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    • 1. 发明专利
    • Compressor of exhaust turbosupercharger
    • 排风机压缩机
    • JP2007127108A
    • 2007-05-24
    • JP2005322761
    • 2005-11-07
    • Mitsubishi Heavy Ind Ltd三菱重工業株式会社
    • SUGIMOTO KOICHIIBARAKI SEIICHIYOKOYAMA TAKAOHIGASHIMORI HIROTAKAOGITA KOJIOSAKO TAKESHIHAGITA ATSUSHI
    • F04D29/44F04D29/66
    • F04D29/4213F04D29/685
    • PROBLEM TO BE SOLVED: To provide a compressor of an exhaust turbosupercharger in which a part of the air flowing through an impeller is taken in from an inlet slit opening to an air passage at the peripheral portion of the impeller and discharged from an outlet slit to a compressor inlet air passage through a recirculation passage and noise is reduced and performance is increased by a simple structure without replacing a compressor housing even in an existing compressor. SOLUTION: This compressor comprises the recirculation passage 8 connecting the inlet slit 7 opening to the air passage at the outer periphery of the impeller 2 and the outlet slit 9 opening to the compressor inlet air passage 100. The part of the air flowing through the impeller is taken in from the inlet slit and discharged from the outlet slit to the inlet air passage through the recirculation passage. A recirculation passage forming member 5 is detachably fitted to the outer periphery of the compressor inlet air passage of a compressor housing 3. The recirculation passage and the outlet slit are formed by the inner surface of the recirculation passage forming member and the inner surface 8a of the compressor housing. COPYRIGHT: (C)2007,JPO&INPIT
    • 要解决的问题:提供一种排气涡轮增压器的压缩机,其中流过叶轮的空气的一部分从在叶轮的周边部分处的空气通道的入口狭缝开口引入并从 出口狭缝通过再循环通道进入压缩机入口空气通道,并且即使在现有的压缩机中也不会更换压缩机壳体,因此通过简单的结构降低了噪音并提高了性能。 解决方案:该压缩机包括将入口狭缝7开口连接到叶轮2的外周边的空气通道的再循环通道8和通向压缩机入口空气通道100的出口狭缝9.空气流动的一部分 通过叶轮从入口狭缝中取出并从出口狭缝排出到通过再循环通道的入口空气通道。 再循环通道形成构件5可拆卸地装配到压缩机壳体3的压缩机入口空气通道的外周。再循环通道和出口狭缝由再循环通道形成构件的内表面和 压缩机外壳。 版权所有(C)2007,JPO&INPIT
    • 2. 发明专利
    • Oil supply structure in connection structure of gas turbine and generator
    • 燃气轮机和发电机连接结构中的供油结构
    • JP2003343284A
    • 2003-12-03
    • JP2002151003
    • 2002-05-24
    • Mitsubishi Heavy Ind Ltd三菱重工業株式会社
    • YOSHIDA SHIROOGITA KOJI
    • F01D15/10F01D25/18F02C7/36F16N7/32
    • PROBLEM TO BE SOLVED: To stably supply an oil to a tooth flank.
      SOLUTION: A gas turbine shaft 1 and a generator shaft 2 are connected by a coupling 3, and the bosses 3b and 3c of a spline formed at both ends of the coupling 3 are engaged with the splines of spline shafts 4 and 6 extrapolated onto the turbine and generator shafts 1 and 2. On the spline shaft 6 of the generator side, a plurality of oil paths 25 for axially passing the oil are made in a peripheral direction. Further, an oil sleeve 27 having an oil reservoir 29 therein is fitted to the spline shaft 6, and has a certain clearance 28 with respect to the peripheral surface of the generator shaft 2. The oil jetted out of an oil jet hole 21 is carried into the oil reservoir 29 through the clearance 28, passes through the oil path 25, and is ejected from its bending part 26 onto the inner wall 3a of the coupling 3. At that time, the oil is spread on the inner wall 3a by a centrifugal force to reach a spline tooth flank.
      COPYRIGHT: (C)2004,JPO
    • 要解决的问题:为了稳定地将油提供给齿面。 解决方案:燃气轮机轴1和发电机轴2通过联轴器3连接,并且形成在联轴器3的两端的花键的凸台3b和3c与花键轴4和6的花键接合 外推到涡轮发电机轴1和发电机轴2上。在发电机侧的花键轴6上,沿周向方向制造多个用于轴向通过油的油路25。 此外,在花键轴6上安装有油槽29的油套27,相对于发电机轴2的周面具有一定的间隙28.由喷油孔21喷出的油被承载 通过间隙28进入储油器29,通过油路25,并从其弯曲部26喷射到联轴器3的内壁3a上。此时,油通过内壁3a扩展 离心力达到花键齿面。 版权所有(C)2004,JPO
    • 4. 发明专利
    • Rolling bearing mechanism and electric equipment using it
    • 使用它的滚动轴承机构和电气设备
    • JP2005240978A
    • 2005-09-08
    • JP2004055031
    • 2004-02-27
    • Mitsubishi Heavy Ind Ltd三菱重工業株式会社
    • YOSHIDA TAKAFUMIKOMATSU YOSHIMIMATSUMOTO IWAOOGITA KOJI
    • F02B39/00F04D29/04F04D29/056F04D29/059F16C25/06F16C27/06F16C33/66
    • F16C25/083F16C25/086F16C27/066F16C2360/44
    • PROBLEM TO BE SOLVED: To provide a rolling bearing mechanism making a pre-load providing function and a damping function compatible.
