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1. 发明申请

WO2006105762A3 ARRANGEMENT FOR MONITORING THERMAL SPRAY PROCESSES 审中-公开
标题翻译：安排监测热喷涂工艺
公开(公告)号：WO2006105762A3
公开(公告)日：2007-04-19
申请号：PCT/DE2006000555
申请日：2006-03-30
申请人： MTU AERO ENGINES GMBH , HERTTER MANUEL , HOESCHELE JOERG , SCHNEIDERBANGER STEFAN , STEINWANDEL JUERGEN
发明人： HERTTER MANUEL , HOESCHELE JOERG , SCHNEIDERBANGER STEFAN , STEINWANDEL JUERGEN
IPC分类号： H05H1/00
CPC分类号： H05H1/0037 , H05H1/0025
摘要： The invention relates to an arrangement for measuring characteristic properties of a plasma beam in a thermal spray process, said arrangement comprising means for introducing spray materials into the plasma, a one-dimensional or two-dimensional array consisting of first optical waveguides (2a) for receiving the light radiation emitted by the plasma (1), and other optical waveguides (2b, 2c) for distributing the light radiation emitted by the plasma (1). According to the invention, means (W) are provided for splitting the light guided in the first optical waveguides (2a) into the other optical waveguides (2b, 2c), one optical waveguide (2c) being connected to the opening diaphragm of a particle flow arrangement (7), and the other optical waveguide (2b) being connected to the opening diaphragm of a spectrometer (3). Means (5, 7) are also provided for determining the current state of the spray process.
摘要翻译：本发明涉及一种装置，用于测量在热喷涂工艺的等离子体束的特征性质，包括：用于供给喷涂材料的等离子体，第一光纤（2a）中从发射（1）的光照射，并进一步等离子体容纳的一维或二维阵列等离子体（1）的光发射的辐射的分布的光纤（2B，2C）。根据本发明，装置是（W）呈现出用于将进入的光的第一光纤（2a）中在所述另外的光纤（2B，2C），其中，所述一个光学纤维（2c）的至颗粒磁通布置的输入孔（7）和其他光纤（2b）中连接到光谱仪（3）和装置的输入孔（5,7），用于确定所述喷射过程的瞬时状态都存在。

2. 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。

3. 发明申请

WO2008049392A3 VAPOUR-DEPOSITED COATING AND THERMALLY STRESSABLE COMPONENT HAVING SUCH A COATING, AND ALSO A PROCESS AND APPARATUS FOR PRODUCING SUCH A COATING 审中-公开
标题翻译：沉积涂层和热稳定成分具有产生这种涂料这种涂料和方法及装置
公开(公告)号：WO2008049392A3
公开(公告)日：2009-10-15
申请号：PCT/DE2007001859
申请日：2007-10-17
申请人： MTU AERO ENGINES GMBH , BAYER ERWIN , STEINWANDEL JUERGEN , LAURE STEFAN
发明人： BAYER ERWIN , STEINWANDEL JUERGEN , LAURE STEFAN
IPC分类号： C23C14/08 , C23C4/12 , C23C14/06 , C23C14/32 , C23C14/58 , C23C16/44
CPC分类号： C23C16/44 , C23C4/134 , C23C4/137 , C23C14/083 , C23C14/228 , C23C14/325 , Y02T50/67 , Y10T428/249953
摘要： The invention relates to a vapour-deposited coating for a thermally stressable component, which comprises deliberately introduced pore formers. This distinguishes it from conventional vapour-deposited coatings which, owing to the coating method, have no pores or from sprayed-on coatings which have no pores or only irregularly shaped pores formed arbitrarily. The invention additionally relates to a process and an apparatus for producing such a coating.
摘要翻译：本发明涉及一种气相沉积涂层上，其包括故意引入孔剂热稳定组分。这从由于类型的涂层，或喷雾涂层，其不具有或仅任意所得的不规则形状的孔的不具有孔隙常规气相沉积的涂层区分开来。本发明还涉及一种用于制造这样的涂层的方法和装置。

4. 发明专利

JP2003183803A METHOD AND APPARATUS FOR COATING SILICON CARBIDE FIBER 审中-公开
公开(公告)号：JP2003183803A
公开(公告)日：2003-07-03
申请号：JP2002236406
申请日：2002-08-14
申请人： MTU AERO ENGINES GMBH , DAIMLER CHRYSLER AG
发明人： BAYER ERWIN , HOESCHELE JOERG , KOPPERGER BERTRAM , STEINWANDEL JUERGEN
IPC分类号： B22F1/02 , C04B41/45 , C04B41/88 , C22C47/04 , C23C4/12 , C23C4/123 , C23C4/134 , C23C16/513 , C23C30/00 , D06M11/00 , C23C4/08 , C23C4/16 , D06M11/83
摘要： PROBLEM TO BE SOLVED: To provide a novel method capable of simply and effectively coating a silicon carbide fiber in an assembly line operation; and an apparatus therefor. SOLUTION: The method for coating the silicon carbide fiber with a titanium alloy by plasma spraying is characterized in that the titanium alloy is thermally sprayed on the silicon carbide fiber 7 by an electrode-free high-pressure plasma 3 which is generated by igniting a process gas introduced under a pressure of 1 bar or higher into a microwave- or electric wave-transparent working tube 2 having a gas injection port 8 and a gas exhaust port 9, is sustained by the absorption of a microwave or electric wave, and flows as a plasma jet 6 through a nozzle 4 arranged at the gas exhaust port 9 of the working tube 2 into a working space 5. COPYRIGHT: (C)2003,JPO

