专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

US20120234294A1 METHOD FOR CORRECTING FUEL INJECTION AMOUNT IN COMMON-RAIL-TYPE FUEL INJECTION CONTROL DEVICE AND COMMON-RAIL-TYPE FUEL INJECTION CONTROL DEVICE 失效
标题翻译：在通用型燃油喷射控制装置和普通型燃油喷射控制装置中校正燃油喷射量的方法
公开(公告)号：US20120234294A1
公开(公告)日：2012-09-20
申请号：US13414017
申请日：2012-03-07
申请人： Shigeyoshi Nakamura , Yasuhito Kirita , Osamu Mori
发明人： Shigeyoshi Nakamura , Yasuhito Kirita , Osamu Mori
IPC分类号： F02D41/38 , F02D41/04
CPC分类号： F02D41/04 , F02D9/06 , F02D41/0007 , F02D41/14 , F02D41/24 , F02D41/2467 , F02D41/247 , F02D2200/1012
摘要： A common-rail-type fuel injection control device where an error in the correction of a fuel injection amount when an exhaust brake is used is eliminated enabling a more reliable correction of a fuel injection amount.A minute injection is performed plural times in a non-injection state. A difference between a reference energizing time, which becomes the reference for a fuel injection valve, and an actual energizing time based on a frequency component corresponding to a variation in an engine speed which is generated in the minute injection is learned. A correction control corrects an energizing time and timing. The correction control is corrected corresponding to a presence or non-presence of an operation of an exhaust brake and a magnitude of a supercharging pressure, and an amount of variation in an engine speed calculated based on a rotational variation frequency component.
摘要翻译：在使用排气制动器时燃料喷射量的校正误差的共轨式燃料喷射控制装置被消除，能够更可靠地校正燃料喷射量。在非注射状态下多次进行微量注射。获取作为燃料喷射阀的基准的基准通电时间与基于在微小喷射中产生的发动机转速的变化对应的频率成分的实际通电时间之间的差。校正控制校正通电时间和定时。对应于排气制动器的操作的存在或不存在以及增压压力的大小以及基于旋转变化频率分量计算出的发动机转速的变化量来校正校正控制。

2. 发明授权

US08739764B2 Method for correcting fuel injection amount in common-rail-type fuel injection control device and common-rail-type fuel injection control device 失效
标题翻译：用于校正共轨式燃料喷射控制装置和共轨式燃料喷射控制装置中的燃料喷射量的方法
公开(公告)号：US08739764B2
公开(公告)日：2014-06-03
申请号：US13414017
申请日：2012-03-07
申请人： Shigeyoshi Nakamura , Yasuhito Kirita , Osamu Mori
发明人： Shigeyoshi Nakamura , Yasuhito Kirita , Osamu Mori
IPC分类号： F02D41/04 , F02D41/24 , F02D41/14
CPC分类号： F02D41/04 , F02D9/06 , F02D41/0007 , F02D41/14 , F02D41/24 , F02D41/2467 , F02D41/247 , F02D2200/1012
摘要： A common-rail-type fuel injection control device where an error in the correction of a fuel injection amount when an exhaust brake is used is eliminated enabling a more reliable correction of a fuel injection amount.A minute injection is performed plural times in a non-injection state. A difference between a reference energizing time, which becomes the reference for a fuel injection valve, and an actual energizing time based on a frequency component corresponding to a variation in an engine speed which is generated in the minute injection is learned. A correction control corrects an energizing time and timing. The correction control is corrected corresponding to a presence or non-presence of an operation of an exhaust brake and a magnitude of a supercharging pressure, and an amount of variation in an engine speed calculated based on a rotational variation frequency component.
摘要翻译：在使用排气制动器时燃料喷射量的校正误差的共轨式燃料喷射控制装置被消除，能够更可靠地校正燃料喷射量。在非注射状态下多次进行微量注射。获取作为燃料喷射阀的基准的基准通电时间与基于在微小喷射中产生的发动机转速的变化对应的频率成分的实际通电时间之间的差。校正控制校正通电时间和定时。对应于排气制动器的操作的存在或不存在以及增压压力的大小以及基于旋转变化频率分量计算出的发动机转速的变化量来校正校正控制。

