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1. 发明专利

JP2011117437A Aircraft starter generator 有权
标题翻译：飞机启动发电机
公开(公告)号：JP2011117437A
公开(公告)日：2011-06-16
申请号：JP2010142267
申请日：2010-06-23
申请人： Kawasaki Heavy Ind Ltd , 川崎重工業株式会社
发明人： GOI TATSUHIKO , TANAKA KENICHIRO , WATANABE KOJI
IPC分类号： F02C7/32 , B64D41/00 , F01D15/10 , F01D15/12 , F02C6/00
CPC分类号： F02N11/04 , F02C7/275 , F02C7/36 , F02D2400/08 , F02N15/022 , F02N15/043 , F02N15/046 , Y02T50/671
摘要： PROBLEM TO BE SOLVED: To provide an aircraft starter generator achieving cost reduction and simplification of a device by carrying out constant frequency power generation by a low pressure shaft of an engine and electric start by a high pressure shaft, by one unit.
SOLUTION: The aircraft starter generator 1 includes an electric rotating machine 26 functioning as a starter and a generator, a continuously variable transmission 25, a high pressure side clutch 27 connected to the high pressure shaft 7 of the engine 10, and a low pressure side clutch 28 connected to the low pressure shaft 8. The rotating machine 26 drives the high pressure shaft 7 through the high pressure side clutch 27 at start and the low pressure shaft 8 drives the rotating machine 26 at constant rotation speed through the low pressure clutch 28 and the continuously variable transmission 25 after the engine 10 enters into a self-sustained operation.
COPYRIGHT: (C)2011,JPO&INPIT
摘要翻译：要解决的问题：提供一种飞机起动发电机，其通过一台发动机的低压轴和高压轴的电启动进行恒定频率发电，从而实现成本降低和简化。解决方案：飞机起动发电机1包括用作起动器的电动旋转机26和发电机，连续变速器25，与发动机10的高压轴7连接的高压侧离合器27，以及低压侧离合器28与低压轴8连接。旋转机26在起动时通过高压侧离合器27驱动高压轴7，低压轴8以恒定的转速驱动旋转机械26通过低压轴压缩离合器28和发动机10进入自持动作后的无级变速器25。版权所有（C）2011，JPO＆INPIT

2. 发明专利

JP2009274522A Power generation-starter device of engine 有权
标题翻译：发动机发电起动装置
公开(公告)号：JP2009274522A
公开(公告)日：2009-11-26
申请号：JP2008126235
申请日：2008-05-13
申请人： Kawasaki Heavy Ind Ltd , 川崎重工業株式会社
发明人： TANAKA KENICHIRO , GOI TATSUHIKO , SUGIMOTO KAZUSHIGE , NAKAMURA MASAHIDE , HIROTA TAKAYUKI , WATANABE KOJI
IPC分类号： B64D41/00 , F16H15/38
CPC分类号： F02N11/04 , F02D2400/12 , F02N15/025 , F02N15/043 , F02N2300/104 , F16H15/38 , F16H61/6649 , Y10T477/71
摘要： PROBLEM TO BE SOLVED: To provide a power generation-starter device of an engine can smoothly start an engine of an aircraft without using a power converter or a rotating machine can output large starting torque, and can stably switch the rotating machine from a starter motor to a power generator. SOLUTION: This power generation-starter device is provided with the rotating machine 1 serving both as the power generator driven by the engine E of the aircraft and the starter motor starting the engine of the aircraft, a power transmitting mechanism 2 connecting the engine E and the rotating machine 1, a starter driving device 3 feeding power to the rotating machine 1 upon start-up and driving this rotating machine 1 as the starter motor, a clutch mechanism 4 cutting off the power transmission from the engine E to the power transmitting mechanism 2 upon start-up, and a clutch control section 7 bringing the clutch mechanism 4 into a connected state when the rotating machine 1 reaches a prescribed rotational speed capable of starting the engine E. COPYRIGHT: (C)2010,JPO&INPIT
摘要翻译：要解决的问题：提供发动机的发电起动装置可以平稳地启动飞机的发动机而不使用电力转换器，或者旋转机器可以输出大的起动转矩，并且可以稳定地将旋转机器从起动马达到发电机。
解决方案：该发电起动装置配备有作为由飞行器的发动机E驱动的发电机和起动飞机的发动机的起动马达的旋转机1，连接发动机E和旋转机1，起动器驱动装置3，其在启动时向旋转机1供电，并且驱动该旋转机1作为起动电动机;离合器机构4，切断从发动机E到动力传递机构2，以及离合器控制部7，当旋转机械1达到能够起动发动机E的规定转速时，离合器机构4成为连接状态。（C）2010 ，JPO＆INPIT

