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21. 发明专利

JP2009292368A System and method for supplying air for fuel cell in aircraft 有权
标题翻译：用于在飞机上为燃料电池供应空气的系统和方法
公开(公告)号：JP2009292368A
公开(公告)日：2009-12-17
申请号：JP2008149222
申请日：2008-06-06
申请人： Shimadzu Corp , 株式会社島津製作所
发明人： SAITO HIDEFUMI
IPC分类号： B64D41/00 , H01M8/00 , H01M8/04 , H01M8/06 , H01M8/12
CPC分类号： Y02T90/36
摘要： PROBLEM TO BE SOLVED: To adequately supply a proper amount of air with proper pressure independent from flight altitude to a fuel cell mounted on an aircraft by effectively using pressure energy of air inside the aircraft and heat energy discharged from the fuel cell. SOLUTION: Air outside the aircraft compressed by a compression device 10 is supplied to an air electrode 1a side of the fuel cell 1 as air necessary for power generation reaction of the fuel cell 1 mounted on the aircraft. Air inside the aircraft discharged from a cabin 14 is used as working fluid of a first turbine 11. Exhaust gas flown out of the air electrode 1a side is used as working fluid of a second turbine 12. Discharge ports of each turbine 11, 12 are communicated with an area outside the aircraft. Generating power of the first turbine 11 and generating power of the second turbine 12 are used as compression power of the air outside the aircraft by the compression device 10. COPYRIGHT: (C)2010,JPO&INPIT
摘要翻译：要解决的问题：通过有效地利用飞行器内的空气的压力和从燃料电池排出的热能来适当地向安装在飞行器上的燃料电池提供适当的压力，以适当的压力独立于飞行高度供应适当的空气。解决方案：由压缩装置10压缩的飞机外部的空气作为安装在飞机上的燃料电池1的发电反应所需的空气供给到燃料电池1的空气电极1a侧。从机舱14排出的飞机内的空气被用作第一涡轮机11的工作流体。从空气电极1a侧流出的排气用作第二涡轮机12的工作流体。各涡轮机11,12的排出口与飞机外的区域通信。第一涡轮机11的发电功率和第二涡轮机12的发电功率被压缩装置10用作飞机外部的空气的压缩功率。（C）2010，JPO和INPIT

22. 发明专利

JP2008297621A Zinc-nickel alloy plating solution and zinc-nickel alloy plating method 有权
标题翻译：锌镍合金镀层解决方案和锌镍合金镀层方法
公开(公告)号：JP2008297621A
公开(公告)日：2008-12-11
申请号：JP2007148252
申请日：2007-06-04
申请人： Asahi Kinzoku Kogyo Kk , Dipsol Chem Co Ltd , Fuji Heavy Ind Ltd , Meira Corp , Shimadzu Corp , Society Of Japanese Aerospace Co Inc , Sumitomo Precision Prod Co Ltd , ディップソール株式会社 , メイラ株式会社 , 住友精密工業株式会社 , 富士重工業株式会社 , 旭金属工業株式会社 , 株式会社島津製作所 , 社団法人日本航空宇宙工業会
发明人： SAITO HIDEFUMI , TANIGUCHI TETSUO
IPC分类号： C25D3/56 , C25D5/26 , C25D5/50
摘要： PROBLEM TO BE SOLVED: To provide a zinc-nickel alloy plating solution capable of attaining a plated layer having corrosion resistance equal to or above that of a cadmium plating or a cadmium-titanium alloy plating and not containing cadmium as a harmful material at all, using a coating film layer not containing 6-valent chromium as a harmful material at all as a protective layer protecting the plated layer and applying plating capable of surely suppressing the occurrence of hydrogen embrittlement on a high strength steel, and to provide a zinc-nickel alloy plating method.
SOLUTION: The zinc-nickel alloy plating solution containing zinc ion, nickel ion, sodium ion and hydroxide ion in the solution is kept so that a water soluble cationic polymer is controlled not to exceed 100 mg in 1 L solution.
COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：提供一种能够获得具有等于或高于镉镀层或镉 - 钛合金电镀并且不含镉作为有害物质的耐腐蚀性的镀层的锌镍合金电镀液完全使用不含6价铬的涂膜作为有害材料作为保护镀层的保护层，并施加能够可靠地抑制高强度钢上的氢脆化的发生的镀层，并且提供锌镍合金电镀法。
解决方案：保持溶液中含有锌离子，镍离子，钠离子和氢氧根离子的锌镍合金电镀溶液，使得水溶性阳离子聚合物在1L溶液中控制不超过100mg。版权所有（C）2009，JPO＆INPIT