3. 发明授权

US06574966B2 Gas turbine for power generation 有权
标题翻译：用于发电的燃气轮机
公开(公告)号：US06574966B2
公开(公告)日：2003-06-10
申请号：US10124406
申请日：2002-04-18
申请人： Kishio Hidaka , Shigeyoshi Nakamura , Yutaka Fukui , Masao Shiga , Ryo Hiraga , Hajime Toriya , Toshio Fujita
发明人： Kishio Hidaka , Shigeyoshi Nakamura , Yutaka Fukui , Masao Shiga , Ryo Hiraga , Hajime Toriya , Toshio Fujita
IPC分类号： F02C700
CPC分类号： C22C38/44 , C21D6/004 , C21D9/0068 , C21D9/28 , C21D2201/04 , C21D2211/008 , C22C19/03 , C22C38/001 , C22C38/04 , C22C38/46 , C22C38/48 , C22C38/52 , F01D5/225 , F01D5/28 , F01D5/3053 , F02C6/18 , F05D2260/201 , F05D2260/205 , F05D2260/2322 , F05D2300/607
摘要： A gas turbine for power generation operated at a turbine nozzle inlet temperature ranging from 1200 to 1650° C., which is improved to obtain a high heat efficiency by making disk blades and nozzles arranged in first to final stages from optimum materials and optimally cooling these disk blades and nozzles, and to obtain a combined power generation system using the gas turbine. The combined power generation system includes a highly efficient gas turbine operated at a turbine nozzle inlet combustion gas temperature ranging from 1200 to 1650° C., and a high pressure-intermediate pressure-low pressure integral type steam turbine operated at a steam inlet temperature of 530° C. or more, wherein the gas turbine is configured such that turbine blades, nozzles and disks are each cooled, and the blades and nozzles are each made from an Ni-based alloy having a single crystal or columnar crystal structure and disks are made from a martensite steel.
摘要翻译：用于发电的燃气轮机在1200至1650℃的涡轮喷嘴入口温度下运行，其通过使盘片和喷嘴从最佳材料的第一到最后阶段排列而最佳地冷却，从而获得高的热效率磁盘叶片和喷嘴，并且获得使用燃气轮机的组合发电系统。组合发电系统包括在涡轮喷嘴入口燃烧气体温度范围为1200至1650℃的高效燃气轮机和高在530℃或更高的蒸气入口温度下工作的压力 - 中压低压一体式蒸汽轮机，其中燃气轮机被构造成使得涡轮机叶片，喷嘴和盘都被冷却，并且叶片和喷嘴各自由具有单晶或柱状晶体结构的Ni基合金制成，圆盘由马氏体钢制成。

4. 发明授权

US06493936B2 Method of making steam turbine blade 有权
标题翻译：制造汽轮机叶片的方法
公开(公告)号：US06493936B2
公开(公告)日：2002-12-17
申请号：US09766978
申请日：2001-01-23
申请人： Hiroyuki Doi , Mitsuo Kuriyama , Shigeyoshi Nakamura , Shinya Imano , Takeshi Onoda
发明人： Hiroyuki Doi , Mitsuo Kuriyama , Shigeyoshi Nakamura , Shinya Imano , Takeshi Onoda
IPC分类号： B23P1500
CPC分类号： C22C14/00 , C22C38/44 , C22C38/46 , C22C38/52 , C22F1/183 , F01D5/28 , F05D2220/31 , F05D2300/133 , Y10T29/49336 , Y10T29/49339
摘要： A steam turbine blade made of Ti-base alloy comprising an &agr;+&bgr; type phase in which a difference of a tensile strength is small between a blade portion and a dovetail portion, a tensile strength at a room temperature of the dovetail portion is equal to or more than 100 kg/mm2 and a suitable toughness is commonly provided together with a strength, as a steam turbine blade having a length of 43 inch or more, a method of manufacturing the same, a steam turbine power generating plant and a low pressure steam turbine. In the steam turbine blade having a blade portion and a plurality of fork type dovetails, wherein the blade is made of Ti-base alloy structured such that a length of the blade portion is equal to or more than 52 inches with respect to a rotational speed 3000 rpm of the blade or equal to or more than 43 inches with respect to the rotational speed 3600 rpm, and a tensile strength at a room temperature of the dovetail is equal to or more than 100 kg/mm2, preferably equal to or more than 110 kg/mm2 and equal to or more than 96 % of the tensile strength at the room temperature of the blade portion.
摘要翻译：一种由钛基合金制成的汽轮机叶片，其包括在叶片部分和燕尾形部分之间拉伸强度差小的α+β型相，燕尾部分室温下的拉伸强度等于或大于100kg / mm 2，并且合适的韧性通常与强度一起提供，作为具有43英寸或更长的长度的蒸汽轮机叶片，其制造方法，蒸汽轮机发电设备和低压汽轮机。在具有叶片部分和多个叉形燕尾形的汽轮机叶片中，其中叶片由Ti基合金制成，使得叶片部分的长度相对于转速等于或大于52英寸相对于转速3600rpm等于或大于43英寸，燕尾榫的室温拉伸强度等于或大于100kg / mm2，优选等于或大于等于或大于 110kg / mm2，等于或大于在叶片部分的室温下的拉伸强度的96％。

