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1. 发明申请

WO2004108354A1 A TURBINE BLADE 审中-公开
标题翻译：涡轮叶片
公开(公告)号：WO2004108354A1
公开(公告)日：2004-12-16
申请号：PCT/JP2004/007919
申请日：2004-06-01
申请人： Ishikawajima-Harima Heavy Industries Co., Ltd.
发明人： NISHIMURA, Keiji , OGI, Takahiro , NISHI, Hideyuki , MATSUMOTO, Toshiyuki
IPC分类号： B24B19/14
CPC分类号： F01D5/14 , F01D5/3007 , F05D2230/10 , F05D2230/68
摘要： A front engagement face 27f of a front engagement member 27 and a rear engagement face 29f of a rear engagement member 29 are respectively configured to be located a little back from a virtual plane VF coplanar with one side of a platform 15 and also to be substantially parallel to the axial direction of a male dovetail 25, and an end face of a front wall Wf integrally molded in the vicinity of a base portion of a front seal fin 21 and an end face of a rear wall Wr integrally molded in the vicinity of a base portion of a rear seal fin 23 are respectively configured to be coplanar with the virtual plane Vf.
摘要翻译：后接合构件29的前接合构件27和后接合面29f的前接合面27f分别构造成从与平台15的一侧共面的虚拟平面VF稍微位于背面，并且还基本上平行于阳形燕尾榫25的轴向方向的前壁Wf的前端壁Wf，以及一体地模制在前密封翅片21的基部附近的前壁Wf的端面和在前密封翅片21的基部附近的后壁Wr的端面后密封翅片23的基部分别构造成与虚拟平面Vf共面。

2. 发明申请

WO2007026725A2 DRUG, DRUG GUDANCE SYSTEM, MAGNETIC DETECTION SYSTEM, AND DRUG DESIGN METHOD 审中-公开
标题翻译：药物，药物系统，磁性检测系统和药物设计方法
公开(公告)号：WO2007026725A2
公开(公告)日：2007-03-08
申请号：PCT/JP2006/317027
申请日：2006-08-23
申请人： ISHIKAWAJIMA-HARIMA HEAVY INDUSTRIES CO., LTD. , ISHIKAWA, Yoshihiro , EGUCHI, Haruki
发明人： ISHIKAWA, Yoshihiro , EGUCHI, Haruki
IPC分类号： A61K41/00
CPC分类号： A61K41/0004 , A61K31/35 , A61K33/24 , G06F19/701 , G06F19/706
摘要： A drug comprises an organic or inorganic compound, and is made magnetic by modification of side chains and/or crosslinking between side chains.
摘要翻译：药物包括有机或无机化合物，并且通过侧链的改性和/或侧链之间的交联而制成磁性。

3. 发明申请

WO2004097183A1 TURBINE NOZZLE SEGMENT 审中-公开
标题翻译：涡轮喷嘴部分
公开(公告)号：WO2004097183A1
公开(公告)日：2004-11-11
申请号：PCT/JP2004/003974
申请日：2004-03-23
申请人： ISHIKAWAJIMA-HARIMA HEAVY INDUSTRIES CO., LTD.
发明人： TSURU, Atsushi , NISHIMURA, Keiji
IPC分类号： F01D25/24
CPC分类号： F01D25/246 , F01D25/285 , F05D2230/60 , Y02T50/671
摘要： A turbine nozzle segment 1 of a turbine nozzle assembly comprises a plurality of stator vanes 7, an arc-like inner band 9 integrally molded at the inner end of a plurality of the stator vanes 7, an arc-like outer band 11 integrally molded at the outer end of a plurality of the stator vanes 7. An outer band 11 includes an outer platform 19, a forward outer leg 21, a aft outer leg 23 and a hook member 29 formed at the back end and also in the central portion in the circumferential direction of the outer platform 19.
摘要翻译：涡轮喷嘴组件的涡轮喷嘴段1包括多个定子叶片7，在多个定子叶片7的内端整体模制的弧形内带9，整体模制在一起的弧形外带11 多个定子叶片7的外端。外带11包括外平台19，前外腿21，后外脚23和钩构件29，该钩构件29形成在后端和中部外平台19的圆周方向。

