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1. 发明授权

US5700743A Carbon fiber-reinforced composite material with a layer which provides protection against erosion 失效
标题翻译：碳纤维增强复合材料，具有防止侵蚀的层
公开(公告)号：US5700743A
公开(公告)日：1997-12-23
申请号：US814446
申请日：1997-03-10
申请人： Franz Puchinger , Axel Rossman , Siegfried Sikorski , Gerhard Wydra
发明人： Franz Puchinger , Axel Rossman , Siegfried Sikorski , Gerhard Wydra
IPC分类号： B29C70/08 , B32B18/00 , B32B33/00 , B64C11/20 , B64D45/02 , C04B41/52 , C04B41/89 , F01D5/28 , B32B5/16
CPC分类号： C04B41/009 , B29C70/088 , B32B18/00 , B32B33/00 , B64C11/205 , B64D45/02 , C04B41/52 , C04B41/89 , F01D5/288 , B29K2105/0023 , B29K2995/0005 , B29K2995/0087 , C04B2111/2038 , C04B2237/385 , Y02T50/67 , Y02T50/672 , Y10T428/266 , Y10T428/269 , Y10T442/3504 , Y10T442/3813 , Y10T442/3846 , Y10T442/699
摘要： A structural component which consists of a fiber-reinforced, composite material is provided with a protective coating against erosion. The protective coating includes an adhesion-promoting, intermediate layer on the component, an electrically insulating baked, inorganic lacquer layer for protection against erosion and an electrically conducting covering layer, for protection against lightning strikes. The covering layer consists of a baked and compressed inorganic lacquer and the lacquer of the lacquer layer and of the covering layer is baked on the component below the temperature which causes damage to the structural component or below the softening or decomposition temperature of the component. The protective layer is advantageously used for the external components of propulsion units, such as housings, nose cones or fan blades.
摘要翻译：由纤维增强的复合材料组成的结构部件具有防止侵蚀的保护层。保护涂层包括部件上的粘附促进中间层，用于防止侵蚀的电绝缘烘烤的无机漆层和用于防止雷击的导电覆盖层。覆盖层由烘烤和压缩的无机漆组成，漆层和覆盖层的漆在组件上烘烤，低于导致结构组分损坏或低于组分的软化或分解温度的温度。保护层有利地用于推进单元的外部部件，例如外壳，鼻锥或风扇叶片。

2. 发明授权

US4878821A Detachable anti-rupture ring for the housing of a turbo power plant 失效
标题翻译：用于涡轮发电厂房屋的可拆卸防爆环
公开(公告)号：US4878821A
公开(公告)日：1989-11-07
申请号：US154142
申请日：1988-02-09
申请人： Werner Huether , Axel Rossman , Siegfried Sikorski
发明人： Werner Huether , Axel Rossman , Siegfried Sikorski
IPC分类号： F01D11/22 , F01D21/04
CPC分类号： F01D11/22 , F01D21/045 , Y02T50/671 , Y10T24/45466
摘要： An anti-rupture ring is slit axially at least at one location and is provided thereat with clamping devices which permit a rapid tightening and loosening of the anti-rupture ring. In one embodiment, the clamping of the anti-rupture ring can be varied hydraulically so as to minimize clearance losses in operation. The invention can be used in all types of turbo engines endangered by breakage of rotor blades, particularly in aircraft gas turbine construction, and it permits simple, damage-free mounting and a well-defined clamping of the anti-rupture ring.
摘要翻译：至少在一个位置轴向地切断防爆环，并在其上设置夹紧装置，其允许抗破裂环的快速紧固和松动。在一个实施例中，抗断裂环的夹紧可以以液压方式变化，以便使操作中的间隙损失最小化。本发明可用于所有类型的涡轮发动机，通过转子叶片的破损，特别是在飞机燃气轮机的结构中受到威胁，并允许简单，无损伤的安装和明确的夹紧防爆环。

3. 发明授权

US4710346A Method for manufacturing powder material and shaped products utilizing the conditions in outer space 失效
标题翻译：利用外层空间条件制造粉末材料和成型制品的方法
公开(公告)号：US4710346A
公开(公告)日：1987-12-01
申请号：US689839
申请日：1985-01-09
申请人： Axel Rossman
发明人： Axel Rossman
IPC分类号： B22F9/00 , B22F9/08 , B22F9/12 , C03B19/10 , C04B35/565 , C04B35/584 , C04B35/626 , C23C14/22 , C23C16/44
CPC分类号： C23C16/4417 , B22F9/00 , B22F9/008 , B22F9/08 , B22F9/12 , C03B19/1005 , C03B19/1015 , C03B19/106 , C04B35/565 , C04B35/584 , C04B35/626 , C23C14/22 , B22F2999/00 , Y10S75/96
摘要： A method and apparatus for manufacturing powders comprising converting a solid starting material from the solid state to the gaseous or vapor phase, and forming powder particles by transferring the starting material in gaseous or vapor phase into a sealed reaction chamber with nucleation agents. The reaction chamber includes a wall of bellows construction to enable the chamber to expand and contract and a radiation reflecting coating is provided on at least a portion of the wall. The reaction chamber is subjected to one or more conditions of outer space. The powder particles can be supplied to a shaping stage in which the powder particles are compressed into compacts or formed into the final shape of a desired component.
摘要翻译：一种用于制造粉末的方法和装置，包括将固体原料从固态转化为气态或气相，并通过将气相或气相中的原料转移到具有成核剂的密封反应室中来形成粉末颗粒。反应室包括波纹管结构的壁，以使得室能够膨胀和收缩，并且在壁的至少一部分上设置辐射反射涂层。反应室受到外部空间的一个或多个条件的影响。粉末颗粒可以被供给到其中粉末颗粒被压缩成压块或形成所需组分的最终形状的成形阶段。

