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1. 发明授权

US08904804B2 Overspeed protection apparatus for gas turbine engine 有权
标题翻译：燃气轮机超速保护装置
公开(公告)号：US08904804B2
公开(公告)日：2014-12-09
申请号：US12861300
申请日：2010-08-23
申请人： Makoto Tezuka , Koji Fukutomi
发明人： Makoto Tezuka , Koji Fukutomi
IPC分类号： F02C9/46 , F02C9/00 , F02G3/00 , F02C9/28
CPC分类号： F02C9/28 , F05D2270/021 , F05D2270/3013
摘要： In an overspeed protection apparatus for a gas turbine engine having a turbine rotated by combustion gas injected from a combustion chamber to drive a compressor, a fuel shutoff valve to shut off fuel to be supplied to the engine and a controller controlling operation of the fuel shutoff valve based on a turbine rotational speed to protect the turbine from overspeed, an outlet pressure of the compressor is detected and compared with a threshold value when a shutoff command is outputted, and the fuel shutoff valve is determined to be failed when the detected pressure is not less than the threshold value, thereby enabling to promptly detect the fuel shutoff valve failure without additional installing sensor, thereby enhancing the reliability.
摘要翻译：在具有由从燃烧室喷射的燃烧气体旋转以驱动压缩机的涡轮机的燃气轮机的超速保护装置中，用于切断供给发动机的燃料的燃料截止阀和控制燃料切断操作的控制器基于涡轮转速以保护涡轮机不超速，在输出关闭指令时检测压缩机的出口压力并将其与阈值进行比较，并且当检测到的压力为检测压力时，确定燃料截止阀失效不低于阈值，从而能够在没有附加安装传感器的情况下迅速检测燃料截止阀故障，从而提高可靠性。

2. 发明授权

US09556800B2 Control apparatus for aeroplane gas turbine engine 有权
标题翻译：飞机燃气轮机发动机控制装置
公开(公告)号：US09556800B2
公开(公告)日：2017-01-31
申请号：US12861292
申请日：2010-08-23
申请人： Makoto Tezuka
发明人： Makoto Tezuka
IPC分类号： F02C9/46 , F01D21/02 , F01D21/14 , F02C9/40
CPC分类号： F02C9/46 , F01D21/02 , F01D21/14 , F02C9/40 , F05D2270/56
摘要： An apparatus for controlling an aeroplane gas turbine engine has various sensors and devices for operating the engine, and two control channels each calculating a command value for controlling operation of the engine based on signals outputted from the sensors. In each of the control channels, it is determined whether any of the sensors and devices is abnormal based on the signals to determine a failure level of the control channel concerned with a numerical value. The failure level is compared with that of the other control channel and based thereon, the command value calculated by the control channel of smaller failure level is sent to the devices. With this, even when both control channels are failed, the engine control can be continued with taking the failure level into account.
摘要翻译：用于控制飞机燃气涡轮发动机的装置具有用于操作发动机的各种传感器和装置，以及两个控制通道，每个控制通道基于从传感器输出的信号计算用于控制发动机的运行的命令值。在每个控制通道中，基于用于确定与数值有关的控制信道的故障等级的信号，确定传感器和设备中的任一个是否异常。将故障等级与其他控制信道的故障等级进行比较，基于此，由故障级别较小的控制信道计算出的命令值发送到设备。由此，即使在两个控制通道都失败的情况下，可以考虑故障等级来继续发动机控制。

