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1. 发明授权

US5318255A Stage separation mechanism for space vehicles 失效
标题翻译：航天器舞台分离机制
公开(公告)号：US5318255A
公开(公告)日：1994-06-07
申请号：US902270
申请日：1992-06-22
申请人： Andrew B. Facciano , Rudolph A. Eisentraut , Stephen D. Haight , Ryan D. Lamberton , John D. Smith
发明人： Andrew B. Facciano , Rudolph A. Eisentraut , Stephen D. Haight , Ryan D. Lamberton , John D. Smith
IPC分类号： B64G1/64 , F42B15/36
CPC分类号： B64G1/641 , F42B15/36
摘要： A mechanism locking and controllably releasing two space vehicles along a preselected separation axis. The mechanism including a mechanical lock/release and a spring separation device that controllably forces the two space vehicles apart. An electrical interconnect maintains electrical communication between the two space vehicles when locked together. The two space vehicles can be reliably separated by activating a single disengagement actuator.
摘要翻译：沿着预先选择的分离轴线锁定并可控地释放两个太空车辆的机构。该机构包括机械锁定/释放和弹性分离装置，其可控制地迫使两个太空车分开。电气互连维持两个空间车辆锁定在一起时的电气连通。通过激活单个分离致动器，两个太空车辆可以可靠地分离。

2. 发明授权

US06354559B1 Instrument suspension system for preserving alignment 失效
标题翻译：用于保持对准的仪表悬挂系统
公开(公告)号：US06354559B1
公开(公告)日：2002-03-12
申请号：US08506060
申请日：1995-07-24
申请人： Rudolph A. Eisentraut
发明人： Rudolph A. Eisentraut
IPC分类号： F41G726
CPC分类号： F41G7/2213
摘要： A passive suspension system for supporting an instrument relative to a rigid support structure while preserving angular alignment of the instrument. The suspension system includes an instrument platform, the instrument being secured to the platform, and first and second vibration isolator systems. The first ends of the isolator systems are attached to the rigid support structure so that axes of the vibration isolators extend transverse to the instrument axis. The first and second isolator systems resist motion transverse to the instrument axis and provide shock and vibration isolation transverse to the instrument axis. First, second and third stabilizing struts extend parallel to each other and the instrument axis, and are of equal length. A first set of bearings connects ends of the struts to the instrument platform in a spaced relationship, and allows motion transverse to the struts. A second set of bearings connects opposing ends of the struts to the rigid support structure in a spaced relationship. The second set of bearings permits motion transverse to the struts.
摘要翻译：一种被动悬架系统，用于相对于刚性支撑结构支撑仪器，同时保持仪器的角度对准。悬架系统包括仪器平台，仪器固定在平台上，以及第一和第二隔振系统。隔离器系统的第一端附接到刚性支撑结构，使得隔振器的轴线横向于仪器轴线延伸。第一和第二隔离器系统抵抗横向于仪器轴线的运动，并提供横向于仪器轴线的冲击和振动隔离。首先，第二和第三稳定支柱彼此平行延伸并且与仪器轴线平行，并具有相等的长度。第一组轴承将支柱的端部以间隔的关系连接到仪器平台，并允许横向于支柱的运动。第二组轴承将支柱的相对端部以间隔的关系连接到刚性支撑结构。第二组轴承允许横向于支柱的运动。

