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    LOCKING FASTENING DEVICE, ADJUSTABLE FASTENING DEVICE, COMPONENT SYSTEM, MAIN WING OF A WIND TUNNEL MODEL AIRCRAFT, AND WIND TUNNEL MODEL AIRCRAFT HAVING SUCH A MAIN WING
    4.
    发明申请
    LOCKING FASTENING DEVICE, ADJUSTABLE FASTENING DEVICE, COMPONENT SYSTEM, MAIN WING OF A WIND TUNNEL MODEL AIRCRAFT, AND WIND TUNNEL MODEL AIRCRAFT HAVING SUCH A MAIN WING 失效
    锁定紧固装置，可调节紧固装置，组件系统，风力发电机模型飞机的主要风力，以及具有这种主要功能的风力隧道模型飞机

    公开(公告)号：US20120138747A1

    公开(公告)日：2012-06-07

    申请号：US13309905

    申请日：2011-12-02

    申请人： Michael Binder

    发明人： Michael Binder

    IPC分类号： B64C1/26 ,  F16B39/00 ,  F16B39/12 ,  F16B33/00

    CPC分类号： G01M9/04 ,  F16B5/0233 ,  F16B5/0283 ,  F16B7/025 ,  F16B9/026 ,  G01M9/08

    摘要： A locking fastening device for fastening a first component to a second component, an adjustable fastening device for adjustably fastening a first component to a second component, and a component system including at least one first component that is fastened to a second component are described. Also described are a main wing of a wind tunnel model aircraft having an adjusting and fastening system which includes at least one locking fastening device and at least two adjustable fastening devices for adjusting and fastening an aerodynamic additional body that is adjustable relative to the main wing by means of a plurality of retaining devices, as well as a wind tunnel model aircraft having such a main wing.

    摘要翻译： 描述了用于将第一部件紧固到第二部件的锁定紧固装置，用于将第一部件可调节地紧固到第二部件的可调紧固装置，以及包括紧固到第二部件的至少一个第一部件的部件系统。 还描述了具有调节和紧固系统的风洞模型飞行器的主翼，该系统包括至少一个锁定紧固装置和至少两个可调节的紧固装置，用于调节和紧固相对于主翼可调节的空气动力学附加体， 多个保持装置的装置，以及具有这种主翼的风洞模型飞机。

    APPARATUS FOR THE PIVOTAL FASTENING OF AN ACTIVE SURFACE, IN PARTICULAR A SPOILER ON A WIND TUNNEL MODEL OF AN AIRCRAFT
    6.
    发明申请
    APPARATUS FOR THE PIVOTAL FASTENING OF AN ACTIVE SURFACE, IN PARTICULAR A SPOILER ON A WIND TUNNEL MODEL OF AN AIRCRAFT 有权
    用于航空器风力发电机模型的特殊功能的主动表面的装置

    公开(公告)号：US20090166475A1

    公开(公告)日：2009-07-02

    申请号：US12343756

    申请日：2008-12-24

    申请人： Michael BINDER

    发明人： Michael BINDER

    IPC分类号： B64C1/06

    CPC分类号： B64C9/32 ,  B64C9/02 ,  G01M9/04 ,  Y10T403/18 ,  Y10T403/32442 ,  Y10T403/32451

    摘要： An apparatus (1) for pivotal fastening of an active surface, in particular a spoiler (3) on a wind tunnel model of an aircraft, comprising a bearing block (2) and a strip (22) accommodated pivotally thereon on a shaft (21), wherein the strip (22) is connected to the active surface, characterized in that the strip (22) is operatively connected to a clamping block (10) and the clamping block (10) can be connected to the bearing block (2) for locking the active surface in an arbitrary angular position (28, 29) of the spoiler (3) between −10° and +45°. Since the operative connection is preferably formed with a ring gear segment (23) disposed underneath the strip (22), which is continuously intermeshed with a rack (19) formed on the clamping block (10), a highly precise adjustment of the angular position (28, 29) of the spoiler (3) is possible. An angular position (28, 29), once set, can be locked very securely against uncontrolled adjustments by fixing the clamping block (10) in the bearing block (2) by means of at least two fastening means, in particular with screws. The lack of sensitivity to undesirable adjustment movements of the spoiler (3) is obtained in particular from the self-inhibiting configuration of the toothing. As a result of the comprehensive adjustability of the apparatus (1), a comprehensive storage of aerodynamic active surfaces with individual adjustment angles is superfluous and at the same time, the retrofitting expenditure is reduced.

