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    • 81. 发明授权
    • Gas turbine combustor
    • 燃气轮机燃烧器
    • US4429538A
    • 1984-02-07
    • US234015
    • 1981-02-12
    • Isao SatoYohji IshibashiYoshimitsu MinakawaTakashi OhmoriZensuke TamuraYoshihiro UchiyamaRyoichiro Ohshima
    • Isao SatoYohji IshibashiYoshimitsu MinakawaTakashi OhmoriZensuke TamuraYoshihiro UchiyamaRyoichiro Ohshima
    • F23R3/04F23R3/06F23R3/12F23R3/14F23R3/34F02C3/14
    • F23R3/06F23R3/12
    • A gas turbine combustor comprising a combustor inner-pipe for forming a head combustion chamber and a rear combustion chamber having a diameter larger than a diameter of head combustion chamber. A combustor outer-pipe covers the combustor inner-pipe, and a fuel nozzle is disposed at an end part of the head combustion chamber for supplying fuel to said combustor inner pipe. A first group of ports are arranged for swirling and feeding air in an axial direction of the combustor inner-pipe. The first group of ports are around the fuel nozzle. A second group of ports for swirling and feeding air in a radial direction of said combustor inner-pipe are disposed in a side wall of the head combustion chamber near the fuel nozzle. A third group of ports for swirling and feeding air in a radial direction of the combustion inner-pipe and a fourth group of ports for feeding air in a radial direction of the combustor inner-pipe are provided and ar both disposed in a side wall of the head combustion chamber near the said rear combustion chamber. A fifth group of ports are disposed in a side wall of the rear combustion chamber near the head combustion chamber and a sixth group of ports are disposed in a side wall of the rear combustion chamber on a downstream side of the fifth group of ports. Another group of ports for swirling and feeding air into the head combustion chamber are disposed in a vicinity of a central portion of an end part of the head combustion chamber along an inner periphery of the fuel nozzle, with this group of ports and the first group of ports being constructed so that air flowing from both groups of ports has the same swirling direction.
    • 一种燃气轮机燃烧器,包括用于形成头部燃烧室的燃烧器内管和具有大于头部燃烧室直径的直径的后燃烧室。 燃烧器外管覆盖燃烧器内管,并且燃料喷嘴设置在头部燃烧室的端部,用于向燃烧器内管供应燃料。 第一组端口布置成在燃烧器内管的轴向上旋转和进给空气。 第一组港口在燃油喷嘴周围。 用于在所述燃烧器内管的径向方向上旋转和进给空气的第二组端口设置在靠近燃料喷嘴的头部燃烧室的侧壁中。 设置有用于在燃烧内管的径向上旋转和进给空气的第三组端口和用于沿着燃烧器内管的径向供给空气的第四组端口,并且ar设置在 靠近所述后燃烧室的头部燃烧室。 第五组端口设置在靠近头部燃烧室的后燃烧室的侧壁中,并且第六组端口设置在第五组端口的下游侧的后燃烧室的侧壁中。 用于将空气旋转并进入头部燃烧室的另一组端口沿着燃料喷嘴的内周设置在头部燃烧室的端部的中心部分的附近,该组端口和第一组 的端口被构造成使得从两组端口流出的空气具有相同的旋转方向。
    • 82. 发明授权
    • Valve device
    • 阀门装置
    • US4364543A
    • 1982-12-21
    • US244393
    • 1981-03-16
    • Masahiro SoyaIsao SatoSeiji Kurose
    • Masahiro SoyaIsao SatoSeiji Kurose
    • F16K31/50F16K41/02F16K41/14F16K41/18F16K43/00
    • F16K31/50Y10T137/6065Y10T137/6106
    • A valve device comprises a valve body having an inflow passage and an outflow passage, a valve seat fixed to the valve body at a position between the passages, a valve element for seating against and separating from the valve seat, a valve stem movable together with the valve element toward and away from the valve seat, a stem holding member secured at a portion thereof to the valve body in the body interior and holding the valve stem at a screw engagement part therewith where a surface at an extremity of the portion of the stem holding member is in abutting contact with a surface of the main body thereby to form a first metal-contact seal, a bonnet which is detachably fixed to the valve body with a sealing member interposed therebetween, and through which the valve stem is rotatably fitted, where the bonnet covers the remainder portion of the stem holding member, and a mechanism for forming a second metal-contact seal at a stem holding part of the stem holding member when the valve is in the fully opened state thereof.
