| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 一种防超载旋转轴 | CN201710766119.3 | 2017-08-30 | CN107339331A | 2017-11-10 | 曾燊平 |
| 本发明公开了一种防超载旋转轴，包括用于动力源电动机的电动机主轴和用于连接需要带动的连接轴，所述连接轴的端部设置有与其一体式结构的连接板结构，所述连接板结构通过螺栓固定在一旋转套筒壳体，所述旋转套筒壳体一端的内部设置有旋转中空凹槽，所述旋转套筒壳体在位于所述旋转中空凹槽的端口设置有限位孔，所述旋转中空凹槽的内部套放一旋转板，所述旋转板侧面的中心设置有半圆形凹槽。本发明用于连接驱动装置的轴体和被驱动装置的轴体，当发生超载现象或者需要制动时，用于连接的部位能够及时脱离，此时，驱动装置的轴体能够正常旋转，并不会受到外力影响，从而防止电动机烧坏现象的发生，此外，该装置安装简便，实用性强。 | ||||||
| 2 | 微电机转轴 | CN201510940556.3 | 2015-12-15 | CN106884852A | 2017-06-23 | 房锦山 |
| 本发明公开了微电机转轴，包括转轴和内轴；转轴体包括输入段、连接筒和传动段，传动段上靠近连接筒的一端开设有一个圆形容纳孔和一个方形传动孔，方形传动孔与圆形容纳孔连通；内轴位于连接筒内，内轴包括第一端和第二端，内轴的第一端与输入段连接，内轴的第二端位于圆形容纳孔内，内轴的第二端的外表面不与圆形容纳孔接触，内轴的第二端上还设置有传动块，传动块位于方形传动孔内，传动块的外表面与方形传动孔的内壁直接存在间隙；输入段、连接筒、传动段、圆形容纳孔和内轴同轴；内轴与连接筒之间存在间隙。本发明设置内轴和连接筒两套扭矩传递部件，在连接筒断裂失效后由内轴传递扭矩，避免动力输出完全中断的情况发生。 | ||||||
| 3 | 机械保护方法和装置 | CN201280004513.9 | 2012-01-03 | CN103314231B | 2016-04-20 | 弗雷德里克·费迪南德·杰克斯·巴特列 |
| 本发明涉及到提供机械保护的装置领域和方法，特别涉及到一种带有传动轴(1)的机械保护装置，所述传动轴弯曲时的共振频率对应于传动轴(1)预定旋转过速，所述传动轴不能充分阻尼到可避免因为所述弯曲共振而造成的传动轴(1)断裂，本发明还涉及到一种机械保护方法，按照这种方法，传动轴(1)会因为弯曲时的这种共振而断裂。 | ||||||
| 4 | 带有起动器/发电机的辅助齿轮箱 | CN201110462031.5 | 2011-12-28 | CN102562316A | 2012-07-11 | 黄豪; J·齐沃特 |
| 本发明涉及带有起动器/发电机的辅助齿轮箱。一种用于燃气涡轮发动机(1)的组件(102)包括：包括驱动齿轮(150)和小齿轮(140)的辅助齿轮箱(100)；和机械地安装到辅助齿轮箱(100)的起动器/发电机(101)。起动器/发电机(101)包括壳体(160)和带有保险断开器(192)的可旋转轴(170)的部分，其中保险断开器(192)设置在起动器/发电机(101)的壳体(160)内。 | ||||||
| 5 | 动力传递装置 | CN201480019902.8 | 2014-03-26 | CN105121885B | 2017-09-19 | 加藤基; 黑须義弘; 神沢贵浩 |
| 本发明提供一种动力传递装置，其具备与动力源连接的滑轮(4)、和位于与滑轮(4)同一轴线上的旋转轴。具备设于旋转轴上的轮毂(11)、和可与该轮毂(11)分离的嵌合的环板(12)。具备将环板(12)向与旋转轴线平行的方向朝轮毂(11)施力的板簧(16)。在旋转轴的负载小于阈值的情况下，轮毂(11)和环板(12)通过摩擦力一体旋转。在旋转轴的负载大于等于阈值时，环板(12)相对于轮毂(11)旋转，通过板簧(16)的弹力向与旋转轴线平行的方向移动，使环板(12)与轮毂(11)分离。可以提供当从动侧旋转体的负载扭矩增大后，在短时间内切断动力传递的动力传递装置。 | ||||||
| 6 | 雷达结构 | CN201610875934.9 | 2016-09-30 | CN107061533A | 2017-08-18 | 劳伦特·卡奥米特; 尼古拉斯·巴尔比耶; 巴斯蒂安·德克特 |
| 本发明涉及一种雷达结构(1)，该雷达结构的类型为包括至少两个减速电动机(2，3)，该减速电动机穿过连接装置(8，9)连接到雷达天线结构上，其特征在于，连接装置(8，9)对于每个减速电动机包括与脱开转矩限制器装置平行工作的自由轮联接装置。 | ||||||
| 7 | 动力传递装置 | CN201480019902.8 | 2014-03-26 | CN105121885A | 2015-12-02 | 加藤基; 黑须義弘; 神沢贵浩 |
| 本发明提供一种动力传递装置，其具备与动力源连接的滑轮(4)、和位于与滑轮(4)同一轴线上的旋转轴。具备设于旋转轴上的轮毂(11)、和可与该轮毂(11)分离的嵌合的环板(12)。具备将环板(12)向与旋转轴线平行的方向朝轮毂(11)施力的板簧(16)。在旋转轴的负载小于阈值的情况下，轮毂(11)和环板(12)通过摩擦力一体旋转。在旋转轴的负载大于等于阈值时，环板(12)相对于轮毂(11)旋转，通过板簧(16)的弹力向与旋转轴线平行的方向移动，使环板(12)与轮毂(11)分离。可以提供当从动侧旋转体的负载扭矩增大后，在短时间内切断动力传递的动力传递装置。 | ||||||
| 8 | 带有起动器/发电机的辅助齿轮箱 | CN201110462031.5 | 2011-12-28 | CN102562316B | 2016-08-17 | 黄豪; J·齐沃特 |
| 本发明涉及带有起动器/发电机的辅助齿轮箱。一种用于燃气涡轮发动机(1)的组件(102)包括：包括驱动齿轮(150)和小齿轮(140)的辅助齿轮箱(100)；和机械地安装到辅助齿轮箱(100)的起动器/发电机(101)。起动器/发电机(101)包括壳体(160)和带有保险断开器(192)的可旋转轴(170)的部分，其中保险断开器(192)设置在起动器/发电机(101)的壳体(160)内。 | ||||||
| 9 | 推拉力过载保护装置 | CN201511007807.9 | 2015-12-29 | CN105485198A | 2016-04-13 | 宋晓伟; 余晓锁 |
| 本发明公开了一种推拉力过载保护装置，包括推拉力动力源、推拉杆、连接套、壳体和锁紧块，推拉力动力源通过第一螺钉与连接套的一端固定连接，连接套、壳体和锁紧块均套设在推拉杆上，壳体的一端与连接套的另一端卡合，壳体内沿轴向设置有安装孔，安装孔内依次设置有滚珠、一端与滚珠抵触的顶杆、一端与顶杆的另一端固定的弹簧，弹簧的另一端固定在壳体上，顶杆的一端为斜坡结构，连接套沿径向设置有与滚珠配合的环形槽，锁紧块通过第二螺钉与壳体的另一端固定连接，锁紧块与推拉杆固定连接。其结构简单、紧凑，设计合理；在工作机与原动机之间形成过载保护既可提高设备运行的安全可靠性，又有效提高了工作效率。 | ||||||
