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1. 发明授权

US08715556B2 Gas turbine engine blade for aircraft and manufacturing method thereof 有权
标题翻译：用于飞机的燃气涡轮发动机叶片及其制造方法
公开(公告)号：US08715556B2
公开(公告)日：2014-05-06
申请号：US12934339
申请日：2009-03-27
申请人： Tsutomu Murakami , Hideo Morita , Takahiro Ogi , Ikuo Okumura , Katsuyoshi Moriya
发明人： Tsutomu Murakami , Hideo Morita , Takahiro Ogi , Ikuo Okumura , Katsuyoshi Moriya
IPC分类号： B23P15/02
CPC分类号： F01D5/282 , B29C70/30 , B29C70/46 , B29D99/0025 , B29K2105/0872 , B29L2031/082 , B29L2031/087 , F01D5/141 , F04D29/023 , F04D29/324 , F04D29/388 , F05D2230/26 , F05D2300/43 , F05D2300/603 , Y02T50/672 , Y02T50/673 , Y10T29/49336
摘要： A gas turbine engine blade for aircraft which has a 3-dimensional blade surface shape twisted around a center line at an angle of 45 degrees or more and 70 degrees or less, wherein the aforementioned blade is provided with multiple composite material prepregs which contain reinforced fiber and which are integrally molded after being laminated in the thickness direction, and the aforementioned reinforced fiber runs continuously without interruption within each layer of the aforementioned composite material prepregs.
摘要翻译：一种用于飞行器的燃气涡轮发动机叶片，其具有以45度以上且70度以下的角度绕中心线扭转的3维叶片表面形状，其中，所述刀片设置有多个复合材料预浸料，其包含增强纤维并且在厚度方向层叠后一体成型，上述复合材料预浸料的各层内的上述增强纤维连续地不间断地延伸。

2. 发明授权

US07058945B2 Information processing method and recording medium therefor capable of enhancing the executing speed of a parallel processing computing device 有权
标题翻译：信息处理方法及其记录介质能够提高并行处理计算装置的执行速度
公开(公告)号：US07058945B2
公开(公告)日：2006-06-06
申请号：US09838166
申请日：2001-04-20
申请人： Katsumi Ichinose , Katsuyoshi Moriya
发明人： Katsumi Ichinose , Katsuyoshi Moriya
IPC分类号： G06F9/46
CPC分类号： G06F9/5066 , G06F2209/5017
摘要： There is provided an information processing method which enhances the executing speed of a parallel processing computing device. A parallel processing block-forming step divides a program to be executed into a plurality of parallel processing blocks. A thread-forming step divides parallel processing blocks formed by the parallel processing block-forming step into a plurality of threads corresponding in number to the processors of a processor group. The processor group executes the threads generated by the thread-forming step. The instructing step instructs each of the processors to execute a thread of a next parallel processing block when it has terminated execution of a thread assigned thereto, and when a predetermined instruction is not given in the program.
摘要翻译：提供了一种提高并行处理计算装置的执行速度的信息处理方法。并行处理块形成步骤将要执行的程序划分成多个并行处理块。线程形成步骤将由并行处理块形成步骤形成的并行处理块划分成与处理器组的处理器相对应的多个线程。处理器组执行由线程形成步骤产生的线程。指示步骤指示每个处理器执行下一个并行处理块的线程，当终止执行分配给其的线程时，以及当程序中未给出预定指令时。

3. 发明授权

US06725448B1 System to optimally create parallel processes and recording medium 失效
标题翻译：系统最佳地创建并行进程和记录介质
公开(公告)号：US06725448B1
公开(公告)日：2004-04-20
申请号：US09715178
申请日：2000-11-20
申请人： Katsuyoshi Moriya , Katsumi Ichinose
发明人： Katsuyoshi Moriya , Katsumi Ichinose
IPC分类号： G06F944
CPC分类号： G06F9/4843 , G06F9/5027 , G06F2209/5018
摘要： An optimizing system, method and computer readable recording medium to increase the speed of parallel processing by allowing a mixture of automatic creation of parallel processes and OpenMP API processing and to prevent reduction in performance during parallel processing by controlling the generation of wasted threads when automatic parallel processing and OpenMP API call each other. The optimizing system, method and recording medium create object code that creates parallel processes from a source program coded in a specific programming language, wherein the program is performed using a plurality of threads. The optimizing system generates object code for a source program which is executed in parallel by generating a plurality of threads. The optimizing device includes a thread management system to store in a memory information regarding the respective threads created, a first parallel processing system to generate code to create a plurality of threads corresponding to notation in the source program for repetitive processes for which there is no instruction for the creation of parallel processes, and a second parallel process creation system to generate code to create threads after referencing information by the thread management system corresponding to the notation for processes for which parallel processing is specified in the source program.
摘要翻译：一种优化系统，方法和计算机可读记录介质，通过允许混合自动创建并行进程和OpenMP API处理来提高并行处理的速度，并通过在自动并行时控制浪费线程的产生来防止并行处理中的性能降低处理和OpenMP API调用对方。优化系统，方法和记录介质创建从以特定编程语言编码的源程序创建并行进程的目标代码，其中使用多个线程来执行该程序。优化系统生成通过生成多个线程并行执行的源程序的目标代码。所述优化装置包括线程管理系统，用于存储关于所创建的相应线程的信息的第一并行处理系统，用于生成与源程序中的符号相对应的多个线程，用于不存在指令的重复处理用于创建并行进程，以及第二并行进程创建系统，用于生成代码以在由对源程序中指定并行处理的进程的符号对应的线程管理系统引用信息之后创建线程。

4. 发明申请

US20110020130A1 GAS TURBINE ENGINE BLADE FOR AIRCRAFT AND MANUFACTURING METHOD THEREOF 有权
标题翻译：用于飞机的燃气涡轮发动机叶片及其制造方法
公开(公告)号：US20110020130A1
公开(公告)日：2011-01-27
申请号：US12934339
申请日：2009-03-27
申请人： Tsutomu Murakami , Hideo Morita , Takahiro Ogi , Ikuo Okumura , Katsuyoshi Moriya
发明人： Tsutomu Murakami , Hideo Morita , Takahiro Ogi , Ikuo Okumura , Katsuyoshi Moriya
IPC分类号： F04D29/38 , B23P15/02
CPC分类号： F01D5/282 , B29C70/30 , B29C70/46 , B29D99/0025 , B29K2105/0872 , B29L2031/082 , B29L2031/087 , F01D5/141 , F04D29/023 , F04D29/324 , F04D29/388 , F05D2230/26 , F05D2300/43 , F05D2300/603 , Y02T50/672 , Y02T50/673 , Y10T29/49336
摘要： A gas turbine engine blade for aircraft which has a 3-dimensional blade surface shape twisted around a center line at an angle of 45 degrees or more and 70 degrees or less, wherein the aforementioned blade is provided with multiple composite material prepregs which contain reinforced fiber and which are integrally molded after being laminated in the thickness direction, and the aforementioned reinforced fiber runs continuously without interruption within each layer of the aforementioned composite material prepregs.
摘要翻译：一种用于飞行器的燃气涡轮发动机叶片，其具有以45度以上且70度以下的角度绕中心线扭转的3维叶片表面形状，其中，所述刀片设置有多个复合材料预浸料，其包含增强纤维并且在厚度方向层叠后一体成型，上述复合材料预浸料的各层内的上述增强纤维连续地不间断地延伸。

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