会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 2. 发明申请
    • Spacecraft three-axis attitude acquisition from sun direction measurement
    • 航天器三轴姿态采集从太阳方向测量
    • US20070228218A1
    • 2007-10-04
    • US11709614
    • 2007-02-22
    • Bruce BrumfieldXenophon PriceGeorge WhitePhilip HirschbergKam Chan
    • Bruce BrumfieldXenophon PriceGeorge WhitePhilip HirschbergKam Chan
    • B64G1/36
    • B64G1/363B64G2001/245G05D1/0883
    • Methods and apparatus for a spacecraft (1) orbiting about a celestial body such as the Earth to reacquire operational three-axis orientation with respect to that body. A method embodiment of the invention comprises determining (201) a set of actual conditions of the spacecraft, comprising a position of the spacecraft (1) in inertial space as a function of time and a set of angular rotation rates of the spacecraft (1) with respect to a coordinate frame of the spacecraft (1), determining (202) an actual instantaneous direction of the sun with respect to the coordinate frame, and propagating (240) an estimated actual sun direction with respect to the coordinate frame as a function of time; determining (260) a desired sun direction with respect to the coordinate frame as a function of time; rotating (270) the spacecraft (1) and adjusting angular rotation rates of the spacecraft (1) so that an actual angle between the spacecraft (1) coordinate frame and the sun as a function of time substantially coincides with the desired sun direction with respect to the coordinate frame as a function of time; and, rotating (280) the spacecraft (1) around an axis defined by a line between the sun and the spacecraft until (1) the celestial body is observed by a celestial body sensor of the spacecraft.
    • 航天器的方法和装置(1)围绕诸如地球之类的天体绕行,以重新获得相对于该身体的操作三轴取向。 本发明的方法实施例包括确定(201)航天器的一组实际状况,包括作为时间的函数的惯性空间中的航天器(1)的位置和航天器(1)的一组角度旋转速率, 相对于航天器(1)的坐标系,确定(202)相对于坐标系的太阳的实际瞬时方向,并且相对于坐标系将估计的实际太阳方向作为函数传播(240) 的时间 确定(260)相对于所述坐标系的期望的太阳方向作为时间的函数; 旋转(270)航天器(1)并调整航天器(1)的角度旋转速率,使得作为时间的函数的航天器(1)坐标系和太阳之间的实际角度基本上与期望的太阳方向重合, 作为时间的函数的坐标框; 并且围绕由太阳和航天器之间的线限定的轴旋转(280)航天器(1),直到(1)天体由天文体的天体传感器观察到。
    • 4. 发明申请
    • QUANTUM RANDOM NUMBER GENERATORS
    • 量子随机数发生器
    • US20060288062A1
    • 2006-12-21
    • US11424808
    • 2006-06-16
    • Yuhui LuoKam Chan
    • Yuhui LuoKam Chan
    • G06F7/58
    • G06F7/588H04L9/0852
    • Disclosed is an all-fiber optical quantum random number generator, an optical coupler having an input port and two output ports; a single photon source connected to the input port, emitting a single photon which is transmitted from the input port to the output ports; a single photon detector connected to each of the two output ports, detecting the photon coming out from either of the output ports; and means for generating random numbers according to the detection result of the single photon detector. The generator of the invention can generate truly random numbers.
    • 公开了一种全光纤量子随机数发生器,具有输入端口和两个输出端口的光耦合器; 连接到输入端口的单个光子源,发射从输入端口传输到输出端口的单个光子; 连接到两个输出端口中的每一个的单个光子检测器,检测从任一输出端口出来的光子; 以及根据单个光子检测器的检测结果产生随机数的装置。 本发明的发电机可以产生真正的随机数。
    • 5. 发明申请
    • Electric spice mill
    • 电动香料磨
    • US20060261197A1
    • 2006-11-23
    • US11131759
    • 2005-05-18
    • Kit ChanKam ChanGeorge Bigelow
    • Kit ChanKam ChanGeorge Bigelow
    • A47J42/00
    • A47J42/06A47J42/44A47J42/46
    • An electric spice mill comprising a power unit coupled to the motor of the mill, the power unit comprising: (i) first and second electric circuits; (ii) a switch in electrical contact with said first and said second electric circuits; and (iii) an actuator movable between first and second positions, wherein, in the first position, the actuator prevents current flow in the first electric circuit and, in the second position, the actuator allows a first current to flow in the first electric circuit and the switch is responsive to the first current in the first electric circuit to allow a second current to flow in the second electric circuit such that the grinding unit of the mill is driven by the motor.
