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    • 1. 发明授权
    • Ultraviolet irradiation system
    • 紫外线照射系统
    • US08487267B2
    • 2013-07-16
    • US13422521
    • 2012-03-16
    • Norimitsu AbeShinji KobayashiTakeshi IdeNaoto YoshizawaAkihiko ShirotaTakahiro Soma
    • Norimitsu AbeShinji KobayashiTakeshi IdeNaoto YoshizawaAkihiko ShirotaTakahiro Soma
    • C02F1/32G01N23/12
    • C02F1/325C02F1/008C02F2201/322C02F2201/324C02F2201/326C02F2209/008C02F2209/40
    • An ultraviolet irradiation system includes: an ultraviolet irradiation apparatus including a plurality of ultraviolet lamps; a flowmeter configured to measure a flow rate of the water to be treated that passes through the ultraviolet irradiation apparatus; and an ultraviolet-dose monitoring and controlling apparatus configured to monitor an ultraviolet dose of the ultraviolet irradiation apparatus and to control outputs of the ultraviolet lamps. The plurality of ultraviolet lamps include a first ultraviolet lamp and a plurality of second ultraviolet lamps. The ultraviolet irradiation apparatus includes: a first measurement head configured to measure an ultraviolet intensity of the first ultraviolet lamp; and a plurality of second measurement heads configured to respectively measure ultraviolet intensities of the plurality of the ultraviolet lamps. A distance between the first ultraviolet lamp and the first measurement head is set to a determined value.
    • 紫外线照射系统包括:紫外线照射装置,包括多个紫外线灯; 流量计,被配置为测量通过所述紫外线照射装置的被处理水的流量; 以及紫外线剂量监视和控制装置,其被配置为监测紫外线照射装置的紫外线剂量并控制紫外线灯的输出。 多个紫外线灯包括第一紫外灯和多个第二紫外线灯。 紫外线照射装置包括:第一测量头,被配置为测量第一紫外线灯的紫外线强度; 以及多个第二测量头,其被配置为分别测量所述多个所述紫外线灯的紫外线强度。 将第一紫外线灯和第一测量头之间的距离设定为确定值。
    • 2. 发明授权
    • Ultraviolet irradiation apparatus
    • 紫外线照射装置
    • US08507875B2
    • 2013-08-13
    • US13421649
    • 2012-03-15
    • Shinji KobayashiNorimitsu AbeAkihiko ShirotaNaoto YoshizawaTakahiro Soma
    • Shinji KobayashiNorimitsu AbeAkihiko ShirotaNaoto YoshizawaTakahiro Soma
    • C02F1/32
    • C02F1/325C02F1/283C02F1/52C02F1/76C02F2201/3223
    • A ultraviolet irradiation apparatus includes: an ultraviolet-irradiation water tank; a protection pipe provided in the ultraviolet-irradiation water tank; an ultraviolet lamp provided in the protection pipe to be lit up with high-frequency discharge at a frequency of 10 kHz to 10 MHz, inclusive; protection covers respectively provided on the two ends of the ultraviolet-irradiation water tank; an electronic ballast provided in one of the protection covers; and a feeder wire electrically connecting the ultraviolet lamp to the electronic ballast. Each of the ultraviolet-irradiation water tank and the protection covers is made of a conductive material with a specific conductivity and a relative magnetic permittivity whose product is equal to or larger than 1, and has a thickness at least three times as large as a skin depth at a frequency of a high-frequency current that flows through the ultraviolet lamp.