| 10 | 机械保护方法和装置 | CN201280004513.9 | 2012-01-03 | CN103314231A | 2013-09-18 | 弗雷德里克·费迪南德·杰克斯·巴特列 |
| 本发明涉及到提供机械保护的装置领域和方法，特别涉及到一种带有传动轴(1)的机械保护装置，所述传动轴弯曲时的共振频率对应于传动轴(1)预定旋转过速，所述传动轴不能充分阻尼到可避免因为所述弯曲共振而造成的传动轴(1)断裂，本发明还涉及到一种机械保护方法，按照这种方法，传动轴(1)会因为弯曲时的这种共振而断裂。 | ||||||
| 11 | 압축기의 동력전달장치 | KR1020100056734 | 2010-06-15 | KR1020110136612A | 2011-12-21 | 김승길; 신충한; 정석제 |
| PURPOSE: A power transmission device for a compressor is provided to prevent damage to components of a compressor due to the fatigue load of the compressor. CONSTITUTION: A power transmission device for a compressor rotates the rotary shaft of a compressor at a pulley in which power is transferred from an engine. The power transmission device comprises a disk(110), a polygonal nut(120), and a hub(130). The disk is rotated by the pulley. A coupling groove(112) is formed in one side of the disk. The polygonal nut is coupled to the coupling groove of the disk and is rotated with the disk. The hub is screwed on the nut and transfers rotational power to the rotary shaft of the compressor. | ||||||
| 12 | 동력전달장치 | KR1020020040663 | 2002-07-12 | KR100723814B1 | 2007-05-31 | 손은기 |
| 본 발명은 초기 시동시 발생되는 기동 토오크를 완화시켜 수명을 향상시키고, 간단한 구조로 이상 토오크가 발생한 경우 구동원으로부터의 해제가 용이하도록 하기 위한 것으로, 구동원에 연결되어 회전력을 공급받는 풀리와, 상기 풀리 상에 적어도 하나 이상 설치되는 것으로, 상기 풀리의 회전 방향으로 돌출된 적어도 하나 이상의 돌기가 구비된 댐퍼와, 종동기기의 회전축에 결합되는 것으로, 상기 댐퍼에 체결되고 상기 댐퍼의 돌기를 지지하는 변형부를 갖는 적어도 하나 이상의 변형부재가 구비되어 상기 풀리로부터 회전력을 공급받아 상기 회전축에 전달하는 커버 플레이트를 포함하여 이루어진 것을 특징으로 하는 동력전달장치에 관한 것이다. | ||||||
| 13 | Automatically actuated disconnect couplings | US15418387 | 2017-01-27 | US10132369B2 | 2018-11-20 | Craig R. Legros; David S. Behling |
| An automatic disconnect coupling includes a retainer and a biasing member. The biasing member is coupled to the retainer and is arranged to communicate excitation from a generator input member to the retainer. The retainer and the biasing member have a fundamental frequency tuned to the rotational speed of the generator input member to automatically disconnect the input member from a drive member when rotating unbalance of the input member exceeds a predetermined level. | ||||||
| 14 | AUTOMATICALLY ACTUATED DISCONNECT COUPLINGS | US15418387 | 2017-01-27 | US20180216678A1 | 2018-08-02 | Craig R. Legros; David S. Behling |
| An automatic disconnect coupling includes a retainer and a biasing member. The biasing member is coupled to the retainer and is arranged to communicate excitation from a generator input member to the retainer. The retainer and the biasing member have a fundamental frequency tuned to the rotational speed of the generator input member to automatically disconnect the input member from a drive member when rotating unbalance of the input member exceeds a predetermined level. | ||||||
| 15 | Connection Device for a Drive Train | US15708282 | 2017-09-19 | US20180003244A1 | 2018-01-04 | Franz SCHNEIDER; Erwin FUSSEDER; Wolfgang STREINZ; Josef HOFSTETTER; Hans BLIENINGER |
