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91. 发明申请

US20130340407A1 CLUSTERED, FIXED CANT, THROTTLEABLE ROCKET ASSEMBLY 审中-公开
标题翻译：集合式，固定式CANT，可折叠式摇摆组件
公开(公告)号：US20130340407A1
公开(公告)日：2013-12-26
申请号：US13397537
申请日：2012-02-15
申请人： David J. Fisher , Gregory S. Mungas
发明人： David J. Fisher , Gregory S. Mungas
IPC分类号： F02K9/00
CPC分类号： F02K9/00 , F02K9/58 , F02K9/82 , F02K9/88 , F05D2240/40 , F05D2250/314
摘要： A clustered, fixed cant, throttleable rocket assembly is used to propel and a steer a vessel in terrestrial or extraterrestrial applications. The fixed cant of each of at least three individual rockets in the cluster provides the steering input to the overall assembly. More specifically, by changing the propellant flow rate to the individual rocket engines relative to one another, the overall thrust vector of the rocket assembly may be selected to provide a desired steering input to the vessel. A measured vessel orientation may be compared with a desired vessel orientation to determine what steering input is required to achieve the desired vessel orientation.
摘要翻译：一个聚集的，固定的倾斜，可节流的火箭组件用于推进和引导在地面或地球外应用中的船只。集群中的至少三个单独火箭中的每一个的固定倾斜部为整个组件提供转向输入。更具体地，通过将推进剂流量相对于彼此改变为单个火箭发动机，可以选择火箭组件的总推力矢量以向船提供期望的转向输入。可以将测量的血管取向与期望的血管方向进行比较，以确定实现所需血管方向所需的转向输入。

92. 发明申请

US20120269633A1 CLOSED GAS GENERATOR AND MICRO POWER UNIT INCLUDING THE SAME 有权
标题翻译：封闭式气体发生器和微功率单元，包括它们
公开(公告)号：US20120269633A1
公开(公告)日：2012-10-25
申请号：US13089441
申请日：2011-04-19
申请人： Jeremy C. Danforth , Richard D. Loehr , Kevin P. Murphy
发明人： Jeremy C. Danforth , Richard D. Loehr , Kevin P. Murphy
IPC分类号： B64D27/24 , H02K7/18 , H02J7/00 , F02K9/62 , F02K1/00
CPC分类号： F02K9/00 , B64C2201/042 , F02K9/42 , F02K9/425 , F02K9/50 , F02K9/52 , F02K9/68 , H02J7/00 , H02K7/1823
摘要： A gas generator assembly includes a propellant chamber housing an amine based propellant. A reaction chamber is coupled with the propellant chamber. The reaction chamber includes a reaction chamber housing, and a porous reaction matrix within the reaction chamber housing. The reaction matrix includes a catalyzing agent, and the catalyzing agent is configured to non-combustibly catalyze the amine based propellant into one or more pressurized gases. An injector is in communication with the propellant chamber. The injector is configured to deliver the amine based propellant to the porous reaction matrix. A discharge nozzle is coupled with the reaction chamber and is configured to accelerate and discharge the one or more pressurized gases. In one example, the gas generator is coupled with one or more of an impulse turbine assembly and an electric generator to form a micro power unit.
摘要翻译：气体发生器组件包括容纳胺基推进剂的推进剂室。反应室与推进剂室结合。反应室包括反应室壳体和反应室壳体内的多孔反应基质。反应基质包括催化剂，并且催化剂被配置为不可燃地将胺基推进剂催化成一种或多种加压气体。喷射器与推进剂室连通。喷射器构造成将胺基推进剂输送到多孔反应基质。排放喷嘴与反应室联接并且构造成加速和排出一个或多个加压气体。在一个示例中，气体发生器与脉冲涡轮机组件和发电机中的一个或多个耦合以形成微动力单元。

