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    TURBO MACHINE
    1.
    发明申请
    TURBO MACHINE 审中-公开
    涡轮机

    公开(公告)号：US20170009602A1

    公开(公告)日：2017-01-12

    申请号：US15159998

    申请日：2016-05-20

    Applicant: Panasonic Intellectual Property Management Co., Ltd.

    Inventor： KAZUYUKI KOUDA ,  HIDETOSHI TAGUCHI ,  AKIRA HIWATA ,  TAKESHI OGATA ,  TADAYOSHI SHOYAMA ,  HIROSHI HASEGAWA

    IPC: F01D25/16 ,  F01D25/04

    Abstract: A turbo machine of the present disclosure includes a cylindrical bearing housing, a rotation shaft, a bearing, a bearing holder, and an end elastic body. The rotation shaft is located in the bearing housing. The bearing rotatably supports the rotation shaft at least in a radial direction of the rotation shaft. The bearing holder faces one end of the bearing and is fixed to the bearing housing. The end elastic body is disposed between the one end of the bearing and the bearing holder in the axial direction of the bearing and is in contact with the bearing and the bearing holder. The end elastic body is formed of a material having a lower modulus of elasticity than a material forming the bearing holder.

    Abstract translation: 本公开的涡轮机包括圆柱形轴承壳体，旋转轴，轴承，轴承保持器和端部弹性体。 旋转轴位于轴承座中。 轴承至少在旋转轴的径向上可转动地支撑旋转轴。 轴承座面向轴承的一端并固定在轴承座上。 端部弹性体沿轴承的轴向设置在轴承的一端和轴承座之间，并与轴承座和轴承座接触。 端部弹性体由具有比形成轴承座的材料低的弹性模量的材料形成。

    TURBO MACHINE
    2.
    发明申请
    TURBO MACHINE 审中-公开
    涡轮机

    公开(公告)号：US20160177961A1

    公开(公告)日：2016-06-23

    申请号：US14877772

    申请日：2015-10-07

    Applicant: Panasonic Intellectual Property Management Co., Ltd.

    Inventor： TAKESHI OGATA ,  TADAYOSHI SHOYAMA ,  AKIRA HIWATA ,  HIDETOSHI TAGUCHI ,  KAZUYUKI KOUDA ,  HIROSHI HASEGAWA

    IPC: F04D29/056 ,  F04D25/02 ,  F04D29/42 ,  F04D29/051 ,  F04D29/063 ,  F04D29/28 ,  F04D17/12 ,  F04D29/053

    CPC classification number: F04D29/056 ,  F04D17/122 ,  F04D25/02 ,  F04D29/047 ,  F04D29/051 ,  F04D29/053 ,  F04D29/057 ,  F04D29/061 ,  F04D29/063 ,  F04D29/284 ,  F04D29/4206

    Abstract: A turbo machine includes a rotation shaft that comprises a first taper portion and a first cylinder portion, the first taper portion decreasing in diameter toward one end of the rotation shaft, the first cylinder portion being constant in diameter in an axial direction of the rotation shaft; a first impeller that is fixed to the rotation shaft and that is used for compressing or expanding working fluid; a first bearing that rotatably supports the first taper portion and the first cylinder portion; and a second bearing that is positioned on an opposite side of the first impeller from the first bearing in the axial direction of the rotation shaft and that supports the rotation shaft both in the axial direction and a radial direction of the rotation shaft.

    Abstract translation: 涡轮机包括旋转轴，该旋转轴包括第一锥形部和第一圆筒部，第一锥形部朝向旋转轴的一端直径减小，第一圆筒部在旋转轴的轴向上的直径恒定 ; 固定在旋转轴上并用于压缩或膨胀工作流体的第一叶轮; 第一轴承，其可旋转地支撑所述第一锥形部和所述第一圆筒部; 以及第二轴承，其在所述旋转轴的轴向上位于所述第一叶轮的与所述第一轴承相反的一侧上，并且在所述旋转轴的轴向和径向方向上支撑所述旋转轴。

    TURBO MACHINE
    5.
    发明申请
    TURBO MACHINE 审中-公开
    涡轮机

    公开(公告)号：US20170016452A1

    公开(公告)日：2017-01-19

    申请号：US15177298

    申请日：2016-06-08

    Applicant: Panasonic Intellectual Property Management Co., Ltd.

