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1. 发明专利

JP2009197833A Planet mechanism 审中-公开
标题翻译： PLANET机制
公开(公告)号：JP2009197833A
公开(公告)日：2009-09-03
申请号：JP2008037620
申请日：2008-02-19
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： NAKAYAMA SHUICHI , SHIMOYAMA KUNIMITSU , SUZUKI KAZUTAKA , ONO YASUHIRO , SAKAI KENJI
IPC分类号： F16H1/36 , B64C27/12
CPC分类号： F16H1/36 , B64C27/12 , F16H2001/2881
摘要： PROBLEM TO BE SOLVED: To provide a planet mechanism which can achieve a large reduction gear ratio while suppressing an increase in weight. SOLUTION: The planet mechanism 10 comprises: a sun gear 11 as an input; a fixed ring gear 12; a planet carrier 13 as an output; a first planet gear 15 which is supported by the planet carrier 13, and engaged with the sun gear 11; and a second planet gear 16 which is supported by the planet carrier 13, and engaged with the ring gear 12. A first rotation shaft 15a of the first planet gear 15 is arranged in the vicinity of a planet carrier rotating shaft 13a of the planet carrier 13 rather than a second rotation shaft 16a of the second planet gear 16. Torque is transmitted to the second planet gear 16 from the first planet gear 15. COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：提供一种能够在抑制重量增加的同时实现大的减速比的行星机构。行星机构10包括：作为输入的太阳齿轮11; 固定齿圈12; 作为输出的行星架13; 第一行星齿轮15，其由行星架13支撑并与太阳齿轮11接合; 以及由行星架13支撑并与环形齿轮12啮合的第二行星齿轮16.第一行星齿轮15的第一旋转轴15a布置在行星架的行星架旋转轴13a附近 13而不是第二行星齿轮16的第二旋转轴16a。扭矩从第一行星齿轮15传递到第二行星齿轮16.版权所有（C）2009，JPO＆INPIT

2. 发明专利

JP2009197842A Planet mechanism 审中-公开
标题翻译： PLANET机制
公开(公告)号：JP2009197842A
公开(公告)日：2009-09-03
申请号：JP2008037848
申请日：2008-02-19
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： NAKAYAMA SHUICHI , SHIMOYAMA KUNIMITSU , SUZUKI KAZUTAKA , ONO YASUHIRO , SAKAI KENJI
IPC分类号： F16H1/30 , F16H1/46
CPC分类号： B64C27/14 , F16H1/30
摘要： PROBLEM TO BE SOLVED: To provide a planet mechanism which can achieve a large reduction gear ratio while suppressing an increase in weight.
SOLUTION: The planet mechanism 10 comprises: a sun gear 11 as an input; a fixed ring gear 12; a planet carrier 13 as an output; and a planet gear unit 14 supported by the planet carrier 13. The planet gear unit 14 comprises: a shaft 17; a first planet gear 15 which is connected to the shaft 17, and engaged with the sun gear 11; and a second planet gear 16 which is connected to the shaft 17, and engaged with the ring gear 12. The planet gear unit 14 rotates around a first rotating shaft 14x with respect to the planet carrier 13. The planet carrier 13 rotates around a second rotating shaft 13x. The first rotating shaft 14x crosses the second rotating shaft 13x.
COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：提供一种能够在抑制重量增加的同时实现大的减速比的行星机构。行星机构10包括：作为输入的太阳齿轮11; 固定齿圈12; 作为输出的行星架13; 以及由行星架13支撑的行星齿轮单元14.行星齿轮单元14包括：轴17; 第一行星齿轮15，其连接到轴17并与太阳齿轮11接合; 以及第二行星齿轮16，其连接到轴17并与环形齿轮12接合。行星齿轮单元14相对于行星架13围绕第一旋转轴14x旋转。行星架13围绕第二旋转轴13x。第一旋转轴14x与第二旋转轴13x交叉。版权所有（C）2009，JPO＆INPIT