5. 发明专利

CA2692979C METHOD AND DEVICE FOR SURFACE PEENING OF A COMPONENT IN THE REGION OF A PASSAGE OPENING 未知
公开(公告)号：CA2692979C
公开(公告)日：2015-02-17
申请号：CA2692979
申请日：2008-06-06
申请人： EADS DEUTSCHLAND GMBH , MTU AERO ENGINES GMBH
发明人： BAYER ERWIN , REESE EGGERT , STEINWANDEL JUERGEN
IPC分类号： B24C1/10
摘要： The invention relates to a method for surface peening, particularly ultrasonic shot peening, of a component (22) in the region of a passage opening (24) in which a vibration device (10) impinging the blasting material is disposed on one side (18) and a counter-element (28) is disposed on an opposite side (26) relative to a component region (20) having the passage opening (24), in which the counter-element (28) is disposed at a distance relative to the corresponding side (26) of the component region (20). The invention also relates to a device for carrying out such a method.

6. 发明专利

DE502005007309D1 未知
公开(公告)号：DE502005007309D1
公开(公告)日：2009-07-02
申请号：DE502005007309
申请日：2005-10-07
申请人： MTU AERO ENGINES GMBH
发明人： BAYER ERWIN , BUSSMANN MARTIN , KRAENZLER THOMAS , PLATZ ALBIN , STEINWANDEL JUERGEN
IPC分类号： B23H3/02

7. 发明专利

DE102007056164A1 未知
公开(公告)号：DE102007056164A1
公开(公告)日：2009-06-04
申请号：DE102007056164
申请日：2007-11-21
申请人： MTU AERO ENGINES GMBH , EADS DEUTSCHLAND GMBH
发明人： BAYER ERWIN , STEINWANDEL JUERGEN
IPC分类号： B64C1/00

8. 发明专利

DE102005033588A1 Radial turbine used as part of exhaust gas turbocharger for reciprocating piston engine comprises inlet coating arranged on inside of housing and comprising metallic matrix and lubricating or sliding additive 未知
公开(公告)号：DE102005033588A1
公开(公告)日：2007-01-25
申请号：DE102005033588
申请日：2005-07-19
申请人： MTU AERO ENGINES GMBH
发明人： FANDEL MARCO , HERTTER MANUEL , KRAENZLER THOMAS , STEINWANDEL JUERGEN
IPC分类号： F01D11/12
摘要： A radial turbine comprises an inlet coating arranged on the inside of a housing and comprising a metallic matrix based on nickel, cobalt and/or iron and a lubricating or sliding additive in the form of hexagonal boron nitride, bentonite and/or graphite. An independent claim is also included for the production of a radial turbine.

9. 发明专利

DE102004048611A1 Method for joining components esp. metallic, gas-turbine components, involves passing ionizing gas between joining-surfaces of component parts 未知
公开(公告)号：DE102004048611A1
公开(公告)日：2006-04-20
申请号：DE102004048611
申请日：2004-10-06
申请人： MTU AERO ENGINES GMBH , DAIMLER CHRYSLER AG
发明人： BAYER ERWIN , STEINWANDEL JUERGEN
IPC分类号： B23K10/02
摘要： A method for joining components involves preparing at least two components (10,11) to be joined together by arranging the component parts so that between the joining-surfaces (12,13) is formed a space/gap. An ionizing gas is passed between the joining-surfaces of the component parts, to provide plasma formation between the joining-surfaces (12,13) by ignition of the gas, where the power required for the ignition process is provided by micro-wave radiation. The components (10,11) are then welded together at the joining-surfaces (12,13).

10. 发明专利

DE10140298B4 未知
公开(公告)号：DE10140298B4
公开(公告)日：2005-02-24
申请号：DE10140298
申请日：2001-08-16
申请人： MTU AERO ENGINES GMBH , DAIMLER CHRYSLER AG
发明人： STEINWANDEL JUERGEN , LAURE STEFAN DR
IPC分类号： H05H1/30 , H05H1/50 , B23K10/02
摘要： Plasma welding using a free radio frequency-induced plasma beam comprises forming a stationary high pressure plasma (2) by igniting a first process gas in a pilot plasma burner (1) and introducing the plasma gas into a radio frequency transparent operating tube (3) comprising a gas inlet opening (4) and a gas outlet opening (5); introducing a second process gas (6) into the tube at a pressure p ≥ 1 bar so it has a tangential flow component; forming a radio frequency plasma (7) in the tube using electroless ignition of the gas mixture (2,6); and forming a plasma beam (8) by introducing the radio frequency plasma into the working chamber (9) through a metallic expansion nozzle (10) on the gas outlet opening of the tube. Preferred Features: The metallic expansion nozzle is cooled. Radio waves in the frequency region of 150 kHz to 150 MHz are used to produce a radio frequency plasma as a result of inductive coupling. The transparent operating tube is made from SiO2 or Al2O3 in pure form without dopants.

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