3. 发明授权

US06928400B2 Method for designing a deployment mechanism 失效
标题翻译：设计部署机制的方法
公开(公告)号：US06928400B2
公开(公告)日：2005-08-09
申请号：US09969453
申请日：2001-10-02
申请人： Rudolph A. Eisentraut , Edgar R. Melkers
发明人： Rudolph A. Eisentraut , Edgar R. Melkers
IPC分类号： B64C5/12 , G06G7/48 , B64C3/56 , F42B10/00
CPC分类号： B64C5/12
摘要： The present invention concerns a method for designing a deployment mechanism for a flight surface on an airborne body, including the steps of determining a stowed position of the flight surface, determining a deployed position of the flight surface, identifying a first rotation axis and respective rotation angle and a second rotation axis and respective rotation angle about and through which the flight surface is rotatable in sequence to move the flight surface from the stowed position to the deployed position, or vice versa, and using the identified first and second rotation axes and rotation angles to determine a single equivalent rotation axis and angle, about and through which the flight surface can be rotated from the stowed position to the deployed position, or vice versa.
摘要翻译：本发明涉及一种用于设计空中机体上的飞行表面的展开机构的方法，包括以下步骤：确定飞行表面的收起位置，确定飞行表面的展开位置，识别第一旋转轴线和相应旋转角度和第二旋转轴线以及相应的旋转角度，飞行表面可以依次旋转，并且通过该旋转角度将飞行表面从收起位置移动到展开位置，反之亦然，并且使用所识别的第一和第二旋转轴线和旋转角度以确定单个等效旋转轴线和角度，飞行表面可以从收起位置旋转到展开位置，反之亦然。

4. 发明授权

US5016476A Optical fiber bending stress proof tester 失效
标题翻译：光纤弯曲应力测试仪
公开(公告)号：US5016476A
公开(公告)日：1991-05-21
申请号：US385030
申请日：1989-07-25
申请人： Stanley P. D. Peterson , Rudolph A. Eisentraut
发明人： Stanley P. D. Peterson , Rudolph A. Eisentraut
IPC分类号： G01M11/08 , G01N3/02 , G01N3/08 , G01N33/38
CPC分类号： G01N3/08 , G01M11/088 , G01N2203/0278 , G01N2203/028 , G01N33/386
摘要： An optical fiber bending stress proof tester 40 which provides multiple mandrels or roller elements 22 and 24 for applying compression and tension stresses to multiple planes on the periphery of an optical fiber 10. In one embodiment, first and second roller elements 22 and 24 are incorporated in a roller block 50 which is stable in either of two angular orientations with respect to the longitudinal axis of the fiber 10. The fiber 10 is bent in an S curve around the two rollers 22 and 24. The rollers 22 and 24 control the bend radius and therefore the stress induced in the outer fibers of the filament. In a specific extension of this embodiment, multiple sets of first and second roller elements are provided in additional roller blocks. Each block is stable in a first loading position and a second test position. In the test position, discrete planes around the entire periphery of the fiber are exposed to bending stress in a single pass through the tester. A device constructed in accordance with the teachings of the invention would effectively bend the fiber in several planes with a controlled bend radius. More significantly, the device would subject the fiber to high stress levels for a very short period of time thereby minimizing the possibility of damaging the fiber.
摘要翻译：一种光纤弯曲应力测试仪40，其提供多个心轴或滚轮元件22和24，用于对光纤10的周边上的多个平面施加压缩和拉伸应力。在一个实施例中，结合了第一和第二滚子元件22和24 在相对于纤维10的纵向轴线的两个角度取向中的任一个中稳定的辊块50中。纤维10围绕两个辊22和24以S曲线弯曲。辊22和24控制弯曲因此在细丝的外纤维中引起的应力。在该实施例的特定的延伸部分中，多组第一和第二滚子元件设置在附加的滚动块中。每个块在第一装载位置和第二测试位置是稳定的。在测试位置，围绕纤维整个周边的离散平面在穿过测试仪的单次通过中暴露于弯曲应力。根据本发明的教导构造的装置将有效地弯曲具有受控弯曲半径的多个平面中的光纤。更重要的是，该设备将使纤维在非常短的时间段内受到高应力水平，从而最小化损坏光纤的可能性。