3. 发明专利

JP2000346053A ROTARY SHAFT SUPPORT DEVICE 失效
公开(公告)号：JP2000346053A
公开(公告)日：2000-12-12
申请号：JP15964399
申请日：1999-06-07
申请人： MITSUBISHI HEAVY IND LTD
发明人： TOTANI HISAYOSHI , ONO YASUHIRO , KIMURA MITSUAKI
IPC分类号： B64D35/00 , F16C13/02
摘要： PROBLEM TO BE SOLVED: To reduce size and weight of a rotary shaft supporting device supporting a driveshaft of a helicopter. SOLUTION: First and second rotary shafts 13, 14 are connected to each other by means of a coupling 15 and adjacently arranged in an axial direction. The first rotary shaft is supported to a bearing support 22 by means of a ball bearing 23. The support 22 is connected to a machine body (fixation member) 11 to compose a rotary shaft support device 21 for a helicopter by means of a bolt inserted through the support 22 and the machine body 11, and a nut screwed with the bolt. Washers 33 are sandwiched, respectively between the support 22 and the machine body 11, between the support 22 and a head 31a of the bolt. The washers 33 have spherical surfaces 33a to be abutted against the support 22. The support 22 can be inclined in respect to the machine body 11 for reducing bending load applied to the ball bearing 23, by the bending load applied to the support 22 accompanied with bending of the coupling 15.

4. 发明专利

JPH08285181A FOREIGN MATTER DETECTING DEVICE FOR GEAR BOX 失效
公开(公告)号：JPH08285181A
公开(公告)日：1996-11-01
申请号：JP8373295
申请日：1995-04-10
申请人： MITSUBISHI HEAVY IND LTD
发明人： HAYASHI TETSUSHI , ONO YASUHIRO
IPC分类号： G01B11/02 , F16H57/04 , F16N29/00 , G01N21/59 , G06M7/00 , G06M11/00
摘要： PURPOSE: To beforehand prevent disruption of a gear box by detecting a foreign matter generated in the gear box in real time even if this is a magnetic substance or a nonmagnetic substance. CONSTITUTION: A phototube oscillator 8 and a phototube receiver 9 to detect a foreign matter in lubricating oil are installed in lubricating oil piping 5 to circulate the lubricating oil to a casing 1 of a gear box by taking out the lubricating oil 2 from the casing 1 of the gear box, and a signal of the phototube receiver 9 is inputted to an analyzer 10, and the size and the number of the foreign matter are analyzed.

5. 发明专利

JP2013251127A Power source device 有权
标题翻译：电源设备
公开(公告)号：JP2013251127A
公开(公告)日：2013-12-12
申请号：JP2012124893
申请日：2012-05-31
申请人： Sanyo Electric Co Ltd , 三洋電機株式会社 , Mitsui O S K Lines Ltd , 株式会社商船三井 , Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： ONO YASUHIRO , OSAKI KAZUO , MATSUO YUKI , KAWAGOE YOSHIKAZU , AWATA KAZUHIKO , HAYAKAWA TAKAHIRO , SANO MASAHITO , SUZUKI NOBUHIRO , TSUZUKI NAGAHIRO
IPC分类号： H01M2/10 , H01M10/42 , H01M10/50
CPC分类号： Y02E60/12
摘要： PROBLEM TO BE SOLVED: To effectively prevent the induction of thermal runaway between battery modules disposed adjacent to each other, effectively prevent thermal runaway caused by heating from the exterior, and unfailingly prevent the induction of the thermal runaway over a long period while making an outer shape compact.SOLUTION: In a power source device, multiple battery modules 1 are disposed adjacent to each other. Each battery module 1 includes multiple chargeable batteries and a fire resistant heat insulation case 2 which houses the batteries, is closed, and is not hermetically sealed. The fire resistant heat insulation case 2 has a lamination structure of metal plates 3 and heat insulation plates 4 that is formed by laminating the heat insulation plates 4 on inner surfaces or outer surfaces of the metal plates 3 and shields fire and heat with the metal plates 3 and the heat insulation plates 4.
摘要翻译：要解决的问题：为了有效地防止彼此相邻布置的电池模块之间的热失控的感应，有效地防止从外部加热引起的热失控，并且可以长期地防止长时间导致热失控，同时制造外部形状紧凑。解决方案：在电源装置中，多个电池模块1彼此相邻设置。每个电池模块1包括多个可充电电池和容纳电池的耐火保温壳体2，其被封闭，并且不被气密密封。耐火保温壳体2具有金属板3和绝热板4的叠层结构，该隔热板4是通过在金属板3的内表面或外表面上层压绝热板4而形成的，并用金属板屏蔽火和热 3和隔热板4。

