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    • 5. 发明申请
    • LIGHTER-THAN-AIR FLYING CRAFT AND METHOD FOR COUNTERBALANCING THE FLYING CRAFT AND FOR SETTING DOWN A LOAD FASTENED TO THE SAME
    • 轻于AIR FLIGHT装置和方法,用于平衡飞行设备,并采取附加的这个最后的
    • WO0073141A3
    • 2002-09-26
    • PCT/EP0004709
    • 2000-05-24
    • UTI HOLDING & MAN AGKNAUER BERTHOLDHOFFMANN BERND
    • KNAUER BERTHOLDHOFFMANN BERND
    • B64B1/02B64B1/22B66C13/08B66F19/00
    • B64B1/22B64B1/02B66C13/08B66F19/00
    • The invention relates to a lighter-than-air flying craft comprising a multitude of ballast tanks (122, 123) and a load hoisting device (125) which can be lowered and which is provided for setting a load (L) fastened in a loading bay (102) on the ground. The inventive craft also comprises a stabilizer (150) and rudder assemblies connected to the craft. A steering system (120) with steering axes (X, Y, Z) is provided for steering the flying craft (100), whereby the flying craft (100) can be positioned in every axis (X, Y, Z) by a rudder deflection ( delta R) of the rudder assembly effected by the steering system (120). Damping elements (10) are also provided in the flying craft (100) in order to reduce arising vibrations to a level that is adequate for conducting a safe flying operation. The flying craft is characterized in that the rudder deflection ( delta R) can be modulated with a control pulse ( DELTA delta R) which comprises an additional rudder deflection with a dampening effect, and in that the load hoisting device (125) is configured such that it can be displaced along a longitudinal direction and/or a transversal direction of the loading bay (102) so that a load (L) can be set down from the air at a precise set-down point. The invention also relates to a method for counterbalancing the position of the lighter-than-air flying craft when setting down a load and additionally relates to a method for setting a load fastened to the lighter-than-air flying craft down on the ground.
    • 本发明涉及一种轻于空气飞行器,其包括用于在地面上的装载托架上沉积(102)固定负载(L)的多个压载舱的(122,123)和一个可降低的载荷提升设备(125),具有其上 附着尾部(150)和舵装置,具有与所述控制轴(X,Y,Z),用于控制所述飞行器(100),由所述控制装置的一个舵装置(120)舵(△R)的控制装置(120) 在各轴(X,Y,Z)飞行装置(100)可以被定位,并且阻尼元件(10)被提供在飞行装置(100),以减少对一个适当存在的安全飞行操作电平的振动。 飞机的特征在于,所述舵(△R)的控制脉冲(DELTA增量R)能够被调制,其包括用汽蒸效果的附加控制表面,并沿着装载托架的纵向方向和/或横向方向上的负载提升装置(125)( 102)被设计为可移动,以便从空气中上了一个活动的点负载(L)是完全扣除。 本发明还涉及到用于放置负载时平衡轻于空气飞行器的位置的方法。 本发明进一步提供用于沉积附着到轻于空气飞行器负载向地面的方法。
    • 6. 发明申请
    • METHOD OF DETECTION OF CLASSICAL SWINE FEVER
    • 检测经典开关的方法
    • WO2006086377A3
    • 2009-05-22
    • PCT/US2006004271
    • 2006-02-08
    • IDEXX LABHOFFMANN BERNDDEPNER KLAUSBEER MARTIN
    • HOFFMANN BERNDDEPNER KLAUSBEER MARTIN
    • C12Q1/68C07H21/02C07H21/04C12P19/34
    • C12Q1/70
    • The invention relates to a multiplex real-time RT-PCR assay with a heterologous internal control system (i.e., EGFP-RNA) for the simple and fast diagnosis of classical swine fever virus (CSFV). Primers and FAM-labeled TaqMan probes, specific for CSFV were selected by analyzing the consensus sequence of the 5 '-non translated region of various CSFV strains. For determining the analytical sensitivity an in vitro transcript (T7-PC3Alf) of the 5' NTR was constructed and tested. Furthermore, a primer - probe system for the detection of the internal control sequence was established, and a multiplex assay using CSF-System 1 and the IC real-time PCR could be performed as a one-tube assay without loss of sensitivity or specificity.
    • 本发明涉及用于简单和快速诊断典型猪瘟病毒(CSFV)的异源内部对照系统(即EGFP-RNA)的多重实时RT-PCR测定。 通过分析各种CSFV毒株5'非翻译区的共有序列,选择引物和FAM标记的TaqMan探针,对CSFV特异性。 为了确定分析灵敏度,构建并测试了5'NTR的体外转录物(T7-PC3Alf)。 此外,建立了用于检测内部控制序列的引物 - 探针系统,使用CSF-System 1和IC实时PCR的多重测定可以作为单管测定进行,而不损失敏感性或特异性。