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    • 2. 发明授权
    • Turbocharger
    • 涡轮增压器
    • US5993173A
    • 1999-11-30
    • US806942
    • 1997-02-26
    • Takaaki KoikeYukio Takahashi
    • Takaaki KoikeYukio Takahashi
    • F01D25/16F16C33/08F02B39/00
    • F01D25/166F16C17/18F16C33/106F05D2220/40F16C2360/24
    • A turbocharger includes a main housing (1) for housing a turbine rotor (2) and a compressor impeller (4). An independent bearing box (23) is provided in the main housing (1). The main housing (1) is comprised of a turbine housing (3) and a compressor housing (5). A rotating shaft (7) connecting the turbine rotor (2) with the compressor impeller (4) is supported by a semi-float metal bearing (24) placed in the bearing box (23). An oil passage (26) is formed in the main housing (1) for feeding an oil to inside and outside of the semi-float metal bearing (24) in the bearing box (23). Oil grooves (37) are formed in end faces of the metal bearing (24) and another grooves (34) are formed at end faces of the bearing box (23) for discharging the oil from the semi-float metal bearing (24). Oil flow in the turbocharger housing (1) is controlled by the oil grooves (34, 37).
    • 涡轮增压器包括用于容纳涡轮机转子(2)的主壳体(1)和压缩机叶轮(4)。 在主壳体(1)中设置独立的轴承箱(23)。 主壳体(1)包括涡轮壳体(3)和压缩机壳体(5)。 将涡轮转子(2)和压缩机叶轮(4)连接的旋转轴(7)由放置在轴承箱(23)中的半浮子金属轴承(24)支撑。 在主壳体(1)中形成油通道(26),用于向轴承箱(23)中的半浮子金属轴承(24)的内部和外部供给油。 油槽(37)形成在金属轴承(24)的端面,另一个槽(34)形成在用于从半浮子金属轴承(24)排出油的轴承箱(23)的端面。 涡轮增压器壳体(1)中的油流由油槽(34,37)控制。
    • 3. 发明授权
    • Thrust bearing arrangement for turbocharger
    • 用于涡轮增压器的推力轴承装置
    • US6126414A
    • 2000-10-03
    • US81383
    • 1998-05-19
    • Takaaki Koike
    • Takaaki Koike
    • F02B39/14F01D25/16F02C6/12F04B17/00
    • F16C17/04F01D25/168F02C6/12F05D2220/40F16C2360/24
    • A thrust bearing arrangement for a turbocharger including a thrust bearing unit having separate normal and reverse thrust bearings, and a thrust member provided on a turbine shaft and interposed between the normal and reverse thrust bearings. Both the normal and reverse thrust bearings are spaced from the turbine shaft in a radial direction of the turbine shaft and a lubrication oil is supplied to a first contact area between the normal thrust bearing and the thrust member. An oil guide portion is formed on a bearing housing for further supplying the lubrication oil to a second contact area between the thrust member and the reverse thrust bearing. A seal member is provided on the turbine shaft in slidable contact with an inner peripheral face of the normal thrust bearing.