3. 发明申请

US20110046863A1 CONTROL APPARATUS FOR AEROPLANE GAS TURBINE ENGINE 有权
标题翻译：机载涡轮发动机的控制装置
公开(公告)号：US20110046863A1
公开(公告)日：2011-02-24
申请号：US12861292
申请日：2010-08-23
申请人： Makoto Tezuka
发明人： Makoto Tezuka
IPC分类号： G06F19/00
CPC分类号： F02C9/46 , F01D21/02 , F01D21/14 , F02C9/40 , F05D2270/56
摘要： An apparatus for controlling an aeroplane gas turbine engine has various sensors and devices for operating the engine, and two control channels each calculating a command value for controlling operation of the engine based on signals outputted from the sensors. In each of the control channels, it is determined whether any of the sensors and devices is abnormal based on the signals to determine a failure level of the control channel concerned with a numerical value. The failure level is compared with that of the other control channel and based thereon, the command value calculated by the control channel of smaller failure level is sent to the devices. With this, even when both control channels are failed, the engine control can be continued with taking the failure level into account.
摘要翻译：用于控制飞机燃气涡轮发动机的装置具有用于操作发动机的各种传感器和装置，以及两个控制通道，每个控制通道基于从传感器输出的信号计算用于控制发动机的运行的命令值。在每个控制通道中，基于用于确定与数值有关的控制信道的故障等级的信号，确定传感器和设备中的任一个是否异常。将故障等级与其他控制信道的故障等级进行比较，基于此，由故障级别较小的控制信道计算出的命令值发送到设备。由此，即使在两个控制通道都失败的情况下，可以考虑故障等级来继续发动机控制。

4. 发明申请

US20110041512A1 OVERSPEED PROTECTION APPARATUS FOR GAS TURBINE ENGINE 有权
标题翻译：燃气轮机发动机过载保护装置
公开(公告)号：US20110041512A1
公开(公告)日：2011-02-24
申请号：US12861300
申请日：2010-08-23
申请人： Makoto Tezuka , Koji Fukutomi
发明人： Makoto Tezuka , Koji Fukutomi
IPC分类号： F02C9/28
CPC分类号： F02C9/28 , F05D2270/021 , F05D2270/3013
摘要： In an overspeed protection apparatus for a gas turbine engine having a turbine rotated by combustion gas injected from a combustion chamber to drive a compressor, a fuel shutoff valve to shut off fuel to be supplied to the engine and a controller controlling operation of the fuel shutoff valve based on a turbine rotational speed to protect the turbine from overspeed, an outlet pressure of the compressor is detected and compared with a threshold value when a shutoff command is outputted, and the fuel shutoff valve is determined to be failed when the detected pressure is not less than the threshold value, thereby enabling to promptly detect the fuel shutoff valve failure without additional installing sensor, thereby enhancing the reliability
摘要翻译：在具有由从燃烧室喷射的燃烧气体旋转以驱动压缩机的涡轮机的燃气轮机的超速保护装置中，用于切断供给发动机的燃料的燃料截止阀和控制燃料切断操作的控制器基于涡轮转速以保护涡轮机不超速，在输出关闭指令时检测压缩机的出口压力并将其与阈值进行比较，并且当检测到的压力为检测压力时，确定燃料截止阀失效不低于阈值，从而能够在没有附加安装传感器的情况下及时检测燃料截止阀故障，从而提高可靠性

5. 发明授权

US06432858B1 Process for the regeneration of hydration catalyst for cyclic olefins 失效
标题翻译：环烯烃水合催化剂再生方法
公开(公告)号：US06432858B1
公开(公告)日：2002-08-13
申请号：US09463382
申请日：2000-01-27
申请人： Makoto Tezuka
发明人： Makoto Tezuka
IPC分类号： B01J2034
CPC分类号： B01J38/12 , B01J29/90 , B01J38/00 , B01J38/70
摘要： This invention relates to a method for regenerating a cyclic olefin hydration catalyst, in which a solid acid catalyst is regenerated after its use in a hydration reaction of a cyclic olefin by mixing a water phase containing the solid acid catalyst and an oil phase containing the cyclic olefin and thereby effecting the reaction, which comprises separating the reaction solution into oil phase and water phase at a temperature of 40° C. or more and subsequently subjecting at least a portion of the solid acid catalyst in the separated water phase to a regeneration treatment. According to the method of this invention, a catalyst used in the hydration of a cyclic olefin can be separated and regenerated efficiently, and it is a particularly suitable catalyst regeneration method for a case in which hydration of a cyclic olefin is carried out for a prolonged period of time by repeating regeneration and use of the catalyst again and again.
摘要翻译：本发明涉及一种再生环烯烃水合催化剂的方法，其中固体酸催化剂在使用后通过将含有固体酸催化剂的水相和含有环状烯烃的油相混合在环状烯烃的水合反应中而再生烯烃，从而进行反应，其包括在40℃或更高的温度下将反应溶液分离成油相和水相，随后将至少一部分在分离的水相中的固体酸催化剂进行再生处理。根据本发明的方法，用于环烯烃水合的催化剂可以有效地分离和再生，并且是一种特别合适的催化剂再生方法，其中环状烯烃的水合进行延长一次又一次地重复再生和使用催化剂的时间。

