A balanced speed reducer of a dual-sun gear variable-line-speed planetary row, comprising:
- a dual-sun gear variable-line-speed planetary row;
- an input end;
- an output end;
- a locking end;
- and
- a bearing auxiliary device,
- wherein the dual-sun gear variable-line-speed planetary row comprises:
- a left sun gear, a right sun gear and a planet carrier with planetary gears, the planet carrier is configured to support the planetary gears,
- wherein reference center distances are defined between respective planetary gear axes and a revolution axis, the reference center distances being equal;
- on a gear axis of each planetary gear, a left planetary gear and a right planetary gear are arranged in sequence,
- wherein each set of a number of teeth of the left sun gear, a number of teeth of the right sun gear, a number of teeth of the left planetary gear, and a number of teeth of the right planetary gear is a teeth number combination;
- the number of teeth of the right sun gear*the number of teeth of the left planetary gear/(the number of teeth of the left sun gear*the number of teeth of the right planetary gear) is a range specifying parameter;
- the number of planetary gear axes supported by the planet carrier is the number K of gear sets,
- wherein for the range specifying parameter, each teeth number combination makes a value of the range specifying parameter be greater than 0.875, less than 1.142857, and not equal to 1.0, and
- wherein the number K of gear sets is an integer not less than two, and when the teeth number combination and the number of gear sets are set, a principle of matching the teeth number combination with the number of gear sets is:
- (1) when an absolute value of a difference between the number of teeth of the left sun gear and the number of teeth of the right sun gear is a multiple of 2, the number of gear sets is 2;
- (2) when an absolute value of a difference between the number of teeth of the left sun gear and the number of teeth of the right sun gear is a multiple of 3, the number of gear sets is 3;
- (3) when an absolute value of a difference between the number of teeth of the left sun gear and the number of teeth of the right sun gear is a multiple of 4, the number of gear sets is 4 or 2;
- (4) when an absolute value of a difference between the number of teeth of the left sun gear and the number of teeth of the right sun gear is a multiple of 5, the number of gear sets is 5;
- (5) when an absolute value of a difference between the number of teeth of the left sun gear and the number of teeth of the right sun gear is a multiple of 6, the number of gear sets is 6, 3 or 2;
- (6) when an absolute value of a difference between the number of teeth of the left sun gear and the number of teeth of the right sun gear is a multiple of 8, the number of gear sets is 8, 4 or 2;
- (7) when an absolute value of a difference between the number of teeth of the left sun gear and the number of teeth of the right sun gear is a multiple of 10, the number of gear sets is 5 or 2;
- wherein the planetary gears are configured by dividing the number of teeth of the left sun gear by the number K of gear sets to obtain a remainder, wherein a value of the remainder ranges from 0 to (K−1) and is an integer;
- during manufacturing of planetary gears, selecting an equiphase surface on a first planetary gear so that the equiphase angle value is a, selecting an equiphase surface on a second planetary gear so that the equiphase angle value is (a+1*2π*remainder value/K), selecting an equiphase surface on a third planetary gear so