公开(公告)号：US5005786A

公开(公告)日：1991-04-09

申请号：US402586

申请日：1989-09-05

申请人： Osamu Okamoto ,  Teruomi Nakaya ,  Seizo Suzuki ,  Naoaki Kuwano ,  Yoshinori Sakai ,  Hiroshi Oda ,  Masao Uegusa ,  Goji Iba

发明人： Osamu Okamoto ,  Teruomi Nakaya ,  Seizo Suzuki ,  Naoaki Kuwano ,  Yoshinori Sakai ,  Hiroshi Oda ,  Masao Uegusa ,  Goji Iba

IPC分类号： B64G1/38 ,  B64G1/64 ,  F16F15/02

CPC分类号： B64G1/646

摘要： A docking and active damping device for space structures is provided, in a docking portion of one space structure to be docked, with a positioning device in which an output rotor can be moved and rotated within a two-dimensional plane by a composite rotation of one or more eccentric rotors capable of being independently driven and controlled by a direct drive motor and the output rotor, and a docking member having a docking ring and a latch mechanism are supported on the output rotor of the positioning device. A probe having a capture device capable of being protruded and driven in an axial direction by a linear motion is provided inwardly of the docking member, and the probe provides a 4-freedom movement according to a position of the passive side to capture and dock a drogue. The docking ring is supported through a strain sensor, a vibration of the passive side structure is detected, and the docking member is moved in a direction of suppressing the vibration to promptly suppress the vibration caused by disturbances from the inside and outside of the space structures.

摘要翻译： 在一个待对接的一个空间结构的对接部分中提供用于空间结构的对接和主动阻尼装置，其具有定位装置，在该定位装置中，输出转子可以在二维平面内通过复合旋转 或更多的能够由直接驱动马达和输出转子独立驱动和控制的偏心转子，并且具有对接环和闩锁机构的对接构件被支撑在定位装置的输出转子上。 具有能够通过线性运动在轴向方向突出并被驱动的捕获装置的探针设置在对接构件的内部，并且探针根据被动侧的位置来捕获和对准一个4自由度的运动 流氓 对接环通过应变传感器支撑，检测到被动侧结构的振动，并且对接构件沿抑制振动的方向移动，以迅速地抑制由空间结构的内部和外部的干扰引起的振动 。

公开(公告)号：US4518261A

公开(公告)日：1985-05-21

申请号：US478884

申请日：1983-03-25

申请人： Yukihiko Sekimoto ,  Osamu Okamoto

发明人： Yukihiko Sekimoto ,  Osamu Okamoto

IPC分类号： E21B43/22 ,  B01F3/12 ,  B01F5/00 ,  B01F15/02

CPC分类号： B01F7/1635 ,  B01F15/0201 ,  B01F15/0272 ,  B01F3/1221 ,  B01F3/1271 ,  B01F5/0068 ,  B01F5/0074

摘要： Equipment for dissolving polyacrylamide powder to obtain an aqueous solution thereof for enhanced oil recovery comprisesfirst and second powder storage tanks for storing polyacrylamide powder under nitrogen atmosphere;a gas conveyor unit for carrying the polyacrylamide powder from the first storage tank to the second storage tank by nitrogen gas flow;a constant powder supply unit for receiving the polyacrylamide powder from the second storage tank, metering the powder, and sending the metered powder toa powder dispersion unit for dispersing in water the polyacrylamide powder.A first liquid supply unit sends the dispersion or solution of polyacrylamide powder obtained from the powder dispersion unit to a dissolution tank for completing dissolution of the polyacrylamide;and a second liquid supply unit transfers the polyacrylamide solution from the dissolution tank to a solution storage tank for storing the polyacrylamide solution.A filtration unit is connected in the liquid supply line between the dissolution tank and the solution storage tank; anda nitrogen gas supply system maintains the interiors of these units filled with nitrogen gas at a pressure higher than atmospheric pressure.