5. 发明授权

US06358004B1 Steam turbine power-generation plant and steam turbine 有权
标题翻译：蒸汽轮机发电厂和汽轮机
公开(公告)号：US06358004B1
公开(公告)日：2002-03-19
申请号：US09605673
申请日：2000-06-28
申请人： Masao Shiga , Takeshi Onoda , Shigeyoshi Nakamura , Yutaka Fukui
发明人： Masao Shiga , Takeshi Onoda , Shigeyoshi Nakamura , Yutaka Fukui
IPC分类号： F01D102
CPC分类号： C22C38/46 , C22C38/44 , F01D5/28
摘要： A compact steam turbine power-generation plant has a compact steam turbine that operates at a high temperature in a range of 600 to 660° C. Ferrite based heat resisting steels provide for thermal efficiency. The main steam temperature and the reheated steam temperature can be set in a range of 600 to 660° C. by making the main parts exposed to the high temperature atmosphere, such as the rotor shaft, from ferrite based forged steels and cast steels and by making a final stage blade of a low pressure turbine from a martensite steel. The final stage blade is made from a ferrite based forged steel having a tensile strength of 120 kgf/mm2 or more; the rotor shaft is made from a ferrite based forged steel having a 105 h creep rupture strength of 11 kgf/mm2 or more; and the inner casing is made from a ferrite based cast steel having a 105 h creep rupture strength of 10 kgf/mm2 or more.
摘要翻译：紧凑型蒸汽轮机发电厂具有紧凑型蒸汽轮机，其工作温度高达600至660°C。铁素体耐热钢可提供热效率。主蒸汽温度和再热蒸汽温度可以设定在600至660℃的范围内，通过使主要部件暴露于诸如转子轴的高温气氛中，从铁素体锻造钢和铸钢以及由从马氏体钢制成低压涡轮机的末级叶片。末级叶片由抗拉强度为120kgf / mm2以上的铁素体型锻钢制成，转子轴由105h蠕变断裂强度为11kgf / mm2以上的铁素体锻造钢制成，并且内壳由具有105kg蠕变断裂强度为10kgf / mm 2以上的铁素体铸钢制成。

6. 发明授权

US5911842A Heat resisting steel and steam turbine rotor shaft and method of making thereof 失效
标题翻译：耐热钢和汽轮机转子轴及其制造方法
公开(公告)号：US5911842A
公开(公告)日：1999-06-15
申请号：US841676
申请日：1997-04-30
申请人： Masao Shiga , Kishio Hidaka , Norio Yamada , Shigeyoshi Nakamura , Yutaka Fukui , Nobuo Shimizu , Ryoichi Kaneko , Yasuhiro Harada , Yasuo Watanabe , Toshio Fujita , Norio Morisada , Yasuhiko Tanaka
发明人： Masao Shiga , Kishio Hidaka , Norio Yamada , Shigeyoshi Nakamura , Yutaka Fukui , Nobuo Shimizu , Ryoichi Kaneko , Yasuhiro Harada , Yasuo Watanabe , Toshio Fujita , Norio Morisada , Yasuhiko Tanaka
IPC分类号： F01D5/02 , C21D9/28 , C21D9/38 , C22C38/00 , C22C38/22 , C22C38/24 , C22C38/26 , C22C38/30 , C22C38/32 , C22C38/54 , F01D5/06 , C21D8/10 , C21D9/30
CPC分类号： C22C38/32 , C21D9/28 , C22C38/001 , C22C38/22 , C22C38/24 , C22C38/26 , C22C38/30 , C21D2211/008
摘要： A heat resisting steel whose metal structure is entirely martensite phase produced by tempering after quenching. The steel comprises, by weight, 0.05 to 0.20% C, not more than 0.15% Si, not more than 1.5% Mn, not more than 1.0% Ni, 8.5 to 13.0% Cr, not more than 3.50% Mo, not more than 3.5% W, 0.05 to 0.30% V, 0.01 to 0.20% Nb, not more than 5.0% Co, 0.001 to 0.020% boron, 0.005 to 0.040% nitrogen, 0.0005 to 0.0050% oxygen and 0.00001 to 0.0002% hydrogen. The steel has preferably not more than 10 of the Cr equivalent. The steel has 10 kgf/mm.sup.2 or more of 100,000 hours creep rupture strength at 650.degree. C.
摘要翻译：淬火后通过回火生产金属结构完全是马氏体相的耐热钢。该钢包含0.05〜0.20％的C，不大于0.15％的Si，不超过1.5％的Mn，不超过1.0％的Ni，8.5〜13.0％的Cr，不大于3.50％的Mo，不大于 3.5％W，0.05〜0.30％V，0.01〜0.20％Nb，5.0％以下的Co，0.001〜0.020％的硼，0.005〜0.040％的氮，0.0005〜0.0050％的氧和0.00001〜0.0002％的氢。钢优选不超过10当量的Cr当量。该钢在650℃下具有10kgf / mm 2以上的100,000小时蠕变断裂强度