23. 发明专利

JP2004332666A Compression device 有权
公开(公告)号：JP2004332666A
公开(公告)日：2004-11-25
申请号：JP2003131841
申请日：2003-05-09
申请人： Shimadzu Corp , 株式会社島津製作所
发明人： ANDO MASANAO , SAITO HIDEFUMI , ISAKA HIROSHI
IPC分类号： F04D17/14 , F04D29/58
摘要： PROBLEM TO BE SOLVED: To improve cooling efficiency of compressed gas and compression efficiency of a second compression part in a two stage compression device.
SOLUTION: Cooling water W is supplied to a back surface of a first impeller 1a. The cooling water W is scattered from an outer circumference end by centrifugal force generated by rotation of the first impeller 1a and is sprayed to the compressed gas. Since the compressed gas is directly cooled by injecting cooling water therein, cooling efficiency can be improved. Since the compressed air of which temperature is raised through the first compression part 1 enters a second compression part 2 after being cooled, compression efficiency of the second compression part can be improved.
COPYRIGHT: (C)2005,JPO&NCIPI

24. 发明专利

JP2004226033A Air-conditioning system 有权
公开(公告)号：JP2004226033A
公开(公告)日：2004-08-12
申请号：JP2003016082
申请日：2003-01-24
申请人： Shimadzu Corp , 株式会社島津製作所
发明人： SAITO HIDEFUMI
IPC分类号： F24F3/147 , F24F3/14 , F24F11/02 , F25B9/00
CPC分类号： F24F3/1423 , F24F2203/1016 , F24F2203/1032 , F24F2203/1056 , F24F2203/1068 , F24F2203/1084
摘要： PROBLEM TO BE SOLVED: To provide an air-conditioning system capable of realizing the air-conditioning felt comfortable by many people by preferentially dropping the humidity than the temperature of indoor air to be ventilated in high-temperature and highly humid environment.
SOLUTION: An air cycle device 1 cools air moving from outdoors to indoors 2 after compression, and then, expanded to form cold air. Water separators 16a and 16b remove moisture in air condensed after cooling. A drying device 4 has moisture adsorption function, and dehumidifies circulated indoor air by moisture adsorbing agent which is regenerated by heating. The calorie of the air heated by compression is utilized in regenerating the moisture adsorbing agent.
COPYRIGHT: (C)2004,JPO&NCIPI

25. 发明专利

JP2003312594A Air conditioner for aircraft 有权
标题翻译：空调器飞机
公开(公告)号：JP2003312594A
公开(公告)日：2003-11-06
申请号：JP2002116489
申请日：2002-04-18
申请人： Shimadzu Corp , 株式会社島津製作所
发明人： MITANI HISASHI , SAITO HIDEFUMI
IPC分类号： B64D13/06 , B01D53/22 , B64D37/32 , F25B9/00
CPC分类号： Y02T70/72
摘要： PROBLEM TO BE SOLVED: To provide an air conditioner for an aircraft capable of effectively using oxygen enriched air from an air separation part, reducing an engine load, performing a fail-safe function, and allowing a proper operation according to a flight condition.
SOLUTION: A plurality of cooling units A changeable between an operation state and a stop state mutually independently generate cold air introduced into a cabin 8 by expanding the air compressed by a compressor 3 by an expansion turbine 5. A plurality of compression units B changeable between an operation state and a stop state mutually independently are provided with premixing compressors 17 compressing the outflow air from the cabin 8. A mixture of engine extraction air and the air compressed by the premixing compressor 17 is compressed by the compressor 3 and separated into nitrogen enrichment gas and oxygen enriched air by a permselective membrane. The setting of the number of cooling units A in the operation state and the number of the compression units B in the operation state can be changed.
COPYRIGHT: (C)2004,JPO
摘要翻译：要解决的问题：提供一种能够有效地使用来自空气分离部件的富氧空气的飞机的空调器，减少发动机负荷，执行故障保护功能，并允许根据飞行的正确操作条件。解决方案：在操作状态和停止状态之间变化的多个冷却单元A相互独立地产生通过膨胀涡轮机5膨胀被压缩机3压缩的空气引入到机舱8中的冷空气。多个压缩单元在操作状态和停止状态之间相互独立地改变的B设置有预混合压缩机17，其从舱8压缩流出空气。发动机提取空气和由预混合压缩机17压缩的空气的混合物被压缩机3压缩并分离通过选择性渗透膜进入富氮气体和富氧空气。可以改变操作状态下的冷却单元A的数量和操作状态下的压缩单元B的数量。版权所有（C）2004，JPO

