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1. 发明专利

JP2004330943A Artificial satellite joint mechanism, spacecraft with the same, and control method 有权
公开(公告)号：JP2004330943A
公开(公告)日：2004-11-25
申请号：JP2003131191
申请日：2003-05-09
申请人： Kawasaki Heavy Ind Ltd , Natl Space Development Agency Of Japan , 宇宙開発事業団 , 川崎重工業株式会社
发明人： ODA MITSUSHIGE , KONO ISAO , UENO HIROSHI , HORIE YOICHI , KUBOTA NOBUYUKI , KAGAYA HIROAKI , MORIYAMA TAKASHI
IPC分类号： B64G1/64
摘要： PROBLEM TO BE SOLVED: To provide an artificial satellite joint mechanism capable of effectively establishing a rendezvous docking with a non-cooperative target satellite launched in the past, and to provide an spacecraft with the same and control method. SOLUTION: A cylindrical frame structure such as PAF I/F (Payload Attach Fitting Interface) 70 that many artificial satellites served as a target satellite have as a common structure is held by oscillating opening/closing operation of two arm members 105, 105 provided with compliance mechanisms 107, 107, thereby capturing a target satellite softly. The PAF I/F 70 which is held is drawn to the service satellite side along with the arm members 25, 25 by a ball screw mechanism 103, and the end face of the PAF I/F 70 is brought into contact with the connection surface (damper plate 111) of the service satellite, thereby rigidly connecting the target satellite. COPYRIGHT: (C)2005,JPO&NCIPI

2. 发明专利

JP2004191423A Retroreflective body 审中-公开
公开(公告)号：JP2004191423A
公开(公告)日：2004-07-08
申请号：JP2002355859
申请日：2002-12-06
申请人： Kawasaki Heavy Ind Ltd , Natl Space Development Agency Of Japan , 宇宙開発事業団 , 川崎重工業株式会社
发明人： KONO ISAO , MOKUNO MASAAKI , SAKATA TAKASHI , KUBOTA NOBUYUKI , ATSUTA TOSHIO , SAKURAI TAKASHI
IPC分类号： G02B5/122
摘要： PROBLEM TO BE SOLVED: To reflect incident light in a comparatively wide region by mitigating retroreflection characteristics.
SOLUTION: A retroreflective body 35 is composed to combine a plurality of μ-CCRs 34. μ-CCR 34 is a triangular pyramid, and the inside of three sides of the triangular pyramid is reflective faces 12-14. Angles α, β and γ making mutually adjacent reflective faces are chosen from the angle separated from 90°. An opening part 16 is formed oppositely to an intersection point 15 of the three reflective faces 12-14, the plurality of μ-CCRs 34 have the opening part arranged on a similar plane, and an arrangement pitch P is chosen so that optical defractive characteristic is optimum. Incident light 18 emitted from the opening part 16 reflects on the three reflective faces 12-14, and emits to six directions inclined at only an angle of ϕ to the incident light 18 from the opening part 16, and since reflective light 19 has broadening due to defractive characteristics, a broadening angle θ to the incident direction of the reflective light 19 is a comparatively wide angle θ4.
COPYRIGHT: (C)2004,JPO&NCIPI

