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公开(公告)号：US5624088A
公开(公告)日：1997-04-29
申请号：US521366
申请日：1995-08-31
申请人： John N. Fiore
发明人： John N. Fiore
摘要： Spacecraft structure for use in the construction of the outer wall of a spacecraft. The construction of the outer wall of the spacecraft includes a hollow cellular honeycomb material that is sandwiched between a thin outer curved solid panel and a thin solid inner panel that has at least a portion that has a substantially flat inner surface. The inner and/or outer panel have provisions for mounting at least a portion of the payload for the spacecraft utilizing a series of inserts secured to the inner or outer panel. The outer and/or inner spacecraft wall panel structure can also include heat pipes for use in heat transfer. In one embodiment of the invention the outer panel also includes a series of substantially flat surfaces. The invention also includes the method of construction of the spacecraft structure and its method of use.
摘要翻译： 用于建造航天器外墙的航天器结构。 航天器外壁的结构包括中空细胞蜂窝状材料，其夹在薄的外部弯曲实心面板和薄的固体内部面板之间，该内部面板具有至少一部分具有基本平坦的内表面。 内板和/或外板具有用于使用固定到内板或外板的一系列插入件来安装用于航天器的有效载荷的至少一部分的装置。 外部和/或内部航天器壁板结构还可以包括用于热传递的热管。 在本发明的一个实施例中，外板还包括一系列基本平坦的表面。 本发明还包括航天器结构的构造方法及其使用方法。
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公开(公告)号：US5326040A
公开(公告)日：1994-07-05
申请号：US51336
申请日：1993-04-23
申请人： Richard E. Kramer
发明人： Richard E. Kramer
CPC分类号： H01Q1/30
摘要： A sphere and cable deployer apparatus for deploying a cable and associated sphere from a vehicle such as a satellite. The sphere and cable deployer apparatus has a drum for storing the cable that is driven by a drive shaft and gears form a drive motor to deploy the cable/sphere away. The drive motor also drives a drive roller through a series of gears and clutches that applies tension to the cable as it is being unwound from the drum. The sphere and cable deployer apparatus also has a sphere housing with two shell-like halves that pivot outward due to spring forces to release the sphere. The pivoting housing halves also provide a storage compartment for a short cable that is attached to the outer surface of the sphere. The pivoting housing halves are held in place by two cables that are under tension and associated pins that fit in holes in the housing halves and are released by cable cutters that cut the cables.
摘要翻译： 用于从诸如卫星的车辆部署电缆和相关球体的球体和电缆部署器装置。 球和电缆部署器设备具有用于存储由驱动轴驱动的电缆的鼓，齿轮形成驱动马达以将电缆/球体部署。 驱动电机还通过一系列齿轮和离合器来驱动驱动辊，当从滚筒展开时，离合器对电缆施加张力。 球和电缆部署器装置还具有球壳，其具有两个壳状半部，其由于弹力而向外枢转以释放球体。 枢转壳体半部还提供用于连接到球体的外表面的短电缆的存储隔间。 枢转壳体半部通过处于张力处的两根电缆和相关销钉保持在适当的位置，所述电缆适配于壳体半部中的孔中并且由切割电缆的电缆切割器释放。
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公开(公告)号：US5191914A
公开(公告)日：1993-03-09
申请号：US708056
申请日：1991-05-30
申请人： Antonio E. Gonzalez
发明人： Antonio E. Gonzalez
CPC分类号： F16L29/04 , F16L37/34 , F16L37/35 , Y10T137/87925 , Y10T137/87949
摘要： A redundant fluid coupling with two coupling assemblies adapted to engage each other and permit fluid flow between the coupling assemblies when they are connected. Each coupling assembly has two functionally independent valves for closing off the fluid flow from the coupling assembly when the coupling assemblies are disconnected. The independent valves are reciprocally operated by coil springs and since they are functionally independent, the failure of one valve of the coupling assembly to operate will not affect the operation of the other valve. The interior portions of each coupling assembly are pivotally mounted which permits the coupling assemblies to be connected together even though they may be offset from each other and/or form an angle with each other.
