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11. 发明授权

US07740202B2 Wing structure for aircraft 有权
标题翻译：机翼结构
公开(公告)号：US07740202B2
公开(公告)日：2010-06-22
申请号：US11978722
申请日：2007-10-30
申请人： Masaki Namaizawa , Kazuhide Hasegawa , Jun Nakazawa , Hirohide Azuma
发明人： Masaki Namaizawa , Kazuhide Hasegawa , Jun Nakazawa , Hirohide Azuma
IPC分类号： B64C3/18
CPC分类号： B64C3/18
摘要： In a wing structure for an aircraft, a rib extends in a chord direction for connecting spars to each other with upper and lower stringer through holes through which stringers of skins pass being formed in upper and lower edges of the rib. A bead is formed on the rib so as to extend between the upper and lower stringer through holes. Upper and lower ends of the bead are formed into arcuate shapes so as to surround the upper and lower stringer through holes, respectively. Thus, it is possible to enhance the buckling strength of the rib against a shear load acting on the wing of the aircraft.
摘要翻译：在用于飞行器的机翼结构中，肋沿着弦方向延伸，用于将翼梁相互连接，具有上和下纵梁通孔，桁条穿过该孔穿过肋条的上下边缘形成。在肋上形成一个珠，以便在上和下纵梁通孔之间延伸。胎圈的上端和下端分别形成为弓形形状，以分别围绕上下纵梁通孔。因此，可以增强肋对抗作用在飞机机翼上的剪切载荷的屈曲强度。

12. 发明申请

US20090015864A1 IMAGE-PROCESSING APPARATUS AND IMAGE-PROCESSING METHOD 失效
标题翻译：图像处理设备和图像处理方法
公开(公告)号：US20090015864A1
公开(公告)日：2009-01-15
申请号：US12171571
申请日：2008-07-11
申请人： Kazuhide Hasegawa
发明人： Kazuhide Hasegawa
IPC分类号： G06F3/12
CPC分类号： H04N1/32112 , G06F3/1212 , G06F3/1245 , G06F3/1285 , H04N2201/3205 , H04N2201/3226 , H04N2201/3242
摘要： An object-data item optimized for print settings is acquired from an image-processing apparatus and/or another image-processing apparatus, and intermediate data including a combination of plural object-data items including the acquired optimized object-data item is generated. The generated intermediate data is converted into bitmap data generated in pages so that intermediate data optimized for the print settings can be used in arbitrary objects. Therefore, printing and outputting can be performed by using the intermediate data with increased speed.
摘要翻译：从图像处理装置和/或其他图像处理装置获取针对打印设定优化的对象数据项，并且生成包括所获取的优化对象数据项的多个对象数据项的组合的中间数据。生成的中间数据被转换成页面中生成的位图数据，使得针对打印设置优化的中间数据可以用于任意对象。因此，可以通过使用具有增加的速度的中间数据来执行打印和输出。

13. 发明申请

US20080164376A1 Leading edge skin height difference adjusting structure and method of assembling leading edge skin 有权
标题翻译：前沿皮肤高差调整结构及前沿皮肤组装方法
公开(公告)号：US20080164376A1
公开(公告)日：2008-07-10
申请号：US11984539
申请日：2007-11-19
申请人： Hiroshi Kato , Ken Ohizumi , Kazuhide Hasegawa , Takahiro Kunichi
发明人： Hiroshi Kato , Ken Ohizumi , Kazuhide Hasegawa , Takahiro Kunichi
IPC分类号： B64C1/12
CPC分类号： B64C3/28 , Y10T29/49771
摘要： A plate material is formed into a height difference adjusting member having a J-shape such that its shim portion and resilient support portion are opposed to each other. The height difference adjusting member is mounted on a spar such that the shim portion and the resilient support portion are resiliently mounted to a flange of the spar. A rear end of a leading edge skin is fixed to the flange by a fastener in a state where the shim portion of the height difference adjusting member is interposed between the leading edge skin and the flange. The shim portion adjusts a difference in height between a front end of a main body skin and the rear end of the leading edge skin. Even if a large number of height difference adjusting members are mounted on the spar, the height difference adjusting members do not fall off and are not displaced.
摘要翻译：平板材料形成为具有J形的高度差调节构件，使得其垫片部分和弹性支撑部分彼此相对。高差差调节构件安装在翼梁上，使得垫片部分和弹性支撑部分弹性地安装在翼梁的凸缘上。前缘皮肤的后端通过紧固件固定在凸缘上，高度差调节件的垫片部分插在前缘皮肤和凸缘之间。垫片部分调节主体皮肤前端与前缘皮肤后端之间的高度差异。即使在翼梁上安装有大量的高差差调整构件，高差差调整构件也不脱落而不发生位移。