    • 紫外线照射装置包括:紫外线照射水箱; 设置在紫外线照射水箱内的保护管; 设置在保护管内的紫外线灯以10kHz至10MHz的频率以高频放电点亮; 分别设置在紫外线照射水箱两端的防护罩; 设置在所述保护盖之一中的电子镇流器; 以及将紫外线灯电连接到电子镇流器的馈线。 紫外线照射水箱和保护罩中的每一个都由具有等于或大于1的比电导率和相对磁介电常数的导电材料制成,并且具有至少三倍于皮肤的厚度 在穿过紫外线灯的高频电流的频率处的深度。
    • 9. 发明授权
    • Gas turbine cooled stationary blade
    • 燃气轮机冷却固定叶片
    • US06572335B2
    • 2003-06-03
    • US09800668
    • 2001-03-08
    • Masamitsu KuwabaraYasuoki TomitaAkihiko ShirotaEisaku Ito
    • Masamitsu KuwabaraYasuoki TomitaAkihiko ShirotaEisaku Ito
    • F04D2958
    • F01D5/187F01D9/041F05D2240/81F05D2260/22141
    • A gas turbine cooled stationary blade has a blade structure and outer and inner shrouds enhancing cooling efficiency and preventing the occurrence of cracks due to thermal stresses. A blade (1) wall thickness, between 75% and 100% of the blade height of a blade leading edge portion, is made thicker, and the blade (1) wall thickness of other portions is made thinner, as compared with a conventional case. Protruding ribs (4) are provided on a blade (1) convex side inner wall between 0% and 100% of the blade height. A blade (1) trailing edge opening portion is made thinner than the conventional case. Outer shroud (2) is provided with cooling passages (5a, 5b) for air flow in both side end portions. Inner shroud (3) is provided with cooling passages (9a, 9b) for air flow and cooling holes (13a, 13b) for air blow in the side end portions. With the blade (1) structure and the shroud (2, 3) cooling passages (5a, 5b, 9a, 9b) and cooling holes (13a, 13b), the cooling effect is enhanced and cracks are prevented from occurring.
    • 燃气轮机冷却的固定叶片具有叶片结构,外部和内部护罩提高冷却效率并防止由于热应力引起的裂纹。 叶片(1)的壁厚在叶片前缘部分的叶片高度的75%和100%之间变得更厚,并且其它部分的叶片(1)的壁厚比常规的情况更薄 。 突出肋(4)设置在叶片高度的0%和100%之间的叶片(1)凸侧内壁上。 叶片(1)后缘开口部分比现有技术更薄。 外护罩(2)设置有用于在两个侧端部中的空气流动的冷却通道(5a,5b)。 内护罩(3)设有用于气流的冷却通道(9a,9b)和用于在侧端部吹气的冷却孔(13a,13b)。 利用叶片(1)结构和护罩(2,3)冷却通道(5a,5b,9a,9b)和冷却孔(13a,13b),冷却效果提高,并且防止发生裂纹。
    • 10. 发明授权
    • Gas turbine moving blade
    • 燃气轮机动叶片
    • US06481967B2
    • 2002-11-19
    • US09790975
    • 2001-02-23
    • Yasuoki TomitaYukihiro HashimotoKiyoshi SuenagaHisato ArimuraShunsuke ToriiJun KubotaAkihiko ShirotaSunao AokiTatsuo Ishiguro
    • Yasuoki TomitaYukihiro HashimotoKiyoshi SuenagaHisato ArimuraShunsuke ToriiJun KubotaAkihiko ShirotaSunao AokiTatsuo Ishiguro
    • F01D518
    • F01D5/20F01D5/186F01D5/187F05D2240/81F05D2250/185F05D2260/22141
    • A gas turbine moving blade is provided which prevents occurrence of cracks caused by thermal stresses due to temperature differences between a blade and a platform while the gas turbine is being stopped. During steady operation time of the moving blade, cooling air enters cooling passages to flow through other cooling passages for cooling the blade, and then to flow out of the blade. A recessed portion having a smooth curved surface is provided in the platform near a blade fitting portion on the blade trailing edge side. A fillet of the blade fitting portion on the blade trailing edge side has a curved surface with curvature larger than that of a conventional blade fitting portion. A hub slot below the fillet, for blowing air, has a cross sectional area larger than other slots of the blade trailing edge. A thermal barrier coating is applied to the blade surface. By the above construction, thermal stresses due to temperature differences between the blade and the platform during gas turbine stoppage are made smaller and occurrence of cracks is prevented.
    • 提供了一种燃气轮机动叶片,其防止在燃气轮机停止时由于叶片和平台之间的温度差引起的热应力的发生。 在运动叶片的稳定运行时间内,冷却空气进入冷却通道,流过其它冷却通道,以冷却叶片,然后流出叶片。 具有光滑曲面的凹部在叶片后缘侧的叶片嵌合部附近设置在平台上。 叶片后缘侧的叶片嵌合部的圆角具有比现有的叶片嵌合部曲率大的曲率的曲面。 在圆角下方的用于吹送空气的轮毂槽的横截面积大于叶片后缘的其它槽。 将热障涂层施加到叶片表面。 通过上述结构,使得在燃气轮机停止期间由于叶片和平台之间的温度差导致的热应力变小,并且防止了裂纹的发生。