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    • 71. 发明授权
    • Conformal airlock assembly and method
    • 共形气锁组件及方法
    • US07997537B2
    • 2011-08-16
    • US11871014
    • 2007-10-11
    • Christopher A. RygaardDanilo Viazzo
    • Christopher A. RygaardDanilo Viazzo
    • B64G1/60
    • B64G1/46B64G1/60
    • A conformal airlock assembly for ingress and egress through a door from a high pressure environment to a low pressure environment. The airlock assembly includes a flexible, gas impermeable membrane that cooperates with a support wall in an airtight manner to form an interior pocket over the door on one side of the wall. A gas displacement system, in flow communication with the interior pocket, is selectively operable to flow air out of the interior pocket, collapsing the membrane toward a collapsed condition. An actuation system coupled to the flexible membrane is operable to displace the flexible membrane, in the collapsed condition, away from the one side of the support wall. Such displacement of the airtight membrane creates a low pressure space in the pocket that is selected to be sufficiently proximate that of the low pressure environment. Hence, the door may be opened to permit ingress and egress therethrough without a large pressure differential.
    • 通过门从高压环境到低压环境进出口的保形气锁组件。 气闸组件包括柔性的不透气膜,其以气密的方式与支撑壁配合,以在壁的一侧上形成在门上的内部袋。 与内部袋口流动连通的气体置换系统可选择性地可操作地将空气流出内部袋,使膜朝向折叠状态折叠。 耦合到柔性膜的致动系统可操作以在折叠状态下将柔性膜从支撑壁的一侧移开。 密封膜的这种位移在袋中产生低压空间,其被选择为足够接近于低压环境。 因此,门可以打开以允许入口和出口通过而没有大的压差。
    • 72. 发明授权
    • Method for manufacturing a solar module in orbit
    • 太阳能电池组件在轨道上的制造方法
    • US07971831B2
    • 2011-07-05
    • US11409697
    • 2006-04-24
    • Paul Roseman
    • Paul Roseman
    • B64G1/00
    • B64G1/428B64G1/12B64G1/14B64G1/222B64G1/402B64G1/405B64G1/44B64G1/46B64G1/646Y10T29/49016
    • A geosynchronous Solar Power Satellite System is created by an artificial gravity, closed ecology, multiple use structure in low earth orbit that manufactures modular solar power panels and transmitter arrays. This facility takes empty fuel tanks and expended rocket boosters from launch vehicles that are sent into low earth orbit, and re-manufactures them into structural components. These components are mated to solar cells that are launched from earth. The modular solar panels are transported to geosynchronous orbit by vehicles with ion engines, where the panels are mated to other solar panels to collect power. Structural components are also mated to transmitter elements launched from earth. These are likewise transported to geosynchronous orbit. They are mated to the solar power collecting panels and they beam the collected power back to earth.
    • 地球同步太阳能发电卫星系统由人造重力,封闭式生态学,低地球轨道多用途结构产生,制造模块化太阳能发电板和发射机阵列。 这个设施将空燃料箱和消耗火箭的助推器从运送到低地球轨道的运载火箭,并将其重新制造成结构部件。 这些组件与从地球发射的太阳能电池相配。 模块化太阳能电池板通过具有离子发动机的车辆运输到地球同步轨道,其中面板与其他太阳能电池板配合以收集电力。 结构部件也适用于从地球发射的发射机元件。 这些同样运送到地球同步轨道。 它们与太阳能收集板相配,并将收集的电力反射回地球。
    • 73. 发明授权
    • Lightweight acoustic damping treatment
    • 轻量级声阻尼处理
    • US07819221B1
    • 2010-10-26
    • US11239440
    • 2005-09-27
    • Steven A. LaneRobert E. RichardSteven F. Griffin
    • Steven A. LaneRobert E. RichardSteven F. Griffin
    • F01N1/06F01N1/22E04B1/82B64C1/40F01N1/00E04B1/74
    • G10K11/172B64G1/22B64G1/38B64G1/46B64G2001/224F01N1/06F01N1/22
    • A flexible membrane is attached to an internal wall of the fairing of a flight vehicle. The membrane is inflated with gas to achieve a shape that couples with and thereby attenuates the first acoustic resonance occurring within the volume enclosed by the fairing. A sensor senses the varying ambient atmospheric pressure during flight. A pressure regulating system includes an inflation valve and pressure relief valve. Based on the sensed ambient atmospheric pressure, this system adjusts the membrane's gauge pressure throughout the flight trajectory to maintain the desired coupling gauge pressure. Acoustic blankets can also be attached to the internal walls of the fairing to abate resonances having frequencies greater than 500 Hz. Inflating the membrane with helium enhances the attenuation otherwise obtained. Multiple membranes can be individually tuned to respectively attenuate multiple acoustic resonances.
    • 柔性膜连接到飞行器整流罩的内壁。 膜用气体充气以实现与由整流罩包围的体积内发生的第一声共振耦合并从而​​衰减的形状。 传感器感测飞行过程中变化的环境大气压力。 压力调节系统包括充气阀和泄压阀。 基于感测到的环境大气压力,该系统在整个飞行轨迹上调整膜的表压,以保持所需的耦合表压。 声学毯也可以连接到整流罩的内壁,以消除频率大于500Hz的谐振。 用氦气充气膜可增强否则获得的衰减。 可以单独调谐多个膜以分别衰减多个声共振。
    • 75. 发明授权
    • Shading device for use in a geostatic satellite
    • 用于地球静止卫星的遮蔽装置
    • US4725023A
    • 1988-02-16
    • US631644
    • 1984-07-17
    • Haruo Shiki
    • Haruo Shiki
    • B64G1/46B64G1/58
    • B64G1/58B64G1/46
    • A geostatic satellite comprises a spinning drum for stabilization which spins around an axis of rotation which is parallel to the axis of the earth. A paddle member loaded with solar cells is directly rotatable about the same axis and is controlled such that the solar cells face the sun. A despun platform supports communication gear and maintains the gear pointed to a relatively fixed point on earth. A shading device for shading the electronics laden despun platform from the sun, is attached to the paddle member and rotatable therewith. Thereby, the shading device will always be disposed between the sun and the despun platform.