4. 发明申请

WO1997036809A1 CONTINUOUS UNLOADER 审中-公开
标题翻译：连续卸载
公开(公告)号：WO1997036809A1
公开(公告)日：1997-10-09
申请号：PCT/JP1997001083
申请日：1997-03-28
申请人： ISHIKAWAJIMA-HARIMA HEAVY INDUSTRIES CO., LTD. , MIYAZAWA, Isao
发明人： ISHIKAWAJIMA-HARIMA HEAVY INDUSTRIES CO., LTD.
IPC分类号： B65G67/60
CPC分类号： B65G67/606
摘要： In a continuous unloader, in which an endless bucket conveyor is passed around an upper sprocket, a base sprocket therebelow and a distal sprocket in front of the upper sprocket, the base sprocket and the distal sprocket are connected to a lower end of a frame which supports the upper sprocket via a link mechanism which lowers the base socket and the distal socket when approaching each other and raises them when separating from each other. The common link mechanism causes the base sprocket and the distal sprocket to move toward and away from each other and ascend and descend, so that the continuous unloader is made simple in construction and small in weight. Also, complicated control is not necessary and a manufacturing cost is made low. The link mechanism may comprise a main link connected at one end thereof to the lower end of the frame and at the other end thereof to the distal sprocket, an auxiliary link connected at one end thereof to an intermediate point of the main link and at the other end thereof to the base sprocket, and a stay link connected at one end thereof to an intermediate point of the auxiliary link and at the other end thereof to the lower end of the frame. Such link mechanism enables the base sprocket and the distal sprocket to move toward and away from each other and to ascend and descend.
摘要翻译：在连续的卸载机中，环形斗式输送机绕着上链轮传递，底座链轮和下链轮前面的远端链轮，底链轮和远端链轮连接到框架的下端，通过连杆机构支撑上链轮，当连接机构相互接近时，底座和远端插座相互下降，并在彼此分离时升高。公共连杆机构使基部链轮和远端链轮相互移动并上下移动，使得连续卸载机构造简单，重量轻。此外，不需要复杂的控制，并且制造成本低。连杆机构可以包括在其一端连接到框架的下端并且在其另一端处连接到远端链轮的主连杆，辅助连杆在其一端连接到主连杆的中间点其另一端连接到基部链轮，以及在其一端处连接到辅助连杆的中间点并且在另一端连接到框架的下端的撑杆连杆。这种连杆机构使得基座链轮和远端链轮能够彼此移动并远离彼此并且上升和下降。

