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11. 发明申请

WO2009065379A3 COMPONENT CONNECTION FOR AN AIRCRAFT 审中-公开
标题翻译：飞机组件连接
公开(公告)号：WO2009065379A3
公开(公告)日：2009-08-06
申请号：PCT/DE2008001851
申请日：2008-11-10
申请人： EADS DEUTSCHLAND GMBH , MTU AERO ENGINES GMBH , BAYER ERWIN , STEINWANDEL JUERGEN
发明人： BAYER ERWIN , STEINWANDEL JUERGEN
IPC分类号： F16B5/00
CPC分类号： F16B5/0072 , F16B2/065 , F16B5/0088
摘要： The invention relates to a component connection (10) for a vehicle, especially an aircraft, comprising at least one metal component (20) and a fiber composite component (30) which are connected to one another by means of a fastening device (40). The fastening device (40) encompasses a bearing element (50) and a fastening element (70) for non-positively connecting the bearing element (50) and the metal component (20) and thus the metal component (20) and the fiber composite component (30). The fiber composite component (30) has no bore that is used for connecting the metal component (20) and the fiber composite component (30). The invention further relates to a method for connecting components for a vehicle, especially an aircraft.
摘要翻译：本发明涉及一种用于车辆，特别是飞机的设备连接（10），其包括至少一个金属部件（20）和纤维复合材料部件（30），其中，所述金属构件（20），并通过固定装置彼此纤维复合构件（30）（40）连接，其中，紧固装置（40）包括支承元件（50）和用于所述支承元件（50）和金属部件（20）的力锁合连接的紧固件（70），并且其特征在于金属组分（20）和纤维复合材料部件（30），并且其中所述纤维复合部件（30）不特别用于连接金属部件（20）和纤维复合部件（30）孔。此外，本发明涉及用于连接车辆，特别是飞机的部件的方法。

12. 发明申请

WO2012069037A2 METHOD FOR THE LAYERED MANUFACTURING OF A STRUCTURAL COMPONENT AND DEVICE 审中-公开
标题翻译：制作组件和装置的方法
公开(公告)号：WO2012069037A2
公开(公告)日：2012-05-31
申请号：PCT/DE2011001966
申请日：2011-11-10
申请人： MTU AERO ENGINES GMBH , HEISS THOMAS , BAYER ERWIN
发明人： HEISS THOMAS , BAYER ERWIN
CPC分类号： B05D3/06 , B22F3/1055 , B22F2003/1056 , B29C64/153 , B33Y40/00 , Y02P10/295
摘要： The invention relates to a method for the layered manufacturing of a structural component from powder, comprising the following steps: establishing at least one parameter (t) of a depression (1) in a produced layer (2) of the structural component; smoothing out the depression (1) if the at least one parameter (t) exceeds a predetermined value; and filling the smoothed-out depression (1) with powder (13).
摘要翻译：本发明提供了一种分层生产粉末组分的方法，包括以下步骤：检测组分的形成层（2）中的凹陷（1）的至少一个参数（t）如果至少一个参数（t）超过预定值，则对凹坑（1）进行平滑处理; 并用粉末（13）填充平滑的凹陷（1）。

13. 发明申请

WO2011050790A3 METHOD AND DEVICE FOR PRODUCING A COMPONENT OF A TURBOMACHINE 审中-公开
标题翻译：方法和器具，用于产生涡轮机的一个组成部分
公开(公告)号：WO2011050790A3
公开(公告)日：2011-06-23
申请号：PCT/DE2010001275
申请日：2010-10-30
申请人： MTU AERO ENGINES GMBH , BAYER ERWIN , HILLER SVEN-J
发明人： BAYER ERWIN , HILLER SVEN-J
IPC分类号： B23K26/34 , B23K26/00
CPC分类号： B23K26/34 , B22F3/1055 , B22F5/04 , B22F2003/1056 , B22F2999/00 , B23K26/0069 , B23K26/32 , B23K26/342 , B23K35/005 , B23K35/007 , B23K35/0244 , B23K2201/001 , B23K2203/08 , B23K2203/14 , B23K2203/26 , B23K2203/52 , B28B1/001 , B32B18/00 , C04B35/16 , C04B35/645 , C04B2235/6026 , C04B2235/665 , C04B2237/341 , Y02P10/295 , B22F2203/13
摘要： The invention relates to a method for producing a component (10) of a turbomachine, especially a structural part of a turbine or a compressor, the method being a generative production method for the layer-by-layer buildup of the component (10). After production of one or more successive component layers pressure is applied to at least sections of the surface of the most recently produced component layer (12), the pressure being induced by laser or plasma. The invention further relates to a device for producing a component (10) of a turbomachine, especially a structural part of a turbine or a compressor, the device (26) comprising at least one powder feed (28) for the deposition of at least one powder component material (16) onto a component platform, at least one radiation source (14) for a local layer-by-layer fusion or sintering of the component material (16) and at least one laser radiation source (20) or at least one plasma impulse source.
摘要翻译：本发明涉及一种用于制造涡轮机的部件（10），特别是涡轮机的或压缩机的一个组成部分，该方法是将成分（10）的层状结构的生成的制造方法和生产的一种或至少连续的多个部件层的后部分中进行时，激光或等离子体引起的压力（12）中产生的器件层最后的表面上。本发明还涉及一种用于制造涡轮机的部件（10），特别是涡轮机的或压缩机的部件，所述装置（26）的至少一个粉末进料（28），用于在组件平台施加至少一种粉状组分材料（16）包括用于逐层和局部熔化或烧结所述部件材料（16）和至少一个激光束源（20）或至少一个脉冲等离子体源中的至少一个辐射源（14）。

