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    • 11. 发明授权
    • Scroll type compressor
    • 涡旋式压缩机
    • US06213741B1
    • 2001-04-10
    • US09153371
    • 1998-09-15
    • Tatsushi MoriShinya YamamotoHiroyuki HayashiShigeru HisanagaYukio OgawaTsuyoshi Takemoto
    • Tatsushi MoriShinya YamamotoHiroyuki HayashiShigeru HisanagaYukio OgawaTsuyoshi Takemoto
    • F03C200
    • F04C18/0269F04C2230/10F04C2230/21
    • A performance of a compressor is enhanced and durability of scroll bodies is enhanced by optimizing relief to machining tolerance at a central end part of spiral members for forming the scroll bodies. In a scroll type compressor in which a reinforced portion (for example, a large radius of curvature R) reinforced more than in other root corner portions 5 is provided in a root corner portion 5 at a central end part in which a stress of the two spiral members 10 and 20 is increased, a first relief is formed in a region in which the two spiral members 10 and 20 come into contact with each other where the reinforced portion is applied only to one of the spiral members 10 and 20, and a second relief larger than the first relief is provided in a region in which the two spiral members come into contact with each other at a portion in which the radius of curvature R is provided in both of the two spiral members, thereby reasonably forming reliefs for avoiding interference at the point of contact of two spiral members.
    • 通过在用于形成涡旋体的螺旋构件的中央端部处优化对加工公差的缓解,增强了压缩机的性能并提高了涡旋体的耐久性。 在一种涡旋式压缩机中,其中在另一个根角部分5中增强的加强部分(例如,大的曲率半径R)比在其中的两个拐角部分5处增强的部分设置在根部拐角部分5的中心端部处, 螺旋构件10和20增加,在两个螺旋构件10和20彼此接触的区域中形成第一凸起,其中加强部分仅施加到螺旋构件10和20中的一个,并且 在两个螺旋构件在两个螺旋构件的两个中设置曲率半径R的部分彼此接触的区域中设置大于第一浮雕的第二浮雕,从而合理地形成用于避免 在两个螺旋构件的接触点处的干涉。
    • 12. 发明授权
    • Scroll type compressor
    • 涡旋式压缩机
    • US06193488B1
    • 2001-02-27
    • US09328292
    • 1999-06-09
    • Haruo KamiyaYusuke SakuraiTsuyoshi TakemotoKimihiko Sato
    • Haruo KamiyaYusuke SakuraiTsuyoshi TakemotoKimihiko Sato
    • F01K102
    • F04C18/0269
    • In a scroll type compressor, the center and outer periphery portions of the spiral elements are provided with relief for preventing the mutual contact of the spiral elements. Both of the spiral elements come to contact with each other at the intermediate portion thereof. The relief at the center portion is formed within the range defined by the winding angle Y=32(X−1) where X is the winding turn of each of the spiral elements. The range of the intermediate portion is 380°. This construction serves to prevent the excessive pressure increase of the operation chamber at the center portion so that the brake down of the spiral elements may be prevented without lowering the efficiency of the compressor.
    • 在涡旋式压缩机中,螺旋元件的中心和外周部分设置有用于防止螺旋元件相互接触的浮雕。 两个螺旋元件在其中间部分彼此接触。 在中心部分处的凸起形成在由绕组角度Y = 32(X-1)限定的范围内,其中X是每个螺旋元件的绕组匝数。 中间部分的范围为380°。 这种结构用于防止操作室在中心部分的过度增压,从而可以在不降低压缩机的效率的情况下防止螺旋元件的制动下降。
    • 13. 发明授权
    • Scroll type compressor
    • 涡旋式压缩机
    • US6152713A
    • 2000-11-28
    • US141955
    • 1998-08-28
    • Shigeru HisanagaTsuyoshi TakemotoYoshitaka AkiyamaShinichi WatanabeHiroyuki HayashiYasushi WatanabeTatsushi MoriIzuru ShimizuMasao Iguchi
    • Shigeru HisanagaTsuyoshi TakemotoYoshitaka AkiyamaShinichi WatanabeHiroyuki HayashiYasushi WatanabeTatsushi MoriIzuru ShimizuMasao Iguchi
    • F04C18/02F04C29/02F04C29/12F01C1/02
    • F04C29/12F04C18/0215F04C29/026
    • A scroll type compressor having a front housing, a rear housing, an intermediate outer shell portion arranged between the front and rear housing to form an integral stationary scroll element having a stationary end plate and a stationary spiral member, a movable scroll element having a movable end plate and a movable spiral element and being engaged with the stationary scroll element to define a plurality of compression chambers shifting and reducing in volume to compress refrigerant gas, containing therein an oil component, in response to an orbiting motion of the movable scroll element, a suction port formed in the intermediate outer shell portion to directly introduce the refrigerant gas into the compression chambers, and a discharge chamber in which the refrigerant gas after compression is discharged from the compression chambers. The rear housing having an oil-separating chamber for separating the oil component from the refrigerant gas after compression and an oil-storing chamber for storing therein the separated oil to be supplied to the interior of the front housing via an oil passage formed in the intermediate outer shell to cool and lubricate movable elements and portions of the compressor.