5. 发明申请

WO1994026583A1 METHOD OF REDUCING FRICTION ON CRUISING BODY, CRUISING BODY WITH REDUCED FRICTION, METHOD OF AND APPARATUS FOR GENERATING MICROBUBBLES FOR USE IN REDUCTION OF FRICTION 审中-公开
标题翻译：降低摩擦摩擦力的方法，减少摩擦力的身体的制动方法，用于产生用于减少摩擦的微生物的方法和装置
公开(公告)号：WO1994026583A1
公开(公告)日：1994-11-24
申请号：PCT/JP1994000727
申请日：1994-04-28
申请人： ISHIKAWAJIMA-HARIMA HEAVY INDUSTRIES CO., LTD. , KATO, Hiroharu , TAKAHASHI, Yoshiaki
发明人： ISHIKAWAJIMA-HARIMA HEAVY INDUSTRIES CO., LTD.
IPC分类号： B63B01/38
CPC分类号： B63B1/38 , B63B2001/387 , Y02T70/122
摘要： A method of reducing a friction on a cruising body, a cruising body (Y) with reduced friction, and a method of and an apparatus for generating microbubbles for use in reduction of friction, aiming at reducing a frictional resistance with a small energy consumption to thereby enhance an overall energy efficiency and make readily practicable a measure of reducing a frictional at resistance. A mixed fluid containing bubbles and water is jetted rearwardly and obliquely away from the submerged surface (4) of the hull (1) into a boundary layer formed in the vicinity of the submerged surface (4) from fluid jetting nozzles (3) so that a kinetic energy of water having a great mass is utilized to inject bubbles more deeply into a desired bottom layer of the boundary layer than in the case where only bubbles are injected, for effective reduction of friction.
摘要翻译：减少摩擦的巡航体，巡航体（Y）的摩擦力的方法以及用于减少摩擦的用于产生微泡的方法和装置，旨在以小的能量消耗降低摩擦阻力从而提高整体能量效率，并且使得降低摩擦阻力的措施变得容易可行。含有气泡和水的混合流体从流体喷射喷嘴（3）向后并且倾斜地从船体（1）的浸没表面（4）喷射到形成在浸没表面（4）附近的边界层中，使得使用具有大质量的水的动能来将气泡更深地注入边界层的期望的底层中，而不仅仅是注入气泡的情况，以有效地减少摩擦。

6. 发明申请

WO2005003519A1 TURBINE SHROUD SEGMENT 审中-公开
标题翻译：涡轮SHROUD分段
公开(公告)号：WO2005003519A1
公开(公告)日：2005-01-13
申请号：PCT/JP2004/009761
申请日：2004-07-02
申请人： ISHIKAWAJIMA-HARIMA HEAVY INDUSTRIES CO., LTD. , TANAKA, Agamu
发明人： TANAKA, Agamu
IPC分类号： F01D11/00
CPC分类号： F01D25/145 , F01D11/005 , F01D11/08 , F01D11/127 , F05D2220/3215 , F05D2230/642 , F05D2240/11 , F05D2260/94 , F05D2260/941 , Y02T50/671 , Y02T50/675
摘要： A shroud segment for being incorporated in a gas turbine engine having a turbine case and a rear turbine case connected with a rear end of the turbine case so as to suppress influence of hot combustion gas on the turbine case and the rear turbine case, is provided with a back plate formed in an arc shape and supported by the turbine case, a touching member integrally formed on an inner surface of the back plate for touching with a rotating turbine blade; and a jet shield extended from a rear end of the back plate and slanted radially inward so as to shield the rear turbine case from a jet of the hot combustion gas.
摘要翻译：提供一种用于结合在具有涡轮壳体和与涡轮机壳体的后端连接的后涡轮机壳体的燃气涡轮发动机中的挡板段，以便抑制热燃气体对涡轮机壳体和后涡轮机壳体的影响具有形成为弧形并由所述涡轮壳体支撑的背板，一体地形成在所述后板的内表面上用于与旋转的涡轮叶片接触的接触构件; 以及从后板的后端延伸并且径向向内倾斜的喷射屏蔽，以便将后涡轮机壳与热燃烧气体的射流进行屏蔽。

