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    • 1. 发明授权
    • System for controlling the display size of a formula bar in a spreadsheet
    • 用于控制电子表格中公式栏显示大小的系统
    • US07805674B2
    • 2010-09-28
    • US11479116
    • 2006-06-29
    • Bo ChenHui WangQingyuan ZhangLi Wan
    • Bo ChenHui WangQingyuan ZhangLi Wan
    • G06F17/00
    • G06F17/246
    • The present invention discloses a system for controlling the display size of a formula bar in a spreadsheet. The system for controlling the display size of the formula bar and a formula bar module are parallel in a main window module of a spreadsheet application, and the system includes a sub-system I which controls the display state of the formula bar and a sub-system II which controls the display range of the specific content in the formula bar. The system continuously executes real-time detecting and measuring of the aforementioned formula bar module while the application is running, and acquires data on the size of the formula bar from the aforementioned formula bar module. If the acquired data exceed the prescribed range, then it issues a command to the aforementioned formula bar module requesting a change in the size of the formula bar. In the mean time, it issues a command to the aforementioned sub-system I and the aforementioned sub-system II.
    • 本发明公开了一种用于控制电子表格中公式栏的显示尺寸的系统。 用于控制公式栏和公式栏模块的显示尺寸的系统在电子表格应用的主窗口模块中是并行的,并且系统包括控制公式栏的显示状态的子系统I, 系统II,其控制公式栏中特定内容的显示范围。 在应用程序运行时,系统连续执行上述公式栏模块的实时检测和测量,并从上述公式栏模块获取关于公式栏的大小的数据。 如果所获取的数据超过规定范围,则向上述公式栏模块发出请求改变公式栏大小的命令。 同时,它向上述子系统I和上述子系统II发出命令。
    • 2. 发明申请
    • System for controlling the display size of a formula bar in a spreadsheet
    • 用于控制电子表格中公式栏显示大小的系统
    • US20070016850A1
    • 2007-01-18
    • US11479116
    • 2006-06-29
    • Bo ChenHui WangQingyuan ZhangLi Wan
    • Bo ChenHui WangQingyuan ZhangLi Wan
    • G06F17/00
    • G06F17/246
    • The present invention discloses a system for controlling the display size of a formula bar in a spreadsheet. Application of this system will make operation of the spreadsheet more convenient. The system for controlling the display size of the formula bar and a formula bar module are parallel in a main window module of a spreadsheet application, and the system includes a sub-system I which controls the display state of the formula bar and a sub-system II which controls the display range of the specific content in the formula bar. The system continuously executes real-time detecting and measuring of the aforementioned formula bar module while the application is running, and acquires data on the size of the formula bar from the aforementioned formula bar module. If the acquired data exceed the prescribed range, then it issues a command to the aforementioned formula bar module requesting a change in the size of the formula bar. In the mean time, it issues a command to the aforementioned sub-system I and the aforementioned sub-system II.
    • 本发明公开了一种用于控制电子表格中公式栏的显示尺寸的系统。 该系统的应用将使电子表格的操作更加方便。 用于控制公式栏和公式栏模块的显示尺寸的系统在电子表格应用的主窗口模块中是并行的,并且系统包括控制公式栏的显示状态的子系统I, 系统II,其控制公式栏中特定内容的显示范围。 在应用程序运行时,系统连续执行上述公式栏模块的实时检测和测量,并从上述公式栏模块获取关于公式栏的大小的数据。 如果所获取的数据超过规定范围,则向上述公式栏模块发出请求改变公式栏大小的命令。 同时,它向上述子系统I和上述子系统II发出命令。
    • 3. 发明申请
    • Stratospheric-Airship-Assisted Orbital Payload Launching System
    • 平流层 - 飞艇辅助轨道载荷发射系统
    • US20150336685A1
    • 2015-11-26
    • US14282987
    • 2014-05-20
    • Li Wan
    • Li Wan
    • B64G1/00B64G1/40B64B1/62B64G1/64B64G1/52B64B1/00B64G1/62
    • B64G1/005B64B1/00B64B1/005B64B1/06B64B1/60B64B1/62B64D5/00B64G1/00B64G1/14B64G1/40B64G1/401B64G1/402B64G1/52B64G1/62B64G1/64B64G5/00
