公开(公告)号：US20090265933A1

公开(公告)日：2009-10-29

申请号：US12385918

申请日：2009-04-23

申请人： Karl Schreiber

发明人： Karl Schreiber

IPC分类号： B23P15/04

CPC分类号： B23K20/12 ,  B23K20/121 ,  B23K20/129 ,  B23K2101/001 ,  F01D5/063 ,  F05B2230/239 ,  Y10T29/49321

摘要： With the manufacture of turbine engine rotor drums, the opposite joining surfaces of rotor disks are brought into contact and at least one of the two rotor disks clamped into a fixture is set in a circular movement until the joining areas reach a pasty state due to the frictional heat. The circular movement of the rotor disks, in which the axis of the rotor disk moves along a circular path, is optically recorded and deviations due to imbalance are corrected by weight compensation at the fixture. Upon reaching the pasty material state the joining areas weld together, with the rotor disks being at rest and in axial alignment. Manufacture is cost-effective and guarantees precise axial alignment of the rotor disks and a long service life of the engine rotor drums.

摘要翻译： 随着涡轮发动机转子鼓的制造，转子盘的相对的接合表面接触，并且夹紧在夹具中的两个转子盘中的至少一个被设置成圆形运动，直到接合区域由于 摩擦热。 旋转盘的轴线沿着圆形路径移动的转子盘的圆周运动被光学记录，并且由于不平衡引起的偏差通过固定装置处的重量补偿来校正。 在达到糊状材料状态时，接合区域焊接在一起，转子盘处于静止并且轴向对准。 制造成本效益高，确保转子盘的精确轴向对准和发动机转子鼓的使用寿命长。

公开(公告)号：US20090087309A1

公开(公告)日：2009-04-02

申请号：US11979547

申请日：2007-11-05

申请人： Karl Schreiber

发明人： Karl Schreiber

IPC分类号： F01D21/00 ,  F01D25/24 ,  F02C7/00

CPC分类号： F01D21/045 ,  F05D2250/283 ,  F05D2300/2102 ,  F05D2300/2112 ,  F05D2300/224 ,  F05D2300/2261 ,  F05D2300/431 ,  F05D2300/603 ,  Y02T50/672

摘要： A protective ring (7) for a fan casing (2) of a gas-turbine engine equipped with a fan having especially metallic fan blades (3) includes a one-piece fiber-composite ring (8) with a ceramic cover (9) arranged on the ring inner surface facing the fan blades, and preferably formed by individual panels embedded in a ductile material, this cover (9)—upon the impingement of broken-off blade fragments—forms a crack network corresponding to an arrangement of the sintered starting ceramic particles and subsequently disintegrates into small particles, thereby absorbing a great part of the kinetic energy caused by the impinging blade fragment. Consequential damage to the protective ring is thereby minimized.

摘要翻译： 一种用于具有特别是金属风扇叶片（3）的风扇的燃气涡轮发动机的风扇壳体（2）的保护环（7）包括具有陶瓷盖（9）的单件式纤维复合环（8） 布置在面向风扇叶片的环内表面上，并且优选地由嵌入在延性材料中的单独面板形成，该覆盖物（9） - 破碎叶片碎片的冲击形成对应于烧结 起始陶瓷颗粒，然后分解成小颗粒，从而吸收由撞击的片段引起的大部分动能。 因此，对保护环的相应损害最小化。

公开(公告)号：US07204089B2

公开(公告)日：2007-04-17

申请号：US10933403

申请日：2004-09-03

申请人： Karl Schreiber

发明人： Karl Schreiber

IPC分类号： F02C1/00 ,  F02G3/00

CPC分类号： F23R3/08 ,  F23D2214/00 ,  Y02T50/675

摘要： An inexpensively manufacturable arrangement for the cooling of thermally highly loaded components, for example the combustion chamber of a gas turbine, comprises cavities (4) provided on the thermally loaded inner surface/air exit side (3) of the wall (1) of the component which are supplied with a cooling medium from the outer surface/air inlet side (5) via cooling air openings (6) and which are covered by a heat resistant wire mesh (7) of a certain permeability. The cavity, which acts as pressure accumulator, forms, in connection with the wire mesh, a uniform pressurized-air film (8) for the cooling and heat shielding of the wall surface.

