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1.发明授权公开(公告)号：US06678059B2
公开(公告)日：2004-01-13
申请号：US09879273
申请日：2001-06-13
申请人： Hyung Suck Cho , Won Shik Park , Yong Kyu Byun , Noh Yeol Park
发明人： Hyung Suck Cho , Won Shik Park , Yong Kyu Byun , Noh Yeol Park
IPC分类号： G01B1114
摘要： An apparatus for measuring six-degree-of-freedom motions by using three-facet reflector, the six-degree-of-freedom motions of an object being measured by using the laser beam proceeding from a laser light source, comprising: a multiple facet reflector in the form of a trigonal pyramid, the multiple facet reflector being fixed on the object for measurement and able to reflect the laser beam in three directions; three position-sensitive detectors for measuring the position and intensity of the laser light points formed on their surfaces, with the movement of the multiple facet reflector, and then providing output signals; and a controlling section for analyzing six-degree-of-freedom motions of the multiple facet reflector by using the position and intensity of the laser light points output from the three position-sensitive detectors. (FIG. 4).
摘要翻译： 一种用于通过使用三面反射器测量六自由度运动的装置，通过使用从激光源进行的激光束来测量物体的六自由度运动，包括：多面 反射器呈三角锥形，多面反射器固定在物体上用于测量，并能够在三个方向上反射激光束; 三个位置敏感检测器，用于测量形成在其表面上的激光点的位置和强度，随着多面反射器的移动，然后提供输出信号; 以及控制部分，用于通过使用从三个位置敏感检测器输出的激光点的位置和强度来分析多面反射器的六自由度运动。 （图4）。
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公开(公告)号：US20100107643A1
公开(公告)日：2010-05-06
申请号：US12422065
申请日：2009-04-10
申请人： Min Chul Lee , Dal Hong Ahn , Yong Jin Joo , Jae Hwa Chung , Si Moon Kim , Jin Pyo Hong , Won Shik Park
发明人： Min Chul Lee , Dal Hong Ahn , Yong Jin Joo , Jae Hwa Chung , Si Moon Kim , Jin Pyo Hong , Won Shik Park
IPC分类号： F02C3/32
摘要： Disclosed is a triple swirl gas turbine combustor using various fuels such as coal gas, DiMethyl Ether, and waste gas generated in an ironworks in a gas turbine. The triple swirl gas turbine combustor combusts three different fuels simultaneously or individually and various fuels such as LCV gas and HCV gas so that fuel flexibility can be improved. Swirl generated in a second swirler of the triple swirler is reversely jetted to increase a mixing degree of a fuel-air mixture and an intensity of a turbulent flow so that combustion efficiency can be increased, harmful exhaust gas can be reduced and vibration can be reduced.
摘要翻译： 公开了使用各种燃料（例如煤气，二甲基醚）和在燃气轮机中的炼铁厂中产生的废气的三重涡旋燃气涡轮机燃烧器。 三重涡轮燃气轮机燃烧器同时或单独地燃烧三种不同的燃料，并且可以提供诸如LCV气体和HCV气体的各种燃料，从而可以提高燃料的灵活性。 在三重旋流器的第二旋流器中产生的漩涡反向喷射以增加燃料 - 空气混合物的混合程度和湍流强度，从而可以提高燃烧效率，可以减少有害排气并减少振动 。
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公开(公告)号：US20090084109A1
公开(公告)日：2009-04-02
申请号：US12215159
申请日：2008-06-25
申请人： Min Chul Lee , Dal Hong Ahn , Yong Jin Joo , Seok Bin Seo , Jae Hwa Chung , Won Shik Park , Hae Kyung Seo
发明人： Min Chul Lee , Dal Hong Ahn , Yong Jin Joo , Seok Bin Seo , Jae Hwa Chung , Won Shik Park , Hae Kyung Seo
摘要： Disclosed herein are a fuel nozzle of a gas turbine combustor for dimethyl ether (DME, CH3OCH3) and a design method thereof. The fuel nozzle includes a pilot fuel injection hole formed at the center of the nozzle and a plurality of fuel injection ports formed at equiangular positions around the pilot fuel injection hole to inject DME. Each of the fuel injection ports includes a pair of upper and lower DME injection orifices communicating with a fuel-air mixture injection swirler. The upper DME injection orifice becomes gradually wider, whereas the lower DME injection orifice becomes gradually narrower. Thus, DME can be optimally combusted in the gas turbine combustor, thereby achieving cost reduction of power plants, enhancement in reliability of the power plants, and diversification of usable fuel.
