Abstract in simplified Chinese:本发明的课题系提供一种具有输入轴承的谐波齿轮单元,其具备由易于制作及组装的轴承设备所支承的输入轴。本发明的解决手段系:谐波齿轮单元(1),系借由第1输入轴承(7)、及第2输入轴承(8)对内置的谐波齿轮设备(5)之输入轴(6)进行支承。由于输入轴(6)系固定于安装在此的谐波产生器(16)之轴方向的位置,所以马达组装作业十分简单。支承着输入轴(6)的第2输入轴承(8)之轴承外壳(21)系夹持可挠性外齿齿轮(15)的圆环状凸面部(15c),再借由紧固螺栓(22)锁紧固定于输出用圆盘(4)。不必对圆环状凸面部(15c)进行切螺纹加工、或凹部等之加工,借由简单之构造即可构成用以将输入轴(6)的轴承设备、及可挠性外齿齿轮(15)固定于输出用圆盘(4)上之固定设备。
Abstract in simplified Chinese:一种具有由分离磁芯连接成环形的定子芯的分离磁芯型电动机定子。每个分离磁芯在两端面形成一个耦合凸起和一个耦合凹槽,在分离磁芯的连接方向耦合凸起能够被可分离的安装在耦合凹槽内。相邻分离磁芯通过使用由耦合凸起和耦合凹槽组成的机械耦合结构连接。定子芯的装配过程因为不需要焊接和粘合工作能够被容易地在短时间内实现。
Abstract in simplified Chinese:一种行星齿轮设备(1)包括从内侧的顺序同心设置的第一,第二以及第三环形件(10,20,30)。太阳齿轮(4)同轴被固定在第一环形件(10)的端面上,行星齿轮(6-1至6-4)的行星轴(61至64)被支承在第二环形件(20)的端面上,将内齿轮(2)同轴固定至第三环形件(30)的端面上。在第一和第二环形件(10,20)之间形成第一十字滚柱轴承(40),在第二和第三环形件(20,30)之间形成第二十字滚柱轴承(50)。每一个部件均同心设置在与设备轴线(1a)垂直的一个平面上,以便获得在设备的轴向非常薄的行星齿轮设备。由于从设备轴向的两侧获得相应的齿轮部分,因此,能够以很大的自由度布置输入端和输出端。
Abstract:
An exemplary encoder assembly includes a substrate, a first encoder, and a second encoder. The substrate has two or more position sensors, each position sensor being configured for detecting a rotary position of a shaft or other rotating element of a machine. The first encoder includes at least one first position sensor of the two or more position sensors. The at least one first position sensor is disposed on the substrate for off-axis alignment with a shaft or other rotating element of a machine. The second encoder includes a second position sensor of the two or more position sensors, the second position sensor being disposed on the substrate for on-axis or off-axis alignment with the shaft or other rotating element of a machine. Each position sensor is configured to detect different or common signal types, and a signal type of the second position sensor excludes optical signals.
Abstract:
A detecting device (1) is provided with first and second discs (6 and 7) fixed to a rotating shaft (2). In the first disc (6), a first slit row (8) and a slit row (9) for encoder are formed as a common slit row (10). In the second disc (7), a second slit row (12) is formed. The light emitted from a photosensor (13) is led by an optical fiber cable (135) through the first and second slit rows (8 and 12). The angular acceleration of the rotating shaft (2) is detected from the relative movement between the slits. An encoder (14) detects the angle of the shaft (2) by detecting the movement of the slit row (9). Since the light wave guide of the photosensor (13) is formed of an optical fiber, the two discs (6 and 7) can be attached to arbitrary positions. In addition, since the slits are commonly used, the manufacture of an optical rotational information detecting device becomes easier. Therefore, a small-sized compact rotational information detecting device having a high degree of freedom in design can be manufactured inexpensively.