    • The present invention is a stratospheric-airship-assisted orbital payload launching system that features with high reusability ratio, low cost, short launch-preparation time and robust reliability. The system consists of an airship-based stratospheric launch platform (1), a stratospheric-launched suborbital shuttle (2, SLSS) and an upper stage (3, a modified version of conventional upper stage or a spaceplane). The airship-based stratospheric launch platform (1) employs hydrogen and helium to provide buoyancy in its ascent and high-altitude cruise stages. Given the substantially lower ambient pressure, the usage of hydrogen at high altitude is much safer than on the ground. The SLSS (2) is mounted beneath the platform (1), and an assembly of payload (4) and upper stage (3) is loaded in the cargo bay (2B) of SLSS (2). In a typical orbital payload launching mission, the airship-based stratospheric launch platform (1) ascends to a predetermined altitude in stratosphere, where the air density is much lower than the sea level and wind is relatively slow and steady comparing with the upper troposhere, and then launches the SLSS (2) in a predetermined position and time. After the SLSS (2) is launched, the platform (1) vents hydrogen lifting gas to swiftly unload the extra buoyancy. Subsequently, the platform (1) descends and returns to its ground base. Meanwhile, the SLSS (2) rockets to a predetermined velocity and altitude (above the atmosphere), opens its cargo bay doors (2D) and releases its cargo (i.e., the assembly of upper stage (3) and payload (4. The upper stage (3) ignites and propels the payload to a predetermined space orbit. At the same time, the SLSS (2) re-enters, and decelerates via aerobraking. It is finally recovered via a conventional wheel landing.
    • 本发明是具有高可重用性,低成本,短启动准备时间和鲁棒可靠性的平流层 - 飞艇辅助轨道有效载荷发射系统。 该系统由基于飞艇的平流层发射平台(1),平流层发射的眶下穿梭(2,SLSS)和上段(3,常规上段或空间飞机的修改版本)组成。 基于飞艇的平流层发射平台(1)采用氢气和氦气在其上升和高空巡航阶段提供浮力。 考虑到环境压力大大降低,高空使用氢气比地面上安​​全得多。 SLSS(2)安装在平台(1)下方,有效载荷(4)和上部(3)的组件装载到SLSS(2)的货舱(2B)中。 在典型的轨道有效载荷发射任务中,基于飞艇的平流层发射平台(1)上升到平流层预定的高度,空气密度远低于海平面,与上层相比,风相对较慢,稳定, 然后在预定的位置和时间上启动SLSS(2)。 SLSS(2)启动后,平台(1)通过排气提升气体,迅速卸载额外的浮力。 随后,平台(1)下降并返回其底座。 同时,SLSS(2)火箭以预定的速度和高度(大气层以上)打开货舱门(2D)并释放其货物(即,上层(3)和有效载荷(4)的装配。 阶段(3)将有效载荷点燃并推进到预定的空间轨道,同时,SLSS(2)通过航空制动重新进入和减速,最终通过传统的轮式降落来恢复。
    • 4. 发明授权
    • Stratospheric-airship-assisted orbital payload launching system
    • 平流层 - 飞艇辅助轨道载荷发射系统
    • US09302788B2
    • 2016-04-05
    • US14282987
    • 2014-05-20
    • Li Wan
    • Li Wan
    • B64C37/02B64G1/00B64B1/00B64G1/40B64G1/62B64G1/64B64G1/52B64B1/62
    • B64G1/005B64B1/00B64B1/005B64B1/06B64B1/60B64B1/62B64D5/00B64G1/00B64G1/14B64G1/40B64G1/401B64G1/402B64G1/52B64G1/62B64G1/64B64G5/00
    • The present invention is a stratospheric-airship-assisted orbital payload launching system that features with high reusability ratio, low cost, short launch-preparation time and robust reliability. The system consists of an airship-based stratospheric launch platform (1), a stratospheric-launched suborbital shuttle (2, SLSS) and an upper stage (3, a modified version of conventional upper stage or a spaceplane). The airship-based stratospheric launch platform (1) employs hydrogen and helium to provide buoyancy in its ascent and high-altitude cruise stages. Given the substantially lower ambient pressure, the usage of hydrogen at high altitude is much safer than on the ground. The SLSS (2) is mounted beneath the platform (1), and an assembly of payload (4) and upper stage (3) is loaded in the cargo bay (2B) of SLSS (2). In a typical orbital payload launching mission, the airship-based stratospheric launch platform (1) ascends to a predetermined altitude in stratosphere, where the air density is much lower than the sea level and wind is relatively slow and steady comparing with the upper troposhere, and then launches the SLSS (2) in a predetermined position and time. After the SLSS (2) is launched, the platform (1) vents hydrogen lifting gas to swiftly unload the extra buoyancy. Subsequently, the platform (1) descends and returns to its ground base. Meanwhile, the SLSS (2) rockets to a predetermined velocity and altitude (above the atmosphere), opens its cargo bay doors (2D) and releases its cargo (i.e., the assembly of upper stage (3) and payload (4)). The upper stage (3) ignites and propels the payload to a predetermined space orbit. At the same time, the SLSS (2) re-enters, and decelerates via aerobraking. It is finally recovered via a conventional wheel landing.