| The invention provides a connection device for a joint shaft in a motor vehicle. The connection device includes an axis of rotation, a first connection area for connecting the connection device to a drive train element, a predetermined breaking region, and a tube region which connects directly to the predetermined breaking region. The connection device has an axial extension in the direction of the axis of rotation, and a radial extension orthogonal to the axis of rotation and is designed, at least substantially, as a tubular hollow body. The predetermined breaking region is arranged between the first connection region and the tube region in the axial direction. A connection area is arranged in the axial direction between the first connection region and the predetermined breaking region. | ||||||
| 16 | Accessory gearbox with a starter/generator | US12979579 | 2010-12-28 | US09650964B2 | 2017-05-16 | Hao Huang; Jan Zywot |
| An assembly for a gas turbine engine comprising an accessory gearbox comprising a drive gear and pinion gear and a starter/generator mechanically mounted to the accessory gearbox. The starter/generator comprising a housing and a portion of a rotatable shaft with a safety disconnect where the safety disconnect is located within the housing of the starter/generator. | ||||||
| 17 | PROTECTION SYSTEM OF A RAILWAY VEHICLE TRACTION SYSTEM, ASSOCIATED TRANSMISSION LINE AND ASSOCIATED RAILWAY VEHICLE | US15018200 | 2016-02-08 | US20160229421A1 | 2016-08-11 | Robert Periot |
| A protection system of a railway vehicle traction system includes an electric motor and an electrical power supply circuit. The system further includes: a mechanical coupler between first and second components of a transmission line, the first component being connected to an output shaft of the electric motor and the second component being connected to an input shaft of an axle of the railway vehicle, the coupler being able to be in an engaged or disengaged state; and a controller able to apply a disengagement signal to the coupling signal, to switch from the engaged state to the disengaged state if a failure of the power supply circuit and/or the electric motor is detected. | ||||||
| 18 | Coupling mechanism between a manual flight control member and a trim actuator of an aircraft | US14330068 | 2014-07-14 | US09193438B2 | 2015-11-24 | Brice Lebernicheux; Andre Le-Gall |
| A coupling mechanism between a control member (1′) that generates manual flight commands and a trim actuator (4) forming part of a mechanical transmission train for transmitting flight commands in an aircraft. The coupling mechanism comprises axial engagement means between a lever arm (3) mechanically connected to the control member (1′) and a pivot shaft (10) forming part of the trim actuator (4). The axial engagement means comprise co-operating interlocking members (13, 14) arranged on coupling members (18, 