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    • 1. 发明授权
    • Relationship prediction system using external databases
    • 使用外部数据库的关系预测系统
    • US08144007B2
    • 2012-03-27
    • US12799210
    • 2010-04-19
    • Edward F. TuckAnn Tuck BadenThomas N. Giaccherini
    • Edward F. TuckAnn Tuck BadenThomas N. Giaccherini
    • G08B1/08
    • G01S13/74G01N33/56977G06F19/18G06Q30/02G06Q30/0277G06Q50/01G08B2001/085G16H50/30
    • A Relationship Prediction System Using External Databases for providing a relationship prediction based on the correlation of personal characteristics and the analysis of genetic characteristics is disclosed. In one embodiment, a first person supplies descriptions of their own personal characteristics, as well as descriptions of the personal characteristics of their ideal match, to a website. The first person also furnishes an odor, tissue or fluid sample to a test facility, where genetic characteristics are analyzed and determined. A relationship match is then generated based on both a combination of both a positive correlation of the personal characteristics of the first person and second person, and a measured dissimilarity between the sequence of genetic characteristics of the first person and second person. In one embodiment, personal characteristics are obtained from one or more external webpages.
    • 公开了使用外部数据库的关系预测系统,用于基于个人特征的相关性和遗传特征的分析来提供关系预测。 在一个实施例中,第一人向网站提供他们自己的个人特征的描述以及他们理想的匹配的个人特征的描述。 第一人还向测试设施提供气味,组织或流体样品,其中分析和确定遗传特征。 然后基于第一人和第二人的个人特征的正相关性和第一人与第二人的遗传特征序列之间的测量的不相似性的组合,生成关系匹配。 在一个实施例中,从一个或多个外部网页获得个人特征。
    • 9. 发明申请
    • IN ORBIT SPACE TRANSPORTATION & RECOVERY SYSTEM
    • 在ORBIT空间运输和恢复系统
    • US20080296436A1
    • 2008-12-04
    • US11651727
    • 2007-01-10
    • Robert F. D'AusilioJames R. StuartThomas N. GiaccheriniFranklin H. Williams, JR.
    • Robert F. D'AusilioJames R. StuartThomas N. GiaccheriniFranklin H. Williams, JR.
    • B64G1/40
    • B64G1/007B64G1/1078B64G1/408B64G1/422B64G1/54B64G1/646
    • An In Orbit Transportation & Recovery System (IOSTAR™) (10) is disclosed. One preferred embodiment of the present invention comprises a space tug powered by a nuclear reactor (19). The IOSTAR™ includes a collapsible boom(11) connected at one end to a propellant tank (13) which stores fuel for an electric propulsion system (12). This end of the boom (11) is equipped with docking hardware (14) that is able to grasp and hold a satellite (15) and as a means to refill the tank (13). Radiator panels (16) mounted on the boom (11) dissipate heat from the reactor (19). A radiation shield (20) is situated next to the reactor (19) to protect the satellite payload (15) at the far end of the boom (11). The IOSTAR™ (10) will be capable of accomplishing rendezvous and docking maneuvers which will enable it to move spacecraft between a low Earth parking orbit and positions in higher orbits or to other locations in our Solar System.
    • 公开了轨道运输和恢复系统(IOSTAR(TM))(10)。 本发明的一个优选实施例包括由核反应堆(19)供电的空间拖船。 IOSTAR TM包括在一端连接到储存用于电力推进系统(12)的燃料的推进剂罐(13)的可折叠起重臂(11)。 起重臂(11)的这一端配备有能够把持和固定卫星(15)的对接硬件(14),并且作为重新装满水箱(13)的装置。 安装在起重臂(11)上的散热器面板(16)从反应器(19)散热。 辐射屏蔽(20)位于反应器(19)旁边,以保护在悬臂(11)的远端处的卫星有效载荷(15)。 IOSTAR(TM)(10)将能够实现会合和对接机动,这将使其能够在低地球停放轨道和较高轨道位置或太阳系中其他位置之间移动航天器。