      SOLUTION: An intermediate ring 12 is inserted into an outer side in the radial direction from an outer ring 8 of a bearing 3 and an inner side from a housing 11 in play. A channel 13 is provided on an inner side of the intermediate ring 12 to hold adhesive lubricant between the intermediate ring 12 and the outer ring 8. A mechanical damper 16 as a damper member is fitted between the intermediate ring 12 and the housing 11. Pre-load is given to the outer ring 8 in the direction of central axis of the bearing 3. When the rolling bearing mechanism is constituted as mentioned above, pre-load is properly transmitted to the outer ring 8 without being absorbed by the damper member 16. A damper member 23 functions so as to damp vibration transmitted to the intermediate ring 12 from the bearing 3. Consequently, this rolling bearing mechanism damps vibration of the shaft by the damper members while applying proper pre-load continuously to support the shaft rotating at ultra-high speed.
      COPYRIGHT: (C)2005,JPO&NCIPI
    • 要解决的问题:提供一种制造预负荷提供功能的滚动轴承机构和兼容的阻尼功能。 解决方案:中间环12从轴承3的外圈8和外壳11的内侧在径向插入外侧。 通道13设置在中间环12的内侧,以在中间环12和外环8之间保持粘合剂润滑剂。作为阻尼构件的机械阻尼器16装配在中间环12和壳体11之间。 在轴承3的中心轴线方向上被赋予外圈8.当滚动轴承机构如上所述构成时,预负载被适当地传递到外圈8而不被阻尼构件16吸收 阻尼构件23用于阻止从轴承3传递到中间环12的振动。因此,该滚动轴承机构通过阻尼构件来减小轴的振动,同时连续施加适当的预加载力以支撑轴在 超高速。 版权所有(C)2005,JPO&NCIPI
    • 5. 发明专利
    • Small gas turbine
    • 小气量涡轮机
    • JP2003307102A
    • 2003-10-31
    • JP2002109412
    • 2002-04-11
    • Mitsubishi Heavy Ind Ltd三菱重工業株式会社
    • YOSHIDA SHIROOGITA KOJI
    • F01D25/16F01D25/18F02C7/06F16C37/00F16N39/02
    • PROBLEM TO BE SOLVED: To provide a small gas turbine with a structure capable of effectively restraining a temperature increase of lubricating oil supplied to a bearing.
      SOLUTION: The small gas turbine 1 is provided with a turbine 101, the bearing 110 to support a rotary shaft 105, and a casing 112 being located on a circumference of the bearing 110 and housing the bearing 110. The casing 112 is provided with a oil supply passage 113, and a pipe 2 to be a passage for the lubricating oil supplied to the bearing is inserted and set in the oil supply passage 113 having a spacing 3 from an internal surface of the oil supply passage. The spacing 3 functions as a heat insulating layer restraining heat transfer from the oil supply passage 113 to the inside of the pipe 2 at operation of the turbine.
      COPYRIGHT: (C)2004,JPO
    • 要解决的问题:提供一种具有能够有效地抑制供给到轴承的润滑油的升温的结构的小型燃气轮机。

      解决方案:小型燃气轮机1设置有涡轮机101,支撑旋转轴105的轴承110和位于轴承110的圆周上并容纳轴承110的壳体112.壳体112是 设置有供油通道113,并且作为供给轴承的润滑油的通道的管2被插入并设置在与供油通道的内表面间隔3的供油通道113中。 间隔3用作在涡轮机运转时抑制从供油路径113向管2内部传热的隔热层。 版权所有(C)2004,JPO

    • 6. 发明专利
    • Cooling structure for bearing housing for turbocharger
    • 滚动轴承轴承冷却结构
    • JP2013011253A
    • 2013-01-17
    • JP2011145859
    • 2011-06-30
    • Mitsubishi Heavy Ind Ltd三菱重工業株式会社
    • KAMISAKA NAOSHIIWAKIRI KENICHIROOGITA KOJI
    • F02B39/00
    • F01D25/125F01D25/14F02B39/005F05D2220/40F05D2260/232
    • PROBLEM TO BE SOLVED: To provide a cooling structure for a bearing housing for a turbocharger, capable of improving cooling performance while improving productivity and also reducing occurrence of a heat soak-back effect.SOLUTION: The cooling structure for a bearing housing for a turbocharger is configured to cool the bearing housing 13 and a bearing 52 by cooling water flowing through an annular cooling water path 13f formed in the bearing housing 13, and is characterized in that a water path inlet 13h which supplies the cooling water and a water path outlet 13j which discharges the cooling water are provided in the bearing housing 13 so as to communicate with the annular cooling water path 13f, and a partial partition 14a for partially closing a water path which forms the shortest route between the water path inlet 13h and the water path outlet 13j is provided.
