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1. 发明授权

US09302623B2 Apparatus for mounting an object to a structure in a vibration-free manner 有权
标题翻译：用于以无振动的方式将物体安装到结构的装置
公开(公告)号：US09302623B2
公开(公告)日：2016-04-05
申请号：US13964251
申请日：2013-08-12
申请人： Deutsches Zentrum fur Luft- und Raumfahrt e.V.
发明人： Joerg Melcher , Bjoern Timo Kletz , Julian Redlich
IPC分类号： F16F1/34 , B60R1/076 , F16F7/104 , F16F15/02 , F16M13/02
CPC分类号： F16F15/022 , B60R1/06 , B60R1/076 , F16F7/104 , F16M13/02
摘要： The invention relates to a device for mounting an object to a structure in a vibration-free manner. The device has an elastic arrangement that supports the object at the structure in a stiff manner in the directions of at least two of the total of six translational and rotational degrees of freedom and in a soft manner in the directions of at least one of the total of six translational and rotational degrees of freedom. Main modes of motion of the object in the directions of the rigid support have natural frequencies that are higher than any main mode of motion of the object in any direction of the soft support at least by a factor of ten. The soft support is undamped, and a damping device is provided for any main mode of motion of the object in any direction of the soft support.
摘要翻译：本发明涉及一种用于以无振动的方式将物体安装到结构上的装置。该装置具有弹性布置，其在结构上以坚硬的方式在总共六个平移和旋转自由度中的至少两个方向上以柔性的方式在该结构中的至少一个的方向上支撑物体六个平移和旋转的自由度。物体在刚性支撑件的方向上的主要运动模式具有比软支撑件的任何方向上的物体的任何主要运动模式高至少十倍的固有频率。柔性支撑件是无阻尼的，并且为软件支撑件的任何方向上的物体的任何主要运动模式提供阻尼装置。

2. 发明授权

US09002660B2 Device and method for determining and indicating climate-relevant effects of a contrail produced by an airplane 有权
标题翻译：用于确定和指示由飞机产生的转盘的气候相关影响的装置和方法
公开(公告)号：US09002660B2
公开(公告)日：2015-04-07
申请号：US13393724
申请日：2010-09-09
申请人： Hermann Mannstein , Ulrich Schumann
发明人： Hermann Mannstein , Ulrich Schumann
IPC分类号： B64D45/00 , B64D47/08 , G01W1/08
CPC分类号： B64D45/00 , B64D47/08 , G01W1/08
摘要： The invention relates to a device and a method for determining and indicating, on board of an airplane, climate-relevant effects of a contrail produced by the airplane. The method for determining and indicating, on board of an airplane, climate-relevant effects of a contrail produced by the airplane includes determining radiation data of short-wave and long-wave atmospheric radiation directed upwards in the earth atmosphere at location of the airplane, determining an air temperature and air humidity at the location of the airplane, determining a zenith angle of the sun at the location of the airplane, determining a radiative forcing value produced by the contrail based on the determined radiation data, the air temperature and air humidity, and the zenith angle, and indicating at least one of the radiative forcing value and variables derived therefrom.
摘要翻译：本发明涉及一种用于在飞机上确定和指示由飞机产生的转盘的气候相关影响的装置和方法。用于确定和指示在飞机上的与飞机产生的转轨的气候相关影响的方法包括确定在飞机位置的地球大气中向上指向的短波和长波大气辐射的辐射数据，确定飞机位置处的空气温度和空气湿度，确定飞机位置处的太阳的天顶角，基于确定的辐射数据，空气温度和空气湿度确定由转盘产生的辐射强迫值和天顶角，并且指示辐射强迫值和从其导出的变量中的至少一个。