3. 发明专利

JP2003306200A Image navigation for rendezvous docking and navigation device 有权
标题翻译：用于RENDEZVOUS DOCKING和NAVIGATION DEVICE的图像导航
公开(公告)号：JP2003306200A
公开(公告)日：2003-10-28
申请号：JP2002111841
申请日：2002-04-15
申请人： Kawasaki Heavy Ind Ltd , Natl Space Development Agency Of Japan , 宇宙開発事業団 , 川崎重工業株式会社
发明人： KONO ISAO , ISHIJIMA YOSHIYUKI , YOKOO ATSUSHI , ENOMOTO MASAYUKI , KANAMARU TAKAO , KUBOTA NOBUYUKI
IPC分类号： B64G1/64 , B64G1/24 , B64G1/66 , G06T7/60
摘要： PROBLEM TO BE SOLVED: To provide an image navigation for a rendezvous docking and navigation device allowing a non-cooperative target satellite having no special marker launched in the past to effectively navigate at rendezvous docking (RVD) by moving a service satellite so as to approach a place, as a target, having an annular satellite-common structure such as a satellite frame part of a target satellite and corresponding to an object portion to be docked. SOLUTION: Image of the target satellite 2 is picked up including the satellite frame part 21 by the service satellite 1, relative distance between the service satellite 1 and the target satellite 2 is measured, relative position of the satellite frame part 21 for the service satellite 1 is calculated, and the satellite frame part 21 in the picked up image is recognized as at least either an ellipse or a circular arc. Thereby, relative attitude of the satellite frame part 21 for the service satellite 1 is calculated, and the service satellite 1 is moved so as for the satellite frame part 21 in the picked up image to be close to a circle on the basis of the calculated relative position and relative attitude. COPYRIGHT: (C)2004,JPO
摘要翻译：要解决的问题：提供用于会合对接和导航装置的图像导航，允许不具有过去发射的特殊标记的非合作目标卫星通过移动服务卫星而在会合对接（RVD）中有效地导航作为目标接近具有诸如目标卫星的卫星帧部分的环形卫星共同结构并对应于待对接的对象部分的地方。解决方案：由服务卫星1拾取包括卫星帧部分21的目标卫星2的图像，测量服务卫星1和目标卫星2之间的相对距离，卫星帧部分21的相对位置用于计算服务卫星1，将拍摄图像中的卫星帧部21识别为椭圆或圆弧中的至少一个。由此，计算出服务卫星1的卫星帧部21的相对姿态，并且，服务卫星1被移动，使得所拾取图像中的卫星帧部21基于计算出的卫星帧部21接近圆相对位置和相对态度。版权所有（C）2004，JPO

4. 发明专利

JP2014042996A Method of manufacturing thermal protection composite material and thermal protection composite material 有权
标题翻译：制备热保护复合材料和热保护复合材料的方法
公开(公告)号：JP2014042996A
公开(公告)日：2014-03-13
申请号：JP2012185003
申请日：2012-08-24
申请人： Denpa Gakuen , 学校法人電波学園 , Kawasaki Heavy Ind Ltd , 川崎重工業株式会社
发明人： OKUYAMA KEIICHI , OYA HIROAKI , KUBOTA NOBUYUKI , SASAYAMA HIROYUKI , TANAKA HIROYUKI , SHIMADA NAOKI , ONO MICHIO
IPC分类号： B29C43/32 , B29C43/12 , B29C43/20 , B29K101/10 , B29K105/08 , B64G1/58
摘要： PROBLEM TO BE SOLVED: To easily manufacture a laminated ablator with a larger area than that of the conventional one without impairing excellent lightness and heat resistance.SOLUTION: A method of manufacturing a thermal protection composite material comprises the steps of: impregnating felt-like reinforced fibers 32, for instance, with a thermosetting resin 31 to obtain a composite material sheet 30; forming a laminate 20 by laminating a plurality of the composite material sheets 30; superimposing and mounting a plate-shaped molding jig on the laminate 20, and then adjusting the thickness; and subsequently heating and pressurizing the laminate 20 with an autoclave. Thereby, a laminated ablator 10 is obtained, which is the thermal protection composite material.
摘要翻译：要解决的问题：容易地制造具有比常规面积大的面积的层压消融器，而不损害优异的耐光性和耐热性。解决方案：制造热保护复合材料的方法包括以下步骤：浸渍毡状增强纤维32，例如用热固性树脂31，以获得复合材料片30; 通过层叠多个复合材料片30来形成层压体20; 将板状成型夹具叠加并安装在层叠体20上，然后调整厚度; 随后用高压釜加热和加压叠层20。由此，获得作为热保护复合材料的层叠消融器10。