    • 地静卫星包括用于稳定的旋转鼓,其围绕平行于地球轴线的旋转轴线旋转。 装载有太阳能电池的桨构件可以围绕相同的轴线直接旋转并被控制,使得太阳能电池面对太阳。 解脱平台支持通信齿轮,并将齿轮指向地球上相对固定的点。 遮阳装置用于将装有电子装置的遮阳平台从太阳遮蔽,并附着在桨叶构件上并随其一起旋转。 因此,遮光装置将始终设置在太阳和脱泡平台之间。
    • 76. 发明授权
    • Space living quarters having artificial gravity environment
    • 具有人造重力环境的空间生活区
    • US4643375A
    • 1987-02-17
    • US748925
    • 1985-06-26
    • Sebree J. Allen
    • Sebree J. Allen
    • B64G1/46B64G1/60
    • B64G1/60B64G1/46
    • Living quarters for a space vehicle including a rotary cylindrical module enclosing a living compartment for human occupancy, and means for rotating the module about its longitudinal central axis to create a force of approximately 1 G within the module adjacent the outer wall, and an entrance opening formed within one end wall of the cylindrical module to permit the passage of a human coccupant from the zero-gravity space within a space vehicle into the artificial-gravity environment of the living compartment. An inside ladder is mounted within the living compartment, extending radially from the entrance opening to the outside wall of the cylindrical housing to permit the occupant to move from a zero-gravity environment gradually toward the 1 G environment. A platform, such as an outside ladder, is preferably rotatably mounted outside the module adjacent the entrance opening to permit an occupant standing upon the platform to easily pass through the entrance opening into the living compartment. The living compartment may be furnished and equipped to provide sleeping, recreational, or restroom facilities within a 1 G environment.
    • 一种用于空间飞行器的生活区,包括一个包围用于人员的居室的旋转圆柱形模块,以及用于使模块围绕其纵向中心轴旋转以在模块内邻近外壁产生大约1G的力的装置,以及一个入口 形成在圆柱形模块的一个端壁内,以允许人类共同组合物从空间载体内的零重力空间通到生活空间的人造重力环境中。 内部梯子安装在起居室内,从入口开口径向延伸到圆柱形壳体的外壁,以允许乘员从零重力环境逐渐向G1环境移动。 诸如外梯子的平台优选地可旋转地安装在邻近入口的模块的外部,以允许驻车台上的乘客容易地通过入口进入生活空间。 起居室可以配备和设备,以在1 G环境内提供睡眠,娱乐或洗手间设施。
    • 77. 发明授权
    • Zero gravity liquid mixer
    • 零重液压混合机
    • US3712591A
    • 1973-01-23
    • US3712591D
    • 1971-11-24
    • NASA
    • BOOTH FBRUCE R
    • B01F5/06B01F11/00B64G1/46B01F15/02
    • B64G1/46B01F5/0685B01F11/0045B01F11/0071
    • Apparatus for mixing liquids under conditions of zero gravity is disclosed. The apparatus is comprised of a closed reservoir for the liquids, having a means for maintaining a positive pressure on the liquids in the reservoir. A valved liquid supply line is connected to the reservoir for supplying the reservoir with the liquids to be mixed in the reservoir. The portion of the reservoir containing the liquids to be mixed is in communication with a pump which alternately causes a portion of the liquids to flow out of the pump and into the reservoir to mix the liquids. In a particular embodiment disclosed, the reservoir comprises a sphere having a flexible diaphragm across the diameter thereof. A fluid pressure is applied to the upper side of the diaphragm and the fluids to be mixed are pumped into a section of the sphere on the opposite side of the diaphragm from the fluid pressure. The fluids in the reservoir are in communication through a conduit with the pump which alternately causes a portion of the fluids to flow out of the pump and into the sphere. The conduit connecting the pump and sphere may contain a nozzle or other jet-forming structure such as a venturi for further mixing the fluids. The reservoir may be completely emptied of liquids stored therein.
    • 公开了在零重力条件下混合液体的装置。 该装置包括用于液体的封闭储存器,具有用于维持储存器中液体的正压力的装置。 阀门液体供应管线连接到储存器,用于向储存器供应要在储存器中混合的液体。 包含要混合的液体的储存器的部分与泵连通,所述泵交替地使一部分液体从泵流出并进入储存器以混合液体。 在所公开的特定实施例中,储存器包括在其直径上具有柔性隔膜的球体。 将流体压力施加到隔膜的上侧,并且待混合的流体被泵送到隔膜相对于流体压力的相对侧的球体的一部分中。 储存器中的流体通过具有泵的管道连通,所述导管交替地使一部分流体从泵流出并进入球体。 连接泵和球体的导管可以包含喷嘴或其他喷射形成结构,例如文丘里管,用于进一步混合流体。 储存器可能被完全清空存储在其中的液体。