3. 发明授权

US08781265B2 Sensor, a system and a method for measuring forces and/or moments 失效
标题翻译：传感器，测量力和/或力矩的系统和方法
公开(公告)号：US08781265B2
公开(公告)日：2014-07-15
申请号：US13306341
申请日：2011-11-29
申请人： Robert Haslinger
发明人： Robert Haslinger
IPC分类号： G02B6/00
CPC分类号： G01B11/18 , G01B1/00 , G01D5/35303 , G01D5/35316 , G01L1/246 , G01L1/26
摘要： A sensor for measuring forces and/or moments on an object, including at least one sensor element for the detection of an expansion of the object in at least one spatial direction, from which expansion a force or a moment can be determined, wherein the sensor element including an optical fiber with a sensor region with a fiber Bragg grating is provided, and the fiber Bragg grating is adapted to be irradiated with light, preferably a broadband light, generating a reflected light having a peak wavelength. The optical fiber is formed by a fiber core and at least one sheath of light-guiding material surrounding the fiber core. The fiber Bragg grating is arranged in the fiber core. The material of the sheath is doped with a fluorescent material and the fluorescent material may be irradiated with an excitation radiation to generate a fluorescent radiation having at least one main emission wavelength.
摘要翻译：一种用于测量物体上的力和/或力矩的传感器，包括用于在至少一个空间方向上检测物体的膨胀的至少一个传感器元件，从该位置可以确定力或力矩的膨胀，其中传感器提供了包括具有光纤布拉格光栅的传感器区域的光纤的元件，并且光纤布拉格光栅适于用光（优选宽带光）照射，产生具有峰值波长的反射光。光纤由纤维芯和围绕纤维芯的光导材料的至少一个护套形成。光纤布拉格光栅布置在光纤芯中。鞘的材料掺杂有荧光材料，并且荧光材料可以用激发辐射照射以产生具有至少一个主发射波长的荧光辐射。

4. 发明申请

US20140146996A1 Device and Method for the Processing of Remote Sensing Data 有权
标题翻译：遥感数据处理装置及方法
公开(公告)号：US20140146996A1
公开(公告)日：2014-05-29
申请号：US14092162
申请日：2013-11-27
申请人： Deutsches Zentrum fur Luft-und Raumfahrt e.V.
发明人： Hans-Hermann Vajen
IPC分类号： G06T5/00
CPC分类号： G06T5/002 , G06K9/0063 , G06K9/6289 , G06T5/20 , G06T5/50 , G06T2207/10032 , G06T2207/20012 , G06T2207/20212 , G06T2207/30181
摘要： The processing of remote sensing data, wherein first image data are processed with the use of second digital image data which, compared with the first image data, have a finer local resolution. The local resolution of the first digital image data is refined temporarily. The local resolution and every pixel of the temporarily refined first image data corresponds to the local resolution and each pixel of the second digital image data. Determining a weighting value for the pixels of the second digital image data which corresponds to a weighting of a image value of the pixel in the ratio of the image value of the pixel to image values of surrounding pixels. A smoothing of the local plot of the image values in the area of the pixel and its environment is implemented such that the weighting value of larger values is based on additional smoothing of image values.
摘要翻译：遥感数据的处理，其中使用与第一图像数据相比较的第二数字图像数据处理第一图像数据具有更精细的局部分辨率。第一数字图像数据的局部分辨率被临时提炼。临时精细化的第一图像数据的局部分辨率和每个像素对应于局部分辨率和第二数字图像数据的每个像素。确定第二数字图像数据的像素的加权值，其对应于像素的图像值与周围像素的图像值的比率的加权。实现像素及其环境的区域中的图像值的局部曲线的平滑化，使得较大值的加权值基于图像值的附加平滑。

5. 发明申请

US20140100776A1 METHOD FOR DETERMINING THE POSITION OF MOVING OBJECTS 有权
标题翻译：确定移动物体位置的方法
公开(公告)号：US20140100776A1
公开(公告)日：2014-04-10
申请号：US14119347
申请日：2012-05-08
申请人： Susanna Kaiser , Mohammed Khider , Patrick Robertson
发明人： Susanna Kaiser , Mohammed Khider , Patrick Robertson
IPC分类号： G01C21/00 , G01C21/20
CPC分类号： G01C21/00 , G01C21/005 , G01C21/16 , G01C21/206
摘要： Method for determining the position of moving objects, wherein the object has a sensor or an apparatus for determining odometry data, having the steps of: transmitting the odometry data to a calculation device, estimating the location and position of the object with the aid of the calculation device, creating a diffusion matrix on the basis of the estimated location and position taking into account environmental data, determining a contour line on the basis of the diffusion matrix, determining the distances between the position and the contour line for different orientations, in particular each orientation, and calculating a probability density function on the basis of the distances determined.
摘要翻译：用于确定移动物体的位置的方法，其中所述物体具有用于确定测距数据的传感器或装置，具有以下步骤：将测距数据传输到计算装置，借助于所述方法估计物体的位置和位置计算装置，基于考虑到环境数据的估计位置和位置创建扩散矩阵，基于扩散矩阵确定轮廓线，确定用于不同取向的位置和轮廓线之间的距离，特别是并根据确定的距离计算概率密度函数。