    • 阀装置包括具有流入通道和流出通道的阀体,在通道之间的位置处固定到阀体的阀座,用于抵靠和离开阀座的阀元件,可与 所述阀元件朝向和远离所述阀座,杆保持构件,其固定在所述阀体的一部分处,并且将所述阀杆保持在与所述阀体的螺纹接合部分处的所述阀体的一部分处的表面, 杆保持构件与主体的表面邻接接触,从而形成第一金属接触密封件,阀盖可拆卸地固定到阀体上,密封构件插入其间,阀杆可旋转地安装在阀体上 其中所述发动机罩覆盖所述杆保持构件的剩余部分,以及用于在所述阀为所述杆保持构件的杆保持构件的杆保持部分处形成第二金属接触密封件的机构 处于完全打开状态。
    • 84. 发明授权
    • Friction welding apparatus
    • 摩擦焊接设备
    • US4247346A
    • 1981-01-27
    • US905018
    • 1978-05-11
    • Kazuo MaeharaIsao Sato
    • Kazuo MaeharaIsao Sato
    • B23K20/12B29C65/00B29C65/06B29C27/08B06B1/16B32B31/20
    • B29C66/54B23K20/1205B29C65/0636B29C65/0645B29C66/8322B29C66/93441B29C66/93451B29C66/939Y10T29/49908Y10T29/49924
    • A friction welding apparatus for welding a pair of members in which the welding surfaces of the members are contacted under pressure with each other, relative circular orbit motion of the members producing friction therebetween thereby heating and melting the welding surfaces and the relative circular orbit motion being stopped to locate the welding surfaces in a predetermined position. The apparatus comprises an eccentric device including a rotary driving shaft, an inertia member disposed around the periphery of the rotary driving shaft, the inertia member being rotated by the rotary driving shaft and being capable of subjecting an angular movement relative thereto and an eccentric shaft rotated by the rotary driving shaft and engaged with the inertia member so as to be moved by the relative angular movement of the inertia member relative to the rotary driving shaft between a co-axial position with the axis of the rotary driving shaft and an eccentric position spaced by a predetermined distance apart therefrom, a movable table engaged through a bearing with the eccentric shaft for supporting the member to be welded, the movable table being connected by a motion restricting device to a fixed frame to be capable of causing substantial relative circular orbit motion in a plane perpendicular to the axis of the rotary driving shaft, the inertia member being angularly moved by rapid increase in the speed of the rotary driving shaft relative thereto from a first position to a second position such that the eccentric shaft is moved from the co-axial position to the eccentric position and the movable table is put in the relative circular orbit motion, and the inertia member being returned by rapid stoppage of the rotary driving shaft from the second position to the first position such that the eccentric shaft is returned to the co-axial position and the movable table is stopped at the predetermined position.
    • 一种用于焊接一对构件的摩擦焊接装置,其中,所述构件的焊接表面在压力下彼此接触,所述构件的相对圆形轨道运动产生摩擦,从而加热和熔化焊接表面,并且相对圆形轨道运动是 停止将焊接表面定位在预定位置。 该装置包括偏心装置,该偏心装置包括旋转驱动轴,围绕旋转驱动轴的周边设置的惯性构件,惯性构件由旋转驱动轴旋转,并且能够相对于其旋转并且偏心轴旋转 通过旋转驱动轴与惯性构件接合,以通过惯性构件相对于旋转驱动轴的相对角度运动在与旋转驱动轴的轴线的同轴位置与间隔开的偏心位置之间移动 通过轴承与活动台相接合,可移动台与偏心轴相接合,用于支撑待焊接的构件,活动台由运动限制装置连接到固定框架上,以能够引起相当大的相对圆周轨道运动 在与旋转驱动轴的轴线垂直的平面中,惯性构件成角度地移动 d,通过使旋转驱动轴相对于第一位置到第二位置的速度快速增加,使得偏心轴从同轴位置移动到偏心位置,并且可移动台被放入相对圆形轨道 运动,并且所述惯性构件通过所述旋转驱动轴从所述第二位置快速停止而返回到所述第一位置,使得所述偏心轴返回到同轴位置,并且所述可动台停止在所述预定位置。
    • 85. 发明授权
    • Gas turbine combustor
    • 燃气轮机燃烧器
    • US4226088A