摘要翻译： 用于溶解聚丙烯酰胺粉末以获得其用于提高油回收率的水溶液的设备包括用于在氮气氛下储存聚丙烯酰胺粉末的第一和第二粉末储存罐; 用于通过氮气流将聚丙烯酰胺粉末从第一储罐运送到第二储罐的气体输送单元; 用于从第二储罐接收聚丙烯酰胺粉末的恒定粉末供应单元，计量粉末，并将计量粉末发送到分散在水中的粉末分散单元的聚丙烯酰胺粉末。 第一液体供应单元将从粉末分散单元获得的聚丙烯酰胺粉末的分散体或溶液发送到溶解槽，以完成聚丙烯酰胺的溶解; 并且第二液体供应单元将聚丙烯酰胺溶液从溶解槽转移到用于储存聚丙烯酰胺溶液的溶液储存罐。 过滤单元连接在溶解槽和溶液储罐之间的液体供应管线中; 并且氮气供给系统将这些单元的内部保持在高于大气压的压力下填充氮气。

公开(公告)号：US08295748B2

公开(公告)日：2012-10-23

申请号：US12836709

申请日：2010-07-15

申请人： Osamu Okamoto

发明人： Osamu Okamoto

IPC分类号： G03G15/01

CPC分类号： G03G15/2064 ,  G03G2215/2022

摘要： A typical belt conveying apparatus and a typical image forming apparatus according to the present invention includes: an endless belt; a supporting member that rotatably supports the belt; a sensor that detects a predetermined breakage at one end of the belt in a belt width direction; and a detecting mechanism that detects a predetermined breakage at the other end of the belt in the belt width direction by the use of the sensor.

摘要翻译： 根据本发明的典型的带式输送装置和典型的图像形成装置包括：环形带; 支撑构件，其可旋转地支撑所述带; 传感器，其在带宽度方向上检测所述带的一端处的预定断裂; 以及检测机构，其通过使用传感器检测带的另一端在带宽度方向上的预定断裂。

公开(公告)号：US06981364B2

公开(公告)日：2006-01-03

申请号：US10623601

申请日：2003-07-22

申请人： Osamu Okamoto ,  Tatsuo Yamanaka ,  Masataka Maita ,  Hideyuki Taguchi ,  Takeshi Tsuchiya

发明人： Osamu Okamoto ,  Tatsuo Yamanaka ,  Masataka Maita ,  Hideyuki Taguchi ,  Takeshi Tsuchiya

IPC分类号： F02K9/78 ,  F02K7/18

CPC分类号： B64G1/402 ,  B64C30/00 ,  B64G1/14 ,  B64G1/401 ,  F02K7/18

摘要： A novel combined engine for a single-stage spacecraft is provided that combines a air-breathing engine utilizing oxygen in the atmosphere as oxidizer and rocket engines for obtaining thrust outside the atmosphere and that does not require a portion whose shape is variable in accordance with the flight speed. Rocket engines 15 are provided on struts 12 that form air introduction channels 10 in the air intake section 4. The rocket jets 18 from the rocket engines 15 control the flow of the airflows 16 introduced into the combustion chamber 20 in accordance with the flight speed. When the spacecraft 1 is stationary or in subsonic flight, the rocket jets 18 promote air intake into the combustion chamber 20 by lowering of static pressure due to expansion (ejector effect). In the subsonic flight condition, it performs the role of air compression, mixing with incoming air, fuel injection and ignition and during supersonic/ultra-supersonic flight it performs the role of a variable diffuser.

摘要翻译： 提供了一种用于单级航天器的新型组合发动机，其将在大气中使用氧气的空气呼吸发动机作为氧化剂和用于在大气外部获得推力的火箭发动机相结合，并且不需要其形状根据 飞行速度。 在引导部分4上形成空气引入通道10的支柱12上设有火箭发动机15。 来自火箭发动机15的火箭喷射器18根据飞行速度来控制引入燃烧室20的气流16的流动。 当航天器1是静止或亚音速飞行时，火箭喷射器18通过由于膨胀（喷射器效应）降低静压而促进进入燃烧室20的空气。 在亚音速飞行条件下，它起到空气压缩，与进入的空气混合，燃料喷射和点燃的作用，并且在超音速/超超音速飞行期间，它执行可变扩散器的作用。