    Inventor： TADAYOSHI SHOYAMA ,  TAKESHI OGATA ,  HIDETOSHI TAGUCHI

    IPC: F04D29/056 ,  F04D29/053 ,  F04D29/063 ,  F04D29/28

    CPC classification number: F04D29/056 ,  F04D17/10 ,  F04D29/0473 ,  F04D29/053 ,  F04D29/057 ,  F04D29/063 ,  F04D29/284 ,  F05D2240/52 ,  F05D2240/53 ,  F05D2240/61 ,  F05D2240/63

    Abstract: A turbo machine according to the present disclosure includes a rotating shaft, an impeller, a first bearing, and a first supply passage. The rotating shaft includes a first taper portion and a first cylindrical portion. The first bearing includes a first taper support surface and a first cylindrical portion support surface, the first taper support surface including a first taper hole forming surface and rotatably supporting the first taper portion, the first cylindrical portion support surface rotatably supporting the first cylindrical portion. The first supply passage is open to a space formed between the first cylindrical portion and first cylindrical portion support surface. An inclination angle of the first taper hole forming surface with respect to the axial direction of the first bearing is greater than an inclination angle of an outer surface of the first taper portion with respect to the axial direction of the rotating shaft.

    Abstract translation: 根据本公开的涡轮机包括旋转轴，叶轮，第一轴承和第一供应通道。 旋转轴包括第一锥形部分和第一圆柱形部分。 所述第一轴承包括第一锥形支撑表面和第一圆柱形部分支撑表面，所述第一锥形支撑表面包括第一锥形孔形成表面，并且可旋转地支撑所述第一锥形部分，所述第一圆柱形部分支撑表面可旋转地支撑所述第一圆柱形部分。 第一供应通道对形成在第一圆柱形部分和第一圆柱形部分支撑表面之间的空间开放。 第一锥形孔形成面相对于第一轴承的轴向的倾斜角度大于第一锥形部的外表面相对于旋转轴的轴向的倾斜角度。

    TURBO MACHINE AND REFRIGERATING CYCLE APPARATUS
    7.
    发明申请
    TURBO MACHINE AND REFRIGERATING CYCLE APPARATUS 审中-公开
    涡轮机和制冷循环装置

    公开(公告)号：US20170002824A1

    公开(公告)日：2017-01-05

    申请号：US15139204

    申请日：2016-04-26

    Applicant: Panasonic Intellectual Property Management Co., Ltd.

    Inventor： AKIRA HIWATA ,  KAZUYUKI KOUDA ,  MAMORU NISHIBU ,  TADAYOSHI SHOYAMA ,  TAKESHI OGATA ,  HIDETOSHI TAGUCHI

    IPC: F04D29/063 ,  F25B1/053 ,  F04D29/046

    Abstract: A turbo machine of the present disclosure includes a rotation shaft, a first bearing, a casing, an impeller, a first space, a second space, a storage tank, a first outlet passage, a supply passage, a pump, a main passage, and a sub-passage. The second space is in communication with a space formed between a bearing surface of the first bearing and an outer surface of the rotation shaft. The main passage is in communication with the second space and extends in the rotation shaft from an end of the rotation shaft in an axial direction of the rotation shaft. The sub-passage is formed in the rotation shaft and allows communication between the space between the bearing surface of the first bearing and the outer surface of the rotation shaft and the main passage.

