-
公开(公告)号：US3948190A
公开(公告)日：1976-04-06
申请号：US512140
申请日：1974-10-04
CPC分类号： B65D19/004 , B65D19/44 , B65D2519/00034 , B65D2519/00069 , B65D2519/00268 , B65D2519/00288 , B65D2519/00318 , B65D2519/00333 , B65D2519/00338 , B65D2519/00407 , B65D2519/0094
摘要： An industrial load-carrying pallet comprising an integral sheet of material formed with strengthening ribs extending thereacross, three centrally disposed pedestals extending downwardly at the center line and generally W-shaped pedestals disposed adjacent the side extremities. Grooves extend downwardly from the upper surface and are disposed along the circumference of four circles for receiving the bottom rims of four drums. The pedestals have recesses therein disposed on the circumference of four circles whereby the pedestals may rest upon and engage the top rims of four drums. The area of the top surface within each circle for receiving the bottom rim of a drum is spherically concave. The side pedestals have spaced converging walls in a downward direction which are joined at the lower extremities by a bottom base. Empty pallets may be stacked by placing the pedestals within one another. However, there is included anti-locking means in the form of shoulders extending inwardly from the side walls of the side pedestals to engage bottom base of a like pedestal of another pallet to prevent stacked pallets from being wedged into binding engagement with one another.
摘要翻译： 一种工业承载托盘，其包括整体的材料片材，其形成有在其上延伸的加强肋，在中心线向下延伸的三个中心布置的基座以及邻近所述侧端布置的大体上为W形的基座。 槽从上表面向下延伸，并且沿着四个圆的圆周设置以接收四个鼓的底部边缘。 基座在四个圆周的圆周上具有凹槽，由此基座可以搁置在四个滚筒的顶部边缘上并与其接合。 用于接收鼓的底部边缘的每个圆中的顶部表面的面积是球形的。 侧基座具有向下方向的间隔的会聚壁，其在下端通过底部底座连接。 可以通过将基座放置在彼此中来堆叠空托盘。 然而，包括从侧座的侧壁向内延伸的肩部形式的防抱死装置，以接合另一个托盘的类似基座的底部基座，以防止堆叠的托盘楔入彼此的结合接合。
-
22.发明授权公开(公告)号：US08530512B2
公开(公告)日：2013-09-10
申请号：US12973078
申请日：2010-12-20
申请人： Aaron P. Monte , M. Shahjahan Kabir , Marc A. Rott , William R. Schwan , James M. Cook, III , Jennifer A. Miskowski , Ranjit Verma , Leah Defoe
发明人： Aaron P. Monte , M. Shahjahan Kabir , Marc A. Rott , William R. Schwan , James M. Cook, III , Jennifer A. Miskowski , Ranjit Verma , Leah Defoe
IPC分类号： A61K31/38 , A61K31/34 , A61K31/404
CPC分类号： C07D213/30 , A61K31/085 , A61K31/381 , A61K36/185 , C07C43/23 , C07D213/64 , C07D213/65 , C07D213/68 , C07D333/16 , C07D333/56 , C07D333/62 , C07D333/64
摘要： The present invention provides compounds and methods of using of the compounds as anti-infective and anthelminitc agents. In a preferred embodiment, the present invention provides the following compound of Formula III: wherein: R1 is not H when R2 is H and R2 is not H when R1 is H, further wherein R1 is OH or CH(2n+1)O, wherein n is 1-10; R2 is OH or CH(2n+1)O, where n is 1-10; W is alkyl, phenyl, halophenyl, pyridyl, piperidyl, or a substituted or unsubstituted aryl group, including unsubstituted and substituted aromatic heterocycles; and L is an optional linker or linking group selected from O, S, NH, CF2, or CH2, and x=0 or 1, i.e., if x=0, no linking group is present and when x=0, W is not phenyl.