6. 发明授权

US4687047A Continuous casting method 失效
标题翻译：连铸法
公开(公告)号：US4687047A
公开(公告)日：1987-08-18
申请号：US892075
申请日：1986-08-01
申请人： Shigeaki Ogibayashi , Mamoru Yamada , Tatsuo Mukai , Makoto Tezuka , Masazumi Hirai
发明人： Shigeaki Ogibayashi , Mamoru Yamada , Tatsuo Mukai , Makoto Tezuka , Masazumi Hirai
IPC分类号： B22D11/12 , B22D11/00
CPC分类号： B22D11/1206 , Y10T29/49991
摘要： A method of the continuous casting of molten metal by continuously withdrawing a strand is disclosed. The method is characterized in that the thickness of the strand is continuously reduced at a rate of 0.5 mm/min to less than 2.5 mm/min in the region between the point of time when the center of the strand has a temperature corresponding to a solid-phase ratio being within the range of 0.1 to 0.3 and the point of time when said temperature has dropped to a level corresponding to the solid-phase ratio at the limit of fluidization, while substantially no reduction in thickness is effected in the region between the point of time when the center of the strand has a temperature corresponding to the solid-phase ratio at the limit of fluidization and the point of time when said temperature has dropped to the solidus line.
摘要翻译：公开了一种通过连续抽出股线连续铸造熔融金属的方法。该方法的特征在于，在线的中心具有对应于固体的温度的时间点之间的区域中，股线的厚度以0.5mm / min的速率连续地减小到小于2.5mm / min 相位比在0.1〜0.3的范围内，并且当所述温度下降到与流化极限时的固相比相对应的水平的时间点，而在实质上没有减小厚度的区域线的中心具有与流化极限下的固相比相对应的温度以及所述温度下降到固相线时的时间点。

7. 发明申请

US20070055435A1 Control system for gas turbine aeroengine 有权
标题翻译：燃气轮机航空发动机控制系统
公开(公告)号：US20070055435A1
公开(公告)日：2007-03-08
申请号：US11431560
申请日：2006-05-11
申请人： Hironori Muramatsu , Yuichi Hattori , Makoto Tezuka
发明人： Hironori Muramatsu , Yuichi Hattori , Makoto Tezuka
IPC分类号： G06F19/00
CPC分类号： F02C7/22 , F02C9/263 , F02C9/28 , F05D2260/80 , F05D2270/094 , F05D2270/301 , F05D2270/3011 , F05D2270/303 , F05D2270/304
摘要： In a gas turbine aeroengine control system, in Ch-A (first control channel), a first CPU monitors the operation of a second CPU and the second CPU monitors the operation of the first CPU; in Ch-B (second control channel), third and fourth CPUs similarly monitor each other, and when the operation of at least one of the first and second CPUs in Ch-A is found not to be normal, the output sent to an FCU (fuel control unit) is switched from the output of one or the other of the first and second CPUs of Ch-A to the output of one or the other of the third and fourth CPUs of Ch-B, thereby achieving improved CPU failure detection and realizing high redundancy and high reliability.
摘要翻译：在燃气轮机航空发动机控制系统中，在Ch-A（第一控制通道）中，第一CPU监视第二CPU的运行，第二CPU监视第一CPU的运行; 在Ch-B（第二控制信道）中，第三和第四CPU类似地彼此监视，并且当发现Ch-A中的第一和第二CPU中的至少一个的操作被发现不正常时，发送到FCU （燃料控制单元）从Ch-A的第一和第二CPU的一个或另一个的输出切换到Ch-B的第三和第四CPU中的一个或另一个的输出，从而实现改进的CPU故障检测实现高冗余，高可靠性。