摘要翻译： 本文公开了一种用于二甲醚（DME，CH 3 OCH 3）的燃气轮机燃烧器的燃料喷嘴及其设计方法。 燃料喷嘴包括形成在喷嘴中心处的先导燃料喷射孔和形成在引燃燃料喷射孔附近的等角位置处的多个燃料喷射口以喷射DME。 每个燃料喷射口包括与燃料 - 空气混合物喷射旋流器连通的一对上部和下部DME喷射孔。 上部DME喷射孔逐渐变宽，而下部DME喷射孔逐渐变窄。 因此，DME可以在燃气轮机燃烧器中最佳地燃烧，从而实现发电厂的成本降低，发电厂的可靠性提高，以及可用燃料的多样化。
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公开(公告)号：US08316645B2
公开(公告)日：2012-11-27
申请号：US12422065
申请日：2009-04-10
申请人： Min Chul Lee , Dal Hong Ahn , Yong Jin Joo , Jae Hwa Chung , Si Moon Kim , Jin Pyo Hong , Won Shik Park
发明人： Min Chul Lee , Dal Hong Ahn , Yong Jin Joo , Jae Hwa Chung , Si Moon Kim , Jin Pyo Hong , Won Shik Park
摘要： Disclosed is a triple swirl gas turbine combustor using various fuels such as coal gas, DiMethyl Ether, and waste gas generated in an ironworks in a gas turbine. The triple swirl gas turbine combustor combusts three different fuels simultaneously or individually and various fuels such as LCV gas and HCV gas so that fuel flexibility can be improved. Swirl generated in a second swirler of the triple swirler is reversely jetted to increase a mixing degree of a fuel-air mixture and an intensity of a turbulent flow so that combustion efficiency can be increased, harmful exhaust gas can be reduced and vibration can be reduced.
摘要翻译： 公开了使用各种燃料（例如煤气，二甲基醚）和在燃气轮机中的炼铁厂中产生的废气的三重涡旋燃气涡轮机燃烧器。 三重涡轮燃气轮机燃烧器同时或单独地燃烧三种不同的燃料，并且可以提供诸如LCV气体和HCV气体的各种燃料，从而可以提高燃料的灵活性。 在三重旋流器的第二旋流器中产生的漩涡反向喷射以增加燃料 - 空气混合物的混合程度和湍流强度，从而可以提高燃烧效率，可以减少有害排气并减少振动 。
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公开(公告)号：US08132415B2
公开(公告)日：2012-03-13
申请号：US12215159
申请日：2008-06-25
申请人： Min Chul Lee , Dal Hong Ahn , Yong Jin Joo , Seok Bin Seo , Jae Hwa Chung , Won Shik Park , Hae Kyung Seo
发明人： Min Chul Lee , Dal Hong Ahn , Yong Jin Joo , Seok Bin Seo , Jae Hwa Chung , Won Shik Park , Hae Kyung Seo
摘要： Disclosed herein are a fuel nozzle of a gas turbine combustor for dimethyl ether (DME, CH3OCH3) and a design method thereof. The fuel nozzle includes a pilot fuel injection hole formed at the center of the nozzle and a plurality of fuel injection ports formed at equiangular positions around the pilot fuel injection hole to inject DME. Each of the fuel injection ports includes a pair of upper and lower DME injection orifices communicating with a fuel-air mixture injection swirler. The upper DME injection orifice becomes gradually wider, whereas the lower DME injection orifice becomes gradually narrower. Thus, DME can be optimally combusted in the gas turbine combustor, thereby achieving cost reduction of power plants, enhancement in reliability of the power plants, and diversification of usable fuel.
摘要翻译： 本文公开了一种用于二甲醚（DME，CH 3 OCH 3）的燃气轮机燃烧器的燃料喷嘴及其设计方法。 燃料喷嘴包括形成在喷嘴中心处的先导燃料喷射孔和形成在引燃燃料喷射孔附近的等角位置处的多个燃料喷射口以喷射DME。 每个燃料喷射口包括与燃料 - 空气混合物喷射旋流器连通的一对上部和下部DME喷射孔。 上部DME喷射孔逐渐变宽，而下部DME喷射孔逐渐变窄。 因此，DME可以在燃气轮机燃烧器中最佳地燃烧，从而实现发电厂的成本降低，发电厂的可靠性提高，以及可用燃料的多样化。
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