    • 一种涡旋式压缩机,具有前壳体,后壳体,布置在前壳体和后壳体之间的中间外壳部分,以形成具有固定端板和固定螺旋构件的一体式固定涡旋件,具有可移动 端板和可动螺旋元件,并与固定涡旋元件接合以限定多个压缩室,以便响应于可动涡旋元件的轨道运动来移动和减小体积以压缩其中容纳有油分量的制冷剂气体, 形成在中间外壳部分中以将制冷剂气体直接引入压缩室的吸入口,以及压缩后的制冷剂气体从压缩室排出的排出室。 后壳体具有用于在压缩后将油分离器与制冷剂气体分离的油分离室,以及用于在其中储存经由形成在中间体中的油路供给到前壳体的内部的分离油的储油室 外壳以冷却和润滑可移动元件和压缩机的部分。
    • 16. 发明授权
    • Scroll compressor having eccentric shaft lubrication
    • 涡旋压缩机具有偏心轴润滑
    • US5575635A
    • 1996-11-19
    • US404828
    • 1995-03-15
    • Yuuji YamamotoShinichi WatanabeTsuyoshi TakemotoShigeru HisanagaTetsuhiko HukanumaShinya Yamamoto
    • Yuuji YamamotoShinichi WatanabeTsuyoshi TakemotoShigeru HisanagaTetsuhiko HukanumaShinya Yamamoto
    • F04C18/02F04C29/00F04C29/02F04C18/04
    • F04C18/0215F04C29/0057F04C29/02
    • An eccentric shaft 5 is radially slidably inserted in a bore 6a of a bushing 6, which is inserted in an opening 8c-1 of a boss portion 8c of a movable scroll member 8 by way of a radial needle bearing 7. An axial space 24 is confined between a rear end of a bushing 6 and a bottom surface of the opening 8c-1. The space 24 is in communication with the radial bearing 7 via an annular gap 26 between faced surfaces of bushing 6 and the opening 8c-1. A radial space 23 is confined between the inner surface of the bore 6a and the eccentric shaft 5, so that a limited radial movement of the eccentric shaft 5 with respect to the bushing 6 is allowed. A washer 21 for obtaining a fixed axial location of the bushing 6 on the eccentric shaft 5 is formed with recess 21b (first passageway 25) for communicating the radial space 23 with the axial space 24. The bushing 6 is further formed with a radial hole 27 (second passageway) for communicating the radial space 23 with a crank chamber R. A recirculation passageway for the lubricant is thus generated between the crank chamber R, the gaps in the needle bearing 7, the gap 26, the axial chamber 24, the first passageway 25, the radial space 23, the second passageway 27 and the crank chamber R.
    • 偏心轴5径向可滑动地插入衬套6的孔6a中,该衬套6通过径向滚针轴承7插入到可动涡旋件8的凸台部分8c的开口8c-1中。轴向空间24 被限制在衬套6的后端和开口8c-1的底表面之间。 空间24通过衬套6的表面和开口8c-1的相对表面之间的环形间隙26与径向轴承7连通。 径向空间23被限制在孔6a的内表面和偏心轴5之间,从而允许偏心轴5相对于衬套6的有限径向运动。 用于获得衬套6在偏心轴5上的固定轴向位置的垫圈21形成有用于将径向空间23与轴向空间24连通的凹部21b(第一通道25)。衬套6还形成有径向孔 27(第二通道),用于将径向空间23与曲柄室R连通。因此,在曲轴室R,滚针轴承7中的间隙,间隙26,轴向室24之间产生用于润滑剂的再循环通道 第一通道25,径向空间23,第二通道27和曲柄室R.