26. 发明专利

JP2003065621A Cooling system 审中-公开
标题翻译：冷却系统
公开(公告)号：JP2003065621A
公开(公告)日：2003-03-05
申请号：JP2001254952
申请日：2001-08-24
申请人： Shimadzu Corp , 株式会社島津製作所
发明人： MITANI HISASHI , SAITO HIDEFUMI
IPC分类号： F01D15/10 , F02C1/02 , F02C3/08 , F02C6/16 , F02C6/18 , F02C7/08 , F02G5/04 , F25B9/00
CPC分类号： Y02E20/14 , Y02E60/15 , Y02T10/166
摘要： PROBLEM TO BE SOLVED: To provide a cooling system which enables effective and efficient use of a surplus power not only for cooling, but also for indoor ventilation and refrigeration. SOLUTION: Compressed air obtained by an air compressing means 1 driven by an electric motor is cooled down by an air cooling means 17. The compressed air flowing out from a compressed air reserving means 20 which reserves the compressed air obtained by the air compressing means 1 is expanded to be cool air. The inlet and outlet of the means 20 for the compressed air is made openable and closable.
摘要翻译：要解决的问题：提供一种冷却系统，其能够有效且有效地使用剩余电力，不仅用于冷却，而且用于室内通风和制冷。解决方案：通过由电动机驱动的空气压缩装置1获得的压缩空气由空气冷却装置17冷却。从压缩空气储存装置20流出的压缩空气，其保留由空气压缩装置1获得的压缩空气被扩展为冷空气。用于压缩空气的装置20的入口和出口被打开和关闭。

27. 发明专利

JP2015003642A 航空機用液冷システムの維持装置および維持方法审中-公开
标题翻译：维修液体冷却系统的设备和维护方法
公开(公告)号：JP2015003642A
公开(公告)日：2015-01-08
申请号：JP2013130605
申请日：2013-06-21
申请人：株式会社島津製作所 , Shimadzu Corp
发明人： SAITO HIDEFUMI , URYU SHOJI
IPC分类号： B64F5/00
摘要：【課題】不凍液を含まない熱移動媒体を用いる場合であっても、駐機時の液冷システム内での熱移動媒体の凍結を抑制することが可能な航空機用液冷システムの維持装置を提供する。【解決手段】この維持装置2は、航空機Aの液冷システム1に接続される維持装置2であって、熱移動媒体3を液冷システム1の第1流路10から排出するための排出用ガス4を第1流路10に注入するガスボンベ21と、ポンプ11の駆動により第1流路10内の熱移動媒体3を第1流路10から排出する制御部24と、ポンプ11の入口側圧力が熱移動媒体3の排出時のポンプ11の負荷を軽減することが可能な圧力となるように、排出用ガス4の注入圧および注入量の少なくとも一方を調整する供給圧力制御弁22とを備える。【選択図】図2
摘要翻译：要解决的问题：提供一种用于飞行器的液体冷却系统的维护装置，即使在使用不含防冻液体的传热介质时，其也可以在停车期间抑制液体冷却系统中的传热介质的冻结。解决方案：维护装置2连接到飞行器A的液体冷却系统1，包括：气瓶21，将排出气体4喷射到液体冷却系统1的第一通道10中，用于从第一通道排出传热介质3 10; 通过驱动泵11从第一通道10排出第一通道10中的传热介质3的控制部分24; 以及调节排出气体4的喷射压力和喷射量中的至少一个的供给压力控制阀22，使得泵11的入口侧压力成为能够减少排出热量期间泵11上的负荷的压力转印介质3。

28. 发明专利

JP2008212844A Adsorption element and adsorption apparatus for carbon dioxide 有权
标题翻译：吸附元素和二氧化碳吸附装置
公开(公告)号：JP2008212844A
公开(公告)日：2008-09-18
申请号：JP2007054552
申请日：2007-03-05
申请人： Kawasaki Heavy Ind Ltd , Shimadzu Corp , 川崎重工業株式会社 , 株式会社島津製作所
发明人： SAITO HIDEFUMI , SHIYOUJI YASUTOSHI , UEDA TADASHI
IPC分类号： B01J20/22 , B01D53/02 , B01D53/04 , B01J20/34
CPC分类号： Y02C10/08
摘要： PROBLEM TO BE SOLVED: To provide a thin and lightweight adsorption element for carbon dioxide which is easily handled and hardly broken. SOLUTION: In the adsorption element 1 for carbon dioxide, at least one surface of a polymer base film 15 is covered with a carrier film 16. The carrier film 16 is formed by oxidizing the surface layer of an aluminum or aluminum alloy foil. The surface layer is a porous aluminum oxide carrier layer 16a, and the remaining part is an aluminum or aluminum alloy supporting layer 16b. An amine group 17 for adsorbing carbon dioxide is adhered on the inside surface of the each hole 16a' of the carrier layer 16a. COPYRIGHT: (C)2008,JPO&INPIT
摘要翻译：要解决的问题：为了提供易于处理和几乎不破裂的二氧化碳薄型轻质吸附元件。解决方案：在用于二氧化碳的吸附元件1中，聚合物基膜15的至少一个表面被载体膜16覆盖。载体膜16通过氧化铝或铝合金箔的表面层而形成。表层是多孔氧化铝载体层16a，其余部分是铝或铝合金支撑层16b。用于吸附二氧化碳的胺基17粘附在载体层16a的每个孔16a'的内表面上。版权所有（C）2008，JPO＆INPIT

