Scroll compressor with control of lubricant flow
    3.
    发明授权
    Scroll compressor with control of lubricant flow 失效
    涡旋压缩机控制润滑油流量

    公开(公告)号:US4762477A

    公开(公告)日:1988-08-09

    申请号:US913349

    申请日:1986-09-30

    CPC分类号: F04C29/023 F04C29/0007

    摘要: A scroll compressor has a channel formed in a compressor member such as main shaft, frame, orbital scroll member, through which lubricating oil can pass easily from the higher pressure side to the lower pressure side under flow control between sliding surfaces of the compressor members without reduction in the sealing between the higher pressure side and the lower pressure side, whereby injecting sufficient lubricating oil between the scroll members improves both the sealing and the lubricating between the scroll members.

    摘要翻译: 涡旋压缩机具有形成在诸如主轴,框架,轨道涡旋构件的压缩机构件中的通道,润滑油可以在压缩机构件的滑动表面之间的流动控制下从低压侧容易地从较高压侧传递到低压侧,而没有 降低高压侧和低压侧之间的密封,从而在涡旋件之间注入足够的润滑油,可以提高涡旋件之间的密封和润滑。

    Scroll compressor with a thrust reduction mechanism
    4.
    发明授权
    Scroll compressor with a thrust reduction mechanism 失效
    带减压机构的涡旋压缩机

    公开(公告)号:US4696630A

    公开(公告)日:1987-09-29

    申请号:US903872

    申请日:1986-09-02

    摘要: In a scroll compressor for compressing gas a scroll unit having stationary and orbiting scroll members with interfitting spiroidal wraps is hermetically enclosed in a housing. During operation, a compression chamber defined between the scroll chambers is given a high pressure, and the space in the housing below the orbiting scroll member is given a low pressure atmosphere. A motor housed in the low pressure atmosphere rotates a drive shaft. This drive shaft causes the orbiting scroll member to orbit. A passage is provided in the orbiting scroll member to connect the low pressure atmosphere and the compression chamber. A thrust reduction mechanism is supported by the housing in the low pressure atomophere. The thrust reduction mechanism receives the pressure of the compression chamber via the passage.

    摘要翻译: 在用于压缩气体的涡旋压缩机中,具有带有相互配合的螺旋形涡卷的固定和绕动涡旋件的涡旋单元气密地封闭在壳体中。 在操作期间,限定在涡旋室之间的压缩室被施加高压,并且在绕动涡旋构件下方的壳体中的空间被赋予低压气氛。 容纳在低压气氛中的马达使驱动轴旋转。 该驱动轴使绕动涡旋构件轨道运动。 在绕动涡旋构件中设置有一个通道,以连接低压气氛和压缩室。 减压机构由低压原子空间中的外壳支撑。 推力减小机构经由通路接收压缩室的压力。