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公开(公告)号：US20140018559A1
公开(公告)日：2014-01-16
申请号：US14007239
申请日：2012-03-23
申请人： Kornel Nagy , Komel Nagy , Frederic Destaillats , Brian Craft
发明人： Kornel Nagy , Komel Nagy , Frederic Destaillats , Brian Craft
IPC分类号： C11B3/00
摘要： The present invention generally relates to the field of refined oils. In particular, the present invention relates to refined plant oils substantially free of chlorinated contaminants, such as monochloropropanediol (MCPD), in particular 3-MCPD diesters, and to a process to produce such oils. To achieve this, plant material is washed to remove chlorine donors before a crude oil is produced that subsequently is further refined.
摘要翻译： 本发明一般涉及精炼油领域。 特别地，本发明涉及基本上不含氯化污染物的精制植物油，例如单氯丙二醇（MCPD），特别是3-MCPD二酯，以及生产这种油的方法。 为了实现这一点，在生产原油之前，将植物材料洗涤以除去氯供体，随后进一步精制。
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公开(公告)号：US20140018562A1
公开(公告)日：2014-01-16
申请号：US14007410
申请日：2012-03-23
IPC分类号： A23D9/04
摘要： The present invention generally relates to the field of refined oils. In particular, the present invention relates to refined plant oils substantially free of chlorinated contaminants, such as monochloropropanediol (MCPD), in particular 3-MCPD di-esters, and to a process to produce such oils. To achieve this, at least one alcohol is added to the oil during refinement.
摘要翻译： 本发明一般涉及精炼油领域。 特别地，本发明涉及基本上不含氯化污染物的精制植物油，例如一氯丙二醇（MCPD），特别是3-MCPD二酯，以及生产这种油的方法。 为了达到这个目的，在精炼过程中至少加入一种醇。
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公开(公告)号：US20140018561A1
公开(公告)日：2014-01-16
申请号：US14007233
申请日：2012-03-23
IPC分类号： A23D9/04
摘要： The present invention generally relates to the field of oil refinement. In particular, the present invention relates to the field of processes to produce refined oils, substantially free of contaminants, such as glycidyl esters, for example. In accordance with the present invention, such refined plant oils free of glycidyl esters may be obtained by using plant oil or a plant oil fractions having a maximum level of 3 weight-% diacylglycerols (DAG) in the oil refinement process.
摘要翻译： 本发明一般涉及油精制领域。 特别地，本发明涉及生产精炼油的方法领域，例如基本上不含污染物，例如缩水甘油酯。 根据本发明，可以通过在油精制过程中使用植物油或具有最大含量为3重量％的二酰基甘油（DAG）的植物油馏分而获得不含缩水甘油酯的这种精制植物油。
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公开(公告)号：US20140018560A1
公开(公告)日：2014-01-16
申请号：US14007036
申请日：2012-03-23
摘要： The present invention generally relates to the field of refined oils. In particular, the present invention relates to refined plant oils substantially free of chlorinated contaminants, such as monochloropropanediol (MCPD), in particular 3-MCPD di-esters, and to a process to produce such oils. To achieve this, crude oil is liquid-liquid extracted to remove chlorine donors before it is further refined.
摘要翻译： 本发明一般涉及精炼油领域。 特别地，本发明涉及基本上不含氯化污染物的精制植物油，例如一氯丙二醇（MCPD），特别是3-MCPD二酯，以及生产这种油的方法。 为了达到这个目的，在进一步精炼之前，原油被液 - 液萃取以除去氯供体。
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公开(公告)号：US5197573A
公开(公告)日：1993-03-30
申请号：US656925
申请日：1991-02-15
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。
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公开(公告)号：US4817895A
公开(公告)日：1989-04-04
申请号：US110060
申请日：1987-10-14
申请人： Carl D. Scott , Kornel Nagy , Barney B. Roberts , Robert C. Ried , Kenneth R. Kroll , Joe Gamble
发明人： Carl D. Scott , Kornel Nagy , Barney B. Roberts , Robert C. Ried , Kenneth R. Kroll , Joe Gamble
摘要： An aerobraking orbital transfer vehicle which includes an aerobraking device which also serves as a heat shield in the shape of a raked-off elliptic or circular cone with a circular or elliptical base, and with an ellipsoid or other blunt shape nose. The aerobraking device is fitted with a toroid-like skirt and is integral with the support structure of the propulsion system and other systems of the space vehicle. The vehicle is intended to be transported in components to a space station in lower earth orbit where it is assembled for use as a transportation system from low earth orbit to geosynchronous earth orbit and return. Conventional guidance means are included for autonomous flight.