摘要翻译： 用于冷却热负荷高的部件（例如燃气轮机的燃烧室）的廉价制造的装置包括设置在所述壁（1）的热负载内表面/空气出口侧（3）上的空腔（4） 该部件经由冷却空气开口（6）从外表面/空气入口侧（5）供应冷却介质，并被一定渗透率的耐热丝网（7）覆盖。 充当压力蓄能器的空腔与丝网结合形成用于壁表面的冷却和热屏蔽的均匀的加压空气薄膜（8）。

公开(公告)号：US06997995B2

公开(公告)日：2006-02-14

申请号：US10415316

申请日：2001-11-16

申请人： Peter Janschek ,  Lothar Knippschild ,  Karl Schreiber ,  Dan Roth-Fagaraseanu

发明人： Peter Janschek ,  Lothar Knippschild ,  Karl Schreiber ,  Dan Roth-Fagaraseanu

IPC分类号： C22C14/00 ,  C22F1/18

CPC分类号： C22F1/183

摘要： The invention relates to a method for producing components with a high load capacity from α+γ TiAl alloys, especially for producing components for aircraft engines or stationary gas turbines. According to this method, enclosed TiAl blanks of globular structure are preformed by isothermal primary forming in the α+γ− or α phase area. The preforms are then shaped out into components with a predeterminable contour by means of at least one isothermal secondary forming process, with dynamic recrystallization in the α+γ− or α phase area. The microstructure is adjusted by solution annealing the components in the α phase area and then cooling them off rapidly.

摘要翻译： 本发明涉及一种从α+γTiAl合金制造具有高负载能力的部件的方法，特别是用于生产用于飞机发动机或固定式燃气轮机的部件。 根据这种方法，球形结构的封闭TiAl空白通过在α+γ或α相区域中的等温初始形成来形成。 然后通过至少一个等温次生形成过程将预制件成形为具有可预定轮廓的部件，在α+γ或α相区域中具有动态重结晶。 通过对α相区域中的组分进行固溶退火，然后快速冷却来调节微观结构。

公开(公告)号：US06532658B2

公开(公告)日：2003-03-18

申请号：US09731984

申请日：2000-12-08

申请人： Karl Schreiber

发明人： Karl Schreiber

IPC分类号： B23P1500

CPC分类号： B23P15/04 ,  F01D5/147 ,  F05C2201/0466 ,  F05D2230/20 ,  F05D2300/132 ,  F05D2300/133 ,  F05D2300/171 ,  F05D2300/172 ,  F05D2300/436 ,  F05D2300/603 ,  F05D2300/614 ,  Y10T29/49336 ,  Y10T29/49337 ,  Y10T29/49339 ,  Y10T29/49805

摘要： In a process for the manufacture of a blade/vane of a turbomachine, the blade/vane is made of a metallic enveloping structure and a supporting structure made of composite material provided inside of the enveloping structure and suitably joined to the enveloping structure. A metal-felt weave is welded or soldered/brazed to the sheet making up the enveloping structure, whereupon this sheet-weave-assembly is shaped by hydroforming or an internal high-pressure forming process to provide the enveloping structure of the blade/vane. Finally, the composite material making up the supporting structure is introduced into the cavity of the enveloping structure.

摘要翻译： 在制造涡轮机的叶片/叶片的方法中，叶片/叶片由金属包封结构和由复合材料制成的支撑结构制成，该复合材料设置在包封结构内部并适当地接合到包络结构。 将金属毡织物焊接或钎焊/钎焊到构成包络结构的片材上，由此通过液压成形或内部高压成形工艺对该片材组合进行成形，以提供叶片/叶片的包络结构。 最后，将构成支撑结构的复合材料引入到包络结构的空腔中。

公开(公告)号：US08827654B2

公开(公告)日：2014-09-09

申请号：US13188759

申请日：2011-07-22

申请人： Karl Schreiber ,  Werner Beck

发明人： Karl Schreiber ,  Werner Beck

IPC分类号： F01D5/28 ,  F04D29/32 ,  F04D29/02

CPC分类号： F01D5/286 ,  F04D29/023 ,  F04D29/324 ,  F05D2230/232 ,  F05D2240/303 ,  F05D2250/12 ,  F05D2300/161 ,  F05D2300/174 ,  Y02T50/672 ,  Y02T50/673

摘要： A compressor blade 1 of a gas-turbine engine has a flow-exposed leading edge 2. A component 3, made of wear-resistant material and featuring a higher erosive wear resistance than the base material, is attached to at least part of a length of the leading edge 2 The component 3 forming the flow-exposed leading edge 2 is strip-shaped, has an essentially rectangular cross-section and, with reference to a sectional plane perpendicular to the radial direction, is arranged only on an inflow side of the compressor blade profile in a partial area of a sectional surface of the inflow area.

摘要翻译： 燃气涡轮发动机的压缩机叶片1具有暴露在外的前缘2.由耐磨材料制成并且具有比基材高的侵蚀性耐磨性的部件3附接到长度的至少一部分 的前缘2形成流动暴露的前缘2的部件3是带状的，具有基本上矩形的横截面，并且相对于垂直于径向方向的截面，仅布置在 压缩机叶片轮廓在流入区域的截面的局部区域中。

公开(公告)号：US20140127005A1

公开(公告)日：2014-05-08

申请号：US14009301

申请日：2012-04-02

申请人： Karl Schreiber

发明人： Karl Schreiber

IPC分类号： B22C9/22 ,  C23C4/02 ,  B22C7/02 ,  F01D5/28 ,  F01D11/12

CPC分类号： B22C9/22 ,  B22C7/02 ,  B22C9/04 ,  C23C4/02 ,  F01D5/28 ,  F01D5/288 ,  F01D11/12 ,  F01D11/125 ,  F05D2230/211 ,  Y02T50/672

摘要： A method for manufacturing a metallic component especially configured and designed for a turbomachine includes a) for a precision-casting process, a wax model with a wax structure is produced, subsequently b) the tip of the wax structure is thermally and/or mechanically treated such that a region with an undercut is formed on the wax structure, subsequently c) the metallic component is manufactured from the wax model in the precision-casting process, with a component structural element with an undercut forming on a surface of the component, and d) the component structural element is provided at least partially with a ceramic coating, a plastic-containing coating, in particular a fibre composite layer and/or a plastic component.

