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1. 发明专利

JP2008255429A Means for uniformalizing electrochemical etching 有权
标题翻译：用于均匀化电化学蚀刻的手段
公开(公告)号：JP2008255429A
公开(公告)日：2008-10-23
申请号：JP2007099612
申请日：2007-04-05
申请人： Japan Aerospace Exploration Agency , 独立行政法人宇宙航空研究開発機構
发明人： SAITO TOSHIHITO , ONO FUMIE , TAKEKOSHI MASAO , UEDA SHUICHI
IPC分类号： C25F7/00 , C25F3/08 , F02K7/14
摘要： PROBLEM TO BE SOLVED: To provide a method by which etching with excellent working accuracy as a whole can be applied by solving a failure where a peripheral part is etched more rapidly than a center part when the whole large surface or a groove structure with a certain pitch is etched.
SOLUTION: The method of uniformalizing the electrochemical etching is carried out by arranging a block of an insulating body on the outermost part of the part-to-be-worked surface of a panel in the electrochemical etching of a hole on the surface of the panel by applying voltage between the panel used as an anode and a cathode of a counter electrode in an aqueous solution tank.
COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：提供一种方法，通过在整个大表面或凹槽结构中通过解决周边部分被蚀刻得比中心部分更快地发生的故障，可以应用整体上具有优异加工精度的蚀刻刻有一定的间距。解决方案：电化学蚀刻均匀化的方法是通过在表面上的孔的电化学蚀刻中在面板的待加工表面的最外部布置绝缘体的块来进行的通过在用于阳极的面板和在水溶液罐中的对电极的阴极之间施加电压来施加电压。版权所有（C）2009，JPO＆INPIT

2. 发明专利

JP2007197785A Electrochemical etching performed in form of reaction liquid fluidized on working face 有权
标题翻译：在工作面上流动的反应液体形式的电化学蚀刻
公开(公告)号：JP2007197785A
公开(公告)日：2007-08-09
申请号：JP2006018464
申请日：2006-01-27
申请人： Japan Aerospace Exploration Agency , 独立行政法人宇宙航空研究開発機構
发明人： SAITO TOSHIHITO , UEDA SHUICHI , ONO FUMIE , TAKEKOSHI MASAO , HAYASAKA OSAMU
IPC分类号： C25F7/00
摘要： PROBLEM TO BE SOLVED: To provide an electrochemical etching method for metal, in which unexpected etching caused by the retainment of an aqueous solution is prevented so as to enable working in desired shape, and further, etching in complicated shape using no mask treatment is made possible.
SOLUTION: Regarding the electrochemical etching method for metal, in one embodiment, counter electrodes are arranged so as to be close to the surface of a work in planar mesh shape, and a reaction liquid injected from a nozzle arranged at the back thereof is atomized as fog, and in an another embodiment, counter electrodes are arranged in a nozzle flow passage, and a reaction liquid injected from a nozzle is injected like a beam so as to reach the surface of a work, in a spot shape.
COPYRIGHT: (C)2007,JPO&INPIT
摘要翻译：要解决的问题：为了提供金属的电化学蚀刻方法，其中防止了由保持水溶液引起的意外蚀刻，以使得能够以期望的形状进行工作，并且还使用无掩模的复杂形状的蚀刻治疗是可能的。解决方案：关于金属的电化学蚀刻方法，在一个实施例中，相对电极被布置成接近平面网状的工件的表面，并且从布置在其后面的喷嘴喷射的反应液作为雾化雾化，在另一实施方式中，对置电极配置在喷嘴流路中，从喷嘴喷射的反应液注入光束，从而以点状到达工件的表面。版权所有（C）2007，JPO＆INPIT

3. 发明专利

JP2010209380A Method for forming ceramic film and base material with ceramic film 有权
标题翻译：用陶瓷膜形成陶瓷膜和基材的方法
公开(公告)号：JP2010209380A
公开(公告)日：2010-09-24
申请号：JP2009054953
申请日：2009-03-09
申请人： Japan Aerospace Exploration Agency , Tohoku Univ , 国立大学法人東北大学 , 独立行政法人宇宙航空研究開発機構
发明人： OGAWA KAZUHIRO , SAYAR MEHDI , SEO DOWON , TAKEKOSHI MASAO , UEDA SHUICHI , ONO FUMIE , SAITO TOSHIHITO
IPC分类号： C23C24/04 , F01D5/28 , F01D25/00 , F02C7/00 , G21C5/00
CPC分类号： Y02E30/40
摘要： PROBLEM TO BE SOLVED: To provide a method for forming a ceramic film capable of imparting satisfactory high temperature oxidation resistance to a base material. SOLUTION: The method for forming the ceramic film is characterized in that the ceramic film having ≥99 mass% ceramic content is formed by using a spray powder made of ceramic particles having ≥99 mass% ceramic content to film-form the spray powder by a cold spray method. COPYRIGHT: (C)2010,JPO&INPIT
摘要翻译：要解决的问题：提供一种能够对基材赋予令人满意的高温抗氧化性的陶瓷膜的形成方法。＆lt; P＆gt;解决方案：陶瓷膜的形成方法的特征在于，陶瓷含量≥99质量％的陶瓷膜通过使用陶瓷粒子含量≥99质量％的陶瓷颗粒制成的喷雾粉末形成喷雾粉末用冷喷雾法。版权所有（C）2010，JPO＆INPIT