    Abstract translation: 本公开的涡轮机包括旋转轴，第一轴承，壳体，叶轮，第一空间，第二空间，储存箱，第一出口通道，供给通道，泵，主通道， 和一个分段。 第二空间与形成在第一轴承的支承表面和旋转轴的外表面之间的空间连通。 主通道与第二空间连通，并且在旋转轴的旋转轴的轴线方向上从旋转轴的端部延伸。 副通道形成在旋转轴中，并且允许第一轴承的支承表面与旋转轴的外表面之间的空间与主通道之间的连通。

    TURBOMACHINE AND REFRIGERATION CYCLE APPARATUS
    8.
    发明申请
    TURBOMACHINE AND REFRIGERATION CYCLE APPARATUS 审中-公开
    涡轮机和制冷循环装置

    公开(公告)号：US20150300697A1

    公开(公告)日：2015-10-22

    申请号：US14680442

    申请日：2015-04-07

    Applicant: Panasonic Intellectual Property Management Co., Ltd.

    Inventor： MAMORU NISHIBU ,  HIDETOSHI TAGUCHI ,  AKIRA HIWATA ,  TADAYOSHI SHOYAMA ,  KAZUYUKI KOUDA

    IPC: F25B11/00 ,  F04D29/056 ,  F04D29/063 ,  F04D29/053

    CPC classification number: F25B11/00 ,  F04D29/04 ,  F04D29/047 ,  F04D29/053 ,  F04D29/056 ,  F04D29/063 ,  F16C33/1055 ,  F25B1/047 ,  F25B1/06 ,  F25B11/04 ,  F25B31/002

    Abstract: A turbomachine for a refrigeration cycle apparatus that uses a refrigerant whose saturated vapor pressure is a negative pressure at ordinary temperature includes a rotation shaft and a bearing for supporting the rotation shaft. The rotation shaft includes a lubricant supply passage for supplying the refrigerant as a lubricant that travels smoothly between the rotation shaft and the bearing. The lubricant supply passage includes a main passage and a sub-passage. The main passage extends from an inlet located at an end of the rotation shaft in an axial direction of the rotation shaft. The sub-passage diverges from the main passage and extends to an outlet located in a side surface of the rotation shaft.

    Abstract translation: 使用饱和蒸汽压为常压下的负压的制冷剂的制冷循环装置的涡轮机包括旋转轴和用于支撑旋转轴的轴承。 旋转轴包括润滑剂供给通道，用于供应制冷剂作为在旋转轴和轴承之间平稳行进的润滑剂。 润滑剂供给通道包括主通道和副通道。 主通道从位于旋转轴的端部处的入口沿着旋转轴的轴向延伸。 副通道从主通道分叉并延伸到位于旋转轴的侧表面中的出口。

    TURBOMACHINE
    9.
    发明申请
    TURBOMACHINE 有权
    涡轮机

    公开(公告)号：US20150300193A1

    公开(公告)日：2015-10-22

    申请号：US14680044

    申请日：2015-04-06

    Applicant: Panasonic Intellectual Property Management Co., Ltd.

    Inventor： TADAYOSHI SHOYAMA

    IPC: F01D11/00 ,  F01D5/12

    CPC classification number: F01D25/16 ,  F01D5/12 ,  F01D11/005 ,  F04D17/122 ,  F04D29/057

    Abstract: A turbomachine of this disclosure includes a rotation shaft, a first impeller, a first bearing, and a second bearing. The first impeller is fixed to the rotation shaft and includes a low-pressure-side surface. The first bearing is adjacent to the low-pressure-side surface of the first impeller and supports the rotation shaft. The second bearing is disposed on an opposite side of the first impeller from the first bearing and supports the rotation shaft. The rotation shaft includes a first tapered portion gradually increasing in diameter toward the first impeller. The first bearing includes a first support surface supporting the first tapered portion.

    Abstract translation: 本公开的涡轮机包括旋转轴，第一叶轮，第一轴承和第二轴承。 第一叶轮固定在旋转轴上并且包括低压侧表面。 第一轴承邻近第一叶轮的低压侧表面并且支撑旋转轴。 第二轴承设置在第一叶轮的与第一轴承相反的一侧上并且支撑旋转轴。 旋转轴包括朝向第一叶轮直径逐渐增大的第一锥形部。 第一轴承包括支撑第一锥形部分的第一支撑表面。

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