    • 要解决的问题:为了提供一种用于涡轮增压器的轴承壳体的冷却结构,其能够在提高生产率的同时提高冷却性能并且还减少热回收效果的发生。 解决方案:用于涡轮增压器的轴承壳体的冷却结构被构造成通过冷却流过形成在轴承壳体13中的环形冷却水通道13f的水来冷却轴承壳体13和轴承52,其特征在于, 供给冷却水的水路入口13h和排出冷却水的水路出口13j设置在轴承壳体13中,以与环形冷却水路13f连通,部分分隔部14a用于部分关闭水 设置形成水路入口13h与水路出口13j之间的最短路径的路径。 版权所有(C)2013,JPO&INPIT
    • 7. 发明专利
    • Method of and tool for connecting gas turbine to generator
    • 将气体涡轮连接到发电机的方法和工具
    • JP2003343285A
    • 2003-12-03
    • JP2002151004
    • 2002-05-24
    • Mitsubishi Heavy Ind Ltd三菱重工業株式会社
    • YOSHIDA SHIROOGITA KOJITANABE KENZO
    • F01D15/10F01D25/00F02C7/36H02K15/16
    • PROBLEM TO BE SOLVED: To suitably connect both turbine and generator shafts.
      SOLUTION: Firstly, the eccentric centers of both shafts are measured using a tool 200, a flange 201 is fitted in the inlay 33 of a compressor scroll 31 in a gas turbine side to judge whether or not a measuring cylinder 203 can be extrapolated on a spline shaft 4 and further, a flange 202 is fitted in the inlay 32 of a casing 17 in a generator side to judge whether or not the cylinder 203 can be extrapolated on a spline shaft 6. In the above judgments, when the eccentric centers of both shafts are within a range of tolerance, the gas turbine and generator are connected through a coupling 3. On the other hand, when the eccentric center of one or both of the shafts exceeds the tolerance, the cause of failure is investigated to correct the failure or replace a component. Then, the tolerance is measured again using the tool 200.
      COPYRIGHT: (C)2004,JPO
    • 要解决的问题:适当地连接涡轮机和发电机轴。 解决方案:首先,使用工具200测量两个轴的偏心中心,将凸缘201装配在燃气轮机侧的压缩机涡旋件31的嵌体33中,以判断量筒203是否可以 外推在花键轴4上,此外,凸缘202装配在发电机侧的壳体17的嵌体32中,以判断气缸203是否可以在花键轴6上外推。在上述判断中,当 两轴的偏心中心在公差范围内,燃气轮机和发电机通过联轴器3连接。另一方面,当一个或两个轴的偏心中心超过公差时,研究故障原因 纠正故障或更换组件。 然后,使用工具200再次测量公差。版权所有(C)2004,JPO
    • 8. 发明专利
    • Small-sized gas turbine
    • 小尺寸气体涡轮
    • JP2003278505A
    • 2003-10-02
    • JP2002085578
    • 2002-03-26
    • Mitsubishi Heavy Ind Ltd三菱重工業株式会社
    • YOSHIDA SHIROOGITA KOJI
    • F01D25/24F02C3/05
    • PROBLEM TO BE SOLVED: To sufficiently meet short starting time, to ensure high efficiency, and to maintain downsizing.
      SOLUTION: A back plate 42 is fixed at a seal housing 25 at relatively low temperatures, and the back plate 42 abuts on a turbine nozzle 20 conditioned to relatively high temperatures. As a result, the back plate 42 maintains a contact condition with the turbine nozzle 20, and is not moved with the thermal expansion of the turbine nozzle 20. Therefore, the back plate 42 is not brought into contact or interference with a turbine rotor 22. At the time of rated operation of the turbine, the back plate 42 and the turbine rotor 22 maintain a preferable clearance C, thus sufficiently meeting short start time, ensuring high efficiency, and maintaining downsizing.
      COPYRIGHT: (C)2004,JPO
    • 要解决的问题:为了充分满足启动时间短,确保高效率,并保持小型化。 解决方案:背板42在相对较低的温度下固定在密封壳体25处,并且背板42抵靠调节到较高温度的涡轮喷嘴20。 结果,背板42与涡轮喷嘴20保持接触状态,并且不随着涡轮喷嘴20的热膨胀而移动。因此,背板42不与涡轮机转子22接触或干涉 在涡轮机的额定运转时,背板42和涡轮转子22保持优选的间隙C,从而充分满足短启动时间,确保高效率并且维持小型化。 版权所有(C)2004,JPO