4. 发明专利

JP2009041418A Air-breathing engine for space transport and method of improving its accelerating performance 审中-公开
标题翻译：用于空间运输的空气呼吸发动机及其提高其性能的方法
公开(公告)号：JP2009041418A
公开(公告)日：2009-02-26
申请号：JP2007206150
申请日：2007-08-08
申请人： Japan Aerospace Exploration Agency , 独立行政法人宇宙航空研究開発機構
发明人： ONO FUMIE , TAKEKOSHI MASAO , SAITO TOSHIHITO , UEDA SHUICHI
IPC分类号： F02K7/18 , C10L1/00 , C10L1/04 , F02K9/42
摘要： PROBLEM TO BE SOLVED: To reduce the size of a space transport equipped with air-breathing engines.
SOLUTION: A hydrocarbon compound of a high density is loaded beforehand as a fuel source of the RBCC engines and is chemically changed into different fuel forms optimum to the respective engines while cooling respective engine walls by the fuel source, and the respective reaction products are used for combustion as fuel of the respective engines, so that the size reduction of the space transport equipped with the air-breathing engines such as the RBCC engines, reduction of air resistance and reduction of a weight of an airframe structure become attainable and accelerating performance is suitably improved.
COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：减少装备有空气呼吸发动机的空间运输的大小。解决方案：预先加载高密度的烃化合物作为RBCC发动机的燃料源，并且通过燃料源将相应的发动机壁冷却，同时化学地改变为对各发动机最佳的不同的燃料形式，并且各自的反应产品用于燃烧作为相应发动机的燃料，使得配备有诸如RBCC发动机的空气呼吸发动机的空间运输的尺寸减小，空气阻力的降低和机体结构的重量的降低变得可以实现，适当提高加速性能。版权所有（C）2009，JPO＆INPIT

5. 发明专利

JP2008101534A Effusion cooling rocket combustor 审中-公开
标题翻译：消防冷却油罐车
公开(公告)号：JP2008101534A
公开(公告)日：2008-05-01
申请号：JP2006284587
申请日：2006-10-19
申请人： Japan Aerospace Exploration Agency , 独立行政法人宇宙航空研究開発機構
发明人： ONO FUMIE , TAKEKOSHI MASAO , SAITO TOSHIHITO , UEDA SHUICHI
IPC分类号： F02K9/64
摘要： PROBLEM TO BE SOLVED: To provide an effusion cooling rocket combustor minimizing deterioration in performance by distributing and supplying the optimum amount of a coolant according to the heat load distribution of a combustion chamber by a simple method, and providing improved durability, a simplified structure, a reduced weight, and a reduced cost.
SOLUTION: A permeation flow flux q
cool of the coolant specified as K
liner ×ΔP/t is set to conform with the heat load distribution of the combustion chamber by changing the thickness of a liner by using a C/C composite material simultaneously having permeability, excellent heat resistance and excellent high temperature strength as a material for a combustion chamber liner 22 and a nozzle liner 32 or by utilizing impregnation/coating of silica glass or anisotropy of transmissivity of the C/C composite material.
COPYRIGHT: (C)2008,JPO&INPIT
摘要翻译：要解决的问题：通过简单的方法，通过根据燃烧室的热负荷分布分配和供应最佳量的冷却剂来提供最小化性能降低的喷射冷却火箭燃烧器，并且提供改善的耐久性，简化结构，减轻重量，降低成本。
解决方案：设定为K 内衬×ΔP/ t的冷却剂的渗透流量q 冷却设定为符合燃烧室的热负荷分布通过使用同时具有渗透性，优异的耐热性和优异的高温强度的C / C复合材料来改变衬里的厚度，作为用于燃烧室衬套22和喷嘴衬垫32的材料或通过利用石英玻璃的浸渍/涂覆或 C / C复合材料的透射率各向异性。版权所有（C）2008，JPO＆INPIT

