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    • 3. 发明授权
    • Spacecraft solar power system
    • 航天器太阳能发电系统
    • US5979834A
    • 1999-11-09
    • US850325
    • 1997-05-02
    • Gerald Falbel
    • Gerald Falbel
    • B64G1/22B64G1/44F24S23/70H01L31/045H01L31/052H01L31/042
    • B64G1/222B64G1/443F24J2/10H01L31/0543H01L31/0547H02S30/20F24J2002/1014Y02E10/40Y02E10/52Y10S136/292
    • A solar power system for orbiting spacecraft includes a collector surface and attached mirror which is retained in a coiled position around the outer surface of the spacecraft in its launch mode. The system is deployed from the orbiting spacecraft by releasing restraining straps and permitting the mirror and attached collector surface to automatically uncoil as a result of the resilient spring characteristics of the mirror. During orbit, the deployed system extends from one side or both sides of the spacecraft such that the mirrored surface faces the sun. Heating pipes are pivotably disposed between the mirror and the collector surface to also function as spacing struts. The collector surface covered with photovoltaic solar cells made of silicon or Gallium Arsenide-Phosphide (GaAsP) in a first embodiment of the invention, can be replaced by a flat heat pipe for conducting heat energy to the input of an external heat engine electric generator in a second embodiment of the invention.
    • 用于轨道航天器的太阳能发电系统包括收集器表面和附接的反射镜,其在其发射模式下保持在围绕航天器的外表面的盘绕位置。 通过释放限制带,从轨道航天器部署系统,由于反射镜的弹性弹簧特性,允许反射镜和附着的收集器表面自动开卷。 在轨道运行期间,部署的系统从航天器的一侧或两侧延伸,使得镜面朝向太阳。 加热管可枢转地设置在反射镜和收集器表面之间,也用作间隔支柱。 在本发明的第一实施例中,由硅或砷化镓 - 磷化物(GaAsP)制成的光伏太阳能电池的收集器表面可以被用于将热能传导到外部热机发电机的输入端的平坦热管 本发明的第二实施例。
    • 4. 发明授权
    • Airborne search and rescue scanner
    • 机载搜索和救援扫描仪
    • US07106430B2
    • 2006-09-12
    • US10820300
    • 2004-04-08
    • Gerald Falbel
    • Gerald Falbel
    • G01B11/26G01C1/00
    • G01C1/00G01S17/74G02B27/64
    • An airborne search and rescue scanner is provided to locate a missing person wearing a reflector for reflecting laser energy emitted from a scanner in a high speed aircraft. The scanner and reflector combination enable scanning of a large search area in a relatively short time period. The system is designed to prevent false readings, as for example, sun glint reflected by the reflector, or false alarms resulting from reflections from the terrain being searched and not the reflector worn by the missing person. In an alternative embodiment of the invention, the active laser scanning system is replaced by a passive infrared scanner by replacing the laser scanner with an infrared detector. In this embodiment, it is not necessary for the missing person to wear a reflector.
    • 提供了一种机载搜索和救援扫描仪,用于定位穿戴反射器的失踪人员,以反映高速飞行器中扫描仪发射的激光能量。 扫描仪和反射器组合使得能够在相对短的时间内扫描大的搜索区域。 该系统设计用于防止错误的读数,例如反射器反射的太阳闪光,或者来自正在搜索的地形的反射引起的虚假警报,而不是失踪人员佩戴的反射镜。 在本发明的替代实施例中,通过用红外检测器代替激光扫描器来将有源激光扫描系统替换为被动红外扫描器。 在本实施例中,失踪人员不必佩戴反射器。
    • 6. 发明授权
    • Immersed photovoltaic solar power system
    • 沉浸式光伏太阳能发电系统
    • US6034319A
    • 2000-03-07
    • US126505
    • 1998-07-30
    • Gerald Falbel
    • Gerald Falbel
    • H01L31/052H01L25/00
    • H01L31/0547Y02E10/52
    • An immersed solar concentrator system has a concentrator element for directing light rays onto a solar cell. The solar cell has a surrounding reflective surface for reflecting light rays which are not absorbed by the solar cell but strike the reflective surface. The immersion medium, which is disposed between the solar cell and the concentrator element, has a refractive index for reflecting the reflected light rays, by total internal reflection, in a direction towards the solar cell so that at least some of the reflected light rays are absorbed by the solar cell.
