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21. 发明申请

US20170312989A9 Friction Stir Processing Tool Having Non-Circumferential Shoulder and Friction Stir Processing Method Performable Therewith 审中-公开
公开(公告)号：US20170312989A9
公开(公告)日：2017-11-02
申请号：US14296125
申请日：2014-06-04
申请人： EADS Deutschland GmbH
发明人： Juergen SILVANUS , Tommy BRUNZEL
IPC分类号： B29C65/06 , B23K20/12
CPC分类号： B29C65/0672 , B23K20/1245 , B23K20/1255
摘要： A friction stir processing tool for friction stir processing includes a shoulder for pressing against a workpiece surface and a pin, which protrudes beyond the shoulder and can be driven to rotate, for plasticizing introduction into at least one workpiece to be processed. The shoulder has an interruption opening on a circumferential region, so that the shoulder is not led around the entire circumference of the pin.

22. 发明授权

US09364917B2 Friction stir processing tool with different shoulder regions 有权
标题翻译：摩擦搅拌加工工具具有不同的肩部区域
公开(公告)号：US09364917B2
公开(公告)日：2016-06-14
申请号：US14299423
申请日：2014-06-09
申请人： EADS Deutschland GmbH
发明人： Juegren Silvanus , Tommy Brunzel
IPC分类号： B23K20/12 , B23K20/22
CPC分类号： B23K20/122 , B23K20/1225 , B23K20/1255 , B23K20/22
摘要： A friction stir processing tool having a shoulder, which is implemented on a body, and which has a friction surface for pressing against at least one workpiece at least partially provided with a surface coating, and a friction reducing unit for reducing the friction resistance between the surface coating and the friction surface.
摘要翻译：一种摩擦搅拌处理工具，其具有肩部，其实施在主体上，并且具有用于按压至少一个至少部分地设置有表面涂层的工件的摩擦表面;以及摩擦减小单元，用于减小所述摩擦阻力表面涂层和摩擦表面。

23. 发明授权

US09283414B2 Solid propellant gas generator, extinguishing device, method for cooling a flowing mixture and method for extinguishing a fire 有权
标题翻译：固体推进剂气体发生器，灭火装置，冷却流动混合物的方法和灭火方法
公开(公告)号：US09283414B2
公开(公告)日：2016-03-15
申请号：US14024091
申请日：2013-09-11
申请人： EADS Deutschland GmbH
发明人： Jens Lemke , Elizabeth Richter , Sebastian Schulz
IPC分类号： A62C35/00 , A62C5/00 , A62C99/00 , A62C3/00 , E03C1/084 , A62D1/06 , F23D14/04 , A62C13/00 , A62C13/20 , A62C13/22
CPC分类号： A62C5/004 , A62C3/00 , A62C5/006 , A62C13/006 , A62C13/20 , A62C13/22 , A62C99/0009 , A62C99/0018 , A62C99/009 , A62D1/06 , E03C1/084 , F23D14/04 , F23Q25/00
摘要： A solid propellant gas generator releases a flowing mixture from a solid propellant, separated from a surrounding area, into the surrounding area. The solid propellant gas generator includes a cooling system for cooling the flowing mixture. The cooling system has at least one feed device for feeding a gas from the surrounding area to the flowing mixture in order to mix the flowing mixture prior to entering into the surrounding area with the gas from the surrounding area.
摘要翻译：固体推进剂气体发生器将与周围区域分离的固体推进剂的流动混合物释放到周围区域。固体推进剂气体发生器包括用于冷却流动混合物的冷却系统。冷却系统具有至少一个进料装置，用于将来自周围区域的气体供给流动的混合物，以便在与来自周围区域的气体进入周围区域之前混合流动的混合物。

24. 发明申请

US20160025075A1 STIRLING ENGINE FOR AN EMISSION-FREE AIRCRAFT 有权
公开(公告)号：US20160025075A1
公开(公告)日：2016-01-28
申请号：US14877102
申请日：2015-10-07
申请人： EADS DEUTSCHLAND GMBH
发明人： Jost SEIFERT
IPC分类号： F03G6/06 , F03G7/06 , F02G1/055
CPC分类号： F03G6/068 , B64C1/16 , B64C3/32 , B64D13/006 , B64D27/02 , B64D27/04 , B64D27/06 , B64D27/08 , B64D27/24 , B64D2027/026 , F01B29/10 , F02G1/04 , F02G1/043 , F02G1/0435 , F02G1/044 , F02G1/053 , F02G1/0535 , F02G1/055 , F02G1/057 , F02G2243/02 , F02G2243/30 , F02G2244/50 , F02G2254/30 , F02G2280/10 , F03G7/06 , F25B9/14 , F25B2309/001 , F25B2309/003 , Y02E10/46 , Y02T50/62
摘要： Aircraft with an emission-free drive and method for emission-free driving of an aircraft. The aircraft includes a drive device structured and arranged to generate thrust, a lift device structured and arranged to generate lift, and a heat engine structured and arranged to convert thermal energy into kinetic energy to drive the drive device. The heat engine includes at least one flat-plate Stirling engine drivable by solar thermal radiation.

