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    • 1. 发明授权
    • Flywheel assembly
    • 飞轮总成
    • US07438166B2
    • 2008-10-21
    • US11373236
    • 2006-03-13
    • Hiroyoshi TsurutaHiroshi UeharaKozo Yamamoto
    • Hiroyoshi TsurutaHiroshi UeharaKozo Yamamoto
    • F16D13/68
    • F16F15/139Y10T74/2131
    • A flywheel assembly that receives torque from a crankshaft of an engine includes a flywheel, a damper mechanism, and a frictional resistance generation mechanism. The damper mechanism elastically connects the flywheel to the crankshaft in a rotational direction. The damper mechanism includes an input member, an output member, elastic members to connect elastically the input member and the output member in the rotational direction. The frictional resistance generation mechanism is located functionally in parallel with the damper mechanism in the rotational direction. The frictional resistance generation mechanism utilizes a portion of the flywheel as a friction surface.
    • 从发动机的曲轴接收扭矩的飞轮组件包括飞轮,阻尼机构和摩擦阻力产生机构。 阻尼器机构沿旋转方向将飞轮弹性地连接到曲轴。 阻尼机构包括输入构件,输出构件,用于沿旋转方向弹性地连接输入构件和输出构件的弹性构件。 摩擦阻力发生机构在功能上与减震机构沿旋转方向平行。 摩擦阻力产生机构利用飞轮的一部分作为摩擦面。
    • 2. 发明申请
    • Flexible flywheel
    • 柔性飞轮
    • US20070099710A1
    • 2007-05-03
    • US10571894
    • 2004-09-07
    • Kozo YamamotoHiroyoshi TsurutaHiroshi Uehara
    • Kozo YamamotoHiroyoshi TsurutaHiroshi Uehara
    • F16F15/121
    • F16F15/1315F16F15/13107
    • A flexible flywheel is a member to which torque is input from a crankshaft 91 of the engine and includes a first flywheel 2 and a damper mechanism 4. The first flywheel 2 includes an inertia member 13, and a flexible plate 11 for connecting the inertia member 13 with the crankshaft 91. The flexible plate is flexibly deformable in the bending direction. The damper mechanism 4 includes an input-side disc-like plate 20 to which torque is input from the crankshaft 91, output plates 32 and 33 located rotatable relative to the input-side disc-like plate 20, and coil springs 34, 35, and 36 to be compressed in the rotational direction when both the plates rotate relative to each other. The first flywheel 2 can move relative to the damper mechanism 4 in the bending direction with a limited range.
    • 柔性飞轮是从发动机的曲轴91输入扭矩的构件,其包括第一飞轮2和减震机构4.第一飞轮2包括惯性构件13和用于将惯性构件 柔性板在弯曲方向上可挠曲地变形。 阻尼机构4包括输入侧盘状板20,从曲轴91输入转矩,相对于输入侧盘状板20可旋转的输出板32,33,以及螺旋弹簧34,35, 并且当两个板相对于彼此旋转时,在旋转方向上被压缩。 第一飞轮2可以在有限的范围内相对于阻尼机构4在弯曲方向上移动。
    • 4. 发明授权
    • Dual-mass flywheel
    • 双质量飞轮
    • US07445552B2
    • 2008-11-04
    • US10897030
    • 2004-07-23
    • Kozo YamamotoHiroyoshi Tsuruta
    • Kozo YamamotoHiroyoshi Tsuruta
    • F16F15/121F16D13/68
    • F16C19/46F16C33/605F16C33/76F16C33/7809F16C2361/55F16F15/13171
    • A flywheel assembly with an improved bearing structure is provided. The flywheel damper (11) is a flywheel assembly for transmitting torque from the crankshaft of an engine, and has a first flywheel assembly (4), a second flywheel assembly (5), a damper mechanism (6), and a needle bearing (43). The first flywheel assembly (4) is fixed to the crankshaft (2). The second flywheel assembly (5) is disposed so as to be able to rotate relative to the first flywheel assembly (4). The damper mechanism (6) elastically connects the second flywheel assembly (5) to the crankshaft (2) in the rotation direction. The needle bearing (43) is a bearing to support rotatably the second flywheel assembly (5) on the crankshaft (2), and has a plurality of needles (44) disposed between the peripheral surfaces (21d) and (37b) of both members.
