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1. 发明授权

US06547189B1 Inflatable vessel and method 有权
标题翻译：充气船和方法
公开(公告)号：US06547189B1
公开(公告)日：2003-04-15
申请号：US09826403
申请日：2001-04-02
申请人： Jasen L. Raboin , Gerard D. Valle , Gregg A. Edeen , Horacio M. de la Fuente , William C. Schneider , Gary R. Spexarth , Shalini Gupta Pandya , Christopher J. Johnson
发明人： Jasen L. Raboin , Gerard D. Valle , Gregg A. Edeen , Horacio M. de la Fuente , William C. Schneider , Gary R. Spexarth , Shalini Gupta Pandya , Christopher J. Johnson
IPC分类号： B64G112
CPC分类号： B64G1/56 , B64G1/12 , B64G1/60 , B64G2001/224
摘要： An inflatable module comprising a structural core and an inflatable shell, wherein the inflatable shell is sealingly attached to the structural core. In its launch or pre-deployed configuration, the wall thickness of the inflatable shell is collapsed by vacuum. Also in this configuration, the inflatable shell is collapsed and efficiently folded around the structural core. Upon deployment, the wall thickness of the inflatable shell is inflated; whereby the inflatable shell itself, is thereby inflated around the structural core, defining therein a large enclosed volume. A plurality of removable shelves are arranged interior to the structural core in the launch configuration. The structural core also includes at least one longeron that, in conjunction with the shelves, primarily constitute the rigid, strong, and lightweight load-bearing structure of the module during launch. The removable shelves are detachable from their arrangement in the launch configuration so that, when the module is in its deployed configuration and launch loads no longer exist, the shelves can be rearranged to provide a module interior arrangement suitable for human habitation and work. In the preferred embodiment, to provide efficiency in structural load paths and attachments, the shape of the inflatable shell is a cylinder with semi-toroidal ends.
摘要翻译：一种可膨胀模块，包括结构芯和可充气壳，其中所述可充气壳密封地附接到所述结构芯。在其发射或预部署配置中，可膨胀壳体的壁厚度通过真空折叠。同样在这种构造中，可膨胀的壳被折叠并有效地围绕结构芯折叠。展开后，充气壳的壁厚膨胀; 从而充气壳本身因此在结构芯周围膨胀，在其中限定了大的封闭容积。在发射配置中，多个可移除的搁架布置在结构核心的内部。结构芯还包括至少一个与架子一起构成发射期间模块的刚性，坚固和轻质的承载结构的长度。可拆卸的货架可以在启动配置中与其布置可拆卸，使得当模块处于其部署配置并且不再存在启动负载时，可以重新布置货架以提供适合于人居住和工作的模块内部装置。在优选实施例中，为了提供结构负载路径和附件的效率，可膨胀壳体的形状是具有半环形端部的圆柱体。

2. 发明授权

US5558182A Bending and torsion load alleviator with automatic reset 失效
标题翻译：具有自动复位的弯曲和扭转负载减轻器
公开(公告)号：US5558182A
公开(公告)日：1996-09-24
申请号：US428743
申请日：1995-04-25
申请人： Horacio M. de la Fuente , Michael C. Eubanks , Anthony X. Dao
发明人： Horacio M. de la Fuente , Michael C. Eubanks , Anthony X. Dao
IPC分类号： F16D3/16 , F16D7/08 , F16F7/09 , F16D63/00
CPC分类号： F16D3/16 , F16D7/08 , F16F7/09
摘要： A force transmitting load alleviator apparatus 10 and method are provided for rotatably and pivotally driving a member to be protected against overload torsional and bending (moment) forces. The load alleviator 10 includes at least one bias spring 42 to resiliently bias cam followers 18 and cam surfaces 22 together and to maintain them in locked engagement unless a predetermined load is exceeded whereupon a center housing 12 is pivotal or rotational with respect to a crown assembly 14. This pivotal and rotational movement results in frictional dissipation of the overload force by an energy dissipator 16. The energy dissipator 16 can be provided to dissipate substantially more energy from the overload force than from the bias force that automatically resets the center housing 12 and crown assembly 14 to the normally fixed centered alignment. The torsional and bending (moment) overload levels can designed independently of each other.
摘要翻译：提供一种力传递负载减轻装置10和方法，用于可旋转地和可枢转地驱动要被保护的构件以防过载扭转和弯曲（力）力。负载减轻器10包括至少一个偏置弹簧42，以将凸轮从动件18和凸轮表面22弹性地偏置在一起并且保持它们处于锁定接合，除非超过预定负载，于是中心壳体12相对于冠组件枢转或旋转该枢转和旋转运动导致由能量消散器16产生的过载力的摩擦耗散。可以提供能量消散器16以从过载力中消耗基本上更多的能量，而不是从自动复位中心壳体12和冠组件14到正常固定的中心对准。扭转和弯曲（力矩）过载水平可以彼此独立设计。