Abstract:
A silk hat flexible engagement gear device (1) has first and second end plates (2 and 3) and an input shaft (4) is rotatably supported, with their ends supported, between the two end plates. A cylindrical body part (61) of a silk hat flexible external gear (6) is disposed on the outer circumference of the input shaft (4). A cross roller bearing (8) which also functions as a device housing and a rigid internal gear (5) are provided on the outer circumference. An annular boss (64) of the flexible external gear is held between the outer ring (81) of the cross roller bearing and the second end plate (3) and these three members are coupled with each other with second fixing bolts (9). The rigid internal gear (5) is held between the inner ring (82) of the cross roller bearing and the first end plate (2) and these three members are coupled with each other with first fixing bolts (11). An additional member which is used as a device housing is not necessary. The members are temporarily fixed and fastened and, further, attached to a housing on the motor side or on the load side with the fixing bolts (9 and 11) only. Therefore, the number of components of the device can be reduced and the size of the device can be reduced.
Abstract:
A meshing type gear device designed to improve further its strength and wear resistance, and more particularly to improve the wear resistance of the tooth surface. In a meshing type gear device (1), a spur gear is used both for a rigid internal gear (2) and a flexible external gear (3), and the number of teeth of the flexible external gear (3) is made greater by two than that of the rigid internal gear (2). The tooth profile of the flexible external gear (3) is formed into a convex tooth profile which is in the form of a curve AC that is to be obtained through similar transformation at a reduction ratio lambda of a convex portion (a curve between A and B) relative to the internal gear of a moving path L by rack approximation drawn by the external gear relative to the internal gear with a limiting point A of the contact between the two gears on the path serving as an origin, while the tooth profile of the rigid internal gear (2) is formed into a concave tooth profile which is in the form of a curve AD that is to be obtained through similar transformation at an enlargement ratio (1 + lambda ) of the same convex portion relative to the internal gear of the moving path with the limiting point A of the contact serving as an origin, whereby a continuously contactable and passing meshing can be produced between the two tooth profiles. With this configuration, it is possible to remarkably increase the capability of maintaining a lubricating oil film between the tooth surfaces and remarkably improve the permissible delivered torque of the flexible meshing type gear device based on the tooth surface wear.
Abstract:
In the rotation angle detector (5) of a flexure engagement gear device (1), a 1st torque detector (6) and a 2nd torque detector (7) are provided at the diaphragm (32) part of a cup-shaped flexible gear (3) at an angular interval of 45 degrees around the center axis (1a). The outputs of the 1st and 2nd torque detectors (6 and 7) are sine waves whose phases are shifted 90 DEG from each other. Therefore, by utilizing the torque detection outputs (6S and 7S), the rotation angle of the output side member of the gear device (1) can be detected.
Abstract:
A planetary gear device (20) comprises a first-stage side planetary gear mechanism (22) and a second-stage side planetary gear mechanism (23). The first-stage side planetary gear mechanism (23) includes an internal gear (25), a carrier (29) rotatably supported by a pair of main bearings (26, 27) disposed on both sides of the internal gear (25), a plurality of planetary gears (31) rotatably supported round a plurality of planetary shafts (30) extending between a pair of right and left carrier portions (28A, 28B) of the carrier (29), a sun gear (33) provided round the outer circumference of a pinion shaft (32) extending in the axial direction of the gear device through the carrier (29), and an output shaft (34) connected to the carrier (29) and extending in the direction of the axis (20a) of the gear device. The carrier (29) and the output shaft (34) are formed as a unitary member, and a pin so driven as to extend between the portions (28A, 28B) of the carrier (29) fabricated as the unitary member is used as the planetary shaft (30). Therefore, the planetary gear device (20) has a reduced number of components, can be produced easily and has high assembly accuracy.
Abstract:
A silk hat flexible external gear (13) of a flexible engagement gear device (11) comprises a body part (22), a diaphragm (23) and a boss (25). The one side of the shape of the cross section which is obtained by cutting a plate-shaped part (28) of the diaphragm (23) along a plane including the device axis (11a) is defined by a straight line (231) extending in a radial direction. The other side of the shape of the cross section is defined by a first convex circular arc (240), a concave circular arc (250) and a second convex circular arc (260) in this order from the boss side. Among those circular arcs, the first convex circular arc (240) has the smallest curvature and the concave circular arc (250) has the largest curvature. The concave circular arc (250) is at the center position of the plate-shaped part (28), which has the smallest thickness in the plate-shaped part (28). If the flexible external gear having this cross section is used, when the axial length is reduced, the stress concentration can be relieved without increasing the outer diameter.