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    • 21. 发明授权
    • Test apparatus
    • 测试仪器
    • US08078424B2
    • 2011-12-13
    • US12240387
    • 2008-09-29
    • Toshiaki Adachi
    • Toshiaki Adachi
    • G01R31/00
    • G01R31/2834G01R31/31907
    • Provided is a test apparatus 10, which includes: a plurality of test modules 150, each of which is connected to any of the plurality of devices under test 100 to supply a test signal to the connected device under test 100; a plurality of site controllers 130 that control the plurality of test modules 150 to test the respective plurality of devices under test 100 simultaneously; a connection setting device 140 that sets a connection mode between the plurality of site controllers 130 and the plurality of test modules 150 so that each of the test modules 150 is connected to any of the plurality of site controllers 130; and a plurality of system controllers 110, each of which controls any of the plurality of site controllers 130, in which a predetermined system controller of the plurality of system controllers 110 assigns, in response to a request from another system controller of the system controllers, a site controller of the site controllers, which is to be controlled by the another system controller.
    • 提供了一种测试装置10,其包括:多个测试模块150,每个测试模块150被连接到被测试的多个被测设备100中的任一个,以向连接的被测设备100提供测试信号; 多个站点控制器130,其控制多个测试模块150同时测试相应的多个待测设备100; 连接设置装置140,其设置多个站点控制器130和多个测试模块150之间的连接模式,使得每个测试模块150连接到多个站点控制器130中的任一个; 以及多个系统控制器110,每个系统控制器110响应于来自系统控制器的另一个系统控制器的请求,控制多个站点控制器130中的任一个,其中多个系统控制器110中的预定系统控制器分配, 站点控制器的站点控制器,由另一个系统控制器控制。
    • 24. 发明授权
    • Turbo charging system of diesel engine
    • 柴油机涡轮增压系统
    • US06311493B1
    • 2001-11-06
    • US09712684
    • 2000-11-14
    • Hirokazu KuriharaTakao KodairaToshiaki AdachiTakao FujisakiTakao InoueNaoki Yanagisawa
    • Hirokazu KuriharaTakao KodairaToshiaki AdachiTakao FujisakiTakao InoueNaoki Yanagisawa
    • F02D2300
    • F02B37/013F02B37/004F02B37/18Y02T10/144
    • A turbo charger system (32) for a diesel engine (1) with a simple structure, but improved in output, torque and fuel consumption rate. A high-stage turbine (3) and low-stage turbine (4) are provided in series on an exhaust gas line (2) of the engine (1). A high-stage compressor (6), which is connected to the high-stage turbine (3), and a low-stage compressor (7), which is connected to the low-stage turbine (4), are provided in series on an intake air line (5) of the engine (1). A bypass line (20) with a valve (21) is provided over the high-stage turbine (3). The bypass valve (21) is completely or substantially completely closed until the engine (1) reaches its maximum torque point (14) so as to raise a supercharging pressure. From the maximum torque point (14) to the maximum output point (15), the bypass valve (21) is gradually opened to adjust the supercharging pressure. The bypass valve is completely or substantially completely opened at the maximum output point (15) to suppress the supercharging pressure.
    • 一种用于柴油发动机(1)的涡轮增压器系统(32),其结构简单,但输出扭矩和燃料消耗率提高。 在发动机(1)的排气管线(2)上串联地设置有高级涡轮机(3)和低级涡轮机(4)。 连接到高级涡轮机(3)的高级压缩机(6)和与低级涡轮机(4)连接的低级压缩机(7)串联设置在 发动机(1)的进气管线(5)。 具有阀(21)的旁通管(20)设置在高级涡轮机(3)的上方。 旁通阀(21)完全或基本上完全关闭,直到发动机(1)达到其最大扭矩点(14)以便提高增压压力。 从最大扭矩点(14)到最大输出点(15),旁通阀(21)逐渐打开以调节增压压力。 旁通阀在最大输出点(15)处完全或基本上完全打开,以抑制增压压力。
    • 25. 发明申请
    • TEST APPARATUS
    • 测试仪器
    • US20100082284A1
    • 2010-04-01
    • US12240387
    • 2008-09-29
    • Toshiaki Adachi
    • Toshiaki Adachi
    • G01R31/00G01N37/00
    • G01R31/2834G01R31/31907
    • Provided is a test apparatus 10, which includes: a plurality of test modules 150, each of which is connected to any of the plurality of devices under test 100 to supply a test signal to the connected device under test 100; a plurality of site controllers 130 that control the plurality of test modules 150 to test the respective plurality of devices under test 100 simultaneously; a connection setting device 140 that sets a connection mode between the plurality of site controllers 130 and the plurality of test modules 150 so that each of the test modules 150 is connected to any of the plurality of site controllers 130; and a plurality of system controllers 110, each of which controls any of the plurality of site controllers 130, in which a predetermined system controller of the plurality of system controllers 110 assigns, in response to a request from another system controller of the system controllers, a site controller of the site controllers, which is to be controlled by the another system controller.
    • 提供了一种测试装置10,其包括:多个测试模块150,每个测试模块150被连接到被测试的多个被测设备100中的任一个,以向连接的被测设备100提供测试信号; 多个站点控制器130,其控制多个测试模块150同时测试相应的多个待测设备100; 连接设置装置140,其设置多个站点控制器130和多个测试模块150之间的连接模式,使得每个测试模块150连接到多个站点控制器130中的任一个; 以及多个系统控制器110,每个系统控制器110响应于来自系统控制器的另一个系统控制器的请求,控制多个站点控制器130中的任一个,其中多个系统控制器110中的预定系统控制器分配, 站点控制器的站点控制器,由另一个系统控制器控制。
    • 27. 发明授权
    • Combustion chamber
    • 燃烧室
    • US4995360A
    • 1991-02-26
    • US394456
    • 1989-08-16
    • Toshiaki Adachi
    • Toshiaki Adachi
    • F02B19/08
    • F02B19/08Y02T10/125
    • A swirl chamber is defined by an approximately spherical cavity formed in a cylinder head of an internal combustion engine with the radius of the swirl chamber being reduced in the direction the swirl flows in the swirl chamber. Therefore, the swirl is accelerated as it flows in the swirl chamber. The swirl chamber communicates with a main combustion chamber formed in a piston top via a passage formed in the cylinder head when the piston is at top dead center, and air in the main combustion chamber is forced into the swirl chamber due to the compression stroke of the piston. The passage is formed in a manner such that it has constant transverse section lengthwise and such that a part of the passage defines a tangential line of the swirl chamber. Therefore, the air forced into the swirl chamber passes through the passage with little friction loss, smoothly enters the swirl chamber and gains velocity in the swirl chamber.