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    • 43. 发明授权
    • Auto-tensioner
    • 自动张紧器
    • US6102820A
    • 2000-08-15
    • US116940
    • 1998-07-17
    • Hiroaki ImaharuHajime NakayamaHiromichi Suzuki
    • Hiroaki ImaharuHajime NakayamaHiromichi Suzuki
    • F16H7/08F16H7/12
    • F16H7/1218F16H2007/081F16H2007/0893
    • An auto-tensioner that inhibits the generation of heat in an insert bearing made of a synthetic resin. An outer shell of an arm member is swingably supported on an inner shaft of a base member through an insert bearing made of a synthetic resin, and a tension pulley carried at a tip end of the arm member, is brought into pressure contact with an endless belt by biasing the arm member with a spring. By subjecting an inner surface of the outer shell in sliding contact with an outer peripheral surface of the insert bearing, to shot peening prior to assembly, the arithmetically averaged roughness Ra and the maximum height Ry of inner peripheral surface are regulated into ranges of1.times.10.sup.-6 m.ltoreq.Ra.ltoreq.10.times.10.sup.-6 mRy.ltoreq.60.times.10.sup.-6 m.
    • 一种自动张紧器,其抑制在由合成树脂制成的插入轴承中产生热量。 臂构件的外壳通过由合成树脂制成的插入轴承可摆动地支撑在基座构件的内轴上,并且承载在臂构件的顶端的张紧轮与环形件 带通过用弹簧偏压臂构件。 通过使外壳的内表面与插入轴承的外周面滑动接触,在组装之前进行喷丸硬化,将内周面的算术平均粗糙度Ra和最大高度Ry调节为1×10 -3 6μmRa = 10x10 -6 m Ry = 60×10 -6 m。
    • 46. 发明授权
    • Air-fuel mixture flow control structure and method of making the same
    • 空燃混合流量控制结构及其制作方法
    • US4672940A
    • 1987-06-16
    • US845632
    • 1986-03-28
    • Hajime NakayamaOsamu AokiShigetoshi NishijimaHaruo HoriuchiTakuya SuginoShuichi Takagi
    • Hajime NakayamaOsamu AokiShigetoshi NishijimaHaruo HoriuchiTakuya SuginoShuichi Takagi
    • F02M29/04F02M29/00
    • F02M29/04
    • A flow control honeycomb structure for use in an intake passage of an engine for producing turbulent flow in an air-fuel mixture flowing through the intake passage, which structure includes a short cylindrical peripheral wall defining therein a circular passage having a substantially circular cross section, a plurality of substantially crisscross partitions joined to and disposed in the peripheral wall and dividing the circular passage into a first group of square passageways each having a substantially square cross section and a second group of four triangular passageways each having a substantially triangular cross section and a relatively large cross-sectional area, and a plurality of ribs extending obliquely from joints of those of the passageways which define the triangular passageways radially outwardly to the peripheral wall through the triangular passageways to divide each of the triangular passageways into a plurality of subpassageways of substantially the same cross-sectional area as the square passages. The square and triangular passageways are progressively narrower downstream in the direction in which the air-fuel mixture flow through the intake passage. A method of making the flow control honeycomb structure molding without producing burrs and ridges in any portion of the final honeycomb structure is also disclosed.
    • 一种流量控制蜂窝结构,其用于在流过所述进气通道的空气燃料混合物中产生湍流的发动机的进气通道,该结构包括限定有具有大致圆形横截面的圆形通道的短圆柱形周壁, 多个基本上十字形的分隔件,其连接并设置在周壁上并将圆形通道分成第一组正方形通道,每个通道具有基本正方形的横截面,第二组四个三角形通道各自具有基本上三角形的横截面, 相当大的横截面面积,以及从通道中的那些通道的接头倾斜延伸的多个肋,这些肋通过三角形通道径向向外限定到周壁,以将每个三角形通道分成几个基本上 相同的横截面 区域作为正方形通道。 正方形和三角形通道在空气 - 燃料混合物流过进气通道的方向上在下游逐渐变窄。 还公开了在最终蜂窝结构体的任何部分中不产生毛刺和脊的流动控制蜂窝结构模制的方法。