公开(公告)号：US20050004363A1

公开(公告)日：2005-01-06

申请号：US10484765

申请日：2002-07-18

申请人： Masaya Hashimoto ,  Osamu Okamoto

发明人： Masaya Hashimoto ,  Osamu Okamoto

IPC分类号： A61P1/00 ,  A61P3/04 ,  A61P7/12 ,  A61P11/06 ,  A61P11/08 ,  A61P11/14 ,  A61P15/10 ,  A61P23/00 ,  A61P25/04 ,  A61P25/16 ,  A61P25/18 ,  A61P25/20 ,  A61P25/22 ,  A61P25/24 ,  A61P25/28 ,  A61P25/36 ,  A61P43/00 ,  C07D471/10 ,  C07D487/10

CPC分类号： C07D471/10

摘要： The invention relates to 4-oxoimidazolidine-2-spiropiperidine derivatives represented by a general formula [I] [in which A1, A2, A3, A4 and A5 stand for optionally halogen-substituted methine, or nitrogen atom; R1 and R2 stand for lower alkyl or the like; R3 stands for hydrogen or lower alkyl; R4 and R5 stand for hydrogen, or lower alkyl which is optionally substituted with hydroxy, or the like]or salts thereof. These compounds act as nociceptin receptor agonist, and are useful as analgesic, reliever from tolerance to narcotic analgesic, reliever from dependence on narcotic analgesic, analgesic enhancer, antiobestic, drug for ameliorating brain function, remedy for schizophrenia, drug for treating regressive neurodegenerative diseases, antianxiety agent or antidepressant and remedy for diabetes insipidus and polyuria; and the like.

摘要翻译： 本发明涉及由通式[I]表示的4-氧代咪唑烷-2-螺哌啶衍生物[其中A1，A2，A3，A4和A5代表任选卤素取代的次甲基或氮原子; R 1和R 2代表低级烷基等; R 3代表氢或低级烷基; R 4和R 5代表氢，或任选被羟基取代的低级烷基等或其盐。 这些化合物作为伤害感受肽受体激动剂起作用，可用作镇痛药，缓解麻醉止痛药耐受性，缓解依赖麻醉止痛药，镇痛增强剂，抗胆固醇药，改善脑功能药物，精神分裂症药物治疗，治疗退行性神经退行性疾病药物， 抗焦虑药或抗抑郁药及其治疗尿崩症及多尿症; 等等。

公开(公告)号：US5866813A

公开(公告)日：1999-02-02

申请号：US751478

申请日：1996-11-18

申请人： Teruomi Nakaya ,  Osamu Okamoto ,  Naoaki Kuwano ,  Seizo Suzuki ,  Shuichi Sasa ,  Hidehiko Nakayasu ,  Masakazu Sagisaka

发明人： Teruomi Nakaya ,  Osamu Okamoto ,  Naoaki Kuwano ,  Seizo Suzuki ,  Shuichi Sasa ,  Hidehiko Nakayasu ,  Masakazu Sagisaka

IPC分类号： G09B9/00 ,  B64F5/00 ,  G01M9/02 ,  G01M9/06 ,  G09B9/08

CPC分类号： G01M9/065 ,  G01M9/06

摘要： A transportable three-dimensional calibration wind tunnel system is comprised of a small wind tunnel portion for creating a three-dimensional calibration air having a suitable wind velocity, and a two-axis rotational deformation device portion for causing said wind tunnel portion to effect a conical motion with a nozzle blow port being an apex to suitably change a flow angle. The two-axis rotational deformation device is comprised of a .beta.-angle rotational deformation device having a .beta.-angle deformation base supported to be rotated horizontally, and a .alpha.-angle rotational deformation device having a .alpha.-angle deformation base supported to be rotated vertically. A rotational axis of the .alpha.-angle deformation base, a rotational axis of the .beta.-angle deformation base and a center axis of the small wind tunnel portion are arranged so that they intersect at a point. In a method for the verification of a flight control system of an aircraft using the transportable three-dimensional calibration wind tunnel system, the nozzle blow port of the three-dimensional calibration wind tunnel system is positioned at the extreme end of an air data sensor probe provided on the aircraft, and the three-dimensional calibration wind tunnel system and an on-board control computer of the aircraft are connected to an out-board control computer so that a suitable three-dimensional airflow is generated by the three-dimensional calibration wind tunnel system to verify the operation and function of the control surface in the stopped state on the ground.