14. 发明申请

US20070266574A1 Shape Measurement Device and Method Thereof 有权
标题翻译：形状测量装置及方法
公开(公告)号：US20070266574A1
公开(公告)日：2007-11-22
申请号：US10598010
申请日：2004-09-15
申请人： Katsushi Ikeuchi , Kazuhide Hasegawa , Tomohito Masuda
发明人： Katsushi Ikeuchi , Kazuhide Hasegawa , Tomohito Masuda
IPC分类号： G01C3/02
CPC分类号： G01S17/89 , G01B11/24 , G01S7/4817
摘要： The present invention is a system for determining the three dimensional shape of an object, having a first measuring means for measuring a first distance and direction from a fixed first observation point to a first group of measurement points on an object, and a second measuring means for measuring a second distance and direction from a movable second observation point to a second group of measurement points on the aforementioned object, at least one point among said second group of measurement points being the same measurement point as at least one point among the aforementioned first group of measurement points, and said second group of measurement points including at least one measurement point not included in the aforementioned first group of measurement points, and further being provided with a calculating means for calculating the traveling velocity vector of the second observation point from the measurement results concerning the aforementioned same measurement point due to the first and second measuring means, correcting the aforementioned second measurement results based upon said traveling velocity vector, and calculating the three dimensional coordinates of the measurement points of the first group and the second group, and a displaying means that displays an image of the object based upon the aforementioned three dimensional coordinates.
摘要翻译：本发明是一种用于确定物体的三维形状的系统，具有用于测量从固定的第一观察点到物体上的第一组测量点的第一距离和方向的第一测量装置和第二测量装置用于测量从上述物体的可移动第二观察点到第二组测量点的第二距离和方向，所述第二组测量点中的至少一个点与上述第一测量点中的至少一个点相同的测量点测量点组，以及所述第二组测量点，其包括不包括在上述第一组测量点中的至少一个测量点，并且还设置有计算装置，用于从第一组测量点计算第二观测点的行进速度矢量，关于上述相同测量点的测量结果第一和第二测量装置，基于所述行进速度矢量校正上述第二测量结果，以及计算第一组和第二组的测量点的三维坐标，以及显示装置，显示基于对象的图像根据上述三维坐标。

15. 发明授权

US06593304B1 RECOMBINANT DNA COMPRISING DNA CODING FOR MYOSIN HEAVY CHAIN SM1 ISO-FORM PROTEIN INSERTED INTO VECTOR DNA MICROORGANISM CARRYING THE RECOMBINANT DNA, AND AN AGENT FOR TREATMENT OF ARTERIOSCLEROSIS COMPRISING THE RECOMBINANT DNA 失效
标题翻译：将包含MYOSIN重链SM1 ISO-FormM蛋白的DNA编码的重组DNA插入载体重组DNA的载体DNA微生物中，以及用于治疗包含重组DNA的病原体的代理
公开(公告)号：US06593304B1
公开(公告)日：2003-07-15
申请号：US08875435
申请日：1997-07-25
申请人： Kazuhide Hasegawa , Emi Arakawa , Shoji Oda , Yuzuru Matsuda , Katsuhito Takahashi , Michihiro Sugahara , Haruo Ishiyama
发明人： Kazuhide Hasegawa , Emi Arakawa , Shoji Oda , Yuzuru Matsuda , Katsuhito Takahashi , Michihiro Sugahara , Haruo Ishiyama
IPC分类号： C07H2100
CPC分类号： C07K14/4716 , A61K38/00
摘要： The present invention relates to recombinant DNA comprising DNA coding for smooth-muscle-type myosin heavy chain SM1 isoform protein inserted into vector DNA, a microorganism carrying the recombinant DNA, and an agent for treatment of arteriosclerosis comprising the recombinant DNA. The recombinant DNA of the present invention can be used effectively as an agent for gene therapy of restenosis after PTCA treatment.
摘要翻译：本发明涉及包含编码插入到载体DNA中的平滑肌型肌球蛋白重链SM1同种型蛋白质的DNA的重组DNA，携带重组DNA的微生物和包含该重组DNA的动脉硬化治疗剂。本发明的重组DNA可以有效地用作PTCA治疗后的再狭窄基因治疗剂。