14. 发明申请

WO2010054633A3 WEAR-RESISTANT LAYER FOR TIAL 审中-公开
标题翻译：穿Tial的防护层
公开(公告)号：WO2010054633A3
公开(公告)日：2010-12-29
申请号：PCT/DE2009001580
申请日：2009-11-07
申请人： MTU AERO ENGINES GMBH , BAYER ERWIN , SMARSLY WILFRIED
发明人： BAYER ERWIN , SMARSLY WILFRIED
IPC分类号： C23C18/08 , C23C18/02 , C23C28/00 , F01D5/28
CPC分类号： C23C18/02 , C23C18/08 , C23C28/021 , C23C28/023 , C23C28/027 , C23C28/028 , F01D5/288 , F05D2260/95 , F05D2300/211 , F05D2300/2112 , F05D2300/2118 , F05D2300/224 , F05D2300/2261 , F05D2300/228 , F05D2300/2284 , Y02T50/67
摘要： The invention relates to a wear-resistant part for high-temperature applications made of a TiAl material, in particular a turbine blade comprising an at least double-layered protective coating (4). A first diffusion barrier layer (2) made of a precious metal and a second hard material layer (3) containing hard material particles that are embedded in a precious metal matrix are applied to the TiAl material (1) as a protective coating. The invention also relates to a corresponding production method.
摘要翻译：本发明涉及一种用于TiAl金属材料的高温应用的磨损保护的构件，尤其是涡轮机叶片具有至少两层的保护层（4），其中，第一扩散阻挡层（2）贵金属和硬质材料（3）的与一个硬质材料颗粒的第二层的贵金属基体被嵌入，被应用于TiAl材料（1）作为保护层和相应的制造工艺。

15. 发明申请

WO2010051799A3 PROCESS CHAMBER FOR REPAIRING A GAS TURBINE COMPONENT 审中-公开
标题翻译：工艺室的燃气涡轮机部件的维修
公开(公告)号：WO2010051799A3
公开(公告)日：2010-07-15
申请号：PCT/DE2009001539
申请日：2009-11-05
申请人： MTU AERO ENGINES GMBH , HUTTNER ROLAND , DUSEL KARL-HEINZ , BAYER ERWIN , PLATZ ALBIN
发明人： HUTTNER ROLAND , DUSEL KARL-HEINZ , BAYER ERWIN , PLATZ ALBIN
IPC分类号： B22F3/105 , B22F7/06 , B23P6/00 , B29C67/00 , F01D5/00
CPC分类号： B22F3/1055 , B22F7/062 , B22F2998/00 , B22F2999/00 , B23P6/007 , F01D5/005 , F01D25/285 , F05D2230/31 , F05D2230/68 , F05D2230/80 , Y02P10/295 , B22F5/04 , B22F3/003 , B22F2202/13
摘要： The invention relates to a repair method for gas turbine components, particularly for gas turbine blades, comprising at least the following steps: a) providing a gas turbine component to be repaired; b) removing a damaged section from the gas turbine component to be repaired to form a level separating surface; c) arranging the gas turbine component to be repaired in a process chamber at least in regions such that the level separating surface runs approximately horizontally inside the process chamber; d) filling the process chamber with a metal powder compatible for bonding with the material of the gas turbine component to be repaired, specifically up to the level of the separating surface; e) building the removed section on the separating surface by applying the metal powder in layers onto the separating surface and by melting the metal powder applied in layers onto the separating surface to the separating surface.
摘要翻译：本发明涉及一种修理燃气涡轮机部件，特别是用于燃气涡轮机叶片的方法，包括至少以下步骤：a）提供一个燃气涡轮机部件进行修理; b）除去的受损部分被修理燃气涡轮机部件，以形成一个平坦的分离面; c）至少部分地布置所述燃气涡轮机部件，以在处理室中被修复，使得平面分离面在围绕处理室内水平地延伸; d）用连接兼容的材料要被修复燃气涡轮机部件的金属粉末填充处理室，即，一直到分型面的水平; e）通过将金属粉末的层涂布在剥离表面，并通过熔合涂布在具有释放表面的释放表面的金属粉末层设置的释放表面上的去除部分的。

