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    • 31. 发明授权
    • Rotary engine with counter-rotating housing and output shaft mounted on stationary spindle
    • 旋转式发动机具有反转壳体和输出轴安装在静止主轴上
    • US06761144B2
    • 2004-07-13
    • US10417364
    • 2003-04-16
    • Paul A. Schwam
    • Paul A. Schwam
    • F02B5300
    • B64D35/06B64D27/02F01C1/22F02B53/00F02B2053/005F04C2/10F04C11/006F04C29/0021F04C2240/603Y02T10/17
    • A counter-rotating rotary-piston engine has an output shaft with a cylindrical inner cavity rotatably mounted on a single support spindle in the frame of an aircraft. The output shaft extends substantially through the length of the engine block, which is suitably journaled on the shaft or the spindle to permit its counter-rotation. Internal combustion power is transmitted to the output shaft by means of an inner rotary piston fixed to the shaft which cooperates in conventional manner with an outer working chamber in the engine block, thereby producing concurrent rotation of the shaft and counter-rotation of the engine block. Dual propellers mounted on the shaft and on the block improve thrust performance, balance the torques and moments of inertia of the two counter-rotating masses, and virtually eliminate any resultant torque to the aircraft.
    • 反转旋转活塞发动机具有输出轴,其具有可旋转地安装在飞行器的框架中的单个支撑主轴上的圆柱形内腔。 输出轴基本上延伸穿过发动机缸体的长度,该发动机缸体适当地轴套在轴或主轴上以允许其反转。 内燃动力通过固定在轴上的内旋转活塞传递到输出轴,该内旋转活塞以常规方式与发动机缸体中的外工作室配合,从而产生轴的同时旋转和发动机缸体的反转 。 安装在轴和块上的双螺旋桨提高了推力性能,平衡了两个反向旋转质量块的扭矩和转动惯量,并且实际上消除了对飞机的任何合成扭矩。
    • 32. 发明授权
    • Shaft load balancing system
    • 轴负载平衡系统
    • US06579076B2
    • 2003-06-17
    • US09766660
    • 2001-01-23
    • John Kenneth Narney, IIDavid Turner Monk
    • John Kenneth Narney, IIDavid Turner Monk
    • F04B1700
    • F04C23/008F04C29/0021F04C2240/603F04C2270/044
    • A shaft load balancing system includes a housing divided into a first chamber at a first operating pressure and a second chamber at a second, lower operating pressure. A shaft passes from the first chamber into the second chamber. The shaft includes a first end in the first chamber, a second end in the second chamber, and a substantially axial channel connecting the first end and the second end. The first end is in fluid communication with a fluid reservoir in the housing. A reaction member engages the second end. The reaction member includes a compression volume in fluid communication with the channel. A pressure differential between the chambers forces fluid from the fluid reservoir through the channel and into the compression volume. The reaction member transmits the fluid force to the housing, allowing the fluid to create a force on the second end of the shaft.
    • 轴负载平衡系统包括在第一操作压力下分为第一室的壳体和处于第二较低工作压力的第二室。 轴从第一腔室进入第二腔室。 轴包括在第一腔室中的第一端,第二腔室中的第二端和连接第一端部和第二端部的基本轴向通道。 第一端与壳体中的流体储存器流体连通。 反作用构件接合第二端。 反应构件包括与通道流体连通的压缩体积。 室之间的压差迫使来自流体储存器的流体通过通道并进入压缩容积。 反作用构件将流体力传递到壳体,允许流体在轴的第二端上产生力。
    • 34. 发明授权
    • Scroll compressor with deflector plate
    • 涡旋压缩机带偏转板
    • US06474964B2
    • 2002-11-05
    • US09836823
    • 2001-04-17
    • Jean De BernardiPierre Ginies
    • Jean De BernardiPierre Ginies
    • F01C102
    • F04C23/008F04C18/0215F04C29/02F04C29/12F04C2240/603
    • A scroll compressor having a cylindric hermetically closed shell, a suction chamber within the shell, a scroll mechanism in the shell, lubrication mist generating elements, a suction gas inlet opening radially into the suction chamber and a deflector plate in overlying relationship with the suction gas inlet and cooperating with the shell to delimit a duct having at least an upper opening feeding suction gas to the scroll mechanism. To uniformly laden the suction chamber with sufficient oil, the upper opening is shaped to deflect suction gas into a region within the suction chamber where an oil mist is generated by the mist generating elements during operation.