摘要翻译： 本发明提供了化合物和使用该化合物作为抗感染和抗栓剂的方法。 在优选的实施方案中，本发明提供以下式III化合物：其中：当R 1为H时，R 1不为H，且R 1为H时R 2不为H，此外，R 1为OH或CH（2n + 1）O， 其中n为1-10; R2是OH或CH（2n + 1）O，其中n是1-10; W是烷基，苯基，卤代苯基，吡啶基，哌啶基或取代或未取代的芳基，包括未取代和取代的芳族杂环; 并且L是选自O，S，NH，CF 2或CH 2，x = 0或1的任选的接头或连接基团，即，如果x = 0，则不存在连接基团，并且当x = 0时，W不是 苯基。
-
公开(公告)号：US08173946B1
公开(公告)日：2012-05-08
申请号：US12198146
申请日：2008-08-26
申请人： William N. Patterson , James H. Dupont , Richard D. Loehr , Henri Y. Kim , Garrett L. Hall , James M. Cook
发明人： William N. Patterson , James H. Dupont , Richard D. Loehr , Henri Y. Kim , Garrett L. Hall , James M. Cook
CPC分类号： F41H11/02 , F41F3/073 , F42B10/661 , F42B15/01 , F42B15/10
摘要： A method of defeating an incoming missile, such as a rocket propelled grenade, includes soft launching an interceptor missile, and then using pitch over motors of the interceptor missile to alter course of the missile to a desired interception direction. By launching at a relatively slow speed, such as a speed less than or equal to 40 m/sec (130 ft/sec), the interceptor missile may reach the desired interception direction within 250 milliseconds of launch. The interceptor missile may be able to cover substantially all interception directions over a hemisphere or greater extent around a launch location. For example, the interceptor missile may be launched vertically from a ground vehicle, and be capable of altering course to any above-ground trajectory within 250 milliseconds.
摘要翻译： 一种击败诸如火箭推进手榴弹的进入导弹的方法包括软启动拦截导弹，然后使用拦截导弹发动机的俯仰角来将导弹的过程改变为所需的拦截方向。 通过以相对较慢的速度（例如小于或等于40米/秒（130英尺/秒）的速度）发射，拦截导弹可以在发射的250毫秒内达到所需的拦截方向。 拦截导弹可以能够围绕发射位置覆盖半球或更大程度上的所有拦截方向。 例如，拦截导弹可以从地面车辆垂直发射，并且能够在250毫秒内改变任何地面上的轨迹。
-
24.发明授权公开(公告)号：US08058596B2
公开(公告)日：2011-11-15
申请号：US12548583
申请日：2009-08-27
CPC分类号： F42B10/661
摘要： A method of controlling flight of a missile includes using gyroscopes, such as pitch rate gyroscopes, to sense when a factor based on the angular rate of change of the missile exceeds a threshold value. One the threshold value is exceeded, a decision may be made to use one or more compensation thrusters to reduce the angular rate of change. The use of the compensation thrusters may correct residual angular velocities from a pitch over maneuver used to put the missile on an intended course. In addition, the compensation thrusters may be used to compensate for errors in missile heading induced after the pitch over maneuver, such as induced by misalignment of thrust provided by a main rocket motor of the missile. Multiple compensation thrusters may be used to compensate for angular changes in the pitch and yaw directions.
摘要翻译： 控制导弹飞行的方法包括使用诸如俯仰速率陀螺仪的陀螺仪来感测何时基于导弹的角速度变化的因子超过阈值。 超过阈值的一个，可以决定使用一个或多个补偿推进器来减小角速度变化。 补偿推进器的使用可以校正用于将导弹放置在预期路线上的机动的俯仰的剩余角速度。 此外，补偿推进器可以用于补偿在机动之后引起的导弹航向的误差，例如由导弹的主火箭发动机提供的推力不对准引起的。 可以使用多个补偿推进器来补偿俯仰和偏航方向上的角度变化。
-
25.发明授权System and method for attitude control of a flight vehicle using pitch-over thrusters and application to an active protection system 有权使用俯仰推进器的飞行器车辆姿态控制系统和方法以及应用于主动保护系统公开(公告)号：US07989743B2
公开(公告)日：2011-08-02
申请号：US12877789
申请日：2010-09-08
CPC分类号： F42B10/661 , G05D1/0883
摘要： A reliable and inexpensive attitude control system uses a plurality of pitch-over thrusters to perform rapid and precise attitude maneuvers for a flight vehicle. The pitch-over thrusters create rotational moments that directly pitch and yaw the flight vehicle. The use of very simple thrusters and control techniques provides for a reliable and cost effective solution. The ability to perform overlapping pitch and yaw maneuvers with single-shot fixed-impulse thrusters provides for high-speed maneuverability. Although this approach is applicable to provide attitude control for any flight vehicle including all types of missiles, kill-vehicles and space craft, it is particularly applicable for smaller highly maneuverable cost-constrained missile systems. One such system is an “Active Protection System” or APS in which a missile system is integrated with a vehicle such as a HumVee or armored personnel carrier to provide defensive counter-measures against possible attack.