93. 发明申请

US20120219408A1 CYLINDRICAL STRUCTURE AND METHOD FOR MANUFACTURING THE SAME 审中-公开
标题翻译：圆柱结构及其制造方法
公开(公告)号：US20120219408A1
公开(公告)日：2012-08-30
申请号：US13505658
申请日：2010-11-05
申请人： Takashi Harada , Yu Shigenari , Masayori Miyashita , Tsutomu Murakami
发明人： Takashi Harada , Yu Shigenari , Masayori Miyashita , Tsutomu Murakami
IPC分类号： B32B37/12 , F04D23/00
CPC分类号： F04D29/522 , B29C53/562 , B29C53/58 , B29C70/32 , F02K9/00
摘要： A method for manufacturing a cylindrical structure having an axial direction includes: winding a fabric around a mandrel in a circumferential direction that is perpendicular to the axial direction, the fabric containing first fibers oriented in a first direction intersecting the circumferential direction; winding a roving into a helical shape around the mandrel, the roving containing second fibers oriented in a longitudinal direction of the roving; and joining the fabric and the roving together by using a resin.
摘要翻译：一种制造具有轴向的圆柱形结构的方法包括：沿与轴向垂直的圆周方向围绕心轴缠绕织物，所述织物包含沿与圆周方向交叉的第一方向取向的第一纤维; 将纱线卷绕在心轴周围的螺旋形状中，粗纱包含沿着粗纱的纵向取向的第二纤维; 并通过使用树脂将织物和粗纱接合在一起。

94. 发明申请

US20100089027A1 MAGNETIC GAS ENGINE AND METHOD OF EXTRACTING WORK 审中-公开
标题翻译：磁性发动机及其提取方法
公开(公告)号：US20100089027A1
公开(公告)日：2010-04-15
申请号：US12578341
申请日：2009-10-13
申请人： Patrick Craig Muldoon
发明人： Patrick Craig Muldoon
IPC分类号： F03H1/00
CPC分类号： F03H1/0081 , F02K1/00 , F02K1/28 , F02K7/00 , F02K7/10 , F02K9/00 , F03H1/00 , F05D2210/12 , F05D2220/10 , F05D2220/34
摘要： The present subject matter overcomes the deficiencies in the prior art by introducing or generating charged particles in an air stream and manipulating the air stream with magnetic fields operating on the charged particles. Embodiments of the present subject mater compress the air stream by accelerating charged particles with a moving magnetic field, where the magnetic field has a velocity perpendicular to its flux lines. The increased velocity of the charged particles increases the statistical mean particle velocity and thereby increases the pressure in the air stream. The compressed air stream is then heated and expanded through a second magnetic field. The expansion of the air stream substantially increases the velocity of the air stream and the charged particles therein. The interaction of the high velocity charged particles and the magnetic field imparts a force perpendicular to the flux lines, this force powers the movement of the magnetic field and can also be extracted in the form of mechanical work.
摘要翻译：本发明通过在空气流中引入或产生带电粒子并利用在带电粒子上运行的磁场来操纵空气流来克服现有技术中的缺陷。本发明的实施例通过用移动磁场加速带电粒子来压缩空气流，其中磁场具有垂直于其通量线的速度。带电粒子的增加的速度增加统计平均粒子速度，从而增加空气流中的压力。然后将压缩空气流通过第二磁场加热和膨胀。空气流的膨胀大大增加了空气流和其中的带电粒子的速度。高速带电粒子与磁场的相互作用赋予垂直于磁通线的力，该力为磁场的运动提供动力，也可以以机械作业的形式提取。