    • 一种用于涡轮增压器的推力轴承装置,其包括具有单独的正向和反向推力轴承的推力轴承单元,以及设置在涡轮轴上并插入在正向和反向推力轴承之间的推力构件。 正反推力轴承与涡轮轴在涡轮轴的径向方向上间隔开,并且润滑油被供应到正推力轴承和推力构件之间的第一接触区域。 导油部分形成在轴承壳体上,用于将润滑油进一步供给到推力构件和反推力轴承之间的第二接触区域。 密封构件设置在涡轮机轴上,与正常推力轴承的内周面可滑动接触。
    • 4. 发明申请
    • BINDER COMPOSITION FOR NON-AQUEOUS SECONDARY BATTERY ELECTRODE
    • 非水性二次电池电极的组合物
    • US20120095131A1
    • 2012-04-19
    • US13138807
    • 2010-04-02
    • Sachiko KinoshitaHiromi YokoyamaTakaaki KoikeKoichiro MiyajimaYasuyuki MoroishiShingo Ikeda
    • Sachiko KinoshitaHiromi YokoyamaTakaaki KoikeKoichiro MiyajimaYasuyuki MoroishiShingo Ikeda
    • C08L33/14C08L33/06C08L33/26C08L43/04C08L43/02
    • H01M4/622H01G11/38H01M4/13H01M4/621H01M10/052H01M10/0525H01M2220/30Y02E60/13
    • Disclosed is a binder composition for a non-aqueous secondary battery electrode, which enables the production of a non-aqueous secondary battery that has excellent adhesion to a current collector or an electrode and can retain a high electric discharge capacity even when charge and discharge are repeated or under a high-temperature environment produced as a result of the generation of heat. Specifically disclosed is a binder composition for a non-aqueous secondary battery electrode, which comprises functional group-containing crosslinked resin microparticles produced by polymerizing the following components (A) to (C): (A) at least one monomer selected from the group consisting of (a) a monomer having one ethylenically unsaturated group per molecule and also having a monofunctional or polyfunctional epoxy group, (b) a monomer having one ethylenically unsaturated group per molecule and also having a monofunctional or polyfunctional amide group, and (c) a monomer having one ethylenically unsaturated group per molecule and also having a monofunctional or polyfunctional hydroxy group; (B) at least one monomer selected from the group consisting of (d) a monomer having one ethylenically unsaturated group per molecule and also having an alkoxysilyl group and (e) a monomer having at least two ethylenically unsaturated groups per molecule; and (C) (k) a monomer which has an ethylenically unsaturated group and is different from the monomers (a) to (e).
    • 公开了一种非水二次电池用电极用粘合剂组合物,其能够制造对集电体或电极具有优异的粘合性的非水系二次电池,并且即使在充放电为 重复或在由于产生热量而产生的高温环境下。 具体公开了一种非水二次电池用电极用粘合剂组合物,其含有通过使以下成分(A)〜(C)聚合而制造的含官能团的交联树脂微粒:(A)至少一种选自 (a)每分子具有一个烯键式不饱和基团并且还具有单官能或多官能环氧基团的单体,(b)每分子具有一个烯键式不饱和基团并且还具有单官能或多官能酰胺基团的单体,和(c) 每分子具有一个烯属不饱和基团并且还具有单官能或多官能羟基的单体; (B)选自(d)每分子具有一个烯键式不饱和基团并且还具有烷氧基甲硅烷基的单体的至少一种单体和(e)每分子具有至少两个烯属不饱和基团的单体; 和(C)(k)具有烯属不饱和基团且不同于单体(a)至(e)的单体。
    • 5. 发明授权
    • Turbine housing of turbocharger
    • 涡轮增压器涡轮机外壳
    • US4693668A
    • 1987-09-15
    • US865358
    • 1986-05-21
    • Takaaki Koike
    • Takaaki Koike
    • F02B39/00F01D9/02F28F7/00
    • F01D9/026
    • Mated engaging grooves are formed at opposing surfaces of sections into which a turbine housing main body is divided with respect to the axial direction of a turbine. A partition wall is fitted in the mated engaging grooves, leaving a clearance in the radial direction. The end of the partition wall on the side of the gas inlet of the turbine housing main body is made into contact with the side surface or surfaces of a partition wall supporting member disposed at the gas inlet such that the partition wall supporting member is in coplanar relationship with a flange surface of the turbine housing main body, whereby thermal deformations in the direction of the gas flow at the gas inlet of the partition wall are permitted and the gas-tightness is ensured at the gas inlet of the turbine housing.
    • 配合的接合槽形成在相对于涡轮机的轴向方向被分开的部分的相对表面处。 分隔壁装配在配合的接合槽中,在径向上留有间隙。 涡轮壳体主体的气体入口侧的分隔壁的端部与设置在气体入口处的分隔壁支撑构件的侧表面或表面接触,使得隔壁支撑构件处于共面 与涡轮壳体主体的凸缘表面的关系,由此允许在分隔壁的气体入口处的气体流动方向上的热变形,并且在涡轮壳体的气体入口处确保气密性。