摘要翻译： 可靠和廉价的姿态控制系统使用多个俯仰推进器来为飞行器执行快速和精确的姿态操纵。 俯仰推进器产生直接俯仰和偏航飞行器的旋转力矩。 使用非常简单的推进器和控制技术提供了可靠且具有成本效益的解决方案。 使用单次固定脉冲推进器执行重叠俯仰和偏航操作的能力提供高速机动性。 虽然这种方法适用于为包括各种类型的导弹，杀伤车辆和航天飞机在内的任何飞行器提供姿态控制，但特别适用于较小的高度机动性的成本受限的导弹系统。 一个这样的系统是一个“主动保护系统”或APS，其中将导弹系统与诸如HumVee或装甲运兵车的车辆集成在一起，以提供防御性对策以防止可能的攻击。
-
公开(公告)号：US20110049289A1
公开(公告)日：2011-03-03
申请号：US12548583
申请日：2009-08-27
CPC分类号： F42B10/661
摘要： A method of controlling flight of a missile includes using gyroscopes, such as pitch rate gyroscopes, to sense when a factor based on the angular rate of change of the missile exceeds a threshold value. One the threshold value is exceeded, a decision may be made to use one or more compensation thrusters to reduce the angular rate of change. The use of the compensation thrusters may correct residual angular velocities from a pitch over maneuver used to put the missile on an intended course. In addition, the compensation thrusters may be used to compensate for errors in missile heading induced after the pitch over maneuver, such as induced by misalignment of thrust provided by a main rocket motor of the missile. Multiple compensation thrusters may be used to compensate for angular changes in the pitch and yaw directions.
摘要翻译： 控制导弹飞行的方法包括使用诸如俯仰速率陀螺仪的陀螺仪来感测何时基于导弹的角速度变化的因子超过阈值。 超过阈值的一个，可以决定使用一个或多个补偿推进器来减小角速度变化。 补偿推进器的使用可以校正用于将导弹放置在预期路线上的机动的俯仰的剩余角速度。 此外，补偿推进器可以用于补偿在机动之后引起的导弹航向的误差，例如由导弹的主火箭发动机提供的推力不对准引起的。 可以使用多个补偿推进器来补偿俯仰和偏航方向上的角度变化。
-
27.发明授权System and method for attitude control of a flight vehicle using pitch-over thrusters 有权使用俯仰推进器的飞行器车辆姿态控制系统和方法公开(公告)号：US07851732B2
公开(公告)日：2010-12-14
申请号：US11470900
申请日：2006-09-07
CPC分类号： F42B10/661 , G05D1/0883
摘要： A reliable and inexpensive attitude control system uses a plurality of pitch-over thrusters to perform rapid and precise attitude maneuvers for a flight vehicle. The pitch-over thrusters create rotational moments that directly pitch and yaw the flight vehicle. The use of very simple thrusters and control techniques provides for a reliable and cost effective solution. The ability to perform overlapping pitch and yaw maneuvers with single-shot fixed-impulse thrusters provides for high-speed maneuverability.
摘要翻译： 可靠和廉价的姿态控制系统使用多个俯仰推进器来为飞行器执行快速和精确的姿态操纵。 俯仰推进器产生直接俯仰和偏航飞行器的旋转力矩。 使用非常简单的推进器和控制技术提供了可靠且具有成本效益的解决方案。 使用单次固定脉冲推进器执行重叠俯仰和偏航操作的能力提供高速机动性。
-
公开(公告)号：US20100130479A1
公开(公告)日：2010-05-27
申请号：US12551149
申请日：2009-08-31
IPC分类号： A61K31/5517 , A61P25/00 , C07D487/04
CPC分类号： C07D487/04 , C07D487/14 , C07D519/00
摘要： The present invention provides molecules and methods for the prevention and/or treatment of memory deficit related conditions and/or enhancement of cognition. In a preferred embodiment, the invention includes compounds, salts and prodrugs thereof for the prevention and/or treatment of these conditions.