5. 发明专利

JP2014228025A デバイス固定装置およびこれを備えるデバイス有权
标题翻译：装置固定装置和具有该装置的装置
公开(公告)号：JP2014228025A
公开(公告)日：2014-12-08
申请号：JP2013106347
申请日：2013-05-20
申请人：独立行政法人宇宙航空研究開発機構 , Japan Aerospace Exploration Agency , 独立行政法人宇宙航空研究開発機構 , 川崎重工業株式会社 , Kawasaki Heavy Ind Ltd
发明人： NAKANISHI HIROKI , KAWAMOTO TOSHIMI , NITTA YOSHIMI , KUBOTA NOBUYUKI , ENOMOTO MASAYUKI
IPC分类号： F16B17/00 , B64G1/64
摘要：【課題】低コストかつ簡素な構成で、任意の物体に任意のデバイスを固定することが可能な、デバイス固定装置等を提供する。【解決手段】デバイス固定装置10は、例えばスペースデブリ除去デバイス20に取り付けられ、前方向に伸展する伸展部11と、伸展部11の前端に取り付けられ、スペースデブリが備えるPAFの内部に挿入される係合部12とを備えている。係合部12は複数の突出部材13と、これら突出部材13を放射状に配置した状態で伸展部11の前端に固定する突出部材固定部材14とを備えている。係合部12は、突出部材13が収納状態にあるときには、当該係合部12全体がPAF(空洞部)の開口よりも小さくなるように構成され、また、伸展部11の伸展によりPAFの開口内に挿入された後には、突出部材13を収納状態から突出状態に移行させるよう構成されている。【選択図】図1
摘要翻译：要解决的问题：提供一种成本低廉且结构简单且能够将任意装置固定在任意物体上的装置固定装置等。装置固定装置10包括：延伸部分11，其附接到空间碎片去除装置20，并且向前延伸; 以及附接到延伸部分11的前端并插入空间碎片的PAF（有效载荷连接配件）中的接合部分12。接合部12包括多个突出构件13和突出构件固定构件14，突出构件固定构件14将突出构件13固定到延伸部11的前端，同时突出构件13径向布置。接合部12构成为：当突出部件13处于收纳状态时，整体卡合部12变得比PAF的开口小于空腔部）; 并且在通过延伸部11的延伸将接合部12插入到PAF的开口中之后，突出构件13可以从存储状态转变到突出状态。

6. 发明专利

JP2014226974A 伸展バネを用いたスペースデブリ除去デバイス固定装置、並びに、これを備えるスペースデブリ除去デバイス有权
标题翻译：使用延伸弹簧的空间去除装置保持器及其相同的空间去除装置
公开(公告)号：JP2014226974A
公开(公告)日：2014-12-08
申请号：JP2013106348
申请日：2013-05-20
申请人：川崎重工業株式会社 , Kawasaki Heavy Ind Ltd
发明人： KUBOTA NOBUYUKI , ENOMOTO MASAYUKI
IPC分类号： B64G1/64 , B64G1/56
摘要：【課題】低コストかつ簡素な構成で、スペースデブリにスペースデブリ除去デバイスを固定することが可能な、デバイス固定装置およびこれを備えるスペースデブリ除去デバイスを提供する。【解決手段】スペースデブリ除去デバイス固定装置10は、少なくとも伸展バネ13で構成される伸展部11と、この伸展部11の前端に取り付けられ、放射状に配置された複数本の伸展バネ13を備える係合部12と、これら伸展バネ13を収納状態で保持し、その保持を解除することにより収納状態から突出状態に復帰させるバネ状態切換部と、を備えている。伸展部11の伸展バネ13が伸展することにより、スペースデブリのPAFの開口内に係合部12を挿入し、その後に、係合部12の伸展バネ13が伸展することにより、PAF内に係合部12が係合される。【選択図】図1
摘要翻译：要解决的问题：提供一种具有简单且低成本结构并可将空间碎片清除装置固定到空间碎片的装置保持器，以及具有装置保持器的空间碎片清除装置。解决方案：空间碎片移除装置保持器10 包括：由至少一个拉伸弹簧13构成的延伸部分11; 一个接合部分12，其被连接到延伸部分11的前端并包括径向设置的多个拉伸弹簧13; 以及弹簧状态切换部，其将这些拉伸弹簧13保持在收容状态，并且通过松开拉伸弹簧13的保持将延伸部13从收纳状态返回到突出状态。卡合部12插入到通过延伸部分11的延伸弹簧13延伸的空间碎片的PAF（有效负载连接配件），然后延伸弹簧13延伸，从而接合部分12与PAF的内部接合。