16. 发明申请

WO2009067992A3 ACTIVE GAP REGULATING DEVICE FOR A ROTOR HOUSING 审中-公开
标题翻译： ACTIVE分裂控制装置转子外壳
公开(公告)号：WO2009067992A3
公开(公告)日：2010-01-28
申请号：PCT/DE2008001916
申请日：2008-11-20
申请人： MTU AERO ENGINES GMBH , BAYER ERWIN , HUTTNER ROLAND
发明人： BAYER ERWIN , HUTTNER ROLAND
IPC分类号： F01D11/22
CPC分类号： F01D11/22 , F05D2240/11 , F05D2260/52 , F05D2260/56
摘要： The invention relates to a gap regulating device for a rotor housing of a turbomachine, comprising a number of housing segments (1) combined to form a ring, and a number of actuators (2) for actuating the housing segments (1) in the radial direction. A rocker arrangement (5) is used to transfer the actuating movement of each actuator (2) to the associated housing segment(s) (1). The housing segments (1) preferably consisting of sinter material are pre-tensioned for an expansion of the ring. The springs (4) required therefor are built into the housing segments and elastically connect two respective adjacent housing segments to each other.
摘要翻译：本发明涉及一种用于具有多个环的涡轮机转子壳体中的间隙控制装置组装的壳体段（1）和一个数字（2），用于在径向方向上驱动所述壳体段（1）致动器。它是提供给相应致动器（2）的致动运动传递到摇臂（5）/相关联的（n）的外壳部分（一个或多个）（1）。优选由壳体段的烧结材料（1）被偏置为所述环的扩张。必要的弹簧（4）一体地与壳体段形成并连接弹性每两个相邻的壳体段。

17. 发明申请

WO2012069037A3 METHOD FOR THE LAYERED MANUFACTURING OF A STRUCTURAL COMPONENT AND DEVICE 审中-公开
标题翻译：用于生产WAY组成与器件的层
公开(公告)号：WO2012069037A3
公开(公告)日：2012-12-20
申请号：PCT/DE2011001966
申请日：2011-11-10
申请人： MTU AERO ENGINES GMBH , HEISS THOMAS , BAYER ERWIN
发明人： HEISS THOMAS , BAYER ERWIN
IPC分类号： B22F3/105 , B29C67/00
CPC分类号： B05D3/06 , B22F3/1055 , B22F2003/1056 , B29C64/153 , B33Y40/00 , Y02P10/295
摘要： The invention relates to a method for the layered manufacturing of a structural component from powder, comprising the following steps: establishing at least one parameter (t) of a depression (1) in a produced layer (2) of the structural component; smoothing out the depression (1) if the at least one parameter (t) exceeds a predetermined value; and filling the smoothed-out depression (1) with powder (13).
摘要翻译：本发明提供一种方法，用于分层制造由粉末的成分，其包括以下步骤：形成在层检测的凹部中的至少一个参数（T）（1）（2）的组分; 平滑，当所述至少一个参数（t）的超过预定值的凹部（1）; 和填充所述凹部平滑（1）与粉末（13）。

18. 发明申请

WO2012097797A3 HEAT EXCHANGER AND JET ENGINE COMPRISING SAME 审中-公开
标题翻译：热交换喷气发动机这样的
公开(公告)号：WO2012097797A3
公开(公告)日：2012-11-15
申请号：PCT/DE2012000031
申请日：2012-01-16
申请人： MTU AERO ENGINES GMBH , NEUHAEUSLER STEFAN , SATZGER WILHELM , SIKORSKI SIEGFRIED , DUSEL KARL-HEINZ , HUTTNER ROLAND , MELZER HANS-CHRISTIAN , BAYER ERWIN
发明人： NEUHAEUSLER STEFAN , SATZGER WILHELM , SIKORSKI SIEGFRIED , DUSEL KARL-HEINZ , HUTTNER ROLAND , MELZER HANS-CHRISTIAN , BAYER ERWIN
IPC分类号： F02C7/143 , B22F3/105 , F02C7/08 , F02K3/115
CPC分类号： F02C7/08 , B22F5/009 , B22F2999/00 , B33Y80/00 , F02C7/143 , F02K3/115 , Y02P10/295 , Y02T50/671 , Y02T50/675 , B22F3/1055
摘要： The invention relates to a heat exchanger (20), in particular for a jet engine, said engine being designed as a structure-mechanical and/or fluid-mechanical element or having an integral element of this type and being at least partially produced by rapid manufacturing.
摘要翻译：的热交换器（20），特别是用于喷气发动机，产生作为结构和/或流体机械元件或一体形成等并至少部分地生成地。