7. 发明申请

WO2005003518A1 TURBINE SHROUD SEGMENT 审中-公开
标题翻译：涡轮SHROUD分段
公开(公告)号：WO2005003518A1
公开(公告)日：2005-01-13
申请号：PCT/JP2004/009756
申请日：2004-07-02
申请人： ISHIKAWAJIMA-HARIMA HEAVY INDUSTRIES CO., LTD. , TANAKA, Agamu
发明人： TANAKA, Agamu
IPC分类号： F01D11/00
CPC分类号： F01D25/145 , F01D9/042 , F01D11/005 , F01D11/127 , F05D2240/11 , Y02T50/671 , Y02T50/675
摘要： A shroud segment is incorporated in a gas turbine engine so as to suppress influence of hot combustion gas on a turbine case which has a groove and a hook for engagement with the shroud segment. The shroud segment is provided with a back plate formed in an arc shape, a front end of the back plate being supported by the groove so as to allow displacement in an axial direction of the gas turbine engine, a slot circumferentially formed on an outer surface of the back plate, the slot being engaged with the hook so as to be immovable in the axial direction and a touching member integrally formed on an inner surface of the back plate for touching with a rotating turbine blade. The slot is configured so as to satisfy an inequality of v
摘要翻译：护罩部分被结合在燃气涡轮发动机中，以便抑制热燃气体对具有槽和钩的汽轮机壳体的影响，从而与护罩段接合。护罩段设置有形成为弧形的背板，后板的前端由槽支撑，以允许在燃气轮机的轴向方向上的位移，周向地形成在外表面上的槽所述槽与所述钩接合而不能沿轴向移动;以及触摸构件一体地形成在所述背板的内表面上，用于与旋转的涡轮叶片接触。槽被配置为满足v

8. 发明申请

WO2004072451A1 PULSE DETONATION ENGINE SYSTEM FOR DRIVING TURBINE 审中-公开
标题翻译：用于驱动涡轮的脉冲爆震发动机系统
公开(公告)号：WO2004072451A1
公开(公告)日：2004-08-26
申请号：PCT/JP2004/001426
申请日：2004-02-10
申请人： Ishikawajima-Harima Heavy Industries Co., Ltd. , MURAYAMA, Motohide , YAMAWAKI, Shigemichi , TOH, Hidemi , KOBAYASHI, Hideo , TAKAHASHI, Katsuyoshi , CHIBA, Kaoru , OHYAGI, Shigeharu
发明人： MURAYAMA, Motohide , YAMAWAKI, Shigemichi , TOH, Hidemi , KOBAYASHI, Hideo , TAKAHASHI, Katsuyoshi , CHIBA, Kaoru , OHYAGI, Shigeharu
IPC分类号： F02C5/10
CPC分类号： F02C6/18 , F02C3/28 , F02C5/10 , Y02E20/14
摘要： A pulse detonation engine system (1) for driving a turbine is comprises a detonation generator section (5) including a detonation tube (7) having a tubular hollow section for permitting detonation to be generated therein during combustion stage of a mixture gas combined with a gas and a fuel, a gas supply section (17) for feeding the gas into the tubular hollow section of the detonation tube (7) at given time intervals, a fuel valve (19) for feeding the fuel into the tubular hollow section of the detonation tube (7) at the given time intervals, and an ignition plug (15) for igniting the mixture gas in the tubular hollow section of the detonation tube (7), and a pulse detonation driven turbine (9) driven directly or indirectly by energy of detonations that are intermittently generated in the tubular hollow section of the detonation tube (7).
摘要翻译：一种用于驱动涡轮机的脉冲爆震发动机系统（1）包括一个爆炸发生器部分（5），其包括一个具有管状中空部分的爆管（7），用于在混合气体与气体和燃料，用于以给定的时间间隔将气体供给到引爆管（7）的管状中空部分中的气体供应部分（17），用于将燃料供给到管状中空部分中的燃料阀爆炸管（7），以及用于点燃引爆管（7）的管状中空部分中的混合气体的火花塞（15）以及直接或间接驱动的脉冲爆震驱动涡轮机（9）在爆管（7）的管状中空部分间歇地产生的爆炸能量。