    • 本发明是具有高可重用性,低成本,短启动准备时间和鲁棒可靠性的平流层 - 飞艇辅助轨道有效载荷发射系统。 该系统由基于飞艇的平流层发射平台(1),平流层发射的眶下穿梭(2,SLSS)和上段(3,常规上段或空间飞机的修改版本)组成。 基于飞艇的平流层发射平台(1)采用氢气和氦气在其上升和高空巡航阶段提供浮力。 考虑到环境压力大大降低,高空使用氢气比地面上安​​全得多。 SLSS(2)安装在平台(1)下方,有效载荷(4)和上部(3)的组件装载到SLSS(2)的货舱(2B)中。 在典型的轨道有效载荷发射任务中,基于飞艇的平流层发射平台(1)上升到平流层预定的高度,空气密度远低于海平面,与上层相比,风相对较慢,稳定, 然后在预定的位置和时间上启动SLSS(2)。 SLSS(2)启动后,平台(1)通过排气提升气体,迅速卸载额外的浮力。 随后,平台(1)下降并返回其底座。 同时,SLSS(2)火箭以预定的速度和高度(大气层以上)打开货舱门(2D)并释放其货物(即上级(3)和有效载荷(4))。 上级(3)点燃并将有效载荷推进到预定的空间轨道。 同时,SLSS(2)重新进入,并通过航空制动减速。 最终通过传统的轮辋着陆来恢复。
    • 8. 发明申请
    • Method for Selecting and Configuring Network Supernodes
    • 选择和配置网络超频的方法
    • US20110128889A1
    • 2011-06-02
    • US12730866
    • 2010-03-24
    • Jianxin LiaoJing WangChun WangWei LiLi WanXiaomin ZhuLei ZhangTong XuLejian ZhangQiwei ShenLimin FanLi Cheng
    • Jianxin LiaoJing WangChun WangWei LiLi WanXiaomin ZhuLei ZhangTong XuLejian ZhangQiwei ShenLimin FanLi Cheng
    • H04L12/28
    • H04L41/0893H04L45/04H04L67/1051H04L67/1093
    • A method for selecting and configuring network supernodes including the following operational steps: in a first set period T1, each node other than the control node in a network sends information on interactions between the node and other nodes to the control node regularly; and in a second set period T2, the control node divides the nodes into a plurality of node clusters according to the received information on interactions among the nodes, and selects supernodes from each node cluster, each node belonging uniquely to a node cluster. The supernode selection according to the invention takes into account both performance and resource conditions of itself and interactions with other nodes. Therefore, when implementing control over other nodes in the node cluster to which it belongs, the selected supernode can find the corresponding node in a short time and shorten the searching time and path, thereby improving the working efficiency. Meanwhile, parameters such as the acquiring period of node interaction information, and the division and adjustment periods of node clusters can be adjusted dynamically with the actual interaction conditions of the network.
    • 一种用于选择和配置网络超节点的方法,包括以下操作步骤:在第一设定周期T1中,除了网络中的控制节点之外的每个节点向节点定期向控制节点发送关于节点与其他节点之间的交互的信息; 并且在第二设定周期T2中,控制节点根据接收到的关于节点之间的交互的信息将节点划分为多个节点簇,并且从每个节点簇选择每个节点的节点簇唯一的节点。 根据本发明的超级节点选择考虑了自身的性能和资源状况以及与其他节点的交互。 因此,当对其所属的节点集群中的其他节点实施控制时,所选择的超节点可以在短时间内找到相应的节点,缩短搜索时间和路径,从而提高工作效率。 同时,可以根据网络的实际交互条件动态调整节点交互信息采集周期等参数,节点集群划分和调整周期。