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1. 发明授权

US06245283B1 Method for production of fiber-bond type ceramic material and engine parts formed thereof 失效
标题翻译：纤维粘结型陶瓷材料的制造方法和由其形成的发动机零件
公开(公告)号：US06245283B1
公开(公告)日：2001-06-12
申请号：US09159581
申请日：1998-09-24
申请人： Shouju Masaki , Takemi Yamamura , Tetsurou Hirokawa , Takeshi Tanamura
发明人： Shouju Masaki , Takemi Yamamura , Tetsurou Hirokawa , Takeshi Tanamura
IPC分类号： C04B3580
CPC分类号： C04B35/645 , C04B35/803
摘要： A fiber-bond type ceramic material 4 is produced by using as raw material fibers 1 inorganic fibers of Si—M—C—O synthesized by melt spinning polycarbosilane, then infusibilizing the produced threads, and firing the set threads, forming from the raw material fibers a woven fabric 2 having all the fibers thereof extended perpendicularly or obliquely relative to the direction of compression during the course of a hot-press fabrication at a weaving step 12, heat-treating the woven fabric in the air, thereby preparing a woven fabric of oxidized fibers 3 provided with an oxide layer on the surface thereof at an oxidizing step 14, and subjecting the woven fabric of oxidized fibers to a hot-press fabrication while compressing the fabric in the direction of the compression thereby causing the oxide layers on the surface to adhere fast to each other and form a matrix at a hot-press step 16.
摘要翻译：通过使用通过熔融纺丝聚碳硅烷合成的Si-MCO的无机纤维作为原料纤维1，然后使所生产的线材熔化，并且对原料纤维进行焙烧，从而制成纤维粘合型陶瓷材料4， 2，在织造步骤12的热压制造过程中，其全部纤维相对于压缩方向垂直或倾斜延伸，对空气中的织物进行热处理，由此制备氧化纤维3的织物在氧化步骤14的表面上设置有氧化物层，并且在压缩织物的方向上对氧化纤维的织物进行热压制造，同时压缩织物，从而使表面上的氧化物层快速粘附并在热压步骤16形成基质。

2. 发明授权

US07114319B2 Unidirectional long fiber three dimensional fiber structure produced by short fiber intertwining and production method thereof 有权
公开(公告)号：US07114319B2
公开(公告)日：2006-10-03
申请号：US10407865
申请日：2003-04-04
申请人： Hideki Sakonjo , Masayasu Ishibashi , Tetsuro Hirokawa , Takeshi Tanamura , Koichi Hashimoto
发明人： Hideki Sakonjo , Masayasu Ishibashi , Tetsuro Hirokawa , Takeshi Tanamura , Koichi Hashimoto
IPC分类号： D02G3/02
CPC分类号： B29C70/24 , B29C70/32 , B29C70/50 , D04H3/105 , Y10T428/23943
摘要： A unidirectional three dimensional fiber structure is provided which does not require weaving, displays a high level of interlayer strength and does not suffer from cracking, and which can also be easily produced with any arbitrary cross-section. A unidirectional three dimensional fiber structure is produced by inserting a plurality of long fibers which have been aligned unidirectionally into an inlet at one end of a cylindrical die with a plurality of needle holes in the peripheral walls thereof, and then performing needlepunch through the needle holes while drawing the plurality of long fibers out from an outlet at the opposite end of the cylindrical die.

3. 发明申请

US20120024866A1 PRESSURE VESSEL AND METHOD OF MANUFACTURING THE SAME 有权
标题翻译：压力容器及其制造方法
公开(公告)号：US20120024866A1
公开(公告)日：2012-02-02
申请号：US13087495
申请日：2011-04-15
申请人： Tetsuya Ozawa , Nozomu Kawasetsu , Kentaro Shindo , Mitsuru Kondo , Akira Fukushima , Masayasu Ishibashi , Takeshi Tanamura , Kazuo Nakajima , Hiroshi Sakai , Tetsuro Hirokawa
发明人： Tetsuya Ozawa , Nozomu Kawasetsu , Kentaro Shindo , Mitsuru Kondo , Akira Fukushima , Masayasu Ishibashi , Takeshi Tanamura , Kazuo Nakajima , Hiroshi Sakai , Tetsuro Hirokawa
IPC分类号： F17C1/06 , B65H81/02
CPC分类号： B29C70/088 , B29C53/588 , B29C70/32 , B29L2031/7156 , F17C1/00 , F17C1/06 , F17C2201/0133 , F17C2201/056 , F17C2203/0619 , F17C2203/0665 , F17C2203/0668 , F17C2203/067 , F17C2209/2154 , F17C2221/033 , F17C2223/0123 , F17C2223/036 , F17C2260/011 , F17C2270/0178 , Y10T156/10
摘要： Provided is a toroidal pressure vessel having extremely high pressure resistance. Laminating latitudinal reinforcing fiber layers (32) enables to improve a strength in a latitudinal direction of a pressure vessel (1). Moreover, putting reinforcing fibers (32a) constituting those laminated latitudinal reinforcing fiber layers (32) in continuity enables to further improve the strength in the latitudinal direction of the pressure vessel (1), for example compared with a case where the reinforcing fibers are divided for each layer.
摘要翻译：提供具有极高耐压性的环形压力容器。层压横向增强纤维层（32）能够提高压力容器（1）的纬向强度。此外，与构成层叠的纬向增强纤维层（32）的增强纤维（32a）连续地形成，例如与增强纤维分割的情况相比，能够进一步提高压力容器（1）的纬向强度对于每一层