19. 发明申请

WO2009074141A3 METHOD FOR REMOVING MATERIAL FROM A COMPONENT, AND ELECTRODE 审中-公开
标题翻译：法测量材料从一个组成部分，除铅
公开(公告)号：WO2009074141A3
公开(公告)日：2010-09-23
申请号：PCT/DE2008002040
申请日：2008-12-05
申请人： MTU AERO ENGINES GMBH , BAYER ERWIN , BUSSMANN MARTIN , PLATZ ALBIN
发明人： BAYER ERWIN , BUSSMANN MARTIN , PLATZ ALBIN
IPC分类号： B23H3/00 , B23H3/10
CPC分类号： B23H3/00 , B23H1/04 , B23H3/04 , B23H3/06 , B23H3/10 , B23H5/10 , B23H7/26
摘要： Disclosed is a method for removing material from a component (10, 10') that is connected as an anode. In said method, an electrode (12) that is connected as a cathode is guided to the component such that a gap (16) is formed, an electrolyte is introduced into the gap, and a closed system is formed for the electrolyte by forming a duct. The electrolyte is continuously conducted from an inlet to an outlet of the duct. Forming the duct, e.g. by means of conducting elements (18) that are mounted on the electrode (12), ensures that only those surface parts of the component (10) to be machined from which material is to be removed enter in contact with the electrode while the other surface parts do not enter in contact with the electrolyte. Since the electrolyte is continuously conducted across said surface, used electrolyte is continuously discharged along with residual matter while fresh electrolyte is delivered such that the method can be carried out in a particularly trouble-free and expedient manner.
摘要翻译：在用于从连接作为阳极的部件（10，10“）去除材料，和一种方法，其中一个切换作为阴极电极（12）被引导到该组件，从而形成一间隙（16），和其中，电解质被引入间隙通过形成通道用于电解质的封闭系统形成。这是连续地从进料口向信道的排出口供给。通过形成的通道，例如，通过在电极（12）上的导向元件（18）是固定的，它保证了仅由组分的那些表面部分被加工（10）接触的电解质加入到从材料烧蚀并且，剩余的表面部分不接触到与电解质接触。通过不断地使电解质随时间废电解质的表面被连续残基一起排出和新鲜电解质供应，因此该方法特别平滑且迅速地进行。

20. 发明申请

WO2009018804A3 DAMPING DEVICE, WELDING SYSTEM FOR ROTARY FRICTION WELDING AND ROTARY FRICTION WELDING METHOD 审中-公开
标题翻译：阻尼装置，焊接SYSTEM FOR旋转旋转焊接及焊接
公开(公告)号：WO2009018804A3
公开(公告)日：2009-09-17
申请号：PCT/DE2008001230
申请日：2008-07-24
申请人： MTU AERO ENGINES GMBH , BAYER ERWIN , WEBER STEFFEN
发明人： BAYER ERWIN , WEBER STEFFEN
IPC分类号： B23K20/12 , F16F15/16
CPC分类号： F16F15/16 , B23K20/12 , F16F2224/048
摘要： The invention relates to a damping device (20), which in order to reduce vibrations occurring during the rotary friction welding of a first to at least one second component (12a, 12b) can be disposed on at least one of said components (12a, 12b), wherein the damping device (20) comprises a casing element (22), which is filled at least partially with a viscoelastic fluid (24). The invention further relates to a welding system (10) and to a method for the rotary friction welding of a first to at least one second component (12a, 12b), and to a component (12), particularly for an aircraft engine.
摘要翻译：本发明涉及一种阻尼装置（20），用于在旋转焊接减少在一起的第一和至少一个第二部件（12A，12B）的振动发生在这些部件中的至少一个（12A，12B）可以被布置，其中，所述减振装置（20）包括一个壳构件（22），其在与粘弹性流体至少部分（24）被充满。本发明还涉及一种焊接设备（10）和旋转的焊接的第一到至少一个第二组件，用于飞行器发动机的方法（12A，12B）和部件（12），尤其如此。

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