6. 发明授权

US08593165B2 Solar generator 有权
标题翻译：太阳能发电机
公开(公告)号：US08593165B2
公开(公告)日：2013-11-26
申请号：US13735725
申请日：2013-01-07
申请人： Deutsches Zentrum für Luft-und Raumfahrt e.V.
发明人： Waldemar Bauer , Oliver Romberg
IPC分类号： G01R31/26
CPC分类号： G01R31/2605 , B64G1/44 , B64G1/56
摘要： A solar generator for spacecraft or satellites, including a solar panel, a detector layer, a first evaluation means and a second evaluation means. The solar panel includes a plurality of solar cells. The detector layer includes first conductors substantially in parallel in a first plane and second conductors substantially in parallel in a second plane. The second plane is substantially in parallel to the first plane such that the first conductors are at an angle to the second conductors. The first evaluation means is for detecting a failure of one or more of the plurality of solar cells. The second evaluation means is for testing electrical status of the first conductors and the second conductors to determine whether the failure detected by the first evaluation means was caused by a space object damaging or severing one or more of the first conductors and the second conductors.
摘要翻译：一种用于航天器或卫星的太阳能发电机，包括太阳能电池板，检测器层，第一评估装置和第二评估装置。太阳能电池板包括多个太阳能电池。检测器层包括在第一平面中基本平行的第一导体和在第二平面中基本平行的第二导体。第二平面基本上平行于第一平面，使得第一导体与第二导体成一定角度。第一评估装置用于检测多个太阳能电池中的一个或多个的故障。第二评估装置用于测试第一导体和第二导体的电气状态，以确定由第一评估装置检测到的故障是否由损坏或切断一个或多个第一导体和第二导体的空间物体引起。

7. 发明授权

US08438462B2 Method for recovery of lost and/or corrupted data 有权
标题翻译：恢复丢失和/或损坏的数据的方法
公开(公告)号：US08438462B2
公开(公告)日：2013-05-07
申请号：US12848495
申请日：2010-08-02
申请人： Gianluigi Liva
发明人： Gianluigi Liva
IPC分类号： H03M13/03
CPC分类号： H04L1/0059 , H03M13/09 , H03M13/1154 , H03M13/373 , H04L1/0045
摘要： A method for recovery of lost and/or corrupted data, whereby this data is encoded by means of an encoder connected to the transmitter device and transmitted via a transmission channel to the receiver device. The transmitted data is decoded by means of a decoder connected to the receiver device wherein lost and/or corrupted data is restored during decoding. Encoding and decoding are performed by using a convolutional code. According to the disclosure the window size, on which the decoder connected to the receiver device operates, is variable so that the window size can be adapted to the erasure rate of the transmission channel and/or to the delay service requirement.
摘要翻译：一种用于恢复丢失和/或损坏的数据的方法，由此该数据通过连接到发射机设备并通过传输信道传输到接收机设备的编码器进行编码。传输的数据通过连接到接收机设备的解码器进行解码，其中在解码期间丢失和/或损坏的数据被恢复。通过使用卷积码来执行编码和解码。根据该公开，连接到接收机设备的解码器工作的窗口大小是可变的，使得窗口大小可以适应于传输信道的擦除率和/或延迟服务需求。

8. 发明申请

US20130000877A1 HEAT TRANSFER TUBE 审中-公开
标题翻译：传热管
公开(公告)号：US20130000877A1
公开(公告)日：2013-01-03
申请号：US13515153
申请日：2010-07-06
申请人： Thomas Bauer , Bernd Hachmann
发明人： Thomas Bauer , Bernd Hachmann
IPC分类号： F28F1/00
CPC分类号： F28F1/20 , F28D20/02 , F28D2020/0004 , F28F2215/10 , F28F2255/16 , Y02E60/145
摘要： The present invention relates to a heat transfer pipe comprising a pipe element and a number of ribs arranged around the outer circumference of the pipe element and extending outwards, annular segments being formed encompassing the ribs on the pipe element and fastened to one another with a spring-elastic clamping device, in particular on two annular segments respectively forming a half shell.
摘要翻译：传热管本发明涉及一种传热管，其包括一管道元件和多个排列在管元件的外圆周周围并向外延伸的肋，环形区段形成为包围管元件上的肋，并用弹簧特别是在分别形成半壳的两个环形段上。