5. 发明授权

US07185847B1 Winged vehicle with variable-sweep cantilevered wing mounted on a translating wing-support body 有权
标题翻译：具有安装在平移翼支撑体上的可变扫描悬臂翼的翼形车辆
公开(公告)号：US07185847B1
公开(公告)日：2007-03-06
申请号：US10845700
申请日：2004-05-13
申请人： Mark L. Bouchard , Purna Gogineni , Rudolph A. Eisentraut , Juan A. Perez , Kevin Greenwood
发明人： Mark L. Bouchard , Purna Gogineni , Rudolph A. Eisentraut , Juan A. Perez , Kevin Greenwood
IPC分类号： B64C3/40
CPC分类号： F42B10/12
摘要： A winged vehicle includes an elongated fuselage, and a wing mechanism affixed to the fuselage. The wing mechanism has a wing-support-body track affixed to and extending lengthwise along the fuselage, a translating wing-support body engaged to and translatable along the wing-support-body track, and exactly two deployable cantilevered wings. Each deployable cantilevered wing has a wing pivot mounted to the translating wing-support body so that the deployable cantilevered wing is pivotable about the translating wing-support body. The two deployable cantilevered wings are each pivotable between a stowed position and a deployed position. An actuation mechanism is operable to controllably move the translating wing-support body along the wing-support-body track and to controllably move the two deployable cantilevered wings between the stowed position and the deployed position.
摘要翻译：有翼的车辆包括细长的机身以及固定在机身上的机翼机构。机翼机构具有固定在机身上并沿着机身纵向延伸的机翼支撑体轨道，平行翼支撑体与机翼支撑体轨道接合并可平移，以及恰好两个可展开的悬臂翼。每个可部署的悬臂翼具有安装到平移翼支撑体的翼形枢轴，使得可展开的悬臂可围绕平移翼支撑体枢转。两个可展开的悬臂翼可以在收起位置和展开位置之间枢转。致动机构可操作以可操作地沿着机翼支撑体轨道移动平移翼支撑体，并且可控制地将两个可展开悬臂的翼移动到收起位置和展开位置之间。

6. 发明授权

US5178313A Pneumatic shoe for high speed filamentary capstan 失效
标题翻译：用于高速丝状绞盘的气动鞋
公开(公告)号：US5178313A
公开(公告)日：1993-01-12
申请号：US706453
申请日：1991-05-28
申请人： George LeCompte , Rudolph A. Eisentraut , Moran Coxon
发明人： George LeCompte , Rudolph A. Eisentraut , Moran Coxon
IPC分类号： B65H51/04 , B65H51/16
CPC分类号： B65H51/04 , B65H51/16
摘要： An apparatus for uniformly applying a compressive force against a filament to pneumatically drive the filament or fiber optic cable against a capstan without any concentrated amount of stress at any point on the filament is effectuated by pneumatically forcing the filament into an equatorial V-groove defined in the capstan. Pneumatic pressure is applied to a predefined segment of the capstan by a pneumatic shoe having an internal shoe pressure chamber. The pressurized gas or air is applied to the segment from the chamber within the shoe into the proximity of the equatorial V-groove on the equator of a disc shaped capstan. The V-groove is vented to atmosphere so that the cable is forced or blown into the V-groove. Side and end clearances between the rotating capstan and the shoe are sized to allow the viscosity of the pressurized gas to operate to retard the escape of the pressurized gas from the predefined segment of the capstan. Annular interleaved baffles may also be provided on the equatorial surface of the capstan and the opposing surface of the shoe to provide additional frictional engagement between the pressurized gas and the elements in the proximity of the predetermined segment of the capstan. Utilizing such an arrangement, approximately 10 kilometers or more of filament can be paid out in approximately 32 seconds or less.
摘要翻译：一种用于均匀地施加针对细丝的压缩力的装置通过气动地强迫灯丝进入限定在其中的赤道V形槽来实现，所述装置通过气动地迫使灯丝进入到绞盘气动压力通过具有内部鞋压力室的气动靴施加到主导轴的预定段。加压气体或空气被施加到从鞋内的腔室到在盘形绞盘的赤道上的赤道V形槽的附近。 V形槽被排放到大气中，使得电缆被迫或吹入V形槽。旋转的绞盘和鞋之间的侧面和端部间隙的尺寸设定为允许加压气体的粘度操作以阻止加压气体从主动轮的预定段分离。也可以在主导轴的赤道表面和鞋的相对表面上提供环形交错挡板，以在加压气体和主动轮的预定段附近的元件之间提供额外的摩擦接合。利用这种布置，可以在大约32秒或更短的时间内支付大约10公里或更长的灯丝。