7. 发明授权

US4988266A Gas turbine and shroud for gas turbine 失效
标题翻译：燃气轮机和燃气轮机罩
公开(公告)号：US4988266A
公开(公告)日：1991-01-29
申请号：US321880
申请日：1989-03-10
申请人： Shigeyoshi Nakamura , Yutaka Fukui , Tetsuo Kashimura
发明人： Shigeyoshi Nakamura , Yutaka Fukui , Tetsuo Kashimura
IPC分类号： C22C19/05 , C22C19/07 , C22C30/00 , C22C38/00 , C22C38/22 , C22C38/44 , F01D5/06 , F01D5/28 , F01D11/08 , F01D11/12
CPC分类号： F01D11/122 , C22C19/055 , C22C19/07 , C22C30/00 , C22C38/22 , C22C38/44 , F01D11/08 , F01D5/28 , F05D2240/11 , F05D2300/608 , F05D2300/609
摘要： A gas turbine includes a turbine stubshaft, a plurality of turbine disks coupled to the shaft by turbine stacking bolts with spacers interposed therebetween, turbing moving blades planted in each of the disks, a shroud provided with a sliding surface in a spaced-apart relation to the tips of the moving blades, a distant piece connected to the disks by the bolts, a plurality of compressor disks coupled to the distant piece by compressor stacking bolts, compressor blades planted in each of the compressor disks, and a compressor stubshaft formed integrally with the compressor disk located at the first stage. At least a sliding portion of the shroud is made of a heat-resistant cast alloy having in turn a chilled layer and columnar grains in a direction oriented from the sliding surface thereof toward the interior thereof. A method of producing a segment-shaped shroud for a gas turbine by casting, comprises the steps of preparing a mold having a coated layer formed on at least a surface thereof which is to be in contact with a casting, the coated layer containing refractory aggregate powder at a main constituent, and refractory agent powder for accelerating generation of crystal nuclei, pouring the molten alloy into the mold, and forced-cooling the outer surface of the mold.

8. 发明申请

US20080018696A1 Ink-jet line printer and image forming apparatus using the same 有权
标题翻译：喷墨线打印机和使用其的成像设备
公开(公告)号：US20080018696A1
公开(公告)日：2008-01-24
申请号：US11806952
申请日：2007-06-05
申请人： Koichi Sanpei , Mitsuhiro Mori , Akira Iwaishi , Shigeyoshi Nakamura , Katsumi Tateno
发明人： Koichi Sanpei , Mitsuhiro Mori , Akira Iwaishi , Shigeyoshi Nakamura , Katsumi Tateno
IPC分类号： B41J2/165
CPC分类号： B41J2/16588 , B41J2/14274 , B41J2/155 , B41J2/165 , B41J2/16585 , B41J2/18
摘要： An ink-jet line printer (30) is constituted by multiple ink-jet heads (1-1 to 1-3). Actuators (3-1 to 3-3) are arranged so as to be moved between a home position and a print position, and backup mechanisms (2-1 to 2-3) are arranged at home positions. In this ink-jet line printer, the ink-jet heads can be protected and recovered by backup mechanisms, thus making high-speed continuous printing possible. Even though the backup mechanisms are incorporated, a compact apparatus can still be achieved.
摘要翻译：喷墨打印机（30）由多个喷墨头（1-1-1-3）构成。致动器（3-1至3-3）布置成在原始位置和打印位置之间移动，并且备用机构（2-1至2-3）被布置在原始位置。在这种喷墨打印机中，喷墨头可以通过备用机构进行保护和回收，从而可以实现高速连续打印。即使配置了备用机构，仍然可以实现紧凑的装置。