29. 发明专利

JP2005112005A Air-conditioner for aircraft 有权
标题翻译：飞机空调
公开(公告)号：JP2005112005A
公开(公告)日：2005-04-28
申请号：JP2003344713
申请日：2003-10-02
申请人： Shimadzu Corp , 株式会社島津製作所
发明人： SAITO HIDEFUMI
IPC分类号： B64D13/06
CPC分类号： Y02C10/08 , Y02C10/10 , Y02T50/56
摘要： PROBLEM TO BE SOLVED: To provide an air-conditioner for an aircraft capable of preventing any increase of the concentration of carbon dioxide while suppressing discharge of water in the air in the aircraft, reducing the ventilation volume by fresh air, and enhancing the environment in the aircraft without increasing any engine load or energy consumption. SOLUTION: Air extracted from an engine 1 cooled by a cooling device is introduced in a cabin 8. Carbon dioxide is separated from a carbon dioxide selection transmission membrane from air in an air passage to introduce air flowing out of the cabin 8 to the cabin 8 again. Water contained in the air in the air passage is adsorbed by an adsorption unit 83. Water adsorbed by the adsorption unit 83 can be introduced into the cabin 8. Carbon dioxide is discharged out of the aircraft through the carbon dioxide transmission membrane. COPYRIGHT: (C)2005,JPO&NCIPI
摘要翻译：要解决的问题：为了提供一种能够防止二氧化碳浓度的任何增加同时抑制飞机上的空气中的水排放的飞机的空调器，通过新鲜空气减少通风量，并且增强飞机上的环境没有增加任何发动机负载或能量消耗。解决方案：从由冷却装置冷却的发动机1中提取的空气被引入舱室8.二氧化碳从二氧化碳选择传递膜与空气通道中的空气分离，以将从舱室8流出的空气引入客舱8再次。包含在空气通道中的空气中的水被吸附单元83吸附。吸附单元83吸附的水可以被引入舱室8.二氧化碳通过二氧化碳透过膜排出飞机外。版权所有（C）2005，JPO＆NCIPI

30. 发明专利

JP2003312596A Air conditioner for aircraft 有权
标题翻译：空调空调
公开(公告)号：JP2003312596A
公开(公告)日：2003-11-06
申请号：JP2002126290
申请日：2002-04-26
申请人： Shimadzu Corp , 株式会社島津製作所
发明人： MITANI HISASHI , SAITO HIDEFUMI
IPC分类号： B64D13/06 , B01D53/22 , B64D37/32
摘要： PROBLEM TO BE SOLVED: To provide an air conditioner for an aircraft capable of effectively using oxygen enriched air from an air separation part, reducing an engine load, and exerting a sufficient air-conditioning function at the time of descent of the aircraft.
SOLUTION: A cooling unit A generates cold air to be introduced into a cabin 8 by expanding air compressed by a compressor 3 by an expansion turbine 5. A compression unit B is provided with a premixing compressor 17 compressing outflow air from the cabin 8. After being mixed, engine extraction air and the air compressed by the premixing compressor 17 are compressed by the compressor 3 and separated into nitrogen enriched gas and oxygen enriched air by an air separation part 16. A first valve 12 adjusts the flow rate of the engine extraction air led from a bypass air flow passage 11 to the cabin 8 without passing the cooling unit A. A second valve 39 adjusts the flow rate of the engine extraction air led to a mixing area with the air compressed by the premixing compressor 17.
COPYRIGHT: (C)2004,JPO
摘要翻译：要解决的问题：提供一种用于能够有效地使用来自空气分离部件的富氧空气的飞机的空调器，减少发动机负载并且在飞行器下降时发挥足够的空调功能。解决方案：冷却单元A通过膨胀涡轮机5膨胀由压缩机3压缩的空气来产生将被引入到舱室8中的冷空气。压缩单元B设置有预压混合压缩机17，其从舱室压缩流出空气 8.混合后，发动机抽出空气和由预混合压缩机17压缩的空气被压缩机3压缩，并通过空气分离部分16分离成富氮气体和富氧空气。第一阀12调节流量发动机提取空气从旁路气流通道11引导到机舱8而不通过冷却单元A.第二阀39调节引导到与由预混合压缩机17压缩的空气混合的混合区域的发动机提取空气的流量版权所有（C）2004，JPO

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