    • 一种涡旋式压缩机,其具有圆筒形密闭壳体,壳体内的吸入室,壳体中的涡旋机构,润滑油产生元件,径向地进入吸入室的吸入气体入口和与吸入气体相关的偏转板 入口并与壳体配合以限定具有至少一个向上述涡旋机构供给吸入气体的上部开口的管道。 为了以足够的油均匀地装载吸入室,上部开口成形为将吸入气体偏转到吸入室内的区域,在操作期间由雾产生元件产生油雾。
    • 38. 发明申请
    • Scroll type compressor and method for compressing gas
    • 涡旋式压缩机和压缩气体的方法
    • US20020039540A1
    • 2002-04-04
    • US09967179
    • 2001-09-28
    • Kazuhiro KurokiHiroyuki GennamiNaohiro NakajimaShinji TsubaiYasushi WatanabeMasahiro Kawaguchi
    • F04C018/04
    • F04C29/128F04C18/0215F04C23/008F04C27/005F04C2240/603
    • A scroll type compressor includes a fixed scroll member, a movable scroll member, an inlet, a discharge port, a discharge valve, a first pressure region and a second pressure region. The inlet is formed through the fixed scroll base plate. The discharge port is formed through the movable scroll member. The discharge valve opens and closes the discharge port. The first pressure region and the second pressure region defined at opposite sides of the movable scroll member apply pressure to the movable scroll member. Gas introduced through the inlet is compressed and highly pressurized in accordance with the movable scroll member orbiting with respect to the fixed scroll member. The highly pressurized gas is discharged from a compression region via the discharge port and the discharge valve. The compressor is provided with a communication passage so as to intercommunicate the first pressure region and the second pressure region during a predetermined period of a compression cycle established by the gas. The gas is flowed between both the pressure regions due to a pressure difference between both pressure regions at timing when the thrust force acting on the back surface of the movable scroll member is large.
    • 涡旋式压缩机包括固定涡旋构件,可动涡旋构件,入口,排出口,排出阀,第一压力区域和第二压力区域。 入口通过固定涡旋基板形成。 排出口通过动涡旋件形成。 排气阀打开和关闭排放口。 限定在可动涡旋件的相对侧的第一压力区域和第二压力区域向可动涡旋件施加压力。 通过入口引入的气体根据相对于固定涡旋件轨道运动的可动涡旋件被压缩和高度加压。 高压气体经由排出口和排出阀从压缩区域排出。 压缩机设置有连通通道,以在由气体建立的压缩循环的预定时段期间使第一压力区域和第二压力区域相互连通。 在作用于动涡旋件的背面的推力大的时刻,由于压力区域之间的压力差,气体在两个压力区域之间流动。
    • 39. 发明申请
    • Scroll compressors
    • 涡旋式压缩机
    • US20020039539A1
    • 2002-04-04
    • US09965982
    • 2001-09-28
    • Shinji TsubaiHiroyuki GennamiMasao IguchiNaohiro NakajimaKazuo KobayashiKazuhiro KurokiMasahiro Kawaguchi
    • F04C018/04
    • H02K7/075F04C18/0215F04C23/008F04C27/009F04C2240/603H02K5/10
    • Scroll compressor may include, for example, a stationary scroll, a drive shaft, a crank shaft coupled to the drive shaft, a bush coupled to the outer surface of the crank shaft and a movable scroll coupled to the crank shaft. The movable scroll is preferably disposed adjacent to the stationary scroll. A boss may be coupled to the movable scroll and the boss preferably protrudes from the movable scroll at the opposite side of the stationary scroll. A seal is preferably disposed in a clearance defined between the bush and the boss. A compression chamber is defined by a space between the stationary scroll and the movable scroll. Fluid is compressed within the compression chamber when the movable scroll revolves or orbits with respect to the stationary scroll. A discharge port is preferably defined within the movable scroll and is adapted to discharge compressed fluid to a side that is opposite of the stationary scroll.
    • 涡旋压缩机可以包括例如固定涡卷,驱动轴,联接到驱动轴的曲轴,联接到曲轴的外表面的衬套和联接到曲轴的可动涡旋。 动涡旋件优选地邻近固定涡卷设置。 凸台可以联接到动涡旋盘上,并且凸台优选地在静涡旋盘的相反侧从可动涡旋件突出。 密封件优选地设置在限定在衬套和凸台之间的间隙中。 压缩室由固定涡旋件和动涡旋件之间的空间限定。 当动涡旋盘相对于静涡旋盘旋转或轨道运动时,流体在压缩室内被压缩。 排出口优选地限定在可动涡旋件内,并且适于将压缩流体排放到与固定涡旋件相对的一侧。