9. 发明授权

US06575700B2 Steam turbine blade, and steam turbine and steam turbine power plant using the same 有权
公开(公告)号：US06575700B2
公开(公告)日：2003-06-10
申请号：US10102668
申请日：2002-03-22
申请人： Masahiko Arai , Shigeyoshi Nakamura , Takeshi Onoda , Masao Shiga
发明人： Masahiko Arai , Shigeyoshi Nakamura , Takeshi Onoda , Masao Shiga
IPC分类号： F01D514
CPC分类号： C22C38/001 , B23K9/04 , B23K35/3046 , C22C38/44 , C22C38/46 , C22C38/48 , C22C38/52 , C22C38/54 , F01D5/28 , F05D2300/171
摘要： A steam turbine blade made of a martensite steel having high strength and high toughness, and a low pressure steam turbine and a steam turbine power generating plant using the steam turbine blades. The steam turbine blade is made of a martensite steel containing C of 0.13-0.40%; Si less than 0.5%; Mn less than 1.5%; Ni of 2-3.5%; Cr of 8-13%; Mo of 1.5-4%; at least one kind of Nb and Ta of 0.02-0.3% in total; V of 0.05-0.35; and N of 0.04-0.15%.

10. 发明授权

US06182439B2 High and low pressure sides-integrating system turbine, long blades thereof and combined cycle power generation system 有权
标题翻译：高低压侧系统涡轮，长叶片和联合循环发电系统
公开(公告)号：US06182439B2
公开(公告)日：2001-02-06
申请号：US09385139
申请日：1999-08-31
申请人： Masao Siga , Takeshi Onoda , Shigeyoshi Nakamura , Ryo Hiraga
发明人： Masao Siga , Takeshi Onoda , Shigeyoshi Nakamura , Ryo Hiraga
IPC分类号： F01D528
CPC分类号： F01D5/142 , C22C38/001 , C22C38/46 , C22C38/48 , F01D5/141 , F01D5/28 , F05D2240/60 , F05D2300/171
摘要： A combined cycle power generation system in which a generator is driven by a steam turbine and a gas turbine includes a steam turbine rotor having a mono-block rotor shaft with blades mounted thereon in multi-stages from a high pressure side to a low pressure side and a casing covering the rotor. An inlet temperature of steam to first stage blades is not less than 530° C. and the rotor shaft is made of a Ni—Cr—Mo—V low alloy steel of bainitic structure having a higher creep rupture strength at the high pressure side than at the low pressure side and a 538° C. and 105 h creep rupture strength not less than 12 kg/mm2 at a central portion, and having mounted thereon at the central portion, first stage blades at the high pressure side or FATT of not more than 20° C. Final stage blades are mounted at the low pressure side having a room temperature V-notch impact value of not less than 4 kg/m, and blades of at least a final stage have a value of blade length in inches times revolution in rpm of not less than 125,000 and are made of martensite stainless steel including 8-13 wt. % Cr.
摘要翻译：发电机由蒸汽轮机和燃气轮机驱动的联合循环发电系统包括具有单块转子轴的汽轮机转子，该单块转子轴具有从高压侧到低压侧多级安装的叶片以及覆盖转子的壳体。第一级叶片的蒸汽入口温度不低于530℃，转子轴由高压侧具有较高蠕变断裂强度的贝氏体组织的Ni-Cr-Mo-V低合金钢制成，在低压侧，538℃和105h蠕变断裂强度在中心部分不小于12kg / mm2，并且在中心部分安装在其上，在高压侧的第一级叶片或不是FATT的FATT 超过20℃。最终级叶片安装在低压侧，其室温V形缺口冲击值不小于4kg / m，并且至少最后一级的叶片具有以英寸为单位的叶片长度的值转速不低于125,000 rpm，由马氏体不锈钢制成，包括8-13wt。％Cr。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式