7. 发明专利

JP2010119958A Heat-resistant carbon dioxide absorbing material and method of manufacturing the same, and carbon dioxide absorbing method using the material and carbon dioxide absorbing apparatus 有权
标题翻译：耐热二氧化碳吸收材料及其制造方法以及使用二氧化碳吸收材料和二氧化碳吸收装置的二氧化碳吸收方法
公开(公告)号：JP2010119958A
公开(公告)日：2010-06-03
申请号：JP2008296374
申请日：2008-11-20
申请人： Kawasaki Heavy Ind Ltd , 川崎重工業株式会社
发明人： SHOJI KIYOTOSHI , SHIIZAKI SHINJI , KUBOTA NOBUYUKI
IPC分类号： B01D53/62 , B01J20/22
CPC分类号： Y02A50/2342 , Y02C10/04 , Y02C10/06
摘要： PROBLEM TO BE SOLVED: To provide a heat-resistant carbon dioxide absorbing material stably demonstrating removal performance of carbon dioxide over a long period, even if carbon dioxide is separated at high temperature, and to provide a method of manufacturing the material. SOLUTION: An aqueous solution of an amine compound and an aqueous solution of a deliquescent compound are each prepared, a porous substance is added to the aqueous solution of the amine compound and aqueous solution of the deliquescent compound to adsorb the amine compound and deliquescent compound. The porous substances are each dried to obtain the carbon dioxide absorbing material and a cooling material, and by mixing the carbon dioxide absorbing material with the cooling material, the heat-resistant carbon dioxide absorbing material is obtained. COPYRIGHT: (C)2010,JPO&INPIT
摘要翻译：解决的问题：即使二氧化碳在高温下分离，也能够长时间稳定地显示二氧化碳的除去性能的耐热二氧化碳吸收材料，并提供制造该材料的方法。解决方案：制备胺化合物的水溶液和潮解化合物的水溶液，向胺化合物的水溶液和潮解化合物的水溶液中加入多孔物质以吸附胺化合物和潮解化合物。各多孔物质被干燥以获得二氧化碳吸收材料和冷却材料，并且通过将二氧化碳吸收材料与冷却材料混合，获得耐热二氧化碳吸收材料。版权所有（C）2010，JPO＆INPIT

8. 发明专利

JP2013119163A Method for producing two-layer ablator 有权
标题翻译：用于生产两层挤压机的方法
公开(公告)号：JP2013119163A
公开(公告)日：2013-06-17
申请号：JP2011266463
申请日：2011-12-06
申请人： Kawasaki Heavy Ind Ltd , 川崎重工業株式会社
发明人： OYA HIROAKI , KUBOTA NOBUYUKI
IPC分类号： B32B5/28 , B64G1/58
摘要： PROBLEM TO BE SOLVED: To provide a method for producing a two-layer ablator, with which the two-layer ablator corresponding to the size of a capsule or the like can be produced, even when the size of the capsule or the like for re-entry into the atmosphere becomes large.SOLUTION: The method for producing the two-layer ablator 100 which includes an outer layer ablator 1 and an inner layer ablator 2 comprising prepreg cloth, includes the steps of: disposing a prepreg sheet obtained by impregnating a first fiber with a first resin and forming ablator members corresponding to divided ones of the outer layer ablator 1 by hot press; disposing the ablator members and the prepreg cloth which is located in the inside of the ablator members and is obtained by impregnating a second fiber that is longer than the first fiber with a second resin to form a laminate; and subjecting the ablator members and the prepreg cloth to co-cure molding in an autoclave to integrally mold the outer layer ablator 1 and the inner layer ablator 2.
摘要翻译：要解决的问题：为了提供一种制造双层消融器的方法，通过该方法可以产生与胶囊等的尺寸相对应的双层消融器，即使胶囊的尺寸或喜欢重入大气变大。解决方案：包括外层消融器1和包括预浸布的内层消融器2的双层消融器100的制造方法包括以下步骤：将通过浸渍第一纤维而获得的预浸料片设置为第一通过热压对应于外层消融器1中的分层的树脂和成形烧瓶构件; 设置消融器构件和位于消融器构件内部的预浸布，并且通过用第二树脂浸渍长于第一纤维的第二纤维以形成层压体而获得; 并且将消融器和预浸布在高压釜中共模成型，以一体地模制外层消融器1和内层消融器2。版权所有：（C）2013，JPO＆INPIT

