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    • 1. 发明授权
    • Process for the highly specific detection of nucleic acids in solid
    • 在溶液中高度特异性检测核酸的方法
    • US5354657A
    • 1994-10-11
    • US993820
    • 1992-12-18
    • Hans J. HoltkeRudolf SeiblChristoph KesslerRalf MattesHermann Graf
    • Hans J. HoltkeRudolf SeiblChristoph KesslerRalf MattesHermann Graf
    • C07H21/00C12Q1/68C07H21/04C12N15/00
    • C07H21/00C12Q1/6804
    • The present invention provides a process for the detection of nucleic acids of definite sequence by hybridisation with two single-stranded nucleic acid probes present in the same solution phase complementary to different regions of the nucleic acid to be detected, one nucleic acid probe serving as detector probe and containing as labelling at least one hapten bound via a chemical linkage and the other nucleic acid probe serving as capturing probe and being bound to a solid matrix, wherein, as hapten, a steroid is used which on at least one position of the detector probe, which does not participate in the hydrogen bridge formation with the nucleic acid to be detected, is covalently bound via a bridge of at least four atoms, the nucleic acid to be detected, present in solution, is incubated with the detector probe and the capturing probe in any desired sequence, whereby the binding of the capturing probe on the matrix with the nucleic acid to be detected is brought about before, during or after the incubation, the remaining solution is separated off from the matrix-bound complex of the capturing probe, nucleic acid to be detected and detector probe and the complex detected via an anti-hapten antibody which is labelled.
    • 本发明提供了通过与存在于​​与要检测的核酸的不同区域互补的相同溶液相中的两个单链核酸探针杂交来检测确定序列的核酸的方法,一个用作检测器的核酸探针 探针并包含作为标记至少一个通过化学连接结合的半抗原,并且另一个核酸探针用作捕获探针并结合到固体基质上,其中作为半抗原,使用类固醇,其在检测器的至少一个位置上 不参与与要检测的核酸的氢桥形成的探针通过至少四个原子的桥共价结合,将存在于溶液中的要检测的核酸与检测器探针和 以任何期望的顺序捕获探针,由此捕获探针在基质上与待检测的核酸的结合在 r后,将剩余的溶液与捕获探针的基质结合复合物,待检测的核酸和检测器探针分离,并通过经标记的抗半抗原抗体检测复合物。
    • 8. 发明授权
    • Stabilizer
    • 稳定剂
    • US08622336B2
    • 2014-01-07
    • US13150790
    • 2011-06-01
    • Hanno BrennerChristoph KesslerWolfgang Kreitmair-Steck
    • Hanno BrennerChristoph KesslerWolfgang Kreitmair-Steck
    • B64C11/00
    • B64D1/22B64C27/04
    • A rotary aircraft which carries a hanging sling load on at least one support cable, benefits from a stabilizer which generates control signals R to be applied or modulated onto the flight control of the aircraft. At least one sling load pendulum motion detecting unit provides the stabilizer with data on the pendulum motion of the sling load. Additionally, the stabilizer is set up with a working range determination unit S3 for determining the space where free movement is possible in which the rotary aircraft with sling load can move without collision. The stabilizer generates control signals R in dependency of the determined pendulum motion of the sling load and the determined working range.
    • 在至少一个支撑电缆上承载吊吊负载的旋转飞机受益于产生要应用或调制到飞行器的飞行控制上的控制信号R的稳定器。 至少一个吊装载荷摆动运动检测单元为吊具提供有关吊索载荷的摆动运动的数据。 此外,稳定器设置有工作范围确定单元S3,用于确定具有悬挂载荷的旋转飞行器可以在没有碰撞的情况下移动的空间。 稳定器根据确定的吊架载荷的摆动和所确定的作业范围产生控制信号R.
    • 9. 发明授权
    • Helicopter rotor control system with individual blade control
    • 直升机转子控制系统,具有独立的叶片控制
    • US08201771B2
    • 2012-06-19
    • US12986664
    • 2011-01-07
    • Christoph KesslerDaniel Furst
    • Christoph KesslerDaniel Furst
    • B64C27/54
    • B64C27/001B64C2027/7216Y02T50/34
    • A method of controlling rotor pitch in a helicopter comprising the steps of: generating at least one blade dynamics signal representing at least one dynamic force acting on at least one of a rotor blade rotating assembly and a helicopter non-rotating assembly, the rotor blade rotating assembly including a plurality of rotor blades and a pitch actuator for each rotor blade; extracting information representing the at least one dynamic force; generating a dynamic force compensation output representing a compensation for at least a portion of the at least one dynamic force; receiving flight control signals directing flight of the helicopter from flight controls of the helicopter; generating from the flight control signals and the dynamic force compensation output a compensated pitch control signal for each blade of the rotor blade rotating assembly, and providing a compensated pitch control signal to compensate for a portion of the at least one dynamic force.
    • 一种在直升机中控制转子节距的方法,包括以下步骤:产生至少一个叶片动力学信号,其表示作用于至少一个转子叶片旋转组件和直升机非旋转组件中的至少一个的动力,转子叶片旋转 组件包括多个转子叶片和每个转子叶片的俯仰致动器; 提取表示所述至少一个动态力的信息; 产生表示对所述至少一个动态力的至少一部分的补偿的动态力补偿输出; 接收飞行控制信号,指挥直升机飞行从直升机的飞行控制; 从飞行控制信号产生并且动态力补偿输出用于转子叶片旋转组件的每个叶片的补偿俯仰控制信号,以及提供经补偿的桨距控制信号以补偿至少一个动态力的一部分。