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    ANALYSIS METHOD
    1.
    发明申请
    ANALYSIS METHOD 审中-公开
    分析方法

    公开(公告)号：WO2011030100A2

    公开(公告)日：2011-03-17

    申请号：PCT/GB2010001700

    申请日：2010-09-08

    申请人： LIVERPOOL JOHN MOORES UNIVERSITY ,  HAGGERTY JOHN ,  LAMB DAVID ,  JONES DAVID LLEWELLY

    发明人： HAGGERTY JOHN ,  LAMB DAVID ,  JONES DAVID LLEWELLY

    IPC分类号： G06Q10/00

    CPC分类号： G06T11/20 ,  G06Q10/107 ,  H04L51/00 ,  H04L67/22

    摘要： A computer implemented method for analysing communication between a plurality of individuals. The method comprises reading data representing communications involving a first individual from a data store. A network of the communications between the first individual and a plurality of other individuals is displayed. In the displayed network, each individual is represented by a node and communication between individuals is represented by a link between nodes.

    摘要翻译： 一种用于分析多个人之间的通信的计算机实现的方法。 该方法包括从数据存储器读取表示涉及第一个体的通信的数据。 显示第一个人和多个其他个人之间的通信的网络。 在所显示的网络中，每个个体由节点表示，并且个体之间的通信由节点之间的链接表示。

    METHOD AND ARRANGEMENT FOR AIRCRAFT FUEL DISPERSION
    3.
    发明申请
    METHOD AND ARRANGEMENT FOR AIRCRAFT FUEL DISPERSION 审中-公开
    用于飞机燃料分配的方法和装置

    公开(公告)号：WO2007008185A2

    公开(公告)日：2007-01-18

    申请号：PCT/US2004/043618

    申请日：2004-12-29

    申请人： GULFSTREAM AEROSPACE CORPORATION ,  WOZNIAK, Gregg ,  LAMB, David ,  LE, Dung

    发明人： WOZNIAK, Gregg ,  LAMB, David ,  LE, Dung

    IPC分类号： B64D37/00

    CPC分类号： B64C17/10 ,  B64D37/00

    摘要： Method and arrangement for dispersing fuel (62) within a fuel containment system (60) of an aircraft (30) including utilizing a fuel containment system on an aircraft that is located at least partially within a wing (34) of the aircraft and defines a reservoir portion (42) and a remote portion (44). Fuel is pumped during aircraft flight from the reservoir portion to the remote portion at a pumped rate (80), while simultaneously fuel that is contained in the remote portion of the fuel containment system is permitted to drain to the reservoir portion at a drainage rate (82). The drainage rate is less than the pumped rate. A fuel mass (64) is accumulated in the remote portion of the fuel containment system because of a difference between the pumped rate and the drainage rate and as a result, a counteractive moment (49) is induced in the aircraft that is opposingly directed to a lift moment (46) caused by wing-lift (45) during aircraft flight.

    摘要翻译： 将燃料（62）分散在飞行器（30）的燃料容纳系统（60）内的方法和装置，包括在至少部分位于飞机的翼（34）内的飞机上使用燃料密封系统，并且限定 储存器部分（42）和远端部分（44）。 在飞行器飞行期间以泵送速率（80）从储存部分向远程部分泵送燃料，同时燃料容纳系统的偏远部分中容纳的燃料以排水速率排放到储存器部分 82）。 排水率小于抽水率。 由于泵送速率和排水速率之间的差异，燃料箱（64）积聚在燃料容纳系统的远端部分，结果是在相对地指向的飞行器中引起了反作用力矩（49） 在飞机飞行期间由机翼提升（45）引起的升力时刻（46）。

    ANALYSIS OF COMMUNICATIONS IN A SOCIAL NETWORK
    4.
    发明申请
    ANALYSIS OF COMMUNICATIONS IN A SOCIAL NETWORK 审中-公开
    社交网络中的交流分析

    公开(公告)号：WO2011030100A3

    公开(公告)日：2011-03-17

    申请号：PCT/GB2010/001700

    申请日：2010-09-08

    申请人： LIVERPOOL JOHN MOORES UNIVERSITY ,  HAGGERTY, John ,  LAMB, David ,  JONES, David, Llewelly

    发明人： HAGGERTY, John ,  LAMB, David ,  JONES, David, Llewelly

    IPC分类号： G06Q10/00 ,  G06Q30/00

    摘要： A computer implemented method for analysing communication between a plurality of individuals. The method comprises reading data representing communications involving a first individual from a data store. A network of the communications between the first individual and a plurality of other individuals is displayed. In the displayed network, each individual is represented by a node and communication between individuals is represented by a link between nodes.