    • 1980-10-07
    • US880109
    • 1978-02-22
    • Satoshi TsukaharaIsao SatoYoshihiro UchiyamaMasanobu Kusaba
    • Satoshi TsukaharaIsao SatoYoshihiro UchiyamaMasanobu Kusaba
    • F23R3/12F23C99/00F23R3/04F23R3/54F02C7/22
    • F23R3/04F23R3/54
    • A combustor for gas turbines includes a stepped cylindrical tube defining first, second and main combustion spaces. Primary air supply openings are formed in the tube portion defining the first combustion space, secondary air supply openings in the tube portion defining the second combustion space, and diluting air supply openings in the tube portion defining the main combustion space. To achieve effective cooling of the combustion gas within the combustion chamber, particularly in the second combustion space, and especially in the central portion thereof, and at the same time to maintain a stable combustion, the tube is formed so, and the cross-sectional areas of the primary, secondary and diluting air supply openings are dimensioned so, that 25 to 32% of the total amount of air supplied to the combustion chamber are used as primary air in the first combustion space, 38 to 50% as secondary air in the second combustion space, and less than 30% as diluting air in the main combustion space.
    • 用于燃气轮机的燃烧器包括限定第一,第二和主燃烧空间的阶梯形圆柱形管。 主要空气供应开口形成在限定第一燃烧空间的管部分中,限定第二燃烧空间的管部分中的二次空气供应开口,以及限定主燃烧空间的管部分中的稀释空气供应开口。 为了有效地冷却燃烧室内的燃烧气体,特别是在第二燃烧空间,特别是在其中心部分,并且同时保持燃烧稳定的燃烧气体,管形成为这样,并且横截面 初级,次级和稀释空气供应开口的区域尺寸使得供应到燃烧室的空气总量的25%至32%用作第一燃烧空间中的一次空气,作为二次空气中的38%至50% 第二燃烧空间,并且在主燃烧空间中稀释空气小于30%。
    • 89. 发明授权
    • Vehicle and control method for vehicle
    • 车辆和车辆控制方法
    • US09457796B2
    • 2016-10-04
    • US14424654
    • 2013-11-14
    • Masaaki SaikoIsao SatoRyo Watanabe
    • Masaaki SaikoIsao SatoRyo Watanabe
    • B60W20/15B60W20/00B60K6/365B60K6/445B60W10/06B60W30/184B60W10/12
    • B60W20/15B60K6/365B60K6/445B60W10/06B60W10/12B60W20/00B60W30/1846B60W2520/10B60W2710/0644Y02T10/6239Y10S903/93Y10T477/606
    • A vehicle includes: an engine; a first electric motor capable of inputting or outputting power; a power split mechanism including a sun gear, a ring gear and a planetary carrier rotatably revolvably supporting pinion gears meshing with the sun and ring gears. The planetary carrier, the sun gear and the ring gear are respectively coupled to an engine output shaft, a first electric motor rotary shaft and a drive wheel. The vehicle further includes a second electric motor capable of inputting or outputting power to or from the drive wheel; and a control device setting an engine operation range determined by a limit value of a rotation speed of the pinion gears. To increase durability of the pinion gears the limit value is higher at a high engine rotation and low vehicle speed side than at a low engine rotation and high vehicle speed side. Engine operation is controlled on the basis of the set engine operation range.
    • 车辆包括:发动机; 能够输入或输出动力的第一电动机; 动力分配机构,包括太阳轮,环形齿轮和行星架,可旋转地支撑与太阳和环形齿轮啮合的小齿轮。 行星架,太阳齿轮和齿圈分别与发动机输出轴,第一电动机旋转轴和驱动轮相连。 车辆还包括能够向驱动轮输入或输出动力的第二电动机; 以及控制装置,其设定由所述小齿轮的转速的极限值确定的发动机运转范围。 为了提高小齿轮的耐久性,在高发动机转速和低车速侧,与低发动机转速和高车速侧相比,极限值更高。 发动机运转是根据设定的发动机运转范围进行控制的。