9. 发明授权

US08246345B2 Burner 有权
标题翻译：刻录机
公开(公告)号：US08246345B2
公开(公告)日：2012-08-21
申请号：US12672158
申请日：2008-07-24
申请人： Harald Schütz , Guido Schmitz
发明人： Harald Schütz , Guido Schmitz
IPC分类号： F23M9/00
CPC分类号： F23R3/286 , F23D14/64 , F23D2203/007
摘要： A burner having an inlet (10) and a mixing path (20) is designed such that the inlet (10) has a rectangular cross section. The mixing path (20) adjacent thereto has a round cross section and a larger diameter, thus forming four transitional steps (25). The transitional steps (25) form four secondary vortices, thus improving the distribution of the fuel in the radial direction. The burner provides combustion with low emission of hazardous substances, and with low emission of nitrogen oxides.
摘要翻译：具有入口（10）和混合路径（20）的燃烧器被设计成使得入口（10）具有矩形横截面。与其相邻的混合路径（20）具有圆形横截面和较大直径，从而形成四个过渡步骤（25）。过渡步骤（25）形成四个次级涡流，从而改善燃料在径向方向上的分布。燃烧器提供低排放有害物质的燃烧，并且氮氧化物排放量低。

10. 发明申请

US20120092212A1 METHOD AND RECEIVER FOR RECEIVING AND PROCESSING ALTBOC-MODULATED SATELLITE NAVIGATION SIGNALS 有权
标题翻译：接收和处理ALTBOC调制卫星导航信号的方法和接收机
公开(公告)号：US20120092212A1
公开(公告)日：2012-04-19
申请号：US13322099
申请日：2010-05-25
申请人： Michael Meurer , Manuel Cuntz
发明人： Michael Meurer , Manuel Cuntz
IPC分类号： G01S19/23
CPC分类号： G01S19/23 , G01S19/33 , G01S19/36
摘要： AltBOC-modulated satellite navigation signals transmitted in the two partial bands E5a and E5b of the so-called E5 frequency band are received using a common antenna (19) and thereafter are processed separately in an analog manner in the HF front-end in two physically different incoming signal paths for the two partial bands and then digitized and coherently summed to form a complete digital E5 band signal, which is fed to a digital signal processor, in which code acquisition and code tracking are performed using PRN reference code sequences produced in the receiver and tracking of the carrier phase is performed and raw data for the final navigation calculation are determined therefrom. From the PRN reference code sequences produced in the receiver, a PRN code calibration signal is produced, which is up-converted to the carrier frequency and then coupled into the HF front-end as a pseudo satellite navigation signal by means of a directional coupler (20) directly after the antenna, which pseudo satellite navigation signal is also tracked in the digital signal processor as an addition signal, which makes it possible to calibrate the HF front-end for the two partial bands during the normal satellite navigation signal reception.For application with Galileo satellite navigation receivers.
摘要翻译：在所谓的E5频带的两个部分频带E5a和E5b中发送的AltBOC调制的卫星导航信号使用公共天线（19）接收，然后在HF前端以模拟方式在两个物理上分别处理用于两个部分频带的不同输入信号路径，然后被数字化和相干相加以形成完整的数字E5频带信号，其被馈送到数字信号处理器，其中使用在所述数字信号处理器中产生的PRN参考码序列来执行代码获取和代码跟踪执行载波相位的接收机和跟踪，并由此确定用于最终导航计算的原始数据。根据在接收机中产生的PRN参考码序列，产生PRN码校准信号，其被上转换为载波频率，然后通过定向耦合器（作为伪卫星导航信号）耦合到HF前端 20）直接在天线之后，哪个伪卫星导航信号也作为附加信号在数字信号处理器中跟踪，这使得可以在通常的卫星导航信号接收期间校准两个部分频带的HF前端。适用于伽利略卫星导航接收机。

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