3. 发明授权

US06321746B1 Portable hyperbaric chamber 失效
标题翻译：便携式高压舱
公开(公告)号：US06321746B1
公开(公告)日：2001-11-27
申请号：US09574758
申请日：2000-05-17
申请人： William C Schneider , James P. Locke , Horacio M De La Fuente
发明人： William C Schneider , James P. Locke , Horacio M De La Fuente
IPC分类号： A61G1000
CPC分类号： A61G10/026
摘要： A portable, collapsible hyperbaric chamber. A toroidal inflatable skeleton provides initial structural support for the chamber, allowing the attendant and/or patient to enter the chamber. Oval hatches mate against bulkhead rings, and the hyperbaric chamber is pressurized. The hatches seal against an o-ring, and the internal pressure of the chamber provides the required pressure against the hatch to maintain an airtight seal. In the preferred embodiment, the hyperbaric chamber has an airlock to allow the attendant to enter and exit the patient chamber during treatment. Visual communication is provided through portholes in the patient and/or airlock chamber. Life monitoring and support systems are in communication with the interior of the hyperbaric chamber and/or airlock chamber through conduits and/or sealed feed-through connectors into the hyperbaric chamber.
摘要翻译：便携式，可折叠高压舱。环形充气骨架为腔室提供初始结构支撑，允许伴随者和/或患者进入腔室。椭圆形舱口与隔板环配合，高压舱被加压。舱口密封O形环，腔室的内部压力提供所需的压力以保持舱口密封。在优选实施例中，高压舱具有气闸以允许服务员在治疗期间进入和离开患者室。通过患者和/或气锁室中的舷窗提供视觉通信。生命监测和支持系统通过导管和/或密封的馈通连接器进入高压舱与高压舱和/或气闸室的内部连通。

4. 发明授权

US5197573A Energy dissipator 失效
标题翻译：耗能器
公开(公告)号：US5197573A
公开(公告)日：1993-03-30
申请号：US656925
申请日：1991-02-15
申请人： Horacio M. De La Fuente , Kornel Nagy , Clarence J. Wesselski
发明人： Horacio M. De La Fuente , Kornel Nagy , Clarence J. Wesselski
IPC分类号： F16F7/02
CPC分类号： F16F7/02
摘要： An all metal energy dissipator construction for dissipating kinetic energy force (F) by rolling balls (26) which are forced by a tapered surface (32) on an expandable sleeve (22) to frictionally load a force rod (15). The balls (26) are maintained in an initial position (FIG. 1) by a plate member (48) which is biased by a spring member (50). A spring member (52) returns the force rod (15) to its initial position after a loading force (F) is removed.
摘要翻译：一种用于通过滚珠（26）消散动能（F）的全金属能量消散器结构，其被可膨胀套筒（22）上的锥形表面（32）强制以摩擦地加载力杆（15）。球（26）通过由弹簧构件（50）偏压的板构件（48）保持在初始位置（图1）。在去除加载力（F）之后，弹簧构件（52）将力棒（15）返回到其初始位置。

