专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

11. 发明授权

US5768940A Sample collector 失效
标题翻译：样品收集器
公开(公告)号：US5768940A
公开(公告)日：1998-06-23
申请号：US848731
申请日：1997-05-22
申请人： Junichiro Kawaguchi , Akira Fujiwara , Shujiro Sawai , Masanao Abe , Akiko Nakamura
发明人： Junichiro Kawaguchi , Akira Fujiwara , Shujiro Sawai , Masanao Abe , Akiko Nakamura
IPC分类号： B64G1/66 , B64G4/00 , E21B7/00 , E21B49/02 , G01N1/04 , G01N1/08
CPC分类号： B64G4/00 , B64G1/66 , E21B49/02 , E21B7/007 , G01N1/04 , B64G2001/1064
摘要： A sample collector of this invention includes a projectile projecting unit n which a projectile is loaded and which has a projecting outlet for projecting out the projectile loaded therein, an enclosed container which is communicated with the projecting outlet of the projectile projecting unit, which has a projectile passing hole arranged at a position located away from the projecting outlet, the passing hole allowing the projectile to pass through it after the projectile is projected out from the projecting outlet, and which covers a space between the projecting outlet of the projectile projecting unit, and a kinetic energy absorbing mechanism which is arranged around a projectile path between the projecting outlet of the projectile projecting unit and the projectile passing hole of the enclosed container. The kinetic energy absorbing mechanism may be an independent active type such as brushes or an integral passive type structured by a part of the container.
摘要翻译：本发明的取样器包括：弹丸投射单元，其中装有弹丸，并且具有用于突出装载在其中的弹丸的突出出口，与弹丸投射单元的突出出口连通的封闭容器，抛射物通过孔布置在远离突出出口的位置处，通过孔允许射弹在突出的出口突出之后穿过突出的出射孔，并且覆盖射弹投影单元的突出出口之间的空间，以及围绕弹丸投射单元的突出出口与封闭容器的射弹通孔之间的射弹路径布置的动能吸收机构。动能吸收机构可以是独立的主动类型，例如由容器的一部分构成的刷子或整体被动型。

12. 发明授权

US08769923B2 Liquid-fuel storage vessel and vapor jet system using the same 有权
标题翻译：液体燃料储存容器和使用其的蒸气喷射系统
公开(公告)号：US08769923B2
公开(公告)日：2014-07-08
申请号：US12401496
申请日：2009-03-10
申请人： Takayuki Yamamoto , Osamu Mori , Junichiro Kawaguchi
发明人： Takayuki Yamamoto , Osamu Mori , Junichiro Kawaguchi
IPC分类号： B64G1/40
CPC分类号： F02K9/42 , B64G1/401 , B64G1/402
摘要： Disclosed is a liquid-fuel storage vessel for use in a vapor jet system to store liquid fuel, wherein the vapor jet system is adapted to jet the fuel in a state after being vaporized inside the liquid-fuel storage vessel, outside the liquid-fuel storage vessel, to obtain a thrust. The liquid-fuel storage vessel comprises: a hollow tank for storing the liquid fuel, wherein the tank has an ejection port for ejecting the vaporized fuel, outside the liquid-fuel storage vessel therethrough; a heating device for heating the tank; and a porous metal formed to have a plurality of interconnected cells and provided inside the tank, wherein at least a part of the liquid fuel is held in the cells of the porous metal, and heat energy given from the heating device to the tank is transferred to the liquid fuel through the porous metal to cause vaporization of at least a part of the liquid fuel. The liquid-fuel storage vessel of the present invention can obtain a stable thrust level and ensure spacecraft attitude control.
摘要翻译：公开了一种用于蒸汽喷射系统中储存液体燃料的液体燃料储存容器，其中蒸气喷射系统适于在液体 - 燃料储存容器内蒸发之前的状态下喷射燃料，在液体燃料外储存容器，以获得推力。液体燃料储存容器包括：用于储存液体燃料的中空罐，其中罐具有用于喷射蒸发燃料的喷射口，在液体燃料储存容器的外面; 用于加热罐的加热装置; 以及形成为具有多个相互连接的电池并设置在所述槽内的多孔金属，其中所述液体燃料的至少一部分保持在所述多孔金属的电池中，并且从所述加热装置向所述罐传递的热能被转移通过多孔金属使液体燃料通过至少一部分液体燃料蒸发。本发明的液体燃料储存容器可获得稳定的推力水平并确保航天器的姿态控制。