4. 发明授权

US07138167B2 Preform precursor for fiber-reinforced composite material, preform for fiber-reinforced composite material, and method of manufacturing the precursor and the preform 有权
标题翻译：纤维增强复合材料用预成型体前体，纤维增强复合材料用预成型体以及前体和预成型体的制造方法
公开(公告)号：US07138167B2
公开(公告)日：2006-11-21
申请号：US10489860
申请日：2002-08-12
申请人： Hideki Sakonjo , Masayasu Ishibashi , Takeshi Tanamura , Koichi Hashimoto , Tetsuro Hirokawa
发明人： Hideki Sakonjo , Masayasu Ishibashi , Takeshi Tanamura , Koichi Hashimoto , Tetsuro Hirokawa
IPC分类号： B32B5/12
CPC分类号： B29B11/16 , Y10T156/1043 , Y10T428/218 , Y10T428/24074
摘要： A preform for a fiber-reinforced composite material including a bent portion along a curved line for bending, a flange portion corresponding to an outer circumferential portion, and a semi-cylindrical portion formed by bending an inner circumferential portion along the curved line for bending located in a flat plane or a curved plane region. The preform is formed from a precursor having a predetermined extension. The outer circumferential portion corresponds to a first region where a first plurality of reinforced fibers is partially disposed in parallel along the curved line for bending. The inner circumferential portion corresponds to a second region constituted solely of a second plurality of reinforced fibers disposed throughout the entire area, so as to intersect the first plurality of reinforced fibers at a predetermined angle in the first region.
摘要翻译： 1.一种纤维增强复合材料用预成型体，其特征在于，具有弯曲弯曲部，弯曲部的弯曲部，与外周部相对应的凸缘部，以及沿着曲线的内周部弯曲弯曲而形成的半圆筒部，在平面或曲面区域。预成型件由具有预定延伸部的前体形成。外周部对应于第一区域，其中第一多根增强纤维沿着弯曲部分平行地部分地设置以进行弯曲。内周部分对应于仅由设置在整个区域中的第二多个增强纤维构成的第二区域，以便在第一区域中以预定角度与第一多根增强纤维相交。

5. 发明申请

US20050042410A1 Preform precursor for fiber-reinforced composite material, preform for fiber-reinforced composite material, and method of manufacturing the precursor and the preform 有权
标题翻译：纤维增强复合材料用预成型体前体，纤维增强复合材料用预成型体以及前体和预成型体的制造方法
公开(公告)号：US20050042410A1
公开(公告)日：2005-02-24
申请号：US10489860
申请日：2002-08-12
申请人： Hideki Sakonjo , Masayasu Ishibashi , Takeshi Tanamura , Koichi Hashimoto , Tetsuro Hirokawa
发明人： Hideki Sakonjo , Masayasu Ishibashi , Takeshi Tanamura , Koichi Hashimoto , Tetsuro Hirokawa
IPC分类号： B29B11/16 , C08J5/04 , C08L101/00 , D04H1/46 , B32B5/12
CPC分类号： B29B11/16 , Y10T156/1043 , Y10T428/218 , Y10T428/24074
摘要： Technical Field of the Invention: A structural member required to have a prescribed strength in an aircraft, an automobile, a vessel or a constructed structure, etc., especially in a circular bore portion or a curved portion such as a wing or a body of an aircraft. Technical Problem: A preform for a fiber-reinforced composite material to be used as a structural member of a fiber-reinforced composite material having a curved portion is to be manufactured through a low-cost mass production. Means of Solving the Problem A preform for a fiber-reinforced composite material (20) including a bent portion (22) along a curved line for bending (12), a flange portion (24) corresponding to an outer circumferential portion (14) and a semi-cylindrical portion (26) formed by bending an inner circumferential portion (16), based on a precursor of a preform for a fiber-reinforced composite material (10) provided with the curved line for bending (12) located in a flat plane or a curved plane region having a predetermined extension; the outer circumferential portion (14) corresponding to a region (a) where a plurality of reinforced fibers is partly disposed in parallel along the curved line for bending (12), and the inner circumferential portion (16) corresponding to the section (b) constituted solely of another plurality of reinforced fibers disposed throughout the entire area, so as to intersect the former plurality of reinforced fibers at a predetermined angle in the region (a). Principal Use: An aircraft, an automobile, a vessel, a constructed structure, etc. Especially a window frame or a fuel inlet of an aircraft.
摘要翻译：技术领域本发明涉及一种在航空器，汽车，船舶或构造结构等中具有规定强度的结构构件，特别是在圆形孔部分或弯曲部分，例如机翼或主体一架飞机技术问题：作为具有弯曲部分的纤维增强复合材料的结构构件的纤维增强复合材料的预成型体将通过低成本的批量生产来制造。解决问题的方案用于纤维增强复合材料（20）的预成型件包括沿弯曲曲线的弯曲部分（22），与外周部分（14）对应的凸缘部分（24）和基于用于纤维增强复合材料（10）的预成型体的前体，弯曲内圆周部分（16）形成的半圆柱形部分（26），其设置有位于平面中的弯曲曲线（12）平面或具有预定延伸部的曲面区域; 对应于多个增强纤维沿弯曲曲线部分平行设置的区域（a）的外圆周部分（14）和对应于部分（b）的内圆周部分（16）仅由设置在整个区域的另外多个增强纤维构成，以便在区域（a）中以预定的角度与前面的多根增强纤维相交。主要用途：飞机，汽车，船舶，建筑结构等。特别是飞机的窗框或燃料入口。