19) constrained to move in rotation respectively with the lever arm (3) and with the pivot shaft (10). Each of the coupling members (18, 19) includes axial passages (26) enabling the other coupling member (18, 19) to pass axially therethrough. An interruption of said axial engagement causes the coupling members (18, 19) to move axially one through the other under the effect of axial thrust (P) exerted by elastically deformable means (15) used for obtaining said axial engagement. | ||||||
| 19 | Torque-limiting coupling | US13980683 | 2012-01-18 | US09051972B2 | 2015-06-09 | Seamus Garvey; James Simonds |
| Described herein is a torque-limiting coupling provided for connecting coaxial, first and second rotating shafts. The coupling includes a first connecting part on an end of the first shaft and a second connecting part on an end of the second shaft. An interconnector joins to the first connecting part at a first engagement formation, and joins to the second connecting part at a second engagement formation. The first engagement formation threadingly joins the interconnector to the first connecting part. The second engagement formation can resist rotational movement of the interconnector relative to the second connecting part but allows movement of the interconnector in the axial direction of the shafts. When a torque transmitted by the shafts exceeds a predetermined value, the interconnector rotates relative to the first connecting part at the threaded engagement formation. The resistance to rotational movement relative to the second connecting part causes the interconnector to move in an axial direction of the shafts, and come out of engagement with the first and/or the second connecting part. | ||||||
| 20 | COUPLING MECHANISM BETWEEN A MANUAL FLIGHT CONTROL MEMBER AND A TRIM ACTUATOR OF AN AIRCRAFT | US14330068 | 2014-07-14 | US20150014480A1 | 2015-01-15 | Brice LEBERNICHEUX; Andre LE-GALL |
| A coupling mechanism between a control member (1′) that generates manual flight commands and a trim actuator (4) forming part of a mechanical transmission train for transmitting flight commands in an aircraft. The coupling mechanism comprises axial engagement means between a lever arm (3) mechanically connected to the control member (1′) and a pivot shaft (10) forming part of the trim actuator (4). The axial engagement means comprise co-operating interlocking members (13, 14) arranged on coupling members (18, 19) constrained to move in rotation respectively with the lever arm (3) and with the pivot shaft (10). Each of the coupling members (18, 19) includes axial passages (26) enabling the other coupling member (18, 19) to pass axially therethrough. An interruption of said axial engagement causes the coupling members (18, 19) to move axially one through the other under the effect of axial thrust (P) exerted by elastically deformable means (15) used for obtaining said axial engagement. | ||||||
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