16. 发明申请

US20130083544A1 LIGHT DIFFUSION FILM FOR LED LIGHTING 审中-公开
标题翻译： LED照明用光扩散膜
公开(公告)号：US20130083544A1
公开(公告)日：2013-04-04
申请号：US13637891
申请日：2011-03-18
申请人： Hidemasa Hosoda , Karin Kuroiwa , Hiroyuki Mori , Kazuhide Hasegawa
发明人： Hidemasa Hosoda , Karin Kuroiwa , Hiroyuki Mori , Kazuhide Hasegawa
IPC分类号： F21V11/00
CPC分类号： F21V11/00 , F21K9/68 , G02B5/0221 , G02B5/0226 , G02B5/0278
摘要： Provided is a light diffusion film for LED lighting that achieves a balance between concealment and light-utilization efficiency. The light diffusion film for LED lighting includes a sheet of substrate, an internal scattering layer and a surface shaping layer. The internal scattering layer contains a binder and particles; the mean particle diameter A of the particles is from 0.5 μm to 5.0 μm; the refractive index difference between the particles and the binder is from more than 0 to 0.15; and the content of the particles is from 10 parts by mass to 120 parts by mass with respect to 100 parts by mass of the binder.
摘要翻译：提供了一种用于LED照明的光扩散膜，其实现了隐蔽性和光利用效率之间的平衡。用于LED照明的光扩散膜包括基片，内部散射层和表面成形层。内部散射层含有粘合剂和颗粒; 颗粒的平均粒径A为0.5μm至5.0μm; 颗粒和粘合剂之间的折射率差异大于0至0.15; 相对于100质量份的粘合剂，粒子的含量为10质量份〜120质量份。

17. 发明申请

US20110299111A1 PRINTING SYSTEM, IMAGE FORMING APPARATUS, INFORMATION PROCESSING APPARATUS, AND PRINTING METHOD 审中-公开
标题翻译：打印系统，图像形成装置，信息处理装置和打印方法
公开(公告)号：US20110299111A1
公开(公告)日：2011-12-08
申请号：US13102987
申请日：2011-05-06
申请人： Kazuhide Hasegawa
发明人： Kazuhide Hasegawa
IPC分类号： G06K15/02
CPC分类号： G06F3/1293 , G06F3/1204 , G06F3/1228 , G06F3/1272 , G06F3/1288 , G06K15/007
摘要： An image forming apparatus which configures a printing system in which a server, comprises: a generation unit configured to generate, as plug-in information, information that associates a user interface provided by the image forming apparatus with the application provided by a server; a holding unit configured to hold the generated plug-in information; a sending unit configured to send the plug-in information to the information processing apparatus when the plug-in information has not been registered in an information processing apparatus; and a providing unit configured, when direct printing is designated, to provide, as the user interface to the information processing apparatus based on the plug-in information held by the holding unit, a direct print screen for accepting a print setting corresponding to the application that has generated print data to be printed.
摘要翻译：一种图像形成装置，其构成其中服务器的打印系统，包括：生成单元，被配置为生成将由所述图像形成装置提供的用户界面与由服务器提供的应用相关联的信息作为插件信息; 保持单元，被配置为保持所生成的插件信息; 发送单元，被配置为当所述插件信息尚未登记在信息处理装置中时，将所述插件信息发送到所述信息处理装置; 以及提供单元，其被配置为当指定直接打印时，基于由所述保持单元保存的插件信息，提供用于接受与所述应用相对应的打印设置的直接打印屏幕作为所述信息处理设备的用户界面已经生成要打印的打印数据。

18. 发明授权

US07938360B2 Main wing structure of aircraft 有权
标题翻译：飞机主翼结构
公开(公告)号：US07938360B2
公开(公告)日：2011-05-10
申请号：US11978717
申请日：2007-10-30
申请人： Jun Nakazawa , Kazuhide Hasegawa , Hirohide Azuma
发明人： Jun Nakazawa , Kazuhide Hasegawa , Hirohide Azuma
IPC分类号： B64B1/24 , B64C3/28
CPC分类号： B64D29/02 , B64C3/18 , B64C3/32 , B64D27/18
摘要： Plural regions are defined within a main wing by a plurality of spars and ribs. Of these regions, predetermined regions extending from a main wing connecting portion of the pylon to an internal space of a leading edge skin are used as wiring/piping accommodating chambers for collectively accommodating wiring and piping which provide communication between an engine and a fuselage, a predetermined region adjacent to parts of the wiring/piping accommodating chambers is used as a landing device accommodating chamber for accommodating a landing device and predetermined regions adjacent to other parts of the wiring/piping accommodating chambers are used as fuel tanks. Thus, the maintainability is improved as compared with the case where the wiring and the piping are distributed within the main wing. In addition, because the wiring/piping accommodating chambers are isolated from the landing device accommodating chamber and the fuel tanks, the operational reliability can be improved.
摘要翻译：多个区域通过多个翼梁和肋条限定在主翼内。在这些区域中，将从塔架的主翼连接部分延伸到前缘皮肤的内部空间的预定区域用作用于集体容纳提供发动机和机身之间的连通的布线和管道的布线/管道容纳室，使用与布线/管道容纳室的部分相邻的预定区域作为用于容纳着陆装置的着陆装置容纳室，并且将与布线/管道容纳室的其他部分相邻的预定区域用作燃料箱。因此，与布线和配管分布在主翼内的情况相比，可维护性提高。另外，由于布线/管道容纳室与着陆装置容纳室和燃料箱隔离，因此可以提高操作可靠性。