摘要翻译： 具有两个联接组件的冗余流体联接件，其适于彼此接合并且当连接组件之间允许流体在联接组件之间流动。 每个联接组件具有两个功能上独立的阀，用于在联接组件断开时封闭来自联接组件的流体流。 独立阀由螺旋弹簧往复操作，并且由于它们在功能上是独立的，联接组件的一个阀的故障不会影响另一个阀的操作。 每个联接组件的内部部分被枢转地安装，这允许联接组件连接在一起，即使它们彼此偏移和/或彼此形成一个角度。
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公开(公告)号：US5095707A
公开(公告)日：1992-03-17
申请号：US478539
申请日：1990-02-12
申请人： Marshall B. Eck
发明人： Marshall B. Eck
CPC分类号： G21D5/02 , B64G1/421 , F02C1/05 , F02C7/052 , Y10S165/903
摘要： A method for generating power and a power supply for use in the atmosphere on Mars that use the Martian atmosphere as a working fluid. The power supply has an open Brayton cycle combined turbocompressor and turbogenerator that use the Martian atmosphere for their operation. The Martian atmosphere working fluid picks up heat derived from a nuclear heat source that transfers the heat to the working fluid by laminar flow heat exchange. The combined turbocompressor and turbogenerator have provisions for separating dust from the dust laden Martian atmosphere and for operating with any residual Martian atmospheric dust that is ingested into the combined turbocompressor and turbogenerator. Reliability of operation is achieved by having two functionally separate power operating units that each have their own combined turbocompressor and turbogenerator and by only using one power unit at a time.
摘要翻译： 一种用于在火星上使用火星大气作为工作流体的大气中使用的电力和电源的方法。 电源有一个开放的Brayton循环组合涡轮压缩机和涡轮发电机，使用火星的气氛进行操作。 火星大气层的工作流体吸收源自核热源的热量，通过层流热交换将热量传递给工作流体。 组合式涡轮压缩机和涡轮发电机具有分离灰尘和满载的火星大气层的作用，以及与吸入涡轮压缩机和涡轮发电机组合的任何残留的火星大气尘埃的运行。 操作的可靠性通过使两个功能分离的动力操作单元各自具有它们自己的组合涡轮压缩机和涡轮发电机以及一次仅使用一个动力单元来实现。
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公开(公告)号：US5474262A
公开(公告)日：1995-12-12
申请号：US193465
申请日：1994-02-08
申请人： John N. Fiore
发明人： John N. Fiore
摘要： Spacecraft structure for use in the construction of the outer wall of a spacecraft. The construction of the outer wall of the spacecraft includes a hollow cellular honeycomb material that is sandwiched between a thin outer curved solid panel and a thin solid inner panel that has at least a portion that has a substantially flat inner surface. The inner and/or outer panel have provisions for mounting at least a portion of the payload for the spacecraft utilizing a series of inserts secured to the inner or outer panel. The outer and/or inner spacecraft wall panel structure can also include heat pipes for use in heat transfer. In one embodiment of the invention the outer panel also includes a series of substantially flat surfaces. The invention also includes the method of construction of the spacecraft structure and its method of use.