25. 发明申请

US20160001396A1 Method for Nano-Structuring Polmer Materials Using Pulsed Laser Radiation in an Inert Atmosphere 审中-公开
标题翻译：在惰性气氛中使用脉冲激光辐射的纳米结构化聚合物材料的方法
公开(公告)号：US20160001396A1
公开(公告)日：2016-01-07
申请号：US14434979
申请日：2013-10-10
申请人： EADS DEUTSCHLAND GMBH
发明人： Erhard BRANDL , Ante KURTOVIC , Tobias MERTENS
IPC分类号： B23K26/00 , B23K26/0622 , B23K26/12
CPC分类号： B23K26/3584 , A61F2002/0081 , A61L27/10 , A61L27/18 , A61L27/427 , A61L27/50 , A61L2400/12 , A61L2400/18 , B23K26/0006 , B23K26/0622 , B23K26/1224 , B23K26/123 , B23K26/125 , B23K2103/42 , C08L63/00 , C08L75/04 , C08L71/12
摘要： In a method for generating a surface having a solid polymeric material, which has surface structures with dimensions in the sub-micrometer range, the untreated surface, on which the structures are to be generated and which are accessible to laser radiation, is scanned once or multiple times using a pulsed laser beam in an inert gas atmosphere in such a way that adjacent light spots of the laser beam adjoin each other in a gapless manner or overlap and a certain range of a specified relation between process parameters is observed.
摘要翻译：在具有固体聚合材料的表面的方法中，其具有尺寸在亚微米范围内的表面结构，将在其上生成结构并且可被激光辐射接近的未处理表面被扫描一次或在惰性气体气氛中使用脉冲激光束多次，使得激光束的相邻光点以无间隙的方式彼此相邻或重叠，并且观察到处理参数之间的指定关系的一定范围。

26. 发明授权

US09193469B2 Aircraft engine with an apparatus for pulsating expiration of gas into the exhaust nozzle 有权
标题翻译：具有用于将气体脉动地排放到排气喷嘴中的装置的飞机发动机
公开(公告)号：US09193469B2
公开(公告)日：2015-11-24
申请号：US14050437
申请日：2013-10-10
申请人： EADS Deutschland GmbH
发明人： Michael Bauer , Ludwig Schauwecker , Daniel Redmann , Josef Steigenberger
IPC分类号： F02K1/34
CPC分类号： B64D33/06 , F02K1/34 , F05D2260/16 , F05D2260/963
摘要： An aircraft jet engine includes an exhaust-gas nozzle having a device configured to blow out an exhaust gas in a pulsating manner into an exhaust-gas stream so as to reduce noise. The exhaust-gas nozzle includes openings distributed along a circumference of the exhaust-gas nozzle and disposed upstream from a nozzle outlet. The openings communicate with the device.
摘要翻译：飞机喷气发动机包括排气喷嘴，该排气喷嘴具有被构造成以脉动的方式将废气吹入排气流中以减少噪声的装置。废气喷嘴包括沿排气喷嘴的圆周分布并且设置在喷嘴出口的上游的开口。开口与设备通信。

27. 发明授权

US09193458B2 Air-to-surface surveillance and/or weapons system and method for air-based inspection and/or engagement of objects on land or sea 有权
标题翻译：空对地监视和/或武器系统和方法，用于陆上或海上物体的空中检查和/或接合
公开(公告)号：US09193458B2
公开(公告)日：2015-11-24
申请号：US13757037
申请日：2013-02-01
申请人： EADS Deutschland GmbH
发明人： Hans Wolfgang Pongratz , Manfred Hiebl
IPC分类号： B64C37/02 , B64C3/00 , B64C39/02
CPC分类号： B64C37/02 , B64C39/024
摘要： An air-to-surface surveillance and/or weapons system includes a base aircraft and an unmanned slave aircraft that can be uncoupled from a base aircraft and coupled back to it again. The base aircraft and slave aircraft are equipped with coupling equipment designed to work together. The base aircraft is equipped with surveillance and monitoring equipment. The slave aircraft is equipped with monitoring equipment and/or weapons. The slave aircraft can be connected to a control station via a data link for data exchange and can be controlled from this control station.
摘要翻译：空对地监视和/或武器系统包括一架基地飞机和一架无人飞机，可以与基地飞机脱离联系并再次耦合回来。基地飞机和奴隶飞机配备有设计在一起的联轴器设备。基地飞机配备有监控和监控设备。奴隶飞机配有监视设备和/或武器。从机可以通过数据链路连接到控制站进行数据交换，并可以从该控制台进行控制。