19. 发明申请

US20080149761A1 Main wing structure of aircraft 有权
标题翻译：飞机主翼结构
公开(公告)号：US20080149761A1
公开(公告)日：2008-06-26
申请号：US11978717
申请日：2007-10-30
申请人： Jun Nakazawa , Kazuhide Hasegawa , Hirohide Azuma
发明人： Jun Nakazawa , Kazuhide Hasegawa , Hirohide Azuma
IPC分类号： B64C3/00 , B64C3/32 , B64C3/18 , B64D27/00
CPC分类号： B64D29/02 , B64C3/18 , B64C3/32 , B64D27/18
摘要： Plural regions are defined within a main wing by a plurality of spars and ribs. Of these regions, predetermined regions extending from a main wing connecting portion of the pylon to an internal space of a leading edge skin are used as wiring/piping accommodating chambers for collectively accommodating wiring and piping which provide communication between an engine and a fuselage, a predetermined region adjacent to parts of the wiring/piping accommodating chambers is used as a landing device accommodating chamber for accommodating a landing device and predetermined regions adjacent to other parts of the wiring/piping accommodating chambers are used as fuel tanks. Thus, the maintainability is improved as compared with the case where the wiring and the piping are distributed within the main wing. In addition, because the wiring/piping accommodating chambers are isolated from the landing device accommodating chamber and the fuel tanks, the operational reliability can be improved.
摘要翻译：多个区域通过多个翼梁和肋条限定在主翼内。在这些区域中，将从塔架的主翼连接部分延伸到前缘皮肤的内部空间的预定区域用作用于集体容纳提供发动机和机身之间的连通的布线和管道的布线/管道容纳室，使用与布线/管道容纳室的部分相邻的预定区域作为用于容纳着陆装置的着陆装置容纳室，并且将与布线/管道容纳室的其他部分相邻的预定区域用作燃料箱。因此，与布线和配管分布在主翼内的情况相比，可维护性提高。另外，由于布线/管道容纳室与着陆装置容纳室和燃料箱隔离，因此可以提高操作可靠性。

20. 发明申请

US20080128552A1 Wing structure for aircraft 有权
标题翻译：机翼结构
公开(公告)号：US20080128552A1
公开(公告)日：2008-06-05
申请号：US11978722
申请日：2007-10-30
申请人： Masaki Namaizawa , Kazuhide Hasegawa , Jun Nakazawa , Hirohide Azuma
发明人： Masaki Namaizawa , Kazuhide Hasegawa , Jun Nakazawa , Hirohide Azuma
IPC分类号： B64C3/18
CPC分类号： B64C3/18
摘要： In a wing structure for an aircraft, a rib extends in a chord direction for connecting spars to each other with upper and lower stringer through holes through which stringers of skins pass being formed in upper and lower edges of the rib. A bead is formed on the rib so as to extend between the upper and lower stringer through holes. Upper and lower ends of the bead are formed into arcuate shapes so as to surround the upper and lower stringer through holes, respectively. Thus, it is possible to enhance the buckling strength of the rib against a shear load acting on the wing of the aircraft.
摘要翻译：在用于飞行器的机翼结构中，肋沿着弦方向延伸，用于将翼梁相互连接，具有上和下纵梁通孔，桁条穿过该孔穿过肋条的上下边缘形成。在肋上形成一个珠，以便在上和下纵梁通孔之间延伸。胎圈的上端和下端分别形成为弓形形状，以分别围绕上下纵梁通孔。因此，可以增强肋对抗作用在飞机机翼上的剪切载荷的屈曲强度。

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