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    • 2. 发明申请
    • RADIAL TURBINE
    • 径向涡轮机
    • US20130121819A1
    • 2013-05-16
    • US13812740
    • 2011-01-24
    • Hirotaka HigashimoriNorihiro FukudaMasayuki KawamiAtsushi Fujii
    • Hirotaka HigashimoriNorihiro FukudaMasayuki KawamiAtsushi Fujii
    • F01D1/06
    • F01D1/06F01D1/08F01D5/048F01K7/16F01K25/10Y02E10/34
    • The present invention provides a radial turbine which uses a fluid having a plurality of pressures in a single turbine wheel, to thereby reduce the number of components and lower the cost. A radial turbine (100) includes a single radial turbine wheel (15) which converts, into rotational power, swirling energy of a swirling fluid with a first pressure that flows into the radial turbine wheel (15) from a main inlet (21) formed at an outer circumferential end through a nozzle (27) with a radial flow velocity component, wherein a sub inlet (29) is formed on an outer circumferential side of the radial turbine wheel (15) at a position radially and axially apart from the main inlet (21), and the low-boiling-point medium whose pressure decreases from the first pressure as the low-boiling-point medium travels to a radial inner side flows into the sub inlet (29) through a nozzle (35).
    • 本发明提供一种使用在单个涡轮机叶轮中具有多个压力的流体的径向涡轮机,从而减少部件的数量并降低成本。 径向涡轮机(100)包括单个径向涡轮机叶轮(15),其将旋转动力转换成具有从形成的主入口(21)流入径向涡轮机叶轮(15)的第一压力的旋转流体的旋转能量 在通过具有径向流速分量的喷嘴(27)的外圆周端处,其中在所述径向涡轮机叶轮(15)的外圆周侧上形成有与所述主流体径向和轴向分开的位置处的子入口(29) 入口(21)和低沸点介质运行到径向内侧时从第一压力下降的低沸点介质通过喷嘴(35)流入副入口(29)。
    • 3. 发明申请
    • Exhaust Gas Analysis Method and Exhaust Gas Analysis Apparatus
    • 废气分析方法和废气分析装置
    • US20090164138A1
    • 2009-06-25
    • US12083521
    • 2006-12-15
    • Katsutoshi GotoMasahiro YamakageTomoyasu IwaseTokio OkanoYoshihiro DeguchiMasanobu MizoguchiAtushi TakitaNorihiro Fukuda
    • Katsutoshi GotoMasahiro YamakageTomoyasu IwaseTokio OkanoYoshihiro DeguchiMasanobu MizoguchiAtushi TakitaNorihiro Fukuda
    • G01N21/31G06F19/00
    • G01N21/3504G01N21/031G01N21/314
    • An exhaust gas analysis method comprises applying a laser beam to the exhaust gas discharged from an internal combustion engine, receiving the laser beam that has passed through the exhaust gas, and measuring the concentration of any of the components contained in the exhaust gas based on the received laser beam. The exhaust gas analysis method further comprises detecting the absorption spectrum of the laser beam absorbed in the exhaust gas by using the received laser beam (S1), calculating the concentration of the specific gas component by using the absorption spectrum (S2), calculating the temperature of the exhaust gas by using the absorption spectrum (S3), calculating the pressure of the exhaust gas by using the absorption spectrum (S4 to S6), correcting the calculated concentration of the component contained in the exhaust gas by using the calculated temperature (S7), correcting the concentration by using the calculated pressure (S8), and outputting the true concentration value (S9). Accordingly, the exhaust gas analysis method is substantially insensitive to variation in pressure and temperature of the exhaust gas and capable of calculating and analyzing the concentration of any of the components contained in the exhaust gas in an accurate, realtime manner.