95. 发明授权

US07602096B2 Magnetic gas engine and method of extracting work 有权
标题翻译：磁性气体发动机及其提取方法
公开(公告)号：US07602096B2
公开(公告)日：2009-10-13
申请号：US11362928
申请日：2006-02-28
申请人： Patrick Craig Muldoon
发明人： Patrick Craig Muldoon
IPC分类号： H02K1/22
CPC分类号： F03H1/0081 , F02K1/00 , F02K1/28 , F02K7/00 , F02K7/10 , F02K9/00 , F03H1/00 , F05D2210/12 , F05D2220/10 , F05D2220/34
摘要： The present subject matter overcomes the deficiencies in the prior art by introducing or generating charged particles in an air stream and manipulating the air stream with magnetic fields operating on the charged particles. Embodiments of the present subject matter compress the air stream by accelerating charged particles with a moving magnetic field, where the magnetic field has a velocity perpendicular to its flux lines. The increased velocity of the charged particles increases the statistical mean particle velocity and thereby increases the pressure in the air stream. The compressed air stream is then heated and expanded through a second magnetic field. The expansion of the air stream substantially increases the velocity of the air stream and the charged particles therein. The interaction of the high velocity charged particles and the magnetic field imparts a force perpendicular to the flux lines, this force powers the movement of the magnetic field and can also be extracted in the form of mechanical work.
摘要翻译：本发明通过在空气流中引入或产生带电粒子并利用在带电粒子上运行的磁场来操纵空气流来克服现有技术中的缺陷。本主题的实施例通过用移动磁场加速带电粒子来压缩空气流，其中磁场具有垂直于其磁通线的速度。带电粒子的增加的速度增加统计平均粒子速度，从而增加空气流中的压力。然后将压缩空气流通过第二磁场加热和膨胀。空气流的膨胀大大增加了空气流和其中的带电粒子的速度。高速带电粒子与磁场的相互作用赋予垂直于磁通线的力，该力为磁场的运动提供动力，也可以以机械作业的形式提取。

96. 发明授权

US07083141B2 Self-propelled projectile 失效
标题翻译：自走式射弹
公开(公告)号：US07083141B2
公开(公告)日：2006-08-01
申请号：US10725100
申请日：2003-12-02
申请人： Edward Nitenson , Robert Cumings
发明人： Edward Nitenson , Robert Cumings
IPC分类号： B64C5/12
CPC分类号： F02K9/00 , F42B10/14 , F42B15/00
摘要： A self-propelled projectile which will maintain a straight trajectory through air or water.
摘要翻译：一种能够通过空气或水保持直线轨迹的自走式射弹。

97. 发明申请

US20050230176A1 Anti-roll thrust system for vehicles 失效
标题翻译：车辆防倾倒推力系统
公开(公告)号：US20050230176A1
公开(公告)日：2005-10-20
申请号：US11049555
申请日：2005-02-02
申请人： Jenne-Tai Wang
发明人： Jenne-Tai Wang
IPC分类号： B60R21/00 , B60R21/0132 , F02K1/00 , F02K9/00
CPC分类号： B60R21/0132 , B60G2202/45 , B60R2021/0018 , B60R2021/01327 , F02K9/00 , F05B2240/94 , F05B2240/941
摘要： A thruster system is provided for a vehicle that can be used to reduce the roll propensity of a motor vehicle. The system utilizes a control system and multiple sets of thrusters which are strategically placed upon the vehicle. The control system is provided for detecting a potential roll condition and activates selected ones of the thrusters to produce a necessary thrust force for counteracting roll forces.
摘要翻译：为车辆提供推进器系统，其可用于降低机动车辆的倾斜倾向。该系统利用了一套控制系统和多组策略性地放置在车辆上的推进器。提供控制系统用于检测潜在的滚动条件并激活所选择的推进器，以产生用于抵消滚动力的必要的推力。

98. 发明授权

US06734331B2 Process for producing olefins and diolefins 失效
标题翻译：生产烯烃和二烯烃的方法
公开(公告)号：US06734331B2
公开(公告)日：2004-05-11
申请号：US10193068
申请日：2002-07-11
申请人： Anthony Cirrito , Bernard Ennis
发明人： Anthony Cirrito , Bernard Ennis
IPC分类号： C07C402
CPC分类号： F02K9/00 , C06D5/00 , C10G2400/20 , F02C3/00 , F02C3/36 , F02G5/00 , Y02E20/16 , Y02E20/18 , Y02P20/128 , Y02P20/582 , Y02T10/166
摘要： A process for producing olefins and diolefins. A flow of gas is compressed with a prime mover in a near adiabatic path. Resistance to the flow within the adiabatic path causes a temperature rise with respect to its pressure, where it enters a near adiabatic tunnel. At least one other gas is provided into the tunnel at a prescribed, independently controlled temperature and pressure. The compressed flow is comingled and mixed with at least one other gas. Hydrogen and oxygen are fed into the tunnel to produce steam. Steam is applied to at least one hydrocarbon for pyrolysis or thermal cracking to yield at least one of olefins and diolefins.
摘要翻译：一种生产烯烃和二烯烃的方法。气体流在一个靠近绝热路径的原动机中被压缩。抵抗绝热路径内的流动导致温度相对于其压力升高，在那里它进入接近绝热的隧道。在规定的独立控制的温度和压力下，至少一个其它气体被提供到隧道内。压缩流体与至少一种其它气体混合并混合。氢气和氧气进入隧道以产生蒸汽。将蒸汽施加至至少一种烃进行热解或热裂解以产生烯烃和二烯烃中的至少一种。

