FUSION GEAR REDUCER

Abstract

A fusion gear reducer includes a first-stage gear reduction unit and a second-stage gear reduction unit both in a housing. The first-stage gear reduction unit includes a sun gear, a planet gears support, planet gears spaced around the sun gear and meshed therewith, and a ring gear around the planet gears and meshed therewith. The second-stage gear reduction unit includes spaced rollers arranged as a circle, roller grooves, wells formed on an inner surface of the housing, and a cam surface formed on an outer surface of the ring gear so that the ring gear is output of the first-stage gear reduction unit and input of the second-stage gear reduction unit. The roller grooves are disposed on outer surfaces of the planet gears so that the planet gears are output of the second-stage gear reduction unit. The simplified fusion gear reducer solves the problem of bulkiness of gear reducer.

Claims

1. A fusion gear reducer comprising: a housing; a first-stage gear reduction unit disposed in the housing, the first-stage gear reduction unit being an epicyclic gear train including a planet gears support, a sun gear as an input, a plurality of planet gears equally spaced around the sun gear and meshed therewith, and a ring gear disposed around the planet gears and meshed therewith; and a second-stage gear reduction unit disposed in the housing, the second-stage gear reduction unit being a harmonic drive including a plurality of equally spaced rollers arranged as a circle, a plurality of roller grooves, a plurality of wells formed on an inner surface of the housing, and a cam surface formed on an outer surface of the ring gear wherein the roller grooves are disposed between the cam surface and the wells, and the rollers are rotatably disposed in the roller grooves and confined by the cam surface, the wells, and the roller grooves; wherein the ring gear is an output of the first-stage gear reduction unit and an input for driving the second-stage gear reduction unit; wherein the rollers rotate the roller grooves; wherein the roller grooves are formed on an outer surface of the planet gears support; and wherein the planet gears support is an output of the second-stage gear reduction unit.

2. The fusion gear reducer of claim 1, wherein the sun gear, the cam surface, and the rotation center of the roller grooves are configured to rotate around the common axis.

3. The fusion gear reducer of claim 1, wherein the roller grooves are disposed between the cam surface and the wells having the rollers disposed therein.

4. The fusion gear reducer of claim 3, wherein the rollers are pushed by the cam surface to partially dispose in the wells to rotate the roller grooves.

5. The fusion gear reducer of claim 4, wherein the cam surface has two arc members on two annular, outer edges respectively, and wherein the rollers are pushed by the arc members to partially dispose in the wells to rotate the roller grooves.

6. The fusion gear reducer of claim 2, wherein the roller grooves are disposed between the cam surface and the wells having the rollers partially disposed therein.

7. The fusion gear reducer of claim 6, wherein the rollers are pushed by the cam surface to partially dispose in the wells to rotate the roller grooves.

8. The fusion gear reducer of claim 7, wherein the cam surface has two arc members on two annular, outer edges respectively, and wherein the rollers are pushed by the arc members to partially dispose in the wells to rotate the roller grooves.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0014] These and other features and advantages of the various embodiments disclosed herein will be better understood with respect to the following descriptions and drawings, in which like numbers refer to like parts throughout, and in which:

[0015] FIG. 1 is an exploded view of a fusion gear reducer according to the invention;

[0016] FIG. 2 is a longitudinal section view of the assembled fusion gear reducer;

[0017] FIG. 3 is a section view along line A-A of FIG. 2;

[0018] FIG. 4 is a partial close view of FIG. 3 showing the roller disposed between the well and the ring gear; and

[0019] FIG. 5 is a view similar to FIG. 3 showing a force balance among the cam surface, the rollers, the roller grooves, and the wells.

DETAILED DESCRIPTION

[0020] Referring to FIGS. 1 to 3, a fusion gear reducer in accordance with a preferred embodiment of the invention comprises a housing 10, a first-stage gear reduction unit 20, and a second-stage gear reduction unit 30 as discussed in detail below.

[0021] The housing 10 includes an axial space 11. The housing 10 is a fixed device for mounting the speed reducer on the equipment. Further, the housing 10 is also used as a mounting seat for the first-stage gear reduction unit 20 and the second-stage gear reduction unit 30 of the fusion gear reducer in the space 11.

[0022] The first-stage gear reduction unit 20 is implemented as an epicyclic gear train including a sun gear 21, a plurality of planet gears 22 and a ring gear 24. The sun gear 21 is the power input of the fusion gear reducer. Specifically, the sun gear 21 is attached to a rotational shaft of a drive (not shown) such as motor. More specifically, the motor is a servo motor or a step motor. The motor can rotate the sun gear 21 in operation.

[0023] The planet gears 22 are equally spaced around the sun gear 21 and mesh therewith. As shown, the planet gears 22 rotate around four axes of a planetary carrier 23 which is circularly disposed in the space 11 by a ring shaped bearing member 40.

[0024] The ring gear 24 is disposed around the planet gears 22 and meshes therewith. That is, the planet gears 22 are disposed between the sun gear 21 and the ring gear 24. The sun gear 21 driven by actuator causes the planet gears 22 to rotate by their own axes and revolute around the sun gear 21. And in turn, the ring gear 24 rotates simultaneously.

