PLANETARY GEAR REDUCER

• US 20130310213A1
• Filed: 11/15/2011
• Published: 11/21/2013
• Est. Priority Date: 11/25/2010
• Status: Active Grant

• Current Assignee: Kawasaki Jukogyo Kabushiki Kaisha (Kawasaki Heavy Industries Limited)
• Original Assignee: Kawasaki Jukogyo Kabushiki Kaisha (Kawasaki Heavy Industries Limited)
• Inventors: Nishikawa, Hiroyasu, Imai, Hideyuki, Goi, Tatsuhiko, Matsuoka, Tetsuya, Sato, Kazuhiro
• Granted Patent: US 8,968,148 B2
• Time in Patent Office: Days
• US Class Current: 475/347
• CPC Class Codes: F16H 1/28 with gears having orbital motion
• CPC Class Codes: F16H 1/2818 by allowing limited movement of the ring gear relative to the casing or shaft
• CPC Class Codes: F16H 57/082 Planet carriers

Abstract

A planetary gear reducer (1) includes: a sun gear (5) having external teeth and fixed concentrically to a power input shaft (3); a plurality of planet gears (7) having external teeth and mashing with the sun gear (5); a ring gear (9) having internal teeth and meshing with the planet gears (7); a planet carrier (11) configured to support a plurality of planet shafts (13), each of which is a rotational axis of a corresponding one of the planet gears (7), and to output revolution of the plurality of planet gears (7) as first power; and a cylindrical support (27) connected to the ring gear (9) such that the cylindrical support (27) is non-rotatable relative to the ring gear (9), the cylindrical support (27) being configured to output rotation of the ring gear (9) as second power. The cylindrical support (27) includes, at its one part along the direction of a central axis, a flexible structure (41) which is curved radially inward and has a V-shaped longitudinal section. This configuration makes it possible to both obtain rigidity and prevent misalignment while suppressing an increase in the weight of the gear reducer.

Claims

1. A planetary gear reducer comprising:

a sun gear fixed concentrically to a power input shaft;

a ring gear provided along an outer periphery of the sun gear;

a plurality of planet gears meshing with the sun gear and the ring gear;

a plurality of planet shafts, each of which is a rotational axis of a corresponding one of the plurality of planet gears;

a planet carrier configured to support the plurality of planet shafts, and to output revolution of the plurality of planet gears around the input shaft as first power; and

a cylindrical support including, at its one part along a direction of a central axis of the input shaft, a flexible structure which is curved radially inward and has a V-shaped longitudinal section, the cylindrical support being connected to the ring gear such that the cylindrical support is non-rotatable relative to the ring gear, the cylindrical support being configured to output rotation of the ring gear as second power.

2. The planetary gear reducer according to claim 1, wherein an angle of the V-shape of the longitudinal section of the flexible structure is in a range from 30°

to 90°

.

3. The planetary gear reducer according to claim 1, wherein the cylindrical support includes a larger-diameter cylindrical portion and a smaller-diameter cylindrical portion, the larger-diameter cylindrical portion being formed nearer to the ring gear than the flexible structure and having a wall thickness smaller than that of the flexible structure, the smaller-diameter cylindrical portion being formed nearer to an output side of the cylindrical support than the flexible structure.

4. The planetary gear reducer according to claim 1, wherein

the ring gear includes an outward flange protruding radially outward,

the cylindrical support includes an inward flange protruding radially inward, and

the ring gear and the cylindrical support are connected to each other via the outward flange and the inward flange.

5. The planetary gear reducer according to claim 4, wherein

connection portions connecting the outward flange and the inward flange are each configured in a form of a chevron-shaped pattern.

6. The planetary gear reducer according to claim 4, wherein

the outward flange protrudes in the direction of the central axis of the input shaft toward the cylindrical support, and includes an annular connection wall having an outer periphery whose shape is such that crests and troughs are formed alternately, and

the inward flange has an inner periphery whose shape is such that crests and troughs are formed alternately, and the crests and troughs mesh with the crests and troughs of the outer periphery of the connection wall.

7. The planetary gear reducer according to claim 3, wherein

The wall thickness of the larger-diameter cylindrical portion is in a range from 85% to 95% of the wall thickness of the flexible structure.

8. The planetary gear reducer according to claim 3, wherein

the flexible structure includes a tapered shape which is formed so as to be inclined radially inward from the larger-diameter cylindrical portion, such that the tapered shape is inclined relative to the direction of the central axis of the input shaft in a range from 45°

to 60°

.

9. The planetary gear reducer according to claim 2, wherein the cylindrical support includes a larger-diameter cylindrical portion and a smaller-diameter cylindrical portion, the larger-diameter cylindrical portion being formed nearer to the ring gear than the flexible structure and having a wall thickness smaller than that of the flexible structure, the smaller-diameter cylindrical portion being formed nearer to an output side of the cylindrical support than the flexible structure.

10. The planetary gear reducer according to claim 5, wherein

the outward flange protrudes in the direction of the central axis of the input shaft toward the cylindrical support, and includes an annular connection wall having an outer periphery whose shape is such that crests and troughs are formed alternately, and

the inward flange has an inner periphery whose shape is such that crests and troughs are formed alternately, and the crests and troughs mesh with the crests and troughs of the outer periphery of the connection wall.