7. 发明授权

US5042914A Lens focusing mechanism 失效
标题翻译：镜头聚焦机制
公开(公告)号：US5042914A
公开(公告)日：1991-08-27
申请号：US426830
申请日：1989-10-25
申请人： George H. Hulderman , Rudolph A. Eisentraut , John O. Breninger , Harold E. Andrews
发明人： George H. Hulderman , Rudolph A. Eisentraut , John O. Breninger , Harold E. Andrews
IPC分类号： F41G3/00 , F42B15/01 , G02B7/02 , G02B7/09 , G02B7/10 , G02B13/22
CPC分类号： G02B13/22 , G02B7/10
摘要： A lens focusing mechanism 10 including a bracket 18 for retaining a lens 14. The bracket 18 has a bearing 22 attached thereto or integral therewith. The bearing 22 is eccentric relative to the leans 14 and is effective to move the lens 14 along an optical axis 16 thereof. Movement is effectuated by a drive mechanism 34 in a smooth manner and without lubrication. In a specific embodiment, the bearing 22 is eccentric and external to a cylindrical volume defined by the periphery of the lens 14.

8. 发明授权

US5038990A Pneumatic shoe for high speed filamentary capstan 失效
标题翻译：用于高速丝状绞盘的气动鞋
公开(公告)号：US5038990A
公开(公告)日：1991-08-13
申请号：US566787
申请日：1990-08-13
申请人： George LeCompte , Rudolph A. Eisentraut , Moran Coxon
发明人： George LeCompte , Rudolph A. Eisentraut , Moran Coxon
IPC分类号： B65H51/04 , B65H51/16
CPC分类号： B65H51/04 , B65H51/16
摘要： An apparatus and methodology for uniformly applying a compressive force against a filament to pneumatically drive the filament or fiber optic cable against a capstan without any concentrated amount of stress at any point on the filament is effectuated by pneumatically forcing the filament into an equatorial V-groove defined in the capstan. Pneumatic pressure is applied to a predefined segment of the capstan by a pneumatic shoe having an internal shoe pressure chamber. The pressurized gas or air is applied to the segment from the chamber within the shoe into the proximity of the equatorial V-groove on the equator of a disc shaped capstan. The V-groove is vented to atmosphere so that the cable is forced or blown into the V-groove. Side and end clearances between the rotating capstan and the shoe are sized to allow the viscosity of the pressurized gas to operate to retard the escape of the pressurized gas from the predefined segment of the capstan. Annular interleaved baffles may also be provided on the equatorial surface of the capstan and the opposing surface of the shoe to provide additional frictional engagement between the pressurized gas and the elements in the proximity of the predetermined segment of the capstan. Utilizing such an arrangement, approximately 10 kilometers or more of filament can be paid out in approximately 32 seconds or less.
摘要翻译：一种用于均匀地施加针对细丝的压缩力以将细丝或光纤电缆气动地驱动以驱动绞盘的装置和方法，而在灯丝上的任何点处没有任何集中的应力，通过气动地迫使灯丝进入赤道V形槽在绞盘中定义。气动压力通过具有内部鞋压力室的气动靴施加到主导轴的预定段。加压气体或空气被施加到从鞋内的腔室到在盘形绞盘的赤道上的赤道V形槽的附近。 V形槽被排放到大气中，使得电缆被迫或吹入V形槽。旋转的绞盘和鞋之间的侧面和端部间隙的尺寸设定为允许加压气体的粘度操作以阻止加压气体从主动轮的预定段分离。也可以在主导轴的赤道表面和鞋的相对表面上提供环形交错挡板，以在加压气体和主动轮的预定段附近的元件之间提供额外的摩擦接合。利用这种布置，可以在大约32秒或更短的时间内支付大约10公里或更长的灯丝。

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