摘要翻译： 本发明提供了用于预防和/或治疗记忆缺陷相关病症和/或增强认知的分子和方法。 在优选的实施方案中，本发明包括用于预防和/或治疗这些病症的化合物，其盐和前药。
-
公开(公告)号：US07235656B2
公开(公告)日：2007-06-26
申请号：US11458739
申请日：2006-07-20
申请人： James M. Cook , Qi Huang , Xiaohui He , Xioayan Li , Jianming Yu , Dongmei Han
发明人： James M. Cook , Qi Huang , Xiaohui He , Xioayan Li , Jianming Yu , Dongmei Han
IPC分类号： C07D495/14 , C07D521/00
CPC分类号： C07D471/04 , C07D243/12 , C07D243/20 , C07D243/24 , C07D487/04 , C07D487/06 , C07D495/04 , C07D495/14 , C07D498/04 , C07D519/00
摘要： Orally active benzodiazepine derivatives and their salts are disclosed. These compounds and their salts have anxiolytic and anticonvulsant activity with reduced sedative/hypnotic/muscle relaxant/ataxic effects.
摘要翻译： 公开了口服活性苯二氮卓衍生物及其盐。 这些化合物及其盐具有抗焦虑和抗惊厥活性，降低镇静/催眠/肌肉松弛/共济失调作用。
-
公开(公告)号：US4254873A
公开(公告)日：1981-03-10
申请号：US943436
申请日：1978-09-18
IPC分类号： B65D19/00
CPC分类号： B65D19/00
摘要： A pallet system including two embodiments of a pallet having a deck including four sides and providing a load-supporting surface. A plurality of spaced hollow legs project from the opposite side of the deck and a plurality of hollow reinforcing ribs project from the opposite surface to define channels in the load-supporting surface. A hollow ridge projects from the opposite surface and extends along the sides at the periphery of the deck to define a groove in the load-supporting surface for receiving the bottom edge of a wall. There is at least one transverse rib projecting from the opposite surface and extending between opposite sides of the deck to define a transverse groove in the load-supporting surface for receiving the bottom edge of a transverse wall whereby walls may extend upwardly from the deck to divide and separate the load-supporting surface into discrete areas. The channels defined by the reinforcing ribs have a larger dimension than do the grooves defined by the ridges for receiving the edges of walls. The reinforcing ribs include a first plurality of ribs extending between corner legs and parallel to opposite sides with a second plurality of ribs extending perpendicular to the first plurality of ribs and having ends terminating short of the first plurality of ribs so as to be spaced therefrom.
摘要翻译： 一种托盘系统，包括托盘的两个实施例，该托盘具有包括四个侧面并且提供承载表面的甲板。 多个间隔开的中空腿从甲板的相对侧突出，并且多个中空的加强肋从相对的表面伸出以限定负载支撑表面中的通道。 中空的脊从相对的表面突出并且沿着甲板的周边的侧面延伸，以在负载支撑表面中限定一个用于接收壁的底部边缘的凹槽。 至少有一个横向肋条从相对表面突出并在甲板的相对侧面之间延伸，以在承载支承表面中限定横向槽，用于接收横向壁的底部边缘，从而壁可以从甲板向上延伸以分开 并将负载支撑表面分离成离散区域。 由加强筋限定的通道具有比用于接收壁边缘的脊限定的凹槽更大的尺寸。 所述加强肋包括在拐角腿之间延伸并且平行于相对侧的第一多个肋，所述第二多个肋具有垂直于所述第一多个肋延伸的第二多个肋，并且具有不超过所述第一多个肋的端部，以便与其间隔开。
-
-
-
-
-
-
-
-
-
搜索结果
39 条记录 (耗时 0.028 秒)