摘要翻译： 一种气动制动轨道转运车辆，其包括气动制动装置，该制动装置还用作具有圆形或椭圆形基部的倾斜的椭圆形或圆锥形的形状的隔热罩，以及椭圆形或其他钝形的鼻部。 航空制动装置配备有环形裙部，与推进系统的支撑结构和空间车辆的其他系统是一体的。 该车辆旨在以组件方式运输到地下轨道的空间站，并将其组装用作从低地球轨道到地球同步轨道和返回的运输系统。 自动飞行包括常规指导手段。
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公开(公告)号：US5407152A
公开(公告)日：1995-04-18
申请号：US996763
申请日：1992-12-24
申请人： Timothy E. Pelischek , Edgar O. Castro , Gregg A. Edeen , David A. Hamilton , Jon B. Kahn , James B. McDede , Kornel Nagy , John V. Rivers , Irene E. Verinder , Donald C. Wade , Clarence J. Wesselski
发明人： Timothy E. Pelischek , Edgar O. Castro , Gregg A. Edeen , David A. Hamilton , Jon B. Kahn , James B. McDede , Kornel Nagy , John V. Rivers , Irene E. Verinder , Donald C. Wade , Clarence J. Wesselski
摘要： The present invention is directed to methods and apparatus relating to design, construction, integration and assembly of a space station. The present invention uses pre-integrated open (unpressurized) truss segments for modular construction of the space station. Each segment includes a truss structure and utility subsystems which may be fully assembled and tested on Earth. The segments may be latched together on orbit using a remote latching system. Utility subsystems, such as solar panels and radiators, are pre-integrated into the appropriate truss segment, and are deployable from the respective truss segment on orbit. Rails run lengthwise along the assembled truss. The rails may be used with a mobile transporter for translating truss segments with respect to the spacecraft as part of the space station assembly process. The rails may also be used with a mobile transporter for carrying crew personnel, a robotic arm, and other equipment.
摘要翻译： 本发明涉及与空间站的设计，构造，集成和组装有关的方法和装置。 本发明使用预集成开放（非加压）桁架段用于空间站的模块化构造。 每个部分包括可在地球上完全组装和测试的桁架结构和效用子系统。 这些段可以使用远程锁定系统在轨道上锁定在一起。 诸如太阳能电池板和散热器之类的效用子系统被预先集成到适当的桁架段中，并且可从轨道上的相应的桁架段部署。 轨道沿组装桁架纵向延伸。 作为空间站组装过程的一部分，轨道可以与移动式运输机一起用于相对于航天器平移桁架段。 轨道还可以与移动运输机一起使用，用于携带机组人员，机器人手臂和其他设备。
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公开(公告)号：US5158331A
公开(公告)日：1992-10-27
申请号：US660755
申请日：1991-02-25
申请人： Clarence J. Wesselski , Kornel Nagy
发明人： Clarence J. Wesselski , Kornel Nagy
IPC分类号： F16B2/18
CPC分类号： F16B2/185
摘要： A latching device which is lever operated sequentially to actuate a set of collet fingers to provide a radial expansion and to actuate a force mechanism to provide a compressive gripping force for attaching first and second devices to one another. The latching device includes a body member having elongated collet fingers which, in a deactuated condition, are insertable through bores on the first and second devices so that gripping terminal portions on the collet fingers are proximate to the end of the bore of the first device while a spring assembly on the body member is located proximate to the outer surface of a second device. A lever is rotatable through 90.degree. to move a latching rod to sequentially actuate and expand collet fingers and to actuate the spring assembly by compressing it. During the first 30.degree. of movement of the lever, the collet fingers are actuated by the latching rod to provide a radial expansion and during the last 60.degree. of movement of the lever, the spring assembly acts as a force mechanism and is actuated to develop a compressive latching force on the devices. The latching rod and lever are connected by a camming mechanism. The amount of spring force in the spring assembly can be adjusted; the body member can be permanently attached by a telescoping assembly to one of the devices; and the structure can be used as a pulling device for removing annular bearings or the like from blind bores.
