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    • 2. 发明授权
    • Scroll type compressor
    • 涡旋式压缩机
    • US6053715A
    • 2000-04-25
    • US164533
    • 1998-09-30
    • Hideo HiranoHiroyuki KawanoHideto OkaMasahiro Tsubokawa
    • Hideo HiranoHiroyuki KawanoHideto OkaMasahiro Tsubokawa
    • F04C18/02F04C29/00F01C1/02
    • F04C29/0014F04C18/0215
    • An orbiting scroll is engaged to and moved orbitally in relation to a fixed scroll at variable speeds. An offset surface is provided in at least one of the wraps of the fixed scroll and/or the orbiting scroll, by which a space S is created in one of the compression chambers formed between the fixed scroll and the orbiting scroll, which is thereby unsealed and opened to the inlet port side. The offset surface has a length from a position in the spiral length which satisfies the required compression ratio of one of the compression chambers in a low speed operation to the end of the spiral. An injection port is positioned such as to open to an unsealed area of this compression chamber, and gas injection shutoff and resumption is controlled through this injection port as appropriate to the situation.
    • 相对于可变速度的固定涡旋盘,绕动涡旋件接合并轨道运动。 在固定涡旋件和/或绕动涡旋件的至少一个涡卷上设置有偏移面,在形成在固定涡旋盘和绕动涡旋件之间的压缩室之间形成有空间S,由此被开封 并通向入口侧。 偏移面具有从螺旋长度的位置的长度,该长度满足在低速操作中的一个压缩室与螺旋的末端所需的压缩比。 喷射口被定位成打开到该压缩室的未密封区域,并且根据情况通过该喷射口来控制气体注入关闭和恢复。
    • 8. 发明授权
    • Method of nondestructive insulation test and a nondestructive insulation
testing apparatus
    • 非破坏性绝缘试验方法和无损绝缘试验装置
    • US5867029A
    • 1999-02-02
    • US691236
    • 1996-08-02
    • Yasuo IijimaMasahiro Tsubokawa
    • Yasuo IijimaMasahiro Tsubokawa
    • G01R31/02G01R31/06G01R31/12
    • G01R31/346G01R31/024
    • A method of nondestructive insulation testing is disclosed which comprises the steps of: (a) placing an electric device, having a core and at least one winding provided on the core, in a reduced atmospheric pressure; (b) insulating the laminated core from the ground; (c) supplying a voltage signal having a first surge waveform to the winding; and detecting a glow discharge which may result from step (c) to detect an insulation condition of the winding, wherein the reduced atmospheric pressure ranges from 65 to 75 Torr and the voltage signal is applied in the first direction of the winding and then, is applied in the second, opposite, direction of the winding. This method may further comprise steps of: (d) supplying a second voltage signal having a second predetermined surge waveform having a peak voltage lower than a peak voltage of the predetermined surge waveform; (e) outputting a second output signal between the winding indicative of a second insulation condition of the winding in response to step (d); (f) measuring intervals corresponding to the wavelengths of the output signal and the second output signal respectively; and (g) judging the insulation condition by comparing the measured intervals to each other. A nondestructive insulation testing apparatus is also disclosed.
    • 公开了一种非破坏性绝缘测试方法,其包括以下步骤:(a)在降低的大气压下放置具有芯体和至少一个设置在芯体上的绕组的电气设备; (b)将层压铁芯与地面绝缘; (c)向绕组提供具有第一浪涌波形的电压信号; 以及检测步骤(c)可能产生的辉光放电以检测绕组的绝缘条件,其中降低的大气压力范围为65至75Torr,并且电压信号沿绕组的第一方向施加,然后是 施加在绕组的第二个相对的方向上。 该方法还可以包括以下步骤:(d)提供具有峰值电压低于预定浪涌波形的峰值电压的第二预定浪涌波形的第二电压信号; (e)响应于步骤(d),在所述绕组之间输出指示所述绕组的第二绝缘条件的第二输出信号; (f)分别测量对应于输出信号和第二输出信号的波长的间隔; 和(g)通过将测量的间隔彼此进行比较来判断绝缘条件。 还公开了一种非破坏性绝缘测试装置。
    • 9. 发明授权
    • Scroll compressor having a back pressure partitioning member
    • 具有背压分隔构件的涡旋压缩机
    • US5848883A
    • 1998-12-15
    • US804844
    • 1997-02-24
    • Masahiro Tsubokawa
    • Masahiro Tsubokawa
    • F04C18/02F04C27/00F04C18/04
    • F04C27/005
    • A scroll compressor is designed to exert a stable pressure on the rear surface of the rotary scroll without causing excessive pressure rise or pressure gradient by the lubricating oil which flows out from a back pressure partitioning member in a very little gap of an axial supporting portion. A bearing member 18 has an inner portion extending radially inwardly from annular groove 22 and an outer portion extending radially outwardly from the annular groove 22 to an inner edge of an axial supporting portion 24. The inner and outer portions of the bearing member 18 are formed in a bottom portion of the bearing member 18 and have a difference in level d relative to a bottom surface of the axial supporting portion 24.
    • 涡旋压缩机被设计成在旋转涡旋盘的后表面上施加稳定的压力,而不会由在轴向支撑部分的非常小的间隙中从背压分隔构件流出的润滑油引起过大的压力升高或压力梯度。 轴承构件18具有从环形槽22径向向内延伸的内部部分和从环形槽22径向向外延伸到轴向支撑部分24的内边缘的外部部分。轴承构件18的内部和外部部分形成 在轴承部件18的底部,并且具有相对于轴向支撑部分24的底面的液面d的差异。