3. 发明专利

JP2008014325A Method and system for controlling continuous variable transmission 有权
标题翻译：用于控制连续可变传输的方法和系统
公开(公告)号：JP2008014325A
公开(公告)日：2008-01-24
申请号：JP2006182842
申请日：2006-06-30
申请人： Kawasaki Heavy Ind Ltd , 川崎重工業株式会社
发明人： WATANABE KOJI , NAKAJIMA KENICHI , GOI TATSUHIKO , AZUMA NARIAKI , FUJII HIROSHI
IPC分类号： F16H61/02 , B64D41/00 , F16H59/42 , F16H59/72 , F16H61/18 , F16H61/664
摘要： PROBLEM TO BE SOLVED: To provide a method and a system for controlling a continuous variable transmission which does not cause instable control during starting. SOLUTION: In this method for controlling the continuous variable transmission 1, the gear ratio of the continuous variable transmission 1 is minimized until the rotational speed of an engine reaches a rotational speed at which a hydraulic pressure can be boosted to a predetermined pressure. The system S for controlling the continuously variable transmission 1 comprises a hydraulic servo mechanism 3 for adjusting the gear ratio of the continuously variable transmission 1 and a controller C for controlling the hydraulic servo mechanism 3. The controller C has a start control part PC for controlling the hydraulic servo mechanism 3 during starting. COPYRIGHT: (C)2008,JPO&INPIT
摘要翻译：要解决的问题：提供一种用于控制在启动期间不引起不稳定控制的连续可变变速器的方法和系统。解决方案：在用于控制连续变速器1的方法中，连续变速器1的齿轮比最小化直到发动机的转速达到可以将液压升高到预定压力的转速。用于控制无级变速器1的系统S包括用于调节无级变速器1的变速比的液压伺服机构3和用于控制液压伺服机构3的控制器C.控制器C具有控制器液压伺服机构3起动时。版权所有（C）2008，JPO＆INPIT

4. 发明专利

JP2003286916A Air cleaner for engine 有权
标题翻译：发动机用空气净化器
公开(公告)号：JP2003286916A
公开(公告)日：2003-10-10
申请号：JP2002091003
申请日：2002-03-28
申请人： Kawasaki Heavy Ind Ltd , 川崎重工業株式会社
发明人： WATANABE KOJI , KAWAMOTO YUICHI , KUJI YASUHIRO , NISHIKAWA ISAMU
IPC分类号： F02M35/16 , B01D39/16 , B01D46/00 , B01D46/10 , B01D46/24 , F02M35/024
CPC分类号： B01D46/0005 , B01D39/1676 , B01D46/2403 , B01D2275/10 , B01D2279/60 , Y10S55/42
摘要： PROBLEM TO BE SOLVED: To provide an air cleaner, in which cleaning ability and assembling property are improved, by keeping a deformed shape of a cleaner element 3.
SOLUTION: The cleaner element 3 of an endless wall-like shape for passing air in a wall thickness direction to clean the air is provided. The cleaner element 3 has a deformed shape seen from a wall height direction, and has a holding plates 7, 8 for holding the deformed shape of a wall is joined to an upper end face and lower end face of the wall.
COPYRIGHT: (C)2004,JPO
摘要翻译：要解决的问题：通过保持清洁元件3的变形形状来提供其中清洁能力和组装性能得到改善的空气滤清器。解决方案：环形壁状的清洁元件3 提供了用于使空气沿壁厚方向通过以清洁空气的形状。清洁器元件3具有从壁高方向看到的变形形状，并且具有用于保持壁的变形形状的保持板7,8接合到壁的上端面和下端面。版权所有（C）2004，JPO

5. 发明专利

JP2010179815A Power-generating device for aircraft 有权
标题翻译：发动机发电装置
公开(公告)号：JP2010179815A
公开(公告)日：2010-08-19
申请号：JP2009026220
申请日：2009-02-06
申请人： Kawasaki Heavy Ind Ltd , 川崎重工業株式会社
发明人： GOI TATSUHIKO , TANAKA KENICHIRO , NAKAMURA MASAHIDE , WATANABE KOJI
IPC分类号： B64D41/00 , H02K7/116 , H02K7/14 , H02K7/18
CPC分类号： F02C7/32 , F05D2260/40311 , F05D2270/024 , F05D2270/304 , F16H15/38 , F16H61/6648 , F16H61/6649 , Y02T50/671
摘要： PROBLEM TO BE SOLVED: To provide a power-generating device for an aircraft, which prohibits an increase in an area of a front face of an aircraft engine with respect to the aircraft engine and which can cope with a large change in a change ratio even when configured to generate a large power.
SOLUTION: The power-generating device 1 includes a traction transmission 22 connected to the rotary shaft 9 of an engine E, a generator 23 arranged above the traction transmission 22 and driven by the output from the traction 22, and an oil pump unit 24 for lubricating oil arranged below the traction transmission 22 and driven by the output from the traction 22, and it is driven by the engine E.
COPYRIGHT: (C)2010,JPO&INPIT
摘要翻译：要解决的问题：为了提供一种用于飞行器的发电装置，其防止飞机发动机的正面相对于飞机发动机的面积增加，并且可以应对飞行器发动机的大的变化即使配置为产生大功率时的变化率。发电设备1包括连接到发动机E的旋转轴9的牵引变速器22，布置在牵引变速器22上方并由牵引力22的输出驱动的发电机23，以及油泵用于润滑油的单元24，其布置在牵引变速器22下方并由牵引力22的输出驱动，并由发动机E驱动。（C）2010，JPO＆INPIT