99. 发明授权

US06314719B1 Ignition system for a propulsion producing engine 有权
标题翻译：用于推进发动机的点火系统
公开(公告)号：US06314719B1
公开(公告)日：2001-11-13
申请号：US09471540
申请日：1999-12-23
申请人： Jeffrey H. Hunt , Herbert R. Lander
发明人： Jeffrey H. Hunt , Herbert R. Lander
IPC分类号： F02K900
CPC分类号： F02C7/264 , F02K9/00 , F02K9/94 , F02K9/95
摘要： The ignition system includes an optical source capable of producing light having physical characteristics sufficient for optically driven chemical disassociation of a hydrogen peroxide oxidizer; and, an optical delivery system for providing optical delivery of light from the optical source to a combustion chamber. The ignition system is used for a propulsion producing engine having a combustion chamber for the introduction of a fuel and a hydrogen peroxide oxidizer. The initiation of combustion is produced by the non-linear, optical interaction of the produced light with a fuel and the oxidizer present in the combustion chamber, thereby leading to molecular disassociation of the oxidizer such that there is initiation of combustion.
摘要翻译：点火系统包括能够产生足以使过氧化氢氧化剂的光学驱动化学分解的物理特性的光的光源; 以及用于提供从光源到燃烧室的光的光学传递的光学传送系统。点火系统用于具有用于引入燃料和过氧化氢氧化剂的燃烧室的推进发动机。通过产生的光与燃料和存在于燃烧室中的氧化剂的非线性光学相互作用产生燃烧的开始，从而导致氧化剂的分子分解，使得发生燃烧。

100. 发明授权

US4585136A Attachment of rings to articles 失效
标题翻译：将环附在物品上
公开(公告)号：US4585136A
公开(公告)日：1986-04-29
申请号：US450061
申请日：1982-12-15
申请人： John Clark
发明人： John Clark
IPC分类号： B29C70/86 , F02K9/00 , F02K9/34 , B32B1/02 , B32B1/08
CPC分类号： F02K9/343 , B29C70/86 , F02K9/00 , B29L2031/3097 , Y10T428/1369 , Y10T428/24479 , Y10T428/24579 , Y10T428/24612
摘要： Attachment of a ring, particularly a metal ring (2), to an article which has walls or skirts (1) of fibre-reinforced resin material. The ring has a plurality of external grooves (3, 4, 5, 6). The skirt comprises, for each groove in sequence, a first (32, 36, 37, 40) and second (33, 38, 39, 41) layer of fibre-reinforced resin material. The fibres in the first layer have a substantial orientation in directions parallel with the axis of the ring and extend from the skirt into the respective grooves. Overlying the first layer is a second layer comprising hoop windings from the skirt towards the groove. The second layer lies at least partly in the groove to lock the first layer in the groove. This layering is repeated for each groove and finally successive hoop windings (45, 46, 47, 48) are wound over the entire article. This is useful for attaching end rings to rocket motor cases or for attaching rings to pressure vessels to define an aperture.
摘要翻译：将环，特别是金属环（2）连接到具有纤维增强树脂材料的壁或裙（1）的物品上。环有多个外槽（3,4,5,6）。每个槽依次包括第一（32,36,37,40）和第二（33,38,39,41）纤维增强树脂材料层。第一层中的纤维在与环的轴线平行的方向上具有基本取向，并且从裙部延伸到相应的凹槽中。覆盖第一层是第二层，包括从裙部朝向槽的环绕。第二层至少部分地位于凹槽中以将第一层锁定在凹槽中。对于每个凹槽重复该层叠，并且最后连续的环绕（45,46,47,48）缠绕在整个制品上。这对于将端环安装到火箭发动机壳体上或者用于将环连接到压力容器以限定孔径是有用的。

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