[0025] The second-stage gear reduction unit 30 is implemented as a wave-driven speed reducer including a plurality of equally spaced rollers 31 arranged as a circle, a plurality of roller grooves 32, a plurality of wells 33, and a wavy cam surface 34 on an outer surface of the ring gear 24 to serve as a mounting seat of the housing 10 as well as a seat of the wells 33. The cam surface 34 are formed on the outer surface of the ring gear 24. The roller grooves 32 are disposed between the cam surface 34 and the wells 33. The rollers 31 are rotatably disposed in the roller grooves 32 and are confined by the cam surface 34, the wells 33 and the roller grooves 32.

[0026] Specifically, the cam surface 34 includes at least one convex arc member 341 formed of spline on either annular, outer edge. The convex arc member 341 bears the force applied by the rotating rollers 31 and thus shapes as a wave. In the embodiment, the rollers 31 are cylindrical. In the other embodiments, the rollers 31 are spherical. The roller grooves 32 are formed on an outer surface of the planetary carrier 23. The planetary carrier 23 functions as a seat of the roller grooves 32. As a result, the planetary carrier 23 serves as an output of the second-stage gear reduction unit 30. Further, the cam surface 34 is formed on the outer surface of the ring gear 24 and the roller grooves 32 are formed on the outer surface of the planetary carrier 23. Thus, the sun gear 21, the cam surface 34 and the roller grooves 32 have a common axis and they rotate around the common axis in operation.

[0027] Referring to FIG. 4 in conjunction with FIGS. 1 to 3, it is an enlarged view of a portion of FIG. 3 showing the roller 31 disposed between the well 33 and the cam surface 34 of the ring gear 24. As shown in the embodiment, the rollers 31 are rotatably supported by the convex arc members 341 of the cam surface 34 and two contour surfaces 331 of the well 33. And in turn, the rollers 31 are rotated by the convex arc members 341 of the cam surface 34 and rotatably contact the contour surfaces 331 of the well 33. And in turn, the roller grooves 32 are rotated. As a result, the planetary carrier 23 is rotated to generate an output having a decreased rotational speed.

[0028] The contour surfaces 331 include a first contour surface 331a and a second contour surface 331b at an angle with respect to the first contour surface 331a. A valley 332 is formed between the first contour surface 331a and the second contour surface 331b. A curved ridge 333 is formed between two adjacent wells 33, i.e., between the first contour surface 331a of one well 33 and the second contour surface 331b of the other well 33. The wells 33 are formed on the inner surface 11a of the housing 10 as shown in FIG. 1.

[0029] Referring to FIG. 5, when the cam surface 34 pushes the roller 31 against the first contour surface 331a and the second contour surface 331b of the well 33, a sufficient force is applied on the roller 31 by the first contour surface 331a and the second contour surface 331b. Also, the force applied on the roller 31 by the first contour surface 331a and the second contour surface 331b in the well 33 transmits to the roller 31 through the cam surface 34. Therefore, the transmission accuracy and the efficiency of the wave-driven speed reducer are improved. And in turn, transmission of the wave-driven speed reducer is more precise.

[0030] As shown in FIGS. 2 and 5, force transmitted by both the first-stage gear reduction unit 20 and the second-stage gear reduction unit 30 is described in detail below. The planet gears 22 driven by the sun gear 21 (i.e., the input) rotate about their own axes. The planet gears 22 not only mesh the ring gear 24 but also rotate the planetary carrier 23. Thus, the ring gear 24 is the output of the first-stage gear reduction unit 20 and the input for driving the second-stage gear reduction unit 30. In detail, the planetary carrier 23 is an idler while transmitting power from the first-stage gear reduction unit 20 to the second-stage gear reduction unit 30. With respect to the first-stage gear reduction unit 20, the ring gear 24 generates an output having a first gear reduction ratio. And in turn, the convex arc members 341 of the cam surface 34 on the outer surface of the ring gear 24 push the rollers 31 to contact the contour surfaces 331 in the wells 33. Thus, force is transmitted to the roller grooves 32. As a result, the planetary carrier 23 generates an output having a second gear reduction ratio. Therefore, an output rotation for driving the planetary carrier 23, which forming the roller grooves 32, as a second gear reduction ratio is generated. The planetary carrier 23, as an idler, is confined by the cam surface 34, the rollers 31, the wells 33 and the roller grooves 32 of the second-stage gear reduction unit 30 in the force imparting process. As a result, an output rotation having a second gear reduction ratio is generated and the output rotation is to be used by the external power requirement terminal.

[0031] In view of above description, the first-stage gear reduction unit 20 and the second-stage gear reduction unit 30 of the fusion gear reducer of the invention have the advantages of greatly increasing gear reduction ratio in a limited space, forming the roller grooves 32 of the wave-driven speed reducer on the outer surface of the planetary carrier 23, functioning the planetary carrier 23 as the seat (or plate) of the roller grooves 32, forming the wells 33 on an inner surface of the housing 10, integrally forming the cam surface with the outer surface of the ring gear 24, simplifying the construction of the fusion gear reducer, and rendering a compact design.

[0032] Although the present invention has been described with reference to the foregoing preferred embodiments, it will be understood that the invention is not limited to the details thereof. Various equivalent variations and modifications can still occur to those skilled in this art in view of the teachings of the present invention. Thus, all such variations and equivalent modifications are also embraced within the scope of the invention as defined in the appended claims.