摘要翻译： 可移动的三维校准风洞系统包括用于产生具有合适风速的三维校准空气的小风洞部分和用于使所述风洞部分实现锥形的两轴旋转变形装置部分 具有喷嘴吹出口作为顶点的运动以适当地改变流动角度。 双轴旋转变形装置由具有被支撑为水平旋转的β角变形基体的β角旋转变形装置和具有被支撑为垂直旋转的α角变形基体的α角旋转变形装置 。 α角变形基底的旋转轴线，β角变形基底的旋转轴线和小风洞部分的中心轴线被布置成使得它们在一个点处相交。 在使用可运输的三维校准风洞系统验证飞机的飞行控制系统的方法中，三维校准风洞系统的喷嘴吹出口位于空气数据传感器探头的末端 飞机上提供的三维校准风洞系统和飞机的车载控制计算机连接到外板控制计算机，从而通过三维校准风产生合适的三维气流 隧道系统验证控制面在地面停止状态下的运行和功能。

公开(公告)号：US5627311A

公开(公告)日：1997-05-06

申请号：US517969

申请日：1995-08-22

申请人： Teruomi Nakaya ,  Osamu Okamoto ,  Naoaki Kuwano ,  Seizo Suzuki ,  Shuichi Sasa ,  Hidehiko Nakayasu ,  Masakazu Sagisaka

发明人： Teruomi Nakaya ,  Osamu Okamoto ,  Naoaki Kuwano ,  Seizo Suzuki ,  Shuichi Sasa ,  Hidehiko Nakayasu ,  Masakazu Sagisaka

IPC分类号： G09B9/00 ,  B64F5/00 ,  G01M9/02 ,  G01M9/06 ,  G01M9/04 ,  G01M17/00

CPC分类号： G01M9/065 ,  G01M9/06

摘要： A transportable three-dimensional calibration wind tunnel system consists of a small wind tunnel portion for creating a three-dimensional airflow having a suitable wind velocity, and a two-axis rotational deformation device portion for causing the wind tunnel portion to effect a conical motion with a nozzle blow port being in close proximity to an apex to suitably change a flow angle. The two-axis rotational deformation device includes a .beta.-angle rotational deformation device having a .beta.-angle deformation base supported to be rotated horizontally, and an .alpha.-angle rotational deformation device having an .alpha.-angle deformation base supported to be rotated vertically. A rotational axis of the .alpha.-angle deformation base, a rotational axis of the .beta.-angle deformation base and a center axis of the small wind tunnel portion are arranged so that they intersect at a point. When verifying a flight control system of an aircraft using the transportable three-dimensional calibration wind tunnel system, the nozzle blow port of the three-dimensional calibration wind tunnel system is positioned at the extreme end of an air data sensor probe provided on the aircraft, and the three-dimensional calibration wind tunnel system and an on-board control computer of the aircraft are connected to an out-board control computer so that a suitable three-dimensional airflow is generated by the three-dimensional calibration wind tunnel system to verify the operation and function of the control surface in the stopped state on the ground.

摘要翻译： 可移动的三维校准风洞系统由用于产生具有合适风速的三维气流的小风洞部分和用于使风洞部分进行锥形运动的双轴旋转变形装置部分组成， 喷嘴吹出口靠近顶点以适当地改变流动角度。 双轴旋转变形装置包括具有被支撑为水平旋转的β角变形基体的β角转动变形装置，以及被支撑为垂直旋转的α角变形基体的α角旋转变形装置。 α角变形基底的旋转轴线，β角变形基底的旋转轴线和小风洞部分的中心轴线被布置成使得它们在一个点处相交。 当使用可运输的三维校准风洞系统验证飞行器的飞行控制系统时，三维校准风洞系统的喷嘴吹出口位于设置在飞行器上的空气数据传感器探头的最末端， 并将飞机的三维校准风洞系统和车载控制计算机连接到外板控制计算机，以便通过三维校准风洞系统产生合适的三维气流，以验证 控制面在地面停止状态下的操作和功能。