6. 发明专利

JP2007255475A Hydraulic control circuit for continuously variable transmission 有权
标题翻译：液压控制电路连续可变变速器
公开(公告)号：JP2007255475A
公开(公告)日：2007-10-04
申请号：JP2006077901
申请日：2006-03-22
申请人： Kawasaki Heavy Ind Ltd , 川崎重工業株式会社
发明人： IMAI HIDEYUKI , WATANABE KOJI , GOI TATSUHIKO , FUJII HIROSHI
IPC分类号： F16H61/00 , F16H61/664
摘要： PROBLEM TO BE SOLVED: To provide a hydraulic control circuit for a continuously variable transmission capable of preventing occurrence of unstable operation of the continuously variable transmission even when acceleration of gravity is changed from a positive value into a negative value during flight and in the reverse case to it.
SOLUTION: This hydraulic control circuit 10 for the continuously variable transmission 1 is provided with an oil return pipe 17 branched from an air separated oil outlet for feeding the oil separated from air of an air separator 57 provided in an oil supply pipe 50 to return predetermined amount of oil onto the upstream side of a branched supply pipe 51. Since this hydraulic control circuit 10 is constituted in this way, unstable operation of the continuously variable transmission 1 due to insufficient amount of oil supply does not occur.
COPYRIGHT: (C)2008,JPO&INPIT
摘要翻译：要解决的问题：为了提供一种用于无级变速器的液压控制电路，其能够防止在飞行中重力加速度从正值变为负值时，连续变速传动装置的运行不稳定反之亦然。解决方案：用于无级变速器1的该液压控制回路10设置有从空气分离的油出口分支的回油管17，用于供给从设置在供油管50中的空气分离器57的空气分离的油将预定量的油返回到分支供给管51的上游侧。由于该液压控制回路10以这种方式构成，所以不会发生由于供油量不足导致的无级变速器1的不稳定运转。版权所有（C）2008，JPO＆INPIT

7. 发明专利

JP2007247800A Hydraulic control circuit of continuously variable transmission 有权
标题翻译：连续可变变速器液压控制电路
公开(公告)号：JP2007247800A
公开(公告)日：2007-09-27
申请号：JP2006072669
申请日：2006-03-16
申请人： Kawasaki Heavy Ind Ltd , 川崎重工業株式会社
发明人： NAKAMURA MASAHIDE , WATANABE KOJI , GOI TATSUHIKO , FUJII HIROSHI
IPC分类号： F16H61/00 , F16H57/04 , F16H59/72 , F16H61/66 , F16H61/664
摘要： PROBLEM TO BE SOLVED: To provide a hydraulic control circuit of a continuously variable transmission, which enables a rapid start of the continuously variable transmission even in a cold district.
SOLUTION: The hydraulic control circuit 10 controls a hydraulic servo mechanism 3 of the continuously variable transmission 1. The hydraulic control circuit 10 includes a warm up pipe 20 installed by a low fuse valve 21 to warm up the servo valve 3a by spraying the oil raised in temperature to the servo valve 3a of the hydraulic servo mechanism 3. Thereby, the servo valve 3a can be rapidly warmed up, which enables the rapid start of the continuously variable transmission 1 in the cold district.
COPYRIGHT: (C)2007,JPO&INPIT
摘要翻译：要解决的问题：提供一种无级变速器的液压控制电路，即使在寒冷地区也能够快速启动无级变速器。解决方案：液压控制回路10控制无级变速器1的液压伺服机构3.液压控制回路10包括由低熔丝阀21安装的预热管20，以通过喷涂来预热伺服阀3a 油的温度升高到液压伺服机构3的伺服阀3a。由此，伺服阀3a能够快速升温，能够在冷区快速启动无级变速器1。版权所有（C）2007，JPO＆INPIT