    • 一种电动香料磨,包括耦合到所述磨机的所述电动机的动力单元,所述动力单元包括:(i)第一和第二电路; (ii)与所述第一和所述第二电路电接触的开关; 和(iii)可在第一和第二位置之间移动的致动器,其中,在第一位置,致动器防止电流在第一电路中流动,并且在第二位置,致动器允许第一电流在第一电路中流动 并且所述开关响应于所述第一电路中的所述第一电流以允许第二电流在所述第二电路中流动,使得所述磨机的磨削单元由所述电动机驱动。
    • 6. 发明授权
    • Spacecraft three-axis attitude acquisition from sun direction measurement
    • 航天器三轴姿态采集从太阳方向测量
    • US07874519B2
    • 2011-01-25
    • US11709614
    • 2007-02-22
    • Bruce BrumfieldXenophon H. PriceGeorge E. WhitePhilip C. HirschbergKam Chan
    • Bruce BrumfieldXenophon H. PriceGeorge E. WhitePhilip C. HirschbergKam Chan
    • B64G1/36
    • B64G1/363B64G2001/245G05D1/0883
    • Methods and apparatus for a spacecraft (1) orbiting about a celestial body such as the Earth to reacquire operational three-axis orientation with respect to that body. A method embodiment of the invention comprises determining (201) a set of actual conditions of the spacecraft, comprising a position of the spacecraft (1) in inertial space as a function of time and a set of angular rotation rates of the spacecraft (1) with respect to a coordinate frame of the spacecraft (1), determining (202) an actual instantaneous direction of the sun with respect to the coordinate frame, and propagating (240) an estimated actual sun direction with respect to the coordinate frame as a function of time; determining (260) a desired sun direction with respect to the coordinate frame as a function of time; rotating (270) the spacecraft (1) and adjusting angular rotation rates of the spacecraft (1) so that an actual angle between the spacecraft (1) coordinate frame and the sun as a function of time substantially coincides with the desired sun direction with respect to the coordinate frame as a function of time; and, rotating (280) the spacecraft (1) around an axis defined by a line between the sun and the spacecraft until (1) the celestial body is observed by a celestial body sensor of the spacecraft.
    • 航天器的方法和装置(1)围绕诸如地球之类的天体绕行,以重新获得相对于该身体的操作三轴取向。 本发明的方法实施例包括确定(201)航天器的一组实际状况,包括作为时间的函数的惯性空间中的航天器(1)的位置和航天器(1)的一组角度旋转速率, 相对于航天器(1)的坐标系,确定(202)相对于坐标系的太阳的实际瞬时方向,并且相对于坐标系将估计的实际太阳方向作为函数传播(240) 的时间 确定(260)相对于所述坐标系的期望的太阳方向作为时间的函数; 旋转(270)航天器(1)并调整航天器(1)的角度旋转速率,使得作为时间的函数的航天器(1)坐标系和太阳之间的实际角度基本上与期望的太阳方向重合, 作为时间的函数的坐标框; 并且围绕由太阳和航天器之间的线限定的轴旋转(280)航天器(1),直到(1)天体由天文体的天体传感器观察到。
    • 7. 发明申请
    • Fluorescent lamp
    • 日光灯
    • US20050067977A1
    • 2005-03-31
    • US10498629
    • 2003-07-28
    • Kam ChanWai Ng
    • Kam ChanWai Ng
    • F21S9/02F21S2/00F21Y103/00H01J5/50H01J61/34H01J61/35H01J61/54H01J61/56H05B41/24H01J7/44H05B37/02
    • H01J61/35H01J5/50H01J61/34H01J61/56
    • A new fluorescent lamp comprises a lamp tube and an electronic ballast, it is characterized in that it is provided with an outer tube, there are respectively an outer plug at both ends of the outer tube, in which inserts a socket for the lamp tube. The electronic ballast is between the outer plug and the socket for the lamp tube at one end, said lamp tube is disposed between two sockets for the lamp tube. There are advantages as follows: an urgent lighting, the electronic ballast and the compact lamp tube are integrated as one whole; it is convenient for mounting and exchanging, a cost for mounting is greatly reduced; it is possible for repacking to maintain an original means, to reduce a contamination of waste; its weight is light; its power factor is high, more than 95%, it is economical in power, a cost for transporting is low; the color rendering index (CRI) is more than 80%; it is ignited immediately after it is turned on, it does not flash; it is applied to lamps having deferent power; the life of the lamp tube is prolonged by 50%; its output brightness is higher than existing lamps by twice or more; the lamp tube still steadily operates when a power supply is unexpected to be shut off, which reduces accident cases; the whole distortion of a resonant wave becomes smaller than 30%.
    • 一种新的荧光灯包括灯管和电子镇流器,其特征在于,其具有外管,外管的两端分别具有外插头,其中插入用于灯管的插座。 电子镇流器位于外插头和插座之间,用于灯管的一端,所述灯管设置在用于灯管的两个插座之间。 有以下优点:紧急照明,电子镇流器和小型灯管整体集成; 安装和更换方便,安装成本大大降低; 重新包装可以保持原有的手段,减少废物的污染; 它的重量轻; 功率因数高,超过95%,功率经济,运输成本低; 显色指数(CRI)超过80%; 开机后立即点火,不闪烁; 它适用于具有不同功率的灯; 灯管寿命延长50%; 其输出亮度高于现有灯两倍以上; 当电源意外关闭时,灯管仍然稳定运行,从而减少事故的发生; 谐振波的整体失真变得小于30%。