9. 发明专利

JP2008247150A Panel device 有权
标题翻译：面板设备
公开(公告)号：JP2008247150A
公开(公告)日：2008-10-16
申请号：JP2007089880
申请日：2007-03-29
申请人： Kawasaki Heavy Ind Ltd , 川崎重工業株式会社
发明人： KUBOTA NOBUYUKI
IPC分类号： B64G1/44 , B64G1/22
摘要： PROBLEM TO BE SOLVED: To provide a panel device capable of developing from a nubby folded state to a large planar state.
SOLUTION: The panel device comprises a plurality of panel bodies 11 and each panel body 11 has a plurality of panel pieces 12. Connection means connect the panel bodies 11 to each other and also connect the panel pieces 12 to each other. Each panel body 11 is capable of primary-developing from a housed state that the panel pieces 12 are overlapping each other (Fig. 1B(1), not shown here) to an intermediate state that the panel pieces are aligned in a planar state (Fig. 1C(3), not shown here) by extending to the overlapping direction Y of the panel pieces in the housed state. Each panel body 11 is capable of secondary-developing from the intermediate state to a developed state that the panel bodies are aligned in a planar state (Fig. 1D(5), not shown here) by extending to the overlapping direction Z of the panel bodies 11 in the intermediate state.
COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：提供一种能够从粗细折叠状态显影到大平面状态的面板装置。解决方案：面板装置包括多个面板体11，每个面板主体11具有多个面板片12.连接装置将面板主体11彼此连接，并将面板件12彼此连接。每个面板体11能够从容纳状态初级显影，使得面板片12彼此重叠（图1B（1），这里未示出）到面板片在平面状态下对准的中间状态图1C（3）（未示出））通过在收容状态下延伸到面板件的重叠方向Y。每个面板体11能够从中间状态到显影状态二次显影，即通过延伸到面板的重叠方向Z，面板体在平面状态下对准（图1D（5），未示出）身体11处于中间状态。版权所有（C）2009，JPO＆INPIT

10. 发明专利

JP2013121786A Ablator 有权
标题翻译： ABLATOR
公开(公告)号：JP2013121786A
公开(公告)日：2013-06-20
申请号：JP2011271248
申请日：2011-12-12
申请人： Kawasaki Heavy Ind Ltd , 川崎重工業株式会社
发明人： OYA HIROAKI , KUBOTA NOBUYUKI
IPC分类号： B64G1/58 , B32B5/28
摘要： PROBLEM TO BE SOLVED: To provide an ablator which can improve work efficiency in mounting the ablator to an airframe structure such as a capsule and also achieve weight reduction compared with an existing ablator having a low-density ablator.SOLUTION: The ablator includes: an inner layer ablator 1 formed of a first fiber impregnated with a first resin; and an outside layer ablator 2 formed of a second fiber impregnated with a second resin and having lower density than that of the inner layer ablator 1 in which the outside layer ablator is sintered outside the inner layer ablator by hot press, an electric furnace or autoclave.

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