会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 1. 发明授权
    • Foreign-object offshore processing system
    • 对外海洋加工系统
    • US09303378B2
    • 2016-04-05
    • US14002394
    • 2011-03-02
    • Shinya IshikawaTakashi SaitoKyoichi ShimizuMasaki SuzukiKota ShiodaMasaru Ieyasu
    • Shinya IshikawaTakashi SaitoKyoichi ShimizuMasaki SuzukiKota ShiodaMasaru Ieyasu
    • E02B5/08E02B8/02E02B9/04E03B1/02E02B1/00
    • E02B9/04E02B1/006E02B5/08E02B5/085E02B8/023E03B1/02
    • Provided is foreign-object offshore processing system, including foreign-object inflow prevention devices configured to prevent inflow of foreign object into water intake and provided at interval. Each device includes: collecting pontoon serving as inlet of foreign object and provided to float on sea surface of pool defined by curtain wall, the pool being for drawing cooling sea water from sea toward water intake; bottom net spreading toward sea bottom on upstream side of water intake channel in triangular shape with collecting pontoon as vertex; longitudinal net fixed to two floating chains in suspended manner to spread out in surface area of sea, the two floating chains extending on sea surface from collecting pontoon in correspondence with two sides extending from vertex of triangular shape forming bottom net; and lateral net spreading between bottom net and at least portion of longitudinal net, wherein horizontal net cover covers interval between adjacent devices.
    • 提供的是外来物体海洋处理系统,包括防止异物进入进水并间隔设置的异物流入防止装置。 每个装置包括:收集作为异物入口的浮筒,并设置在浮动在幕墙限定的游泳池的海面上,该池用于将海水从海水中抽出,进入吸水口; 底部网向三角形进水通道上游侧向海底扩散,收集浮桥为顶点; 纵向网以悬挂的方式固定在两个浮动链上,以扩散到海面,两条浮动链从收集浮船延伸,对应于从三角形形成底网的顶点延伸的两侧; 以及底网和纵向网的至少部分之间的横向网扩展,其中水平网盖覆盖相邻设备之间的间隔。
    • 3. 发明授权
    • Hydraulic clutch and transmission device provided with the same
    • 液压离合器和传动装置配有相同的
    • US08839929B2
    • 2014-09-23
    • US13419013
    • 2012-03-13
    • Hiroshi KatoToshihiko AokiMichio NobataMasaki Suzuki
    • Hiroshi KatoToshihiko AokiMichio NobataMasaki Suzuki
    • F16D25/12
    • F16D13/683F16D25/0638F16D25/10F16D25/12F16D2048/029
    • A hydraulic clutch includes a clutch drum with an outer cylinder that slidably holds a plurality of clutch plates, an inner cylinder that axially extends from an inner circumference of a sidewall, and a sleeve fitted inside the inner cylinder. A clutch piston presses the clutch plates. A plate and the clutch piston define an oil chamber that cancels centrifugal hydraulic pressure. An oil passage that communicates with the oil chamber is on an inner circumferential surface of the inner cylinder. One surface of the sleeve contacts a step formed on the inner cylinder. The sleeve includes a passage in communication with the oil passage and formed on an outer periphery of the sleeve to axially extend toward the end surface, and a second passage formed more axially recessed than an end surface and radially extending to provide communication between the first passage and an inner portion of the sleeve.
    • 液压离合器包括具有可滑动地保持多个离合器片的外筒的离合器鼓,从侧壁的内周轴向延伸的内筒和装配在内筒内的套筒。 离合器活塞压紧离合器片。 板和离合器活塞限定了油室,其消除了离心液压。 与油室连通的油路在内筒的内周面上。 套筒的一个表面接触形成在内筒上的台阶。 套筒包括与油通道连通的通道并且形成在套筒的外周上以朝向端表面轴向延伸,以及形成为比端表面更轴向凹入的径向延伸以提供第一通道 和套筒的内部。
    • 8. 发明申请
    • HYDRAULIC CLUTCH AND TRANSMISSION DEVICE PROVIDED WITH THE SAME
    • 液压离合器和传动装置
    • US20120247906A1
    • 2012-10-04
    • US13419013
    • 2012-03-13
    • Hiroshi KATOToshihiko AOKIMichio NOBATAMasaki SUZUKI
    • Hiroshi KATOToshihiko AOKIMichio NOBATAMasaki SUZUKI
    • F16D25/10F16D11/04
    • F16D13/683F16D25/0638F16D25/10F16D25/12F16D2048/029
    • A hydraulic clutch includes a clutch drum with an outer cylinder that slidably holds a plurality of clutch plates, an inner cylinder that axially extends from an inner circumference of a sidewall, and a sleeve fitted inside the inner cylinder. A clutch piston presses the clutch plates. A plate and the clutch piston define an oil chamber that cancels centrifugal hydraulic pressure. An oil passage that communicates with the oil chamber is on an inner circumferential surface of the inner cylinder. One surface of the sleeve contacts a step formed on the inner cylinder. The sleeve includes a passage in communication with the oil passage and formed on an outer periphery of the sleeve to axially extend toward the end surface, and a second passage formed more axially recessed than an end surface and radially extending to provide communication between the first passage and an inner portion of the sleeve.
    • 液压离合器包括具有可滑动地保持多个离合器片的外筒的离合器鼓,从侧壁的内周轴向延伸的内筒和装配在内筒内的套筒。 离合器活塞压紧离合器片。 板和离合器活塞限定了油室,其消除了离心液压。 与油室连通的油路在内筒的内周面上。 套筒的一个表面接触形成在内筒上的台阶。 套筒包括与油通道连通的通道并且形成在套筒的外周上以朝向端表面轴向延伸,以及形成为比端表面更轴向凹入的径向延伸以提供第一通道 和套筒的内部。
    • 9. 发明授权
    • Air shifter toy model
    • 空气换档玩具模型
    • US08246414B2
    • 2012-08-21
    • US12820294
    • 2010-06-22
    • Masaki Suzuki
    • Masaki Suzuki
    • A63H27/18A63H27/30
    • A63H27/02A63H30/04
    • The present invention provides an unconventional and proprietary radio control (RC) or infrared remote control (IR) toy model/airplane which can intentionally shift or change its center of gravity (COG) to different positions along the longitudinal centerline of the aircraft or fuselage. The incremental shifting or moving of the COG from front to rear or vice versa incrementally changes the “angle of attack” of the wing, thereby producing a variable range of viable flight attitudes and resultant terminal velocities (top speeds). Therefore, users can easily select an appropriate speed for the airplane to fly in limited indoor spaces or in larger outdoor areas. Additionally, the COG shifting of the present invention can be applied not only to RC and IR controlled toy models/aircrafts but may also be implemented into real aircrafts including manned and unmanned aircraft for civilian and/or military applications.
    • 本发明提供了一种非常规和专有的无线电控制(RC)或红外遥控(IR)玩具模型/飞机,其可以有意地将其重心(COG)移动或改变到沿飞机或机身的纵向中心线的不同位置。 COG从前到后的增量移动或移动反过来逐渐改变机翼的“迎角”,从而产生可行的飞行姿态和最终的最终速度(最高速度)的可变范围。 因此,用户可以轻松地选择合适的速度使飞机在有限的室内空间或较大的户外区域内飞行。 此外,本发明的COG转移不仅可以应用于RC和IR控制的玩具模型/飞机,而且还可以被实现为真正的飞机,包括用于民用和/或军事应用的载人和无人飞行器。