    • 一种浸没的太阳能集中器系统具有用于将光线引导到太阳能电池上的集中器元件。 太阳能电池具有用于反射未被太阳能电池吸收但撞击反射表面的光线的周围反射表面。 设置在太阳能电池和集中器元件之间的浸没介质具有用于通过全内反射在朝向太阳能电池的方向上反射反射光线的折射率,使得至少一些反射光线为 被太阳能电池吸收。
    • 7. 发明授权
    • Horizon sensor
    • 地平线传感器
    • US4328421A
    • 1982-05-04
    • US124429
    • 1980-02-25
    • Gerald Falbel
    • Gerald Falbel
    • G01S3/786G01S3/789G01J1/00
    • G01S3/789G01S3/7868
    • A family of two axis horizon sensors using the same basic scan technique is provided which achieves a relatively wide altitude range with a minimum of moving parts for performing vehicle attitude control and guidance. The horizon sensor for indicating the orientation of a space vehicle senses a line of discontinuity in optical radiation between a reference planet and outer space in at least two planes using a single sensor which includes a single detector means for detecting the optical radiation. The detector is scanned across the line of discontinuity in at least two planes. The scanner includes a rotary element driven by a single motor having at least two stationary reflecting elements positioned therearound. A phase reference signal generator is coupled to the motor and driven in synchronism therewith for generating at least two reference signals at predetermined points in the scan. Electronic circuitry is provided utilizing the reference signals and the signals generated by the detector for measuring rotational intervals between the reference signals and the detector signals for determining the attitude of the sensor in the two mutually perpendicular axes.The stationary reflecting mirrors may be two, three or four in number each of which scans the detector over a different pattern across the planet used as a reference for attitude control. Advantageously, in accordance with the present invention, the family of two axis sensors requires only one sensor head, one scanning motor, one detector all of which are housed in one package.
    • 提供使用相同基本扫描技术的两轴水平传感器系列,其具有用于执行车辆姿态控制和引导的最小的运动部件的相对较宽的高度范围。 用于指示空间车辆的取向的水平传感器使用包括用于检测光辐射的单个检测器装置的单个传感器在至少两个平面中感测参考行星架和外部空间之间的光辐射线。 检测器在至少两个平面中的不连续线上扫描。 扫描器包括由单个电动机驱动的旋转元件,其具有定位在其周围的至少两个固定反射元件。 相位参考信号发生器耦合到电动机并与其同步地驱动以在扫描中的预定点产生至少两个参考信号。 使用参考信号和由检测器产生的信号来提供电子电路,用于测量参考信号和检测器信号之间的旋转间隔,以确定传感器在两个相互垂直的轴中的姿态。 固定反射镜可以是两个,三个或四个,每个扫描通过跨越用作姿态控制的参考的行星的不同图案扫描检测器。 有利地,根据本发明,两轴传感器系列仅需要一个传感器头,一个扫描电机,一个检测器,所有这些都被容纳在一个封装中。
    • 9. 发明授权
    • Horizon sensor compensation for radiance variations
    • 水平传感器补偿辐射变化
    • US5079419A
    • 1992-01-07
    • US534448
    • 1990-06-06
    • Gerald Falbel
    • Gerald Falbel
    • G01S3/786
    • G01S3/7868
    • A horizon sensor scans an infrared detector over the earth's horizon generating first (A) and second (B) signals of finite pulse width representing radiation from the fields of view of the infrared detector as it is scanned across the earth's horizon. Signals (A-B) and (A+B)/3 are derived from the first (A) and second (B) signals. The horizon is detected when a threshold is exceeded when the absolute value (A-B) is less than the absolute value of (A+B)/3 whereby the detected horizon is essentially independent of the radiance variations of the earth's horizon. Sun and moon signals appearing in the field of view of the infrared detector are eliminated based on the smaller pulse width of such signals in comparison with the finite pulse width of the first and second signals. The method of radiance compensation can be implemented using a dual field of view for the infrared detector in a horizon crossing indicator sensor where the scanning of the detector is provided by the rotation of the satellite. In another embodiment, wherein the scanning of a single field of view is provided by a conical scanner in the sensor, the signal is digitized and delayed to provide the dual fields of view in which the horizon is detected in the same manner as the embodiment using two separate detectors with similar beneficial results.