6. 发明专利

JP2010064099A Joining method of cylindrical object by brazing or diffusion bonding 审中-公开
标题翻译：通过烧结或扩散接合接合圆柱体的方法
公开(公告)号：JP2010064099A
公开(公告)日：2010-03-25
申请号：JP2008231889
申请日：2008-09-10
申请人： Japan Aerospace Exploration Agency , Kinzoku Giken Kk , 独立行政法人宇宙航空研究開発機構 , 金属技研株式会社
发明人： SAITO TOSHIHITO , TAKEKOSHI MASAO , ONO FUMIE , UEDA SHUICHI , YAMASHITA SATOSHI
IPC分类号： B23K3/00 , B23K1/00 , B23K20/00 , B23K20/24 , F02K9/62
摘要： PROBLEM TO BE SOLVED: To provide a new hot joining method for integrating an inner cylinder and an outer cylinder made of metal and concentrically overlapped without requiring large-scale facilities in an HIP method, and also to provide a method enabling joining of materials having high rigidity. SOLUTION: The joining method of an inner cylindrical member and an outer cylindrical member comprises a step for processing the outer surface of the inner cylindrical member to be bonded into a design shape, a step for mounting a brazing material on the outer surface of the inner cylindrical member, a step for fitting the inner cylindrical member in the outer cylindrical member to be bonded, a step for covering the outer cylindrical member with a holder comprising a C/C material, a step for heating the inner cylindrical member, the outer cylindrical member, and the holder which are in a nested state to a temperature above the melting temperature of the brazing material and applying contacting pressure caused by the difference of thermal expansions of the inner cylindrical member, the outer cylindrical member, and the holder, and a step for taking out the members from the holder after cooling them. COPYRIGHT: (C)2010,JPO&INPIT
摘要翻译：要解决的问题：为了提供一种新的热连接方法，用于将由金属制成的内圆筒和外圆筒整合在一起，而不需要HIP方法中的大规模设备，并且还提供一种能够连接高刚性材料解决方案：内圆柱形构件和外圆柱形构件的接合方法包括用于加工要被接合为设计形状的内圆柱形构件的外表面的步骤，用于将钎焊材料安装在外表面上的步骤内圆柱形构件的一个步骤，用于将内圆柱形构件安装在待接合的外圆柱形构件中的步骤，用包括C / C材料的保持件覆盖外圆柱形构件的步骤，用于加热内圆筒构件的步骤，所述外圆柱形构件和所述保持器处于嵌套状态，其温度高于所述钎焊材料的熔化温度，并施加由所述内圆柱形构件，所述外圆筒构件和所述保持器的热膨胀差引起的接触压力，以及冷却后从持有人中取出成员的步骤。版权所有（C）2010，JPO＆INPIT

7. 发明专利

JP2007120316A Regenerative cooling system of combined cycle engine 有权
标题翻译：组合循环发动机再生冷却系统
公开(公告)号：JP2007120316A
公开(公告)日：2007-05-17
申请号：JP2005309576
申请日：2005-10-25
申请人： Japan Aerospace Exploration Agency , 独立行政法人宇宙航空研究開発機構
发明人： SAITO TOSHIHITO , UEDA SHUICHI , ONO FUMIE , TAKEKOSHI MASAO
IPC分类号： F02K7/18
摘要： PROBLEM TO BE SOLVED: To provide a regenerative cooling system of a combined cycle engine capable of supplying fuel as a coolant optimal for a flying condition.
SOLUTION: When a heat receiving quantity received from the combined cycle engine CE to hydrogen as the coolant and fuel is lower than a design value, the temperature of the hydrogen flowing in a fuel supply line 2 is raised by mixing a part of the hydrogen heated by flowing inside a heat exchanger 4 with low temperature hydrogen while being pressurized by a second pump 11 by a return line 9. The temperature of the hydrogen flowing in the fuel supply line 2 can also be adjusted to an optional value by changing the mixing ratio of the low temperature hydrogen and the heated hydrogen by controlling a flow rate of the returning heated hydrogen by a second flow regulating valve 10.
COPYRIGHT: (C)2007,JPO&INPIT
摘要翻译：要解决的问题：提供一种组合循环发动机的再生冷却系统，其能够提供作为飞行状态最佳的冷却剂的燃料。解决方案：当从联合循环发动机CE接收到的氢作为冷却剂和燃料的热量低于设计值时，在燃料供应管线2中流动的氢气的温度通过混合一部分氢气通过在具有低温氢气的热交换器4内流动而被加热，同时由第二泵11通过返回管线9加压。在燃料供应管线2中流动的氢气的温度也可以通过改变通过第二流量调节阀10控制返回的加热氢气的流量来控制低温氢气和加热的氢气的混合比例。（C）2007，JPO＆INPIT

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