6. 发明授权

US08991641B2 Pressure vessel and method of manufacturing the same 有权
标题翻译：压力容器及其制造方法
公开(公告)号：US08991641B2
公开(公告)日：2015-03-31
申请号：US13087495
申请日：2011-04-15
申请人： Tetsuya Ozawa , Nozomu Kawasetsu , Kentaro Shindo , Mitsuru Kondo , Akira Fukushima , Masayasu Ishibashi , Takeshi Tanamura , Kazuo Nakajima , Hiroshi Sakai , Tetsuro Hirokawa
发明人： Tetsuya Ozawa , Nozomu Kawasetsu , Kentaro Shindo , Mitsuru Kondo , Akira Fukushima , Masayasu Ishibashi , Takeshi Tanamura , Kazuo Nakajima , Hiroshi Sakai , Tetsuro Hirokawa
IPC分类号： F17C1/06 , B29C70/08 , B29C53/58 , B29C70/32 , B29L31/00
CPC分类号： B29C70/088 , B29C53/588 , B29C70/32 , B29L2031/7156 , F17C1/00 , F17C1/06 , F17C2201/0133 , F17C2201/056 , F17C2203/0619 , F17C2203/0665 , F17C2203/0668 , F17C2203/067 , F17C2209/2154 , F17C2221/033 , F17C2223/0123 , F17C2223/036 , F17C2260/011 , F17C2270/0178 , Y10T156/10
摘要： A toroidal pressure vessel having extremely high pressure resistance has laminated latitudinal reinforcing fiber layers to improve a strength in a latitudinal direction of the pressure vessel. Moreover, putting reinforcing fibers constituting those laminated latitudinal reinforcing fiber layers in continuity enables further improvement of strength in the latitudinal direction of the pressure vessel, for example compared with a case where the reinforcing fibers are divided for each layer.
摘要翻译：具有极高耐压性的环形压力容器具有层叠的纬向增强纤维层，以提高压力容器的纬向强度。此外，与将层叠的纬向增强纤维层的增强纤维连续地连接起来，能够进一步提高压力容器的纬向强度，例如与增强纤维分割为各层的情况相比。

7. 发明授权

US07384585B2 Method for producing dry preform for composite material 有权
标题翻译：生产复合材料干燥预制件的方法
公开(公告)号：US07384585B2
公开(公告)日：2008-06-10
申请号：US10448449
申请日：2003-05-28
申请人： Masayasu Ishibashi , Koichi Hashimoto , Hideki Sakonjo , Akira Iriguchi , Kazunori Morimoto , Takeshi Tanamura , Tetsuro Hirokawa
发明人： Masayasu Ishibashi , Koichi Hashimoto , Hideki Sakonjo , Akira Iriguchi , Kazunori Morimoto , Takeshi Tanamura , Tetsuro Hirokawa
IPC分类号： B29C45/14
CPC分类号： B29C70/222 , B29B11/16 , B29C70/207
摘要： A novel process for producing a dry preform for a composite material takes advantage of the fact that a reinforcing filament assembly, when consisting of a fiber reinforcement layer a, formed by stringing a first set of parallel strands of fiber reinforcement over a part or all of the plane within any desired shape along the straight axis 2, and a fiber reinforcement layer b, formed by stringing a second set of parallel strands of fiber reinforcement over the plane at an angle θ with respect to the straight axis 2, such that 0°
摘要翻译：用于生产用于复合材料的干燥预成型件的新颖方法利用以下事实：增强丝组件，当由纤维增强层a组成时，通过将第一组平行的纤维增强纤维束穿过部分或全部沿着直轴2的任何期望形状的平面以及纤维增强层b，其通过在平面上以相对于直轴2的角度θ的方式将第二组平行的纤维增强纤维股线拉成，使得0° 仅仅由纤维增强材料b构成的增强丝组件的部分可根据需要变形。根据该方法，使用如图1和图2所示的纤维增强线夹具将纤维增强体的绳股c串起。图8（A）和图8（B）。通过诸如缝合之类的简单手段将纤维增强物的串联的层组合在一起。然后将整合的层成形为增强细丝组件3,4，其被组合以形成干预制体1，用于制造具有任何期望的纤维增强对准的复合材料。

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