    • 地平线传感器扫描地球上的地平线上的红外探测器,产生有效脉冲宽度的第一(A)和第二(B)信号,表示当红外探测器沿着地平线扫描时,来自红外探测器视场的辐射。 信号(A-B)和(A + B)/ 3从第一(A)和第二(B)信号导出。 当绝对值(A-B)小于(A + B)/ 3的绝对值时,超过阈值时检测到水平线,由此检测到的水平线基本上与地球天际线的辐射度变化无关。 与第一和第二信号的有限脉冲宽度相比,基于这种信号的较小的脉冲宽度,消除了出现在红外检测器的视野中的太阳和月亮信号。 辐射补偿的方法可以使用在水平交叉指示器传感器中的红外检测器的双视野来实现,其中检测器的扫描由卫星的旋转提供。 在另一个实施例中,其中单个视野的扫描由传感器中的锥形扫描器提供,该信号被数字化和延迟,以提供与其中使用的实施例相同的方式检测水平线的双视场 两个独立的探测器具有类似的有益效果。
    • 10. 发明授权
    • Yaw sensing conical scanner horizon sensor
    • Yaw感应锥形扫描仪水平传感器
    • US4791297A
    • 1988-12-13
    • US31436
    • 1987-03-26
    • Robert C. SavocaGerald Falbel
    • Robert C. SavocaGerald Falbel
    • G01S3/789G01J5/08
    • G01S3/789
    • A radiation detector is scanned over two fan fields of view by first and second cylindrical lenses spaced about the axis of rotation of a common optical element positioned on the axis of rotation. The optical element is rotated about the optical axis by a motor or the rotation of the orbiting body on which the scanner is mounted. In one form the common optical element is a chisel mirror having the first and second cylindrical lenses positioned on opposite sides thereof and tilted at an angle of 45.degree. with respect to the axis of rotation producing two fan fields which are 180.degree. apart in phase. As an alternative the common optical element may comprise a cylinder having the second cylindrical lens positioned along with a bevelled reflective upper surface for producing a vertical fan field. The cylindrical lenses and common optical element may be incorporated in a conical scanner employing an infrared detector which systems can be combined to produce yaw, pitch, roll, attitude information in a single horizon sensor head.
    • 通过位于旋转轴线上的公共光学元件的旋转轴线隔开的第一和第二柱面透镜在两个风扇视场上扫描辐射探测器。 光学元件通过电动机围绕光轴旋转或者安装有扫描仪的轨道体的旋转。 在一种形式中,普通光学元件是凿子镜,其具有位于其相对侧上的第一和第二柱面透镜,并且相对于旋转轴线以45°的角度倾斜,产生相位相差180°的两个扇形场。 作为替代,普通光学元件可以包括具有与倾斜的反射上表面一起定位的第二柱面透镜的圆柱体,用于产生竖直扇形场。 柱面透镜和普通光学元件可以结合在使用红外检测器的锥形扫描仪中,该系统可以被组合以在单个水平传感器头中产生偏航,俯仰,滚动,姿态信息。