摘要翻译： 用于制造特别为涡轮机构配置和设计的金属部件的方法包括：a）对于精密铸造工艺，制造具有蜡结构的蜡模型，随后b）蜡结构的末端被热和/或机械处理 使得在蜡结构上形成具有底切的区域，随后c）在精密铸造工艺中由蜡模制造金属部件，在部件的表面上形成具有底切的部件结构元件，以及 d）部件结构元件至少部分地设置有陶瓷涂层，含塑料的涂层，特别是纤维复合层和/或塑料部件。

公开(公告)号：US08647011B2

公开(公告)日：2014-02-11

申请号：US12855095

申请日：2010-08-12

申请人： Karl Schreiber

发明人： Karl Schreiber

IPC分类号： A47B96/06

CPC分类号： F01D5/02 ,  F01D5/282 ,  F05D2230/239 ,  F05D2300/224 ,  F05D2300/603 ,  F05D2300/614 ,  F16C3/026 ,  F16C2360/23 ,  Y02T50/672 ,  Y10T403/65

摘要： On an engine shaft of hybrid design with an externally toothed power transmission element connected at the ends of a fiber-composite plastic tube, the power transmission element is of a two-part design and includes a toothed part made of steel of a specific hardness and, frontally weldedly connected thereto, a tapering adapter part enclosed by a fiber-composite material to form a scarf-type joint and having a thermal expansion approximately equal to the expansion behavior of the fiber-composite material.

摘要翻译： 在混合设计的发动机轴上，在纤维复合塑料管的端部连接有外齿的动力传递元件，动力传递元件是两部分设计的，包括由具有特定硬度的钢制成的齿形部分， 与前面焊接连接的一个锥形接头部分，由纤维复合材料包围以形成围巾型接头，其热膨胀近似等于纤维复合材料的膨胀行为。

公开(公告)号：US08246478B2

公开(公告)日：2012-08-21

申请号：US12613164

申请日：2009-11-05

申请人： Karl Schreiber ,  Raimund Grothaus

发明人： Karl Schreiber ,  Raimund Grothaus

IPC分类号： F16D1/068

CPC分类号： F01D5/06 ,  B29C53/8016 ,  B29C70/86 ,  B29L2031/75 ,  F05D2240/61 ,  F05D2300/603 ,  F05D2300/614 ,  F16C3/026 ,  F16C2360/23

摘要： On a low-pressure turbine shaft made of fiber-composite material, the connection to the metallic driven protrusion or the driving protrusion (1), respectively, is made via an adapter (3) formed onto the latter, with pylons (6) extending beyond the circumferential area of the latter and on which the fibers (4) are deflected and guided in accordance with the fiber orientation in the fiber-composite material, enabling high torsional forces to be transmitted via the small connecting zone.

摘要翻译： 在由纤维复合材料制成的低压涡轮轴上，分别通过形成在其上的适配器（3）与金属从动突起或驱动突起（1）的连接形成，塔（6）延伸 超过纤维复合材料中的纤维取向而使纤维（4）偏转和引导到纤维复合材料的周向区域之后，能够通过小的连接区传递高的扭转力。

公开(公告)号：US20120017663A1

公开(公告)日：2012-01-26

申请号：US13187024

申请日：2011-07-20

申请人： Karl SCHREIBER ,  Werner BECK

发明人： Karl SCHREIBER ,  Werner BECK

IPC分类号： B21D22/00

CPC分类号： B21D22/02 ,  B21D31/00 ,  B21D37/20 ,  B21F27/12 ,  F01D5/147 ,  F04D29/023 ,  F04D29/324 ,  F04D29/542 ,  F05D2230/00 ,  F05D2230/20 ,  F05D2300/16 ,  F05D2300/502 ,  Y02T50/672

摘要： A method for manufacturing a workpiece 1, 2 uses a forming tool 4, 5 having a cavity 3. An embossing element 6 profiled on at least one surface is arranged on at least one surface of the forming tool 4, 5 for producing a surface structure, and with the profile of the embossing tool 6 is imparted to the surface of the workpiece 1, 2 during a forming process.

摘要翻译： 用于制造工件1,2的方法使用具有空腔3的成形工具4,5。在成形工具4,5的至少一个表面上布置有至少一个表面上形成的压花元件6，用于产生表面结构 并且在成形过程中将压花工具6的轮廓赋予工件1,2的表面。