5. 发明授权

US06231010B1 Advanced structural and inflatable hybrid spacecraft module 有权
标题翻译：先进的结构和充气混合航天器模块
公开(公告)号：US06231010B1
公开(公告)日：2001-05-15
申请号：US09236785
申请日：1999-01-25
申请人： William C. Schneider , Horacio M. de la Fuente , Gregg A. Edeen , Kriss J. Kennedy , James D. Lester , Shalini Gupta , Linda F. Hess , Chin H. Lin , Richard H. Malecki , Jasen L. Raboin
发明人： William C. Schneider , Horacio M. de la Fuente , Gregg A. Edeen , Kriss J. Kennedy , James D. Lester , Shalini Gupta , Linda F. Hess , Chin H. Lin , Richard H. Malecki , Jasen L. Raboin
IPC分类号： B64G112
CPC分类号： B64G1/60 , B64G1/12 , B64G1/56 , B64G2001/224
摘要： An inflatable module comprising a structural core and an inflatable shell, wherein the inflatable shell is sealingly attached to the structural core. In its launch configuration, the wall thickness of the inflatable shell is collapsed by vacuum. Also in this configuration, the inflatable shell is collapsed and efficiently folded around the structural core. Upon deployment, the wall thickness of the inflatable shell is inflated; whereby the inflatable shell itself, is thereby inflated around the structural core, defining therein a large enclosed volume. A plurality of removable shelves are arranged interior to the structural core in the launch configuration. The structural core also includes at least one longeron that, in conjunction with the shelves, primarily constitute the rigid, strong, and lightweight load-bearing structure of the module during launch. The removable shelves are detachable from their arrangement in the launch configuration so that, when the module is in its deployed configuration and launch loads no longer exist, the shelves can be rearranged to provide a module interior arrangement suitable for human habitation and work. In the preferred embodiment, to provide efficiency in structural load paths and attachments, the shape of the inflatable shell is a cylinder with semi-toroidal ends.
摘要翻译：一种可膨胀模块，包括结构芯和可充气壳，其中所述可充气壳密封地附接到所述结构芯。在其发射构造中，可膨胀壳体的壁厚度通过真空折叠。同样在这种构造中，可膨胀的壳被折叠并有效地围绕结构芯折叠。展开后，充气壳的壁厚膨胀; 从而充气壳本身因此在结构芯周围膨胀，在其中限定了大的封闭容积。在发射配置中，多个可移除的搁架布置在结构核心的内部。结构芯还包括至少一个与架子一起构成发射期间模块的刚性，坚固和轻质的承载结构的长度。可拆卸的货架可以在启动配置中与其布置可拆卸，使得当模块处于其部署配置并且不再存在启动负载时，可以重新布置货架以提供适合于人居住和工作的模块内部装置。在优选实施例中，为了提供结构负载路径和附件的效率，可膨胀壳体的形状是具有半环形端部的圆柱体。

6. 发明授权

US5441221A Heavy-lift vehicle-launched space station method and apparatus 失效
标题翻译：重型车载空间站方法和装置
公开(公告)号：US5441221A
公开(公告)日：1995-08-15
申请号：US161038
申请日：1993-12-03
申请人： Donald C. Wade , Horacio M. De La Fuente , Reginald B. Berka , Steven L. Rickman , Edgar O. Castro , Kornel Nagy , Clarence J. Wesselski , Timothy E. Pelischek , John A. Schliesing
发明人： Donald C. Wade , Horacio M. De La Fuente , Reginald B. Berka , Steven L. Rickman , Edgar O. Castro , Kornel Nagy , Clarence J. Wesselski , Timothy E. Pelischek , John A. Schliesing
IPC分类号： B64G1/12 , B64G1/14 , B64G1/24 , B64G1/28 , B64G99/00 , B64G1/60 , B64G1/22 , B64G1/44
CPC分类号： B64G1/28 , B64G1/12 , B64G1/14 , B64G1/24 , B64G9/00
摘要： Methods and apparatus are provided for a single heavy-lift launch to place a complete, operational space station on-orbit. A payload including the space station takes the place of a Shuttle Orbiter using the launch vehicle of the Shuttle Orbiter. The payload includes a forward shroud, a core module, a propulsion module, and a transition module between the core module and the propulsion module. The essential subsystems are pre-integrated and verified on Earth. The core module provides means for attaching international modules with minimum impact to the overall design. The space station includes six control moment gyros for selectably operating in either LVLH (local-vertical local-horizontal) or SI (solar inertial) flight modes.
摘要翻译：为单个重型起重机提供了方法和装置，以便在轨上放置一个完整的，可操作的空间站。包括空间站的有效载荷代替了Shuttle Orbiter，使用Shuttle Orbiter的运载火箭。该有效载荷包括前护罩，芯模块，推进模块以及在核心模块和推进模块之间的过渡模块。基本子系统是在地球上预先集成和验证的。核心模块提供了连接国际模块的方法，对整体设计的影响最小。空间站包括六个控制力矩陀螺仪，用于可选择地在LVLH（局部垂直局部水平）或SI（太阳能惯性）飞行模式下操作。

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