    • 排气分析方法包括对从内燃机排出的排气施加激光,接收通过废气的激光束,并且基于该废气测定废气中含有的任何成分的浓度 接收激光束。 废气分析方法还包括通过使用接收的激光束(S1)检测吸收在废气中的激光束的吸收光谱,通过使用吸收光谱(S2)计算特定气体成分的浓度,计算温度 通过使用吸收光谱(S3)来计算排气的压力,通过使用吸收光谱(S4〜S6)计算废气的压力,通过使用计算出的温度来校正计算出的废气中成分的成分浓度(S7 ),通过使用计算出的压力来校正浓度(S8),并输出真浓度值(S9)。 因此,排气分析方法对废气的压力和温度的变化基本上不敏感,并且能够以准确的实时方式计算和分析废气中包含的任何组分的浓度。
    • 4. 发明授权
    • Multi-pressure radial turbine system
    • 多压径向涡轮系统
    • US09500205B2
    • 2016-11-22
    • US14002468
    • 2012-07-05
    • Hirotaka HigashimoriNorihiro FukudaMasayuki Kawami
    • Hirotaka HigashimoriNorihiro FukudaMasayuki Kawami
    • F04D31/00F04D29/58F01K7/18F01D9/02F22B33/14F01K25/08
    • F04D29/58F01D9/026F01K7/18F01K25/08F22B33/14
    • A multi-pressure radial turbine system including a high-pressure pump and a low-pressure pump for pressurizing liquid-phase heating media introduced therein to different pressures; a high-pressure evaporator and a low-pressure evaporator for vaporizing the liquid-phase heating media delivered from the high-pressure pump and the low-pressure pump by absorbing heat from a high-temperature heat source; one multi-pressure radial turbine that expands the gaseous heating media having different pressures and temperatures, supplied from the high-pressure evaporator and the low-pressure evaporator, to obtain output power; and a condenser for condensing the gaseous heating medium expanded in the multi-pressure radial turbine by making the medium release heat to a low-pressure heat source. A cycle circuit is formed through which the heating medium circulates while repeatedly changing its state between vapor and liquid.
    • 一种多压力径向涡轮机系统,包括高压泵和低压泵,用于将引入其中的液相加热介质加压到不同的压力; 用于通过从高温热源吸收热量来蒸发从高压泵和低压泵输送的液相加热介质的高压蒸发器和低压蒸发器; 一个多压力径向涡轮,其膨胀由高压蒸发器和低压蒸发器供应的具有不同压力和温度的气态加热介质,以获得输出功率; 以及冷凝器,用于通过使介质向低压热源释放热量来冷凝在多压径向涡轮机中膨胀的气态加热介质。 形成一循环回路,加热介质通过该循环循环,同时重复地改变其在蒸气和液体之间的状态。
    • 5. 发明申请
    • MULTI-PRESSURE RADIAL TURBINE SYSTEM
    • 多压径向涡轮机系统
    • US20130336768A1
    • 2013-12-19
    • US14002468
    • 2012-07-05
    • Hirotaka HigashimoriNorihiro FukudaMasayuki Kawami
    • Hirotaka HigashimoriNorihiro FukudaMasayuki Kawami
    • F04D29/58
    • F04D29/58F01D9/026F01K7/18F01K25/08F22B33/14
    • A multi-pressure radial turbine system including a high-pressure pump and a low-pressure pump for pressurizing liquid-phase heating media introduced therein to different pressures; a high-pressure evaporator and a low-pressure evaporator for vaporizing the liquid-phase heating media delivered from the high-pressure pump and the low-pressure pump by absorbing heat from a high-temperature heat source; one multi-pressure radial turbine that expands the gaseous heating media having different pressures and temperatures, supplied from the high-pressure evaporator and the low-pressure evaporator, to obtain output power; and a condenser for condensing the gaseous heating medium expanded in the multi-pressure radial turbine by making the medium release heat to a low-pressure heat source. A cycle circuit is formed through which the heating medium circulates while repeatedly changing its state between vapor and liquid.
    • 一种多压力径向涡轮机系统,包括高压泵和低压泵,用于将引入其中的液相加热介质加压到不同的压力; 用于通过从高温热源吸收热量来蒸发从高压泵和低压泵输送的液相加热介质的高压蒸发器和低压蒸发器; 一个多压力径向涡轮,其膨胀由高压蒸发器和低压蒸发器供应的具有不同压力和温度的气态加热介质,以获得输出功率; 以及冷凝器,用于通过使介质向低压热源释放热量来冷凝在多压径向涡轮机中膨胀的气态加热介质。 形成一循环回路,加热介质通过该循环循环,同时重复地改变其在蒸气和液体之间的状态。