikorski , Karl-Heinz Dusel , Wilhelm Meir , Bertram Kopperger , Josef Waermann , Andreas Jakimov , Manuel Hertter , Hans-Christian Melzer , Thomas Hess
IPC分类号： G01N35/00 , B22F3/105 , B29C67/00 , B33Y40/00 , G01N25/72
CPC分类号： G01N35/00 , B22F3/105 , B22F3/1055 , B22F2003/1056 , B22F2003/1057 , B29C64/153 , B29C64/20 , B29C64/386 , B33Y10/00 , B33Y30/00 , B33Y40/00 , B33Y50/02 , G01N25/72 , Y02P10/295
摘要： Disclosed is a method for monitoring a generative fabrication process in which a component is formed in an installation space from a multiplicity of layers by using a three-dimensional data model and a following layer is fixed to a preceding layer by means of a high-energy beam. The method comprises detecting the component at least optically and detecting the installation space thermally during layer application. Also disclosed is a device for carrying out the method.

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