    • 提供了具有改进的轴承结构的飞轮组件。 飞轮阻尼器(11)是用于从发动机的曲轴传递扭矩的飞轮组件,并且具有第一飞轮组件(4),第二飞轮组件(5),阻尼机构(6)和滚针轴承 43)。 第一飞轮组件(4)固定在曲轴(2)上。 第二飞轮组件(5)被布置成能够相对于第一飞轮组件(4)旋转。 阻尼器机构(6)沿着旋转方向将第二飞轮组件(5)弹性地连接到曲轴(2)。 滚针轴承(43)是用于将第二飞轮组件(5)可旋转地支撑在曲轴(2)上的轴承,并且具有设置在外周表面(21d)和(37b)之间的多个针(44) 两个成员。
    • 5. 发明申请
    • Dual-mass flywheel
    • 双质量飞轮
    • US20050037848A1
    • 2005-02-17
    • US10897030
    • 2004-07-23
    • Kozo YamamotoHiroyoshi Tsuruta
    • Kozo YamamotoHiroyoshi Tsuruta
    • F16C33/78F16C19/46F16C33/60F16C33/66F16C33/76F16C35/07F16D7/00F16F15/131F16F15/30
    • F16C19/46F16C33/605F16C33/76F16C33/7809F16C2361/55F16F15/13171
    • A flywheel assembly with an improved bearing structure is provided. The flywheel damper (11) is a flywheel assembly for transmitting torque from the crankshaft of an engine, and has a first flywheel assembly (4), a second flywheel assembly (5), a damper mechanism (6), and a needle bearing (43). The first flywheel assembly (4) is fixed to the crankshaft (2). The second flywheel assembly (5) is disposed so as to be able to rotate relative to the first flywheel assembly (4). The damper mechanism (6) elastically connects the second flywheel assembly (5) to the crankshaft (2) in the rotation direction. The needle bearing (43) is a bearing to support rotatably the second flywheel assembly (5) on the crankshaft (2), and has a plurality of needles (44) disposed between the peripheral surfaces (21d) and (37b) of both members.
    • 提供了具有改进的轴承结构的飞轮组件。 飞轮阻尼器(11)是用于从发动机的曲轴传递扭矩的飞轮组件,并且具有第一飞轮组件(4),第二飞轮组件(5),阻尼机构(6)和滚针轴承 43)。 第一飞轮组件(4)固定在曲轴(2)上。 第二飞轮组件(5)被布置成能够相对于第一飞轮组件(4)旋转。 阻尼器机构(6)沿着旋转方向将第二飞轮组件(5)弹性地连接到曲轴(2)。 滚针轴承(43)是用于将第二飞轮组件(5)可旋转地支撑在曲轴(2)上的轴承,并且具有设置在两个构件的周边表面(21d)和(37b)之间的多个针(44) 。
    • 6. 发明授权
    • Damper mechanism and damper disk assembly
    • 减震器机构和阻尼盘组件
    • US07172509B2
    • 2007-02-06
    • US10787171
    • 2004-02-27
    • Kozo YamamotoHiroshi Uehara
    • Kozo YamamotoHiroshi Uehara
    • F16F15/121
    • F16F15/12366F16H45/02F16H2045/0226
    • A damper mechanism or a damper disk assembly realizing a low rigidity using a pair of elastic members is provided to achieve a further low rigidity in a region with small torques. The damper mechanism has a drive member 52, a driven member 53, a pair of first torsion springs 58A and 58B, and a second torsion spring 59. The springs 58A and 58B are functionally provided in series with each other in a rotational direction. The spring 59 is functionally provided in parallel with the springs 58A and 58B in such a way that the spring 59 is compressed in the rotational direction after the springs 58A and 58B are compressed to a certain angle when the drive member 52 and the driven member 53 rotate relative to each other.
    • 提供使用一对弹性构件实现低刚性的阻尼器机构或阻尼盘组件,以在具有小扭矩的区域中实现更低的刚性。 阻尼机构具有驱动构件52,从动构件53,一对第一扭转弹簧58A和58B以及第二扭转弹簧59。 弹簧58A和58B在旋转方向上在功能上彼此串联设置。 弹簧59在功能上与弹簧58A和58B平行地设置,使得当驱动构件52和58被弹簧58A和58B压缩到一定角度时,弹簧59沿旋转方向被压缩 从动构件53相对于彼此旋转。
    • 7. 发明授权
    • Flywheel assembly
    • 飞轮总成
    • US08568243B2
    • 2013-10-29
    • US13059017
    • 2009-08-06
    • Kozo YamamotoKeisuke FujiokaTomoki Hada
    • Kozo YamamotoKeisuke FujiokaTomoki Hada
    • F16D3/14
    • F16F15/1343F16F15/13469
    • A first flywheel assembly a first flywheel, a second flywheel, a first spring set, a first spring seat, and a second spring set. The first spring set is arranged between the first flywheel and the second flywheel in a pre-compressed state. The first spring seat is a member that supports an end portion of the first spring set and is pushed in a radially outward direction against the first flywheel. The second spring set is a member having a lower stiffness than a stiffness of the first spring set and is arranged between the second flywheel and the first spring set in a pre-compressed state such that it acts in series with the first spring set.