6. 发明专利

JP2007168561A Power transmission device for helicopter 审中-公开
标题翻译：用于直升机的动力传动装置
公开(公告)号：JP2007168561A
公开(公告)日：2007-07-05
申请号：JP2005367659
申请日：2005-12-21
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： SHIMOYAMA KUNIMITSU , NAKAYAMA SHUICHI , TOUZAKI YASUYOSHI , UMEDA AKIHIKO , FUJIMOTO HIRO , TOTANI HISAYOSHI , ONO YASUHIRO
IPC分类号： B64C27/12 , F16H1/08 , F16H1/22
摘要： PROBLEM TO BE SOLVED: To provide a power transmission device for a helicopter capable of balancing thrust load generated in a helical gear engaging part and dead weight of a driving shaft and minimizing axial direction displacement amount generated by a torque distribution of a double helical structure.
SOLUTION: This transmission device is provided with a first vertical shaft 12 provided with a driven side bevel gear 22 engaged with a driving side bevel gear 21 provided in an output shaft 11 and a pair of upper and lower driving side helical gears 23A and 23B, second vertical shafts 13A and 13B provided with driven side helical gears 24A and 24B and rotor shaft driving gears 25A and 25B, and a main gear 26 rotating integrally with a rotor shaft 2. In two pairs of helical engaging parts with which the driving side helical gears 23A and 23B and the driven side helical gears 24A and 24B are engaged, each of tooth trace inclination directions is made an opposite direction, and tooth trace inclination angles have an angle difference to cancel the thrust load corresponding to the dead weight of the first vertical shaft.
COPYRIGHT: (C)2007,JPO&INPIT
摘要翻译：要解决的问题：提供一种用于能够平衡在斜齿轮啮合部分中产生的推力负载和驱动轴的自重的直升机的动力传递装置，并且使由双重扭矩分配产生的轴向位移量最小化螺旋结构。解决方案：该传动装置设置有第一竖直轴12，该第一垂直轴12设置有与设置在输出轴11中的驱动侧锥齿轮21啮合的从动侧锥齿轮22和一对上下驱动侧斜齿轮23A 23B，设有从动侧螺旋齿轮24A，24B和转子轴驱动齿轮25A，25B的第二纵轴13A，13B，以及与转子轴2一体地旋转的主齿轮26.在两对螺旋接合部中，驱动侧斜齿轮23A和23B以及从动侧斜齿轮24A和24B接合，每个齿轨倾斜方向成相反方向，并且齿迹倾斜角度具有角度差以抵消对应于自重的推力载荷的第一垂直轴。版权所有（C）2007，JPO＆INPIT

7. 发明专利

JPS58168851A METHOD OF DEFROSTING AIR HEAT SOURCE HEAT PUMP 失效
公开(公告)号：JPS58168851A
公开(公告)日：1983-10-05
申请号：JP5092382
申请日：1982-03-31
申请人： MITSUBISHI HEAVY IND LTD
发明人： ONO YASUHIRO , KANOU ISAMU , YOSHIDA SHIYOUJI
IPC分类号： F25B47/02 , F25B13/00

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