公开(公告)号：US5550121A

公开(公告)日：1996-08-27

申请号：US312619

申请日：1994-09-27

申请人： Susumu Nakagawa ,  Shinji Kato ,  Satoshi Murase ,  Osamu Okamoto ,  Ryuji Mitomo ,  Katsumi Yamamoto ,  Koji Yamada ,  Hiroshi Fukatsu

发明人： Susumu Nakagawa ,  Shinji Kato ,  Satoshi Murase ,  Osamu Okamoto ,  Ryuji Mitomo ,  Katsumi Yamamoto ,  Koji Yamada ,  Hiroshi Fukatsu

IPC分类号： C07D207/12 ,  C07D477/20 ,  C07D487/04 ,  A61K31/40

CPC分类号： C07D477/20 ,  C07D207/12

摘要： A compound of the formula: ##STR1## wherein R.sup.1 is a hydrogen atom or a methyl group, R.sup.2 is a hydrogen atom or a negative charge, R.sup.3 is a hydrogen atom, a halogen atom, a hydroxyl group, a lower alkoxy group, a lower alkanoyloxy group, an amino group, an N-lower alkylamino group, an N,N-di-lower alkylamino group, a lower alkanoylamino group, an aroylamino group, a (lower alkylsulfonyl)amino group, a sulfamoylamino group, a cyano group, a nitro group, a group of --COOR.sup.4 (wherein R.sup.4 is a hydrogen atom or a lower alkyl group) or a group of --CON(R.sup.5)R.sup.6 (wherein each of R.sup.5 and R.sup.6 which may be the same or different, is a hydrogen atom or a lower alkyl group, or R.sup.5 and R.sup.6 form together with the adjacent nitrogen atom a heterocyclic group selected from the group consisting of an aziridinyl group, an azetidinyl group, a pyrrolidinyl group, a piperidyl group, a piperazinyl group, a 4-lower alkyl piperazinyl group and a morpholino group), A is a linear or branched lower alkylene group, X is a group of --N(R.sup.7)R.sup.8 (wherein each of R.sup.7 and R.sup.8 which may be the same or different, is a hydrogen atom or a lower alkyl group) or a group of --N.sup.+ (R.sup.9)(R.sup.10)R.sup.11 (wherein each of R.sup.9, R.sup.10 and R.sup.11 which may be the same or different, is a lower alkyl group), provided that when A is a linear lower alkylene group, R.sup.3 is other than a hydrogen atom; or a pharmaceutically acceptable salt or ester thereof.

摘要翻译： 下式的化合物：其中R1是氢原子或甲基，R2是氢原子或负电荷，R3是氢原子，卤素原子，羟基，低级烷氧基 低级烷酰氧基，氨基，N-低级烷基氨基，N，N-二低级烷基氨基，低级烷酰基氨基，芳酰氨基，（低级烷基磺酰基）氨基，氨磺酰氨基， 氰基，硝基，-COOR 4（其中R 4是氢原子或低级烷基）或-CON（R 5）R 6（其中R 5和R 6可以相同或不同）的基团 是氢原子或低级烷基，或者R 5和R 6与相邻的氮原子一起形成选自氮丙啶基，氮杂环丁烷基，吡咯烷基，哌啶基，哌嗪基的杂环基 ，4-低级烷基哌嗪基和吗啉代基），A为直链或支链低级亚烷基，X为杂环 -N（R 7）R 8（其中可以相同或不同的R7和R8各自为氢原子或低级烷基）或-N +（R 9）（R 10）R 11（其中每个 R 9，R 10和R 11可以相同或不同，为低级烷基），条件是当A为直链低级亚烷基时，R 3不是氢原子; 或其药学上可接受的盐或酯。

公开(公告)号：US5079727A

公开(公告)日：1992-01-07

申请号：US374457

申请日：1989-06-30

申请人： Masahiro Yasue ,  Osamu Okamoto ,  Masaaki Yamaguchi ,  Noriyuki Ono ,  Yoshiteru Sunachi