28. 发明申请

US20150299889A1 Self-Cleaning and Superhydrophobic Surfaces Based on TIO2 Nanotubes 审中-公开
标题翻译：基于TIO2纳米管的自清洁和超疏水表面
公开(公告)号：US20150299889A1
公开(公告)日：2015-10-22
申请号：US14367667
申请日：2012-12-11
申请人： EADS Deutschland Gmbh
发明人： Tobias MERTENS , Dominik RAPS , Juergen WEHR
IPC分类号： C25D11/26
CPC分类号： C25D11/26
摘要： A method for producing a superhydrophobic coating with self-cleaning properties on a metallic substrate involves providing a metallic substrate that titanium and an electrolyte solution that includes a fluoride salt. At least part of a surface of the metallic substrate is contacted with the electrolyte solution. The metallic substrate is anodized in order to produce a nanoporous layer having nanotubes including titanium dioxide on the metallic substrate. A superhydrophobising coating is applied onto the nanoporous layer comprising nanotubes including titanium dioxide, wherein the electrolyte solution includes a further water-soluble salt selected from the group comprising ammonium sulphate, sodium sulphate, sodium bisulphate, potassium sulphate, potassium bisulphate and mixtures thereof.
摘要翻译：在金属基底上制造具有自清洁性能的超疏水涂层的方法包括提供金属基底，钛和包含氟化物盐的电解质溶液。金属基材的表面的至少一部分与电解质溶液接触。阳极氧化金属基底，以便在金属基底上产生纳米多孔层，其纳米管包括二氧化钛。将超疏水涂层施加到包含二氧化钛的纳米多孔层上，其中电解质溶液包括选自硫酸铵，硫酸钠，硫酸氢钠，硫酸钾，硫酸氢钾及其混合物的另外的水溶性盐。

29. 发明申请

US20150246726A1 ROTORCRAFT WITH AT LEAST ONE MAIN ROTOR AND AT LEAST ONE COUNTER-TORQUE ROTOR 审中-公开
标题翻译：具有至少一个主转子和至少一个反转矩转子的转子
公开(公告)号：US20150246726A1
公开(公告)日：2015-09-03
申请号：US14630980
申请日：2015-02-25
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GMBH , EADS DEUTSCHLAND GMBH
发明人： Reinhard PONGRATZ , Sascha SCHNEIDER
IPC分类号： B64C27/82 , B64C27/32 , B64C27/00
CPC分类号： B64C27/82 , B64C27/001 , B64C27/32 , B64C2027/8254
摘要： A rotorcraft with at least one main rotor 1a and at least one counter-torque rotor, comprising: at least one duct-type portion provided with a shroud that defines at least one transverse duct, the at least one counter-torque rotor comprising a plurality of counter-torque rotor blades and being rotatably arranged within the at least one transverse duct, and a drive shaft fairing that is fixedly supported within the at least one transverse duct and that rotatably supports the at least one counter-torque rotor, the drive shaft fairing comprising a leading edge facing the at least one counter-torque rotor, the leading edge being at least partially equipped with associated acoustical damping means.
摘要翻译：具有至少一个主转子1a和至少一个反扭矩转子的旋翼航空器，包括：至少一个导管型部分，其设置有限定至少一个横向管道的护罩，所述至少一个反扭矩转子包括多个并且可旋转地布置在所述至少一个横向管道内;以及驱动轴整流装置，其固定地支撑在所述至少一个横向管道内并且可旋转地支撑所述至少一个反扭矩转子，所述驱动轴整流罩包括面向所述至少一个反扭矩转子的前缘，所述前缘至少部分地配备有相关联的声阻尼装置。

30. 发明申请

US20150153448A1 Rotor Blade with an Integrated Radar Absorber for a Wind Power Plant 审中-公开
标题翻译：具有用于风力发电厂的集成雷达吸收器的转子叶片
公开(公告)号：US20150153448A1
公开(公告)日：2015-06-04
申请号：US14559499
申请日：2014-12-03
申请人： EADS Deutschland GmbH
发明人： Joachim BETTERMANN , Andreas FRYE
IPC分类号： G01S13/88 , F03D1/06 , H01Q17/00 , F03D11/00
CPC分类号： G01S13/88 , F03D1/0675 , F03D80/00 , F03D80/10 , F05B2260/99 , F05B2280/6003 , F05B2280/6011 , F05B2280/6013 , F05C2253/04 , F05C2253/12 , F05C2253/16 , H01Q1/12 , H01Q17/00 , Y02E10/721 , Y02E10/722
摘要： A rotor blade comprising fiber-reinforced plastic for a wind power plant is provided with a radar absorber embedded into the fiber-reinforced plastic. The rotor blade includes a layer close to the surface with a defined electrical sheet resistivity of 100 to 800 ohm/square, which is located at a depth of 2 to 5 mm below the surface. The rotor blade also includes a layer far removed from the surface with a defined electrical sheet resistivity of at a maximum 50 ohm/square at a distance to the layer close to the surface of 5 to 16 mm. The integrated radar absorber covers one or several discrete surface sections of the rotor blade, without covering the entire surface of the rotor blade.
摘要翻译：包括用于风力发电厂的纤维增强塑料的转子叶片设置有嵌入到纤维增强塑料中的雷达吸收器。转子叶片包括靠近表面的层，其具有100至800欧姆/平方厘米的限定电阻率，其位于表面下方2至5mm的深度。转子叶片还包括远离表面的层，其具有最大50欧姆/平方厘米的距离与接近表面的层的距离为5至16mm的限定电阻率。集成雷达吸收器覆盖转子叶片的一个或多个离散的表面部分，而不覆盖转子叶片的整个表面。

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