13. 发明授权

US08347298B2 Autonomous distributed control involving constraint on resources 有权
标题翻译：自主分布式控制涉及资源约束
公开(公告)号：US08347298B2
公开(公告)日：2013-01-01
申请号：US11866366
申请日：2007-10-02
申请人： Junichiro Kawaguchi , Osamu Mori , Yuichi Tsuda , Koji Nakaya
发明人： Junichiro Kawaguchi , Osamu Mori , Yuichi Tsuda , Koji Nakaya
IPC分类号： G06F9/46
CPC分类号： H04L47/70
摘要： Disclosed is a distributed control method of cooperatively allowing a control strategy for satisfying a constraint on an aggregated resource and simultaneously achieving or maintaining a performance of a system to be determined in a real-time manner by any one of a plurality of entities which have the highest need for the resource at any given time, without providing a specified management entity. The proposed method or “card game scheme” of the present invention is designed to dynamically carry out a function of satisfying a constraint on an aggregate resource and simultaneously achieving or maintaining a performance of the entire system, based on a distributed control with high flexibility, wherein an “agent”, i.e., a software having a function of performing autonomous determination and control, is set in each of the entities, to allow the entities to dynamically take turns to perform a processing of determining a strategy for resource allocation.
摘要翻译：公开了一种分散控制方法，其协作地允许控制策略以满足对聚合资源的约束，并且同时实现或维持由多个实体中的任何一个实时地确定的系统的性能，所述多个实体具有在任何给定时间对资源的最高需求，而不提供指定的管理实体。本发明提出的方法或卡片游戏方案被设计为基于具有高灵活性的分布式控制，动态地执行满足聚合资源的约束并同时实现或维持整个系统的性能的功能，其中代理，即具有执行自主确定和控制的功能的软件被设置在每个实体中，以允许实体动态轮流执行确定资源分配策略的处理。

14. 发明授权

US07806369B2 Ultrahigh altitude sun-synchronous orbit satellite system 有权
标题翻译：超高空太阳同步轨道卫星系统
公开(公告)号：US07806369B2
公开(公告)日：2010-10-05
申请号：US11630087
申请日：2004-06-22
申请人： Junichiro Kawaguchi
发明人： Junichiro Kawaguchi
IPC分类号： B64G1/10 , B64G1/00
CPC分类号： B64G1/242 , B64G1/1007 , B64G1/1021
摘要： An ultrahigh altitude sun-synchronous orbit satellite system having one or plural satellites orbiting the sun such that the satellites revolve around the earth in a substantially circular or elliptic motion at an altitude of several million kilometers from the earth, beyond the sphere of earth gravity influence. The satellites are placed on an orbital plane relative to both the sun and the earth and keep a distance and geometry between the satellites, sun and earth substantially constant. The satellite system performs any one of the services of space observation, global observation, and satellite communication. The satellites orbit the sun with both inclination and eccentricity distinct from those of the revolution of the earth and revolve around the earth with a sun synchronous property in which the local solar time is kept constant at a point on the surface of the earth directly beneath the satellite.
摘要翻译：一个超高空太阳同步轨道卫星系统，其中有一颗或多颗卫星绕着太阳转动，使得卫星以大地圆形或椭圆运动绕地球几百万公里的高度旋转，超出地球重力影响范围。卫星相对于太阳和地球放置在轨道平面上，并保持卫星之间的距离和几何形状，太阳和地球基本上恒定。卫星系统执行空间观测，全球观测和卫星通信的任何一项服务。卫星与太阳的倾斜和偏心不同于地球革命的轨道，以太阳同步性质围绕地球旋转，其中当地的太阳时间保持恒定在地球表面正下方的一个点卫星。

15. 发明申请

US20080082981A1 AUTONOMOUS DISTRIBUTED CONTROL INVOLVING CONSTRAINT ON RESOURCES 有权
标题翻译：涉及资源约束的自动分配控制
公开(公告)号：US20080082981A1
公开(公告)日：2008-04-03
申请号：US11866366
申请日：2007-10-02
申请人： Junichiro Kawaguchi , Osamu Mori , Yuichi Tsuda , Koji Nakaya
发明人： Junichiro Kawaguchi , Osamu Mori , Yuichi Tsuda , Koji Nakaya
IPC分类号： G06F9/50
CPC分类号： H04L47/70
摘要： Disclosed is a distributed control method of cooperatively allowing a control strategy for satisfying a constraint on an aggregated resource and simultaneously achieving or maintaining a performance of a system to be determined in a real-time manner by any one of a plurality of entities which have the highest need for the resource at any given time, without providing a specified management entity. The proposed novel method or “card game scheme” of the present invention is designed to dynamically carry out a function of satisfying a constraint on an aggregate resource and simultaneously achieving or maintaining a performance of the entire system, based on a distributed control with high flexibility, wherein an “agent”, i.e., a software having a function of performing autonomous determination and control, is set in each of the entities, to allow the entities to dynamically take turns to perform a processing of determining a strategy for resource allocation, without specifying the agent serving as a management entity having an authority to determine the strategy, so as to provide a processing method with high versatility.
摘要翻译：公开了一种分散控制方法，其协作地允许控制策略以满足对聚合资源的约束，并且同时实现或维持由多个实体中的任何一个实时地确定的系统的性能，所述多个实体具有在任何给定时间对资源的最高需求，而不提供指定的管理实体。本发明提出的新颖方法或“卡片游戏方案”被设计为基于具有高灵活性的分布式控制来动态地执行满足聚合资源的约束并同时实现或维持整个系统的性能的功能，其中在每个实体中设置“代理”，即具有执行自主确定和控制功能的软件，以允许实体动态轮流执行确定资源分配策略的处理，而无需指定作为具有确定策略的权限的管理实体的代理，以提供具有高通用性的处理方法。