摘要翻译： 用于建造航天器外墙的航天器结构。 航天器外壁的结构包括中空细胞蜂窝状材料，其夹在薄的外部弯曲实心面板和薄的固体内部面板之间，该内部面板具有至少一部分具有基本上平坦的内表面。 内板和/或外板具有用于使用固定到内板或外板的一系列插入件来安装用于航天器的有效载荷的至少一部分的装置。 外部和/或内部航天器壁板结构还可以包括用于热传递的热管。 在本发明的一个实施例中，外板还包括一系列基本平坦的表面。 本发明还包括航天器结构的构造方法及其使用方法。
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公开(公告)号：USD310827S
公开(公告)日：1990-09-25
申请号：US159644
申请日：1988-02-24
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公开(公告)号：US5776797A
公开(公告)日：1998-07-07
申请号：US887430
申请日：1997-07-02
IPC分类号： H01L23/538 , H01L25/065 , H01L21/60
CPC分类号： H01L23/5387 , H01L25/0657 , H01L2224/16225 , H01L2224/32145 , H01L2224/32225 , H01L2224/73204 , H01L2224/73253 , H01L2225/06517 , H01L2225/06579 , H01L2225/06582 , H01L2225/06586 , H01L2924/01079 , H01L2924/09701 , H01L2924/10253 , H01L2924/15311 , H01L2924/16152
摘要： A three dimensional flexible assembly of integrated circuits and method of fabricating the assembly of circuits including a folded flexible substrate with integrated circuit chips. The invention has provisions for allowing mechanical and electrically functional attachment of integrated circuit chips to one or both sides of the flexible substrate using flip chip assembly techniques. In addition, a rigid package substrate is provided upon which the folded substrate is secured with the associated chips. The chips are electrically connected to the flexible substrate and the flexible substrate is in turn electrically connected to the rigid substrate. A cover is also provided that covers and protects the flexible substrate and the associated chips as well as a portion of the connected rigid package substrate. In an additional embodiment, the cover and rigid substrate are omitted and instead the combined folded flexible substrate and integrated circuit chips are encapsulated with a suitable compound.
摘要翻译： 集成电路的三维柔性组件和制造电路组件的方法，包括具有集成电路芯片的折叠柔性衬底。 本发明具有允许使用倒装芯片组装技术将集成电路芯片机械和电功能地附接到柔性衬底的一侧或两侧的部件。 此外，提供刚性封装衬底，折叠衬底与相关联的芯片固定在其上。 芯片电连接到柔性基板，柔性基板又电连接到刚性基板。 还提供了覆盖并保护柔性基板和相关芯片以及连接的刚性封装基板的一部分的盖。 在另外的实施例中，盖和刚性衬底被省略，而是组合的折叠的柔性衬底和集成电路芯片用合适的化合物封装。
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公开(公告)号：US5646446A
公开(公告)日：1997-07-08
申请号：US577843
申请日：1995-12-22
IPC分类号： H01L23/538 , H01L25/065 , H01L23/34
CPC分类号： H01L23/5387 , H01L25/0657 , H01L2224/16225 , H01L2224/32145 , H01L2224/32225 , H01L2224/73204 , H01L2224/73253 , H01L2225/06517 , H01L2225/06579 , H01L2225/06582 , H01L2225/06586 , H01L2924/01079 , H01L2924/09701 , H01L2924/10253 , H01L2924/15311 , H01L2924/16152
摘要： A three dimensional flexible assembly of integrated circuits and method of fabricating the assembly of circuits including a folded flexible substrate with integrated circuit chips. The invention has provisions for allowing mechanical and electrically functional attachment of integrated circuit chips to one or both sides of the flexible substrate using flip chip assembly techniques. In addition, a rigid package substrate is provided upon which the folded substrate is secured with the associated chips. The chips are electrically connected to the flexible substrate and the flexible substrate is in turn electrically connected to the rigid substrate. A cover is also provided that covers and protects the flexible substrate and the associated chips as well as a portion of the connected rigid package substrate In an additional embodiment, the cover and rigid substrate are omitted and instead the combined folded flexible substrate and integrated circuit chips are encapsulated with a suitable compound.