8. 发明专利

JP2004161133A Transmission device for rough ground traveling vehicle 审中-公开
公开(公告)号：JP2004161133A
公开(公告)日：2004-06-10
申请号：JP2002329572
申请日：2002-11-13
申请人： Asahi Denso Co Ltd , Kawasaki Heavy Ind Ltd , 川崎重工業株式会社 , 朝日電装株式会社
发明人： MAEDA KAZUHIRO , WATANABE KOJI , TAMAKI HIDEKAZU
IPC分类号： B60K20/02 , B62K23/04 , B62M25/04 , F16H59/02
CPC分类号： B60K37/06 , B60K2350/102 , B60Y2200/20 , B62K23/04 , B62M25/04 , F16H59/02 , F16H2059/048 , F16H2059/081 , Y10T74/19251 , Y10T74/2003 , Y10T74/20049 , Y10T74/20256 , Y10T74/20262
摘要： PROBLEM TO BE SOLVED: To improve ease of shifting operation of switching between forward/reverse movement, and to easily recognize a shifting position for reverse shifting in a transmission device for a rough ground traveling vehicle. SOLUTION: This rough ground traveling vehicle has a V-belt type non-step transmission 5, and a forward/reverse switching device 6 switchable to forward, neutral, and reverse positions. The forward/reverse switching device 6 is accommodated at a rear part of a crankcase 4, and has a rotating-type shifting device 26 for switching between forward/reverse at a handle bar 12 part adjacent to a handle grip 23, and the shifting device 26 and the forward/reverse switching device 6 are interlocked by cable transmitting devices 77, 78. The shifting device 26 is provided with a locking mechanism for locking at the neutral position to prevent it from shifting from the neutral position to the reverse position. A rider rotates a rotating member for shift while pushing a lock release knob with the finger to shift to a desired switching position. COPYRIGHT: (C)2004,JPO

9. 发明专利

JP2004161132A Transmission device for rough ground traveling vehicle 审中-公开
公开(公告)号：JP2004161132A
公开(公告)日：2004-06-10
申请号：JP2002329560
申请日：2002-11-13
申请人： Kawasaki Heavy Ind Ltd , 川崎重工業株式会社
发明人： MAEDA KAZUHIRO , WATANABE KOJI
IPC分类号： B60K20/02 , B62K5/00 , B62K11/14 , F16H59/02
CPC分类号： B62K5/01 , B60K37/06 , B60K2350/102 , B62K11/14 , F16H59/02 , F16H2059/0256 , F16H2059/081 , Y10T74/2022 , Y10T74/20262 , Y10T74/20287
摘要： PROBLEM TO BE SOLVED: To improve ease of shifting operation of switching between forward/reverse movement, and to easily recognize a shifting position for reverse shifting in a transmission device for a rough ground traveling vehicle. SOLUTION: This rough ground traveling vehicle has a V-belt type non-step transmission 5, and a forward/reverse switching device 6 switchable to forward, neutral, and reverse positions. The forward/reverse switching device 6 is accommodated at a rear part of a crankcase 4, and has a rotating-type shifting device 26 for switching between forward/reverse at a handle bar 12 part adjacent to a handle grip 23, and the shifting device 26 and the forward/reverse switching device 6 are interlocked by cable transmitting devices 77, 78. The forward/reverse switching device 6 has a stopper mechanism for stopping movement from the neutral position to the reverse position. The stopper mechanism is interlocked with the brake device so as not to shift to the reverse movement unless the brake device is switched on. COPYRIGHT: (C)2004,JPO

10. 发明专利

JPH10115255A START METHOD OF JET ENGINE AND JET ENGINE 失效
公开(公告)号：JPH10115255A
公开(公告)日：1998-05-06
申请号：JP28768496
申请日：1996-10-08
申请人： KAWASAKI HEAVY IND LTD
发明人： YOSHIDA KIMINORI , KORI KENJI , MATSUOKA SUKENORI , WATANABE KOJI
IPC分类号： F02C7/27 , F02K9/78
摘要： PROBLEM TO BE SOLVED: To dispense with a gunpowder cartridge by starting a jet engine by using one part of the injection gas of a booster rocket. SOLUTION: A gas produced by a booster rocket R is injected from an exhaust nozzle 10 so as to fly a flight object M and also its one part is supplied to the compressor 2 of a jet engine J or a turbine 3 so as to rotate a rotor 4 by a gas flow passage 1. Then, a rotary shaft 5 integrated with this rotor 4 is also rotated and thereby, the drive shaft of a fuel pump 31 is also rotated. The fuel of a fuel tank 30 is supplied to a combustion vessel 40 through a fuel pipe and an igniter 41 is ignited and the combustion of the fuel is started and the jet engine J is started.

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