摘要翻译： 锁定装置，其被连续地操作以致动一组夹头以提供径向膨胀并且致动力机构以提供用于将第一和第二装置彼此附接的压缩夹持力。 锁定装置包括主体构件，其具有细长的夹爪，其处于停用状态，可通过第一和第二装置上的孔插入，使得夹头上的夹紧端部接近第一装置的孔的端部， 主体构件上的弹簧组件位于第二装置的外表面附近。 杠杆可旋转90°以移动闩锁杆，以顺序地致动并膨胀夹头，并通过压缩来致动弹簧组件。 在杠杆的前30°运动期间，夹头由锁闩杆致动以提供径向膨胀，并且在杆的最后60°运动期间，弹簧组件用作力机构并被致动以产生 设备上的压缩锁定力。 闩锁杆和杠杆通过凸轮机构连接。 可以调节弹簧组件中的弹簧力量; 主体构件可以通过伸缩组件永久地附接到装置之一; 并且该结构可以用作从盲孔去除环形轴承等的牵引装置。
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公开(公告)号：US4763762A
公开(公告)日：1988-08-16
申请号：US118992
申请日：1987-11-10
IPC分类号： F16D65/12
CPC分类号： F16D65/122 , F16D65/126
摘要： A disc brake system for a shuttle orbiter including an annular disc element (10) having internal radially directed and angularly spaced relief slots (12) and trapezoidial shaped carbon pad members (15) disposed circumferentially around the disc element. T Clips (19, 19') snugly engage the outer ends of the pad members and are attached to rivet heads (34, 35) and (34', 35') and have guide members (51, 51') slidably received in guide grooves (50, 50') in a spring housing (20). Springs (61) provide a force tending to move the T Clips toward the center of the disc where the magnitude of the force can be adjusted by a screw (65).
摘要翻译： 一种用于穿梭轨道运动器的盘式制动系统，其包括环形盘元件（10），所述环形盘元件具有沿盘状元件周向设置的具有内部径向和间隔开的释放槽（12）和梯形形状的碳垫构件（15）。 T夹（19,19'）紧密地接合衬垫构件的外端并且附接到铆钉头（34,35）和（34 + 40,35'），并且具有可滑动地容纳在其中的引导构件（51,51'） 在弹簧壳体（20）中的引导槽（50,50'）。 弹簧（61）提供趋向于将T夹头移动到盘的中心的力，其中力的大小可以通过螺钉（65）来调节。
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公开(公告)号：US4579302A
公开(公告)日：1986-04-01
申请号：US587764
申请日：1984-03-09
申请人： William C. Schneider , Reginald B. Berka , Herbert C. Kavanaugh , Kornel Nagy , Richard C. Parish , John A. Schliesing , Paul D. Smith , Frederick J. Stebbins , Clarence J. Wesselski
发明人： William C. Schneider , Reginald B. Berka , Herbert C. Kavanaugh , Kornel Nagy , Richard C. Parish , John A. Schliesing , Paul D. Smith , Frederick J. Stebbins , Clarence J. Wesselski
CPC分类号： B64G9/00 , Y10S136/292
摘要： A triangular space station deployable in orbit. The framework is comprised of three trusses, formed of a pair of generally planar faces comprised of foldable struts which expand and lock into rigid structural engagement forming a repetition of equilateral triangles and non-folding diagonal struts interconnecting the two faces. The struts are joined together by node fittings. The framework can be packaged into a size and configuration which can be transported by a space shuttle orbiter in a single orbital flight and when deployed, provides large work/construction area and ample planar surface area for solar panels and thermal radiators. A plurality of modules are secured to the framework and then joined by tunnels to comprise an interconnected modular array disposed along the free edges of the framework. Thruster units for space station orientation and altitude maintenance are provided. The triangular space station provides a structurally stable unit having sufficiently high structural integrity and natural frequency for facilitating docking, satellite servicing and launch operations.
摘要翻译： 可在轨道上部署的三角形空间站。 该框架由三个桁架构成，由一对大体上平坦的面构成，该平面由可折叠的支柱膨胀并锁定成刚性结构接合，形成重复的等边三角形和互相连接两个面的非折叠对角支柱。 支柱通过节点配件连接在一起。 框架可以包装成一个尺寸和配置，可以在单轨道飞行中由航天飞机轨道运输，并且部署时，为太阳能电池板和散热器提供大的工作/建筑面积和宽的平面表面积。 多个模块被固定到框架上，然后由隧道连接以包括沿框架的自由边缘设置的互连的模块化阵列。 提供了用于空间站定向和高度维护的推进装置。 三角空间站提供了具有足够高的结构完整性和固有频率的结构稳定的单元，以便于对接，卫星维修和发射操作。
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