摘要翻译： 集成电路的三维柔性组件和制造电路组件的方法，包括具有集成电路芯片的折叠柔性衬底。 本发明具有允许使用倒装芯片组装技术将集成电路芯片机械和电功能地附接到柔性衬底的一侧或两侧的部件。 此外，提供刚性封装衬底，折叠衬底与相关联的芯片固定在其上。 芯片电连接到柔性基板，柔性基板又电连接到刚性基板。 还提供了覆盖并保护柔性基板和相关联的芯片以及连接的刚性封装衬底的一部分的盖。在另外的实施例中，省略了盖和刚性衬底，而代之以组合的折叠柔性衬底和集成电路芯片 用合适的化合物包封。
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公开(公告)号：US5494234A
公开(公告)日：1996-02-27
申请号：US193463
申请日：1994-02-08
申请人： Richard E. Kramer
发明人： Richard E. Kramer
摘要： A sphere and cable deployer apparatus for deploying a cable and associated spheres from a vehicle such as a spinning satellite. The sphere and cable deployer apparatus has a drum for storing the cable that is driven by a drive shaft and gears form a drive motor to deploy the cable and sphere away from the satellite. The drive motor also drives a drive roller through a series of gears and clutch that applies tension to the cable as it is being unwound from the drum. The sphere and cable deployer apparatus also has a housing with an outer and inner pair of shell-like halves that pivot outward due to spring forces to release the spheres. Each pair of pivoting housing halves also provide a storage compartment for a short cable portion that is attached to that sphere. The outer set of pivoting housing halves are held in place by two cables that are under tension and associated pins that fit in holes in the housing halves and are released by cable cutters that cut the cables, and the inner housing halves are held in place by explosive bolts that may be activated by a protrusion on the cable portion located between the spheres and an associated microswitch as the cable portion is deployed.
摘要翻译： 一种用于从诸如旋转卫星的车辆部署电缆和相关球体的球体和电缆部署器装置。 球和电缆部署器设备具有用于存储由驱动轴驱动的电缆的鼓，齿轮形成驱动马达以将电缆和球体远离卫星展开。 驱动电机还通过一系列齿轮和离合器驱动驱动辊，当电缆从滚筒展开时，该电缆对电缆施加张力。 球体和电缆部署器装置还具有壳体，外壳和内部一对壳状半部由于弹簧力向外转动以释放球体。 每对枢转的外壳半部还提供一个用于连接到该球体的短电缆部分的储存室。 外部的一组旋转壳体半部通过处于张力下的两根电缆保持在适当的位置，并且相关联的销适合于壳体半部中的孔中，并且由切割电缆的电缆切割器释放，并且内壳体半部被保持在适当位置 当电缆部分展开时，可能由位于球体和相关联的微型开关之间的电缆部分上的突起激活的爆炸螺栓。
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公开(公告)号：US5356095A
公开(公告)日：1994-10-18
申请号：US924489
申请日：1992-08-04
申请人： Gary I. Aker
发明人： Gary I. Aker
CPC分类号： B64G1/222 , B64G1/44 , B64G1/64 , Y10T16/53826 , Y10T16/53888 , Y10T16/55963
摘要： Deployment apparatus for use in deploying an articulating structure. The deployment apparatus includes two pivotally connected hinge members and a spring that biases the hinge members in their open or deployed positions. An attenuator is also connected to one of the hinge members that prevents oscillatory movement between the hinge members as they are assuming their deployed positions and a cam member and a lobe on one of the hinge members lock the hinge members in position together as the hinge members are being extended to their deployed positions. The attenuator is adjustable and can be used to precisely fix the position of the deployed hinge members. The deployment apparatus is particularly suited for a wide variety of spacecraft applications where it can be used to extend spacecraft structures such as solar panels.
摘要翻译： 用于展开铰接结构的展开装置。 展开装置包括两个枢转连接的铰链构件和弹簧，其将铰链构件偏压在其打开或展开位置。 衰减器还连接到铰链构件中的一个，当它们处于展开位置时，防止铰链构件之间的摆动运动，并且凸轮构件和其中一个铰链构件上的凸角将铰链构件一起锁定在一起，因为铰链构件 正在扩展到他们的部署职位。 衰减器是可调节的，可用于精确地固定展开的铰链构件的位置。 该展开装置特别适用于各种各样的航天器应用，其中它们可用于延伸航天器结构，如太阳能电池板。
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