8. 发明授权

US07840336B2 Control system for gas turbine aeroengine 有权
标题翻译：燃气轮机航空发动机控制系统
公开(公告)号：US07840336B2
公开(公告)日：2010-11-23
申请号：US11431560
申请日：2006-05-11
申请人： Hironori Muramatsu , Yuichi Hattori , Makoto Tezuka
发明人： Hironori Muramatsu , Yuichi Hattori , Makoto Tezuka
IPC分类号： G06F19/00
CPC分类号： F02C7/22 , F02C9/263 , F02C9/28 , F05D2260/80 , F05D2270/094 , F05D2270/301 , F05D2270/3011 , F05D2270/303 , F05D2270/304
摘要： In a gas turbine aeroengine control system, in Ch-A (first control channel), a first CPU monitors the operation of a second CPU and the second CPU monitors the operation of the first CPU; in Ch-B (second control channel), third and fourth CPUs similarly monitor each other, and when the operation of at least one of the first and second CPUs in Ch-A is found not to be normal, the output sent to an FCU (fuel control unit) is switched from the output of one or the other of the first and second CPUs of Ch-A to the output of one or the other of the third and fourth CPUs of Ch-B, thereby achieving improved CPU failure detection and realizing high redundancy and high reliability.
摘要翻译：在燃气轮机航空发动机控制系统中，在Ch-A（第一控制通道）中，第一CPU监视第二CPU的运行，第二CPU监视第一CPU的运行; 在Ch-B（第二控制信道）中，第三和第四CPU类似地彼此监视，并且当发现Ch-A中的第一和第二CPU中的至少一个的操作被发现不正常时，发送到FCU （燃料控制单元）从Ch-A的第一和第二CPU的一个或另一个的输出切换到Ch-B的第三和第四CPU中的一个或另一个的输出，从而实现改进的CPU故障检测实现高冗余，高可靠性。

9. 发明授权

US5900482A Process for the preparation of .epsilon.-caprolactam 失效
标题翻译：制备ε-己内酰胺的方法
公开(公告)号：US5900482A
公开(公告)日：1999-05-04
申请号：US820095
申请日：1997-03-19
申请人： Kouji Teramoto , Yu Kanda , Makoto Tezuka , Toshio Uchibori , Hidefumi Sano
发明人： Kouji Teramoto , Yu Kanda , Makoto Tezuka , Toshio Uchibori , Hidefumi Sano
IPC分类号： C07D201/04
CPC分类号： C07D201/04
摘要： The present invention provides a method for producing .epsilon.-caprolactam, which comprises subjecting cyclohexene to a hydration reaction to obtain cyclohexanol, subjecting the cyclohexanol to a dehydrogenation reaction to obtain cyclohexanone, subjecting the cyclohexanone to an oxime-forming reaction to obtain cyclohexanone oxime, and subjecting the cyclohexanone oxime to a Beckmann rearrangement reaction to obtain .epsilon.-caprolactam, wherein methylcyclopentanones contained in the cyclohexanone subjected to the oxime-forming reaction are controlled to be not more than 400 ppm.According to the present invention, it is possible to produce .epsilon.-caprolactam having a quality not inferior to conventional quality at a low cost.
摘要翻译：本发明提供了ε-己内酰胺的制造方法，其包括使环己烯进行水合反应得到环己醇，使环己醇进行脱氢反应得到环己酮，使环己酮进行肟形成反应，得到环己酮肟，使环己酮肟进行贝克曼重排反应，得到ε-己内酰胺，其中将进行了肟形成反应的环己酮中所含的甲基环戊酮控制为不大于400ppm。根据本发明，可以以低成本生产质量不劣于常规质量的ε-己内酰胺。