9. 发明申请

WO1997020728A1 METHOD OF REDUCING FRICTION RESISTANCE OF HULL, SHIP WHOSE FRICTION RESISTANCE IS REDUCED BY THE METHOD, AND METHOD OF ANALYZING JETTED BUBBLES ON SHIP 审中-公开
标题翻译：降低船体耐摩擦性的方法，通过该方法减少耐摩擦阻力的方法和分析喷射喷枪的方法
公开(公告)号：WO1997020728A1
公开(公告)日：1997-06-12
申请号：PCT/JP1996003526
申请日：1996-12-03
申请人： ISHIKAWAJIMA-HARIMA HEAVY INDUSTRIES CO., LTD. , KATO, Hiroharu , TAKAHASHI, Yoshiaki , YOSHIDA, Yuki , MASUKO, Akira , WATANABE, Osamu
发明人： ISHIKAWAJIMA-HARIMA HEAVY INDUSTRIES CO., LTD.
IPC分类号： B63B01/38
CPC分类号： B63B1/38 , B63B9/002 , B63B2001/387 , F15D1/12 , G01M10/00 , Y02T70/122
摘要： The friction resistance of the hull (2) of a ship (1) while navigating is reduced by jetting out minute air bubbles (8) of a predetermined diameter from positions of small static pressure near starting points of flow lines (F.L.) of water, which extend toward the bottom (5) of the ship from positions of small draft in a submerged part of the bow (4) of the hull (2) along both side surfaces of the hull (2), and allowing the minute air bubbles (8) to move down to the bottom (5) of the ship (1) along the flow lines (F.L.), thereby distributing minute air bubbles (8) over at least a part of a region around the submerged part of the hull (2).
摘要翻译：船舶（1）的船体（1）在航行时的摩擦阻力通过从水的流水线（FL）的起始点附近的小静态压力的位置喷射预定直径的微小气泡（8）来减少，其沿着船体（2）的两个侧表面从船体（2）的船首（4）的淹没部分的小抽风位置延伸到船的底部（5），并允许微小的气泡 8）沿着流动线（FL）向下移动到船（1）的底部（5），从而在船体的浸没部分周围的区域的至少一部分上分配微小气泡（8））。

10. 发明申请

WO1997020727A1 METHOD FOR REDUCING THE FRICTIONAL RESISTANCE OF A HULL AND A FRICTIONAL RESISTANCE REDUCED VESSEL EMPLOYING THE SAME METHOD 审中-公开
标题翻译：降低拉力摩擦阻力的方法和使用相同方法的减速电机
公开(公告)号：WO1997020727A1
公开(公告)日：1997-06-12
申请号：PCT/JP1996002101
申请日：1996-07-26
申请人： ISHIKAWAJIMA-HARIMA HEAVY INDUSTRIES CO., LTD. , KATO, Hiroharu , TAKAHASHI, Yoshiaki , YOSHIDA, Yuki , MASUKO, Akira , WATANABE, Osamu
发明人： ISHIKAWAJIMA-HARIMA HEAVY INDUSTRIES CO., LTD.
IPC分类号： B63B01/38
CPC分类号： G01M10/00 , B63B1/38 , B63B9/002 , B63B2001/387 , Y02T70/122
摘要： A method for reducing the frictional resistance of a hull (2) and a frictional resistance reduced vessel employing the same method. The method comprises the steps of blowing out fine air bubbles (8) having a required diameter from positions which are in the vicinity of starting points of flowing lines (F.L.) of water extending from light-draft positions in submerged portions of a bow portion (4) of the hull (2) of a vessel (1) to a vessel bottom (5) along the hull surface on both gunwales and where the static pressure is small, and distributing the fine air bubbles (8) to at least a part of the area surrounding the submerged portions of the hull (2) by causing the blown-out fine air bubbles to move around the vessel bottom (5) along the flowing lines (F.L.) so as to reduce the frictional resistance of the hull when cruising.
摘要翻译：使用相同方法降低船体（2）和摩擦阻力减小的船舶的摩擦阻力的方法。该方法包括以下步骤：从位于弓形部分的淹没部分的淡水位置的水的流动线（FL）的起始点附近的位置吹出具有所需直径的细小气泡（8） 4）船舶（1）的船体（2）到两个炮瓦的船体表面上的容器底部（5），静压力小，并且将细小气泡（8）分配到至少一部分通过使吹出的细小气泡沿着流动线（FL）在容器底部（5）周围移动而围绕船体（2）的浸没部分的区域，以便在巡航时降低船体的摩擦阻力。

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