4. 发明授权

US4339229A Rotor wheel for axial-flow turbomachinery 失效
标题翻译：用于轴流涡轮机的转子轮
公开(公告)号：US4339229A
公开(公告)日：1982-07-13
申请号：US137873
申请日：1980-04-07
申请人： Axel Rossman
发明人： Axel Rossman
IPC分类号： F01D5/30 , F01D21/04
CPC分类号： F01D5/30 , F01D21/045 , F01D5/3053
摘要： A rotor wheel, particularly for compressors, including a rotor disc and a plurality of radially-projecting metal blades arranged along the periphery of the disc. A plurality of locating rings, formed predominantly of directionalized fibers, are provided, each locating ring being adjacent to all the blade roots and serving to resist centrifugal loads on the blades. An attachment ring formed predominantly of undirectionalized fibers surrounds the periphery of the rotor disc, and all the blade roots and locating rings are embedded in the attachment ring. The attachment ring serves to attach the blades to the rotor disc. Each blade root may have a T-shape and each locating ring engages over the cross bar of the T of each root. Alternatively, each blade root may have a hole accommodating a pin, and each locating ring engages over the pin of each blade root. Each blade root may have a plurality of sections, a single pin passing through holes in all of the sections of each root.
摘要翻译：特别是用于压缩机的转子轮，包括转子盘和沿盘的周边布置的多个径向突出的金属刀片。主要由方向化纤维形成的多个定位环被设置，每个定位环与所有叶片根部相邻并且用于抵抗叶片上的离心载荷。主要由不定向纤维形成的附接环围绕转子盘的周边，并且所有叶片根部和定位环嵌入附接环中。附接环用于将叶片附接到转子盘。每个叶片根部可以具有T形，并且每个定位环接合在每个根部的T的横杆上。或者，每个叶片根部可以具有容纳销的孔，并且每个定位环接合在每个叶片根部的销上。每个叶片根部可以具有多个部分，单个销通过每个根部的所有部分中的孔。

5. 发明授权

US4285634A Composite ceramic gas turbine blade 失效
标题翻译：复合陶瓷燃气轮机叶片
公开(公告)号：US4285634A
公开(公告)日：1981-08-25
申请号：US65062
申请日：1979-08-09
申请人： Axel Rossman , Wilhelm Hoffmuller , Wolfgang Kruger
发明人： Axel Rossman , Wilhelm Hoffmuller , Wolfgang Kruger
IPC分类号： F01D5/14 , F01D5/28 , F01D5/18
CPC分类号： F01D5/14 , F01D5/284
摘要： A gas turbine blade constituted of a supportive metallic blade core and a thin-walled ceramic blade airfoil, in which the airfoil is supported against a tip plate of the blade core. The blade core consists of rod or wire-shaped pins which have widened bases at their radially inner ends. Through these widened bases, the pins are retained in a metallic adapter slidable into a turbine disc.
摘要翻译：一种由支撑金属叶片芯和薄壁陶瓷叶片翼型构成的燃气轮机叶片，其中翼型件被支撑在叶片芯的顶板上。刀片芯由杆或线形销组成，在其径向内端具有加宽的基座。通过这些加宽的基座，销被保持在可滑动到涡轮盘中的金属适配器中。

6. 发明授权

US4271112A Process for the manufacture of rotationally-symmetrical components from short-fibered molding material 失效
标题翻译：用于从短纤维成型材料制造旋转对称组分的方法
公开(公告)号：US4271112A
公开(公告)日：1981-06-02
申请号：US50539
申请日：1979-06-21
申请人： Axel Rossman , Herbert Zech
发明人： Axel Rossman , Herbert Zech
IPC分类号： B29C70/14 , D04H1/74 , B29J1/02
CPC分类号： B29C70/14
摘要： Process for producing a high-strength, rotationally-symmetrical component by appending short fibers of glass, carbon or aramid in an organic solvent, and depositing the fiber material in a rotating sieve-like receptacle through a radially movable nozzle. The produced preform is impregnated with a matrix of resin and hardener and pressed into its final shape.
摘要翻译：通过在有机溶剂中附加玻璃，碳或芳族聚酰胺的短纤维，并通过可径向移动的喷嘴将纤维材料沉积在旋转的筛状容器中来生产高强度，旋转对称的组分的方法。生产的预成型件用树脂和硬化剂基体浸渍并压制成其最终形状。

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