10. 发明授权

US5855696A Ultra low carbon, cold rolled steel sheet and galvanized steel sheet having improved fatigue properties and processes for producing the same 失效
标题翻译：具有改善的疲劳特性的超低碳冷轧钢板和镀锌钢板及其制造方法
公开(公告)号：US5855696A
公开(公告)日：1999-01-05
申请号：US737909
申请日：1997-03-19
申请人： Makoto Tezuka , Kohsaku Ushioda , Shiro Fujii , Atsushi Itami , Yasuharu Sakuma , Tatsuo Yokoi
发明人： Makoto Tezuka , Kohsaku Ushioda , Shiro Fujii , Atsushi Itami , Yasuharu Sakuma , Tatsuo Yokoi
IPC分类号： C21D8/04 , C22C38/00 , C22C38/06 , C22C38/12 , C22C38/14 , C23C2/02 , C23C2/06 , C23C2/40 , C22C38/04
CPC分类号： C22C38/12 , C21D8/0436 , C22C38/001 , C22C38/06 , C22C38/14 , C23C2/02 , C23C2/06 , C23C2/40 , C21D8/0426 , C21D8/0473 , C21D8/0478
摘要： The cold rolled steel sheet or galvanized steel sheet comprises by weight C: 0.0001 to 0.0026%, Si: not more than 1.2%, Mn: 0.03 to 3.0%, P: 0.015 to 0.15%, S: 0.0010 to 0.020%, Al: 0.005 to 0.1%, N: 0.0005 to 0.0080% and B: 0.0003 to 0.0030% with the balance consisting of Fe and unavoidable impurities. A process for producing the above steel sheet is also provided which comprises the steps of: performing hot roll finishing of a slab having the above chemical composition at the Ar.sub.3 transformation point or above; preferably, then cooling the hot rolled strip, within 1.5 sec after the completion of the hot rolling, to 750.degree. C. at a rate of not less than 50.degree. C./sec; coiling the strip in the temperature range of from room temperature to 750.degree. C.; cold rolling the coiled strip a reduction ratio of not less than 70%; subjecting the cold rolled strip to continuous annealing at 600.degree. to 900.degree. C. or to continuous galvanizing by the sendzimer method; and performing temper rolling with a reduction ratio of not less than 1.5.times.(1-400.times.C) % and not less than 2080.times.(C - 0.0015) wherein C represents the carbon content in % by weight.
摘要翻译： PCT No.PCT / JP96 / 00805 Sec。 371日期1997年3月19日 102（e）1997年3月19日PCT PCT 1996年3月27日PCT公布。出版物WO96 / 30555 日期：1996年10月3日冷轧钢板或镀锌钢板以C：0.0001〜0.0026％，Si：1.2％以下，Mn：0.03〜3.0％，P：0.015〜0.15％，S：0.0010〜 0.020％，Al：0.005〜0.1％，N：0.0005〜0.0080％，B：0.0003〜0.0030％，余量由Fe和不可避免的杂质构成。还提供了一种生产上述钢板的方法，其包括以下步骤：在Ar 3相变点或更高温度下进行具有上述化学组成的板坯的热轧精加工; 优选在热轧结束后的1.5秒内将热轧带材冷却至750℃以上，不低于50℃/秒; 在室温至750℃的温度范围内卷取带材; 冷轧卷取钢带的减速比不小于70％; 使冷轧带材在600〜900℃下进行连续退火，或通过sendzimer法连续镀锌; 并且以不小于1.5×（1-400×℃）％且不小于2080×（C-0.0015）的还原率进行调质轧制，其中C表示碳含量以重量％计。

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