    摘要翻译： 用于分析多个个体之间的通信的计算机实现的方法。 该方法包括从数据存储器读取表示涉及第一个体的通信的数据。 显示第一个人和多个其他个人之间的通信网络。 在显示的网络中，每个人都由一个节点来表示，个人之间的通信由节点之间的链接来表示。

    METHOD AND ARRANGEMENT FOR AIRCRAFT FUEL DISPERSION
    7.
    发明申请
    METHOD AND ARRANGEMENT FOR AIRCRAFT FUEL DISPERSION 审中-公开
    飞机燃油分配的方法和安排

    公开(公告)号：WO2007008185A3

    公开(公告)日：2007-04-12

    申请号：PCT/US2004043618

    申请日：2004-12-29

    申请人： GULFSTREAM AEROSPACE CORP ,  WOZNIAK GREGG ,  LAMB DAVID ,  LE DUNG

    发明人： WOZNIAK GREGG ,  LAMB DAVID ,  LE DUNG

    IPC分类号： B64D37/00 ,  B64C17/10

    CPC分类号： B64C17/10 ,  B64D37/00

    摘要： Method and arrangement for dispersing fuel (62) within a fuel containment system (60) of an aircraft (30) including utilizing a fuel containment system on an aircraft that is located at least partially within a wing (34) of the aircraft and defines a reservoir portion (42) and a remote portion (44). Fuel is pumped during aircraft flight from the reservoir portion to the remote portion at a pumped rate (80), while simultaneously fuel that is contained in the remote portion of the fuel containment system is permitted to drain to the reservoir portion at a drainage rate (82). The drainage rate is less than the pumped rate. A fuel mass (64) is accumulated in the remote portion of the fuel containment system because of a difference between the pumped rate and the drainage rate and as a result, a counteractive moment (49) is induced in the aircraft that is opposingly directed to a lift moment (46) caused by wing-lift (45) during aircraft flight.

    摘要翻译： 用于将燃料（62）分散在飞机（30）的燃料容纳系统（60）内的方法和装置，包括利用飞机上的燃料容纳系统，该飞机至少部分地位于飞机的机翼（34）内并限定 储存器部分（42）和远程部分（44）。 燃料在飞机飞行期间以泵送速率（80）从储存器部分泵送至远程部分，同时允许容纳在燃料容纳系统的远程部分中的燃料以排出速率排出至储存器部分（ 82）。 排水率低于抽水率。 由于泵送速率与排放速率之间的差异，燃料容积（64）积聚在燃料容纳系统的远端部分中，并且因此在飞机中引起反作用力矩（49），该力矩相反地指向 在飞机飞行期间由机翼升力（45）引起的升力矩（46）。

    CONTROL FOR GEOTHERMAL HEATING SYSTEM
    8.
    发明申请
    CONTROL FOR GEOTHERMAL HEATING SYSTEM 审中-公开
    地热加热系统控制

    公开(公告)号：WO2012155258A1

    公开(公告)日：2012-11-22

    申请号：PCT/CA2012/050096

    申请日：2012-02-17

    申请人： HEAT-LINE CORPORATION ,  HEISE, Lorne, R. ,  NEWTON, Fraser, F. ,  LAMB, David, S.

    发明人： HEISE, Lorne, R. ,  NEWTON, Fraser, F. ,  LAMB, David, S.

    IPC分类号： F24J3/08 ,  F25B30/00 ,  F25B49/00

    CPC分类号： F28D20/0034 ,  Y02E60/142 ,  Y02E70/30

    摘要： A geothermal energy transfer system has a heat transfer loop associated with a heat pump and a heat absorption loop to circulate fluid through an energy source, such as the ground or body of water. The loops are connected through a reservoir and each loop has a circulating pump to circulate fluid through respective loops. The flow rates of the pumps are selected to optimise energy transfer in each loops and differences in the flow rates are absorbed in the reservoir.

    摘要翻译： 地热能传递系统具有与热泵和热吸收回路相关联的传热回路，以使流体通过能量源（例如地面或水体）循环。 环通过储存器连接，每个回路具有循环泵，以使流体循环通过相应的回路。 选择泵的流量以优化每个回路中的能量传递，并且流量的差异被吸收在储存器中。

    FAULT DETECTION
    10.
    发明申请
    FAULT DETECTION 审中-公开
    故障检测

    公开(公告)号：WO2007113582A2

    公开(公告)日：2007-10-11

    申请号：PCT/GB2007/001290

    申请日：2007-04-05

    申请人： THE QUEEN'S UNIVERSITY OF BELFAST ,  SEZER, Sakir ,  LAMB, David, Martin ,  SCOTT, Colm ,  MULHOLLAN, LIAM ,  KAVANAGH, Garret, David ,  MCLOUGHLIIN, Garret, Michael, Anthony

    发明人： SEZER, Sakir ,  LAMB, David, Martin ,  SCOTT, Colm ,  MULHOLLAN, LIAM ,  KAVANAGH, Garret, David ,  MCLOUGHLIIN, Garret, Michael, Anthony

    CPC分类号： H02H1/0007 ,  G01R31/088 ,  H02H3/042

    摘要： An electricity network fault detection system comprising at least two fault detectors which detect a signal comprising a sferic caused by a fault in the network, and a system processor which receives details of the detected sferic from each of the detectors, and determines the approximate location of generation of the sferic. When a fault occurs in an electricity network, a fault current is generated. These, in conjunction with a part of the network where the fault current has occurred which acts as an antenna, produce electromagnetic radiation in the form of atmospheric radio waves or sferics. It has been realised that these sferics may be used to detect a fault and to determine its approximate location.

    摘要翻译： 一种电网故障检测系统，包括至少两个故障检测器，所述故障检测器检测包括由所述网络中的故障引起的信号的信号;以及系统处理器，其从每个所述检测器接收检测到的误差的细节，并且确定 一代的sferic。 当电网发生故障时，会产生故障电流。 这些与作为天线发生故障电流的网络的一部分结合起来产生大气无线电波或辐射的形式的电磁辐射。 已经意识到，这些信号可以用于检测故障并确定其大致位置。