    • 第一飞轮组件,第一飞轮,第二飞轮,第一弹簧组,第一弹簧座和第二弹簧组。 第一弹簧组以预压缩状态布置在第一飞轮和第二飞轮之间。 第一弹簧座是支撑第一弹簧组件的端部并且朝向第一飞轮沿径向向外的方向推动的构件。 第二弹簧组是具有比第一弹簧组的刚度低的刚度的构件,并且以预压缩状态布置在第二飞轮和第一弹簧组之间,使得其与第一弹簧组串联起来。
    • 8. 发明授权
    • Damper mechanism
    • 阻尼机制
    • US06488139B1
    • 2002-12-03
    • US09273540
    • 1999-03-22
    • Kozo Yamamoto
    • Kozo Yamamoto
    • F16D4702
    • F16F15/1238
    • An input rotary member 2 and an output rotary member 3 are circumferentially and elastically coupled together via first and second damper mechanisms 4 and 5 arranged in parallel. The first damper mechanism 4 includes first springs 8. The first springs 8 are arranged between the input and output rotary members 2 and 3 for transmitting torque therebetween. Compression of the first springs 8 does not start before a torsion angle reaches a first torsion angle 1. The second damper mechanism 5 includes second springs 13 and a high hysteresis torque generating mechanism 15 arranged in series. The second springs 13 can be compressed only within a range of a torsion angle &thgr;AC smaller than the first torsion angle &thgr;1.
    • 输入旋转构件2和输出旋转构件3通过平行布置的第一和第二阻尼器机构4和5周向地弹性地联接在一起。 第一阻尼机构4包括第一弹簧8.第一弹簧8布置在输入和输出旋转构件2和3之间,用于在它们之间传递扭矩。 第一弹簧8的压缩在扭转角达到第一扭转角1之前不开始。第二阻尼机构5包括串联布置的第二弹簧13和高滞后扭矩产生机构15。 第二弹簧13只能在小于第一扭转角θ1的扭转角度θAC的范围内被压缩。
    • 9. 发明授权
    • Flywheel assembly
    • 飞轮总成
    • US6044727A
    • 2000-04-04
    • US120323
    • 1998-07-22
    • Kozo Yamamoto
    • Kozo Yamamoto
    • F16F15/12F16D13/70F16F15/131F16F15/134F16F15/139F16F15/16F16F15/30G05G1/00F16F15/10F16D13/68
    • F16F15/13142F16D13/70F16F15/13107
    • A flywheel assembly is provided for transmitting torque from a crankshaft 2 to a main drive shaft 3. The flywheel assembly 1 basically includes a first flywheel 4, a second flywheel 5, a damper mechanism 6, a bearing 17 and a flexible plate 41. The flywheel assembly is designed to suppress the transmission of bending vibrations to the second flywheels. The second flywheel 5 is disposed adjacent to a side of the first flywheel 4 which is remote from the crankshaft 2. The damper mechanism 6 elastically couples the first and second flywheels 4 and 5 together in the circumferential direction. The flexible plate 41 is arranged axially between the first and second flywheels 4 and 5 for supporting the second flywheel 5 with respect to the first flywheel 4. The flexible plate 41 is flexible in the bending direction. The bearing 17 is arranged between the flexible plate 41 and one of the first and second flywheels 4 and 5.
    • 飞轮组件提供用于将扭矩从曲轴2传递到主驱动轴3.飞轮组件1基本上包括第一飞轮4,第二飞轮5,阻尼机构6,轴承17和柔性板41。 飞轮组件被设计成抑制向第二飞轮的弯曲振动的传递。 第二飞轮5邻近第一飞轮4的远离曲轴2的一侧设置。阻尼机构6使圆周方向上的第一和第二飞轮4和5弹性连接。 柔性板41轴向布置在第一和第二飞轮4和5之间,用于相对于第一飞轮4支撑第二飞轮5.柔性板41在弯曲方向上是柔性的。 轴承17布置在柔性板41和第一和第二飞轮4和5之一之间。