16. 发明申请

US20060241824A1 Method of injecting plurality of spacecrafts into different orbits individually 有权
标题翻译：将多个航天器分别注入不同轨道的方法
公开(公告)号：US20060241824A1
公开(公告)日：2006-10-26
申请号：US11326440
申请日：2006-01-06
申请人： Junichiro Kawaguchi , Yasuhiro Kawakatsu , Osamu Mori
发明人： Junichiro Kawaguchi , Yasuhiro Kawakatsu , Osamu Mori
IPC分类号： G06F17/00
CPC分类号： B64G1/242 , B64G1/007 , B64G1/1085
摘要： Disclosed is a method for injecting a plurality of spacecrafts into different circum-earth or interplanetary orbits individually in a single launch. A plurality of spacecrafts coupled to an assist module are injected into an interplanetary orbit having a periodicity synchronous with the earth's revolution period. Then, in a maneuver for allowing the assist module to re-counter with and pass near to the earth Earth swing-by), the assist module appropriately performs an orbital change maneuver and a separation maneuver for each of the spacecrafts in a sequential order. Through these maneuvers, a closest-approach point to the earth is changed for each of the spacecrafts so as to drastically change a subsequent orbital element for each of the spacecrafts. The assist module takes a sufficient time to determine a target orbit for each of the spacecrafts with a high degree of accuracy until a half month to several days before a closest-approach time in the Earth swing-by. Based on the determined orbit, the assist module makes an orbit correction of about several m/sec in a sequential order, and then separates the spacecrafts therefrom in a sequential order. In this process, an inertia navigation is performed based on an accelerometer mounted in the assist module and information about attitude.
摘要翻译：公开了一种在单次发射中单独地将多个航天器注入不同的环形或星际轨道的方法。耦合到辅助模块的多个航天器被注入具有与地球旋转周期同步的周期的行星际轨道。然后，辅助模块在一个允许辅助模块重新对抗并通过接近地球地球的方法中，辅助模块按照顺序适当地执行每个航天器的轨道改变机动和分离机动。通过这些演习，对于每个航天器来说，对地球的最接近的点都是改变的，以便大幅改变每个航天器的后续轨道元素。辅助模块需要足够的时间以高精确度确定每个航天器的目标轨道，直到地球最近接近时间之前的半个月至几天。基于所确定的轨道，辅助模块按顺序进行约几m /秒的轨道校正，然后以顺序的顺序分离其中的航天器。在该过程中，基于安装在辅助模块中的加速度计和关于姿态的信息执行惯性导航。

17. 发明授权

US5775094A Apparatus and method for controlling thruster valve 失效
标题翻译：用于控制推进器阀的装置和方法
公开(公告)号：US5775094A
公开(公告)日：1998-07-07
申请号：US698083
申请日：1996-08-15
申请人： Junichiro Kawaguchi , Tatsuaki Hashimoto , Yasuhiro Morita
发明人： Junichiro Kawaguchi , Tatsuaki Hashimoto , Yasuhiro Morita
IPC分类号： B64G1/26 , B64G1/40 , F02K9/52 , F02K9/80 , F02K9/58
CPC分类号： B64G1/402 , B64G1/26 , F02K9/805
摘要： When the operation of an electromagnetic thruster valve disposed in a fluidassage for establishing the connection between a gas tank and a thruster unit for jetting gas filled in the gas tank is controlled to follow a thrust command, rise time of thrust at certain thrust is measured based on a state of the operation of the electromagnetic thruster valve. Then, the measured value and a predetermined delay value are subject to a comparison. The obtained difference is used as previous delay time to correct delay time of operation control of the electromagnetic thruster valve with respect to a next thrust command when the operation of the electromagnetic valve is controlled.
摘要翻译：当设置在用于建立气罐和用于喷射填充在气罐中的气体的推进器单元之间的连接的流体通道中的电磁推力阀的操作被控制为遵循推力指令时，测量在某个推力下的推力的上升时间基于电磁推进器阀的操作状态。然后，将测量值和预定延迟值进行比较。当控制电磁阀的操作时，获得的差值用作先前的延迟时间来校正电磁推力阀相对于下一推力命令的操作控制的延迟时间。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式