发明人： Masahiro Yasue ,  Osamu Okamoto ,  Masaaki Yamaguchi ,  Noriyuki Ono ,  Yoshiteru Sunachi

IPC分类号： B28C7/00 ,  G05B19/418 ,  G05D1/00 ,  G05D11/13 ,  G07C3/14 ,  G07C5/00 ,  G07C5/08

CPC分类号： G07C5/0858 ,  B28C7/0007 ,  G05B19/4183 ,  G05D11/133 ,  G07C3/14 ,  G07C5/008 ,  Y02P90/04 ,  Y02P90/10 ,  Y02P90/22

摘要： A system wherein raw material excavated from a plurality of pit faces on a mine are conveyed to and collected at a specific collecting location at the foot of a mountain by a plurality of vehicles and the degree of quality of collected raw material is then properly controlled at the specific collecting location is generally called a mining site control process. To practically execute such a mining control process, the degree of quality of conveyed raw material previously analyzed per each pit face and a quantity of conveyance thereof are confirmed at every time when the raw material is conveyed to the collecting location. Then, the degree of quality of raw material required to be next conveyed so as to allow the degree of quality predetermined as a target with respect to raw material to be collected is determined on the basis of the confirmed degree of quality and quantity of conveyance, and the manner of operating the respective vehicles is determined on a real time base so as to allow the thus determined degree of quality to be realized. When such a manner of operating the vehicles is to be determined, the most effective arrangement is selected for them in view of the representative state of actual operations of the vehicles and their loading capacity. All information in relation to such a mining site control process are electrically processed using a variety of sensors arranged at the respective pit faces and the collecting location, a computer installed in a control center and the like means.

摘要翻译： 将从矿山上的多个坑面挖出的原料通过多个车辆输送到山脚下的特定收集位置并收集在其中的系统，然后将所收集的原料的质量程度适当地控制在 具体的收集位置通常称为采矿现场控制过程。 为了实际执行这样的采矿控制过程，在原料被输送到收集位置的每一次，都确认了每个凹坑面先前分析的输送原料的质量程度和输送量。 然后，基于所确认的质量和运送量来确定需要接下来传送的原料的质量程度，以使得能够收集关于原料被预先确定为目标的质量的程度， 并且以实时基准确定操作各车辆的方式，以便实现如此确定的质量程度。 当确定这种操作车辆的方式时，鉴于车辆的实际操作的代表性状态及其承载能力，选择最有效的安排。 关于这种采矿现场控制过程的所有信息使用布置在相应凹坑面和收集位置处的各种传感器，安装在控制中心等中的计算机进行电加工。

公开(公告)号：US4455556A

公开(公告)日：1984-06-19

申请号：US262860

申请日：1981-05-12

申请人： Tatsukichi Koshio ,  Osamu Okamoto

发明人： Tatsukichi Koshio ,  Osamu Okamoto

IPC分类号： G01S13/78 ,  G01S13/76 ,  G01S7/28

CPC分类号： G01S13/788

摘要： In a distance measuring equipment for measuring the distance between an interrogator and a transponder with high precision by detecting the time from transmission of an interrogation pulse from the interrogator to reception of a reply pulse transmitted from the transponder on the basis of timing positions of said respective pulses; as leading edges of the interrogation pulse and reply pulse, a waveform represented by the formula of: ##EQU1## where E and F represent finite positive values and T represents time, is used, or else as a leading edge of the interrogation pulse, a waveform which can be approximated by the above formula is used, while as a leading edge of the reply pulse, a waveform obtained by passing a waveform approximately expressed by the formula of: ##EQU2## through a low-pass filter having a predetermined cut-off frequency, is used.

摘要翻译： 在距离测量设备中，通过检测从询问器传送询问脉冲到接收从应答器发送的应答脉冲的时间，基于所述相应的定时位置来测量询问器和应答器之间的距离， 脉冲 作为询问脉冲和应答脉冲的前沿，由以下公式表示的波形：其中E和F表示有限正值，T表示时间，或者作为前导边 使用询问脉冲，可以使用上述公式近似的波形，而作为应答脉冲的前沿，通过将由以下公式近似表示的波形传递得到的波形： + TR 通过 使用具有预定截止频率的低通滤波器。