    摘要翻译： 一种用于枢转地紧固飞机的风洞模型上的活动表面，特别是扰流器（3）的装置（1），包括轴承座（2）和在轴（21）上枢转地容纳在其上的条带 ），其中所述带（22）连接到所述有源表面，其特征在于，所述带（22）可操作地连接到夹紧块（10），并且所述夹紧块（10）可以连接到所述轴承座（2） 用于将所述主动表面锁定在所述扰流板（3）的任意角度位置（28,29）之间-10°至+ 45°之间。 由于操作连接优选地形成有与形成在夹紧块（10）上的齿条（19）连续啮合的条带（22）下方的环形齿轮段（23），所以高度精确地调整角位置 （3）的（28,29）是可能的。 通过至少两个紧固装置，特别是用螺钉将夹紧块（10）固定在轴承座（2）中，可以非常牢固地锁定角度位置（28,29），以防止不受控制的调节。 对扰流器（3）的不期望的调节运动的敏感性的缺乏特别是从齿的自抑制构造获得。 由于设备（1）的综合调整性，具有各种调节角度的空气动力学活动面的综合存储是多余的，同时减少了改装费用。

    Nucleotide sequences which code for the rpsL gene
    9.
    发明授权
    Nucleotide sequences which code for the rpsL gene 有权
    编码rpsL基因的核苷酸序列

    公开(公告)号：US06939695B2

    公开(公告)日：2005-09-06

    申请号：US10075460

    申请日：2002-02-15

    申请人： Bettina Moeckel ,  Brigitte Bathe ,  Stefan Hans ,  Caroline Kreutzer ,  Thomas Hermann ,  Walter Pfefferle ,  Michael Binder

    发明人： Bettina Moeckel ,  Brigitte Bathe ,  Stefan Hans ,  Caroline Kreutzer ,  Thomas Hermann ,  Walter Pfefferle ,  Michael Binder

    IPC分类号： C07K14/34 ,  C12N15/31 ,  C12P13/04 ,  C07H21/04

    CPC分类号： C07K14/34

    摘要： An isolated polynucleotide comprising a polynucleotide sequence chosen from the group consisting of a) polynucleotide which is identical to the extent of at least 70% to a polynucleotide which codes for a polypeptide which comprises the amino acid sequence of SEQ ID No. 2, b) polynucleotide which codes for a polypeptide which comprises an amino acid sequence which is identical to the extent of at least 70% to the amino acid sequence of SEQ ID No. 2, c) polynucleotide which is complementary to the polynucleotides of a) or b), and d) polynucleotide comprising at least 15 successive nucleotides of the polynucleotide sequence of a), b) or c), and a process for the fermentative preparation of L-amino acids using coryneform bacteria in which at least the rpsL gene is present in enhanced form, as well as the use of polynucleotides which comprise the sequences according to the invention as hybridization probes.

    摘要翻译： 一种分离的多核苷酸，其包含选自以下的多核苷酸序列：a）与编码包含SEQ ID No.2的氨基酸序列的多肽的多核苷酸的程度相同的多核苷酸，b） 编码多肽的多核苷酸，其包含与SEQ ID No.2的氨基酸序列至少70％相同的氨基酸序列，c）与a）或b）的多核苷酸互补的多核苷酸， 和d）包含a），b）或c）的多核苷酸序列的至少15个连续核苷酸的多核苷酸，以及使用棒状细菌发酵制备L-氨基酸的方法，其中至少存在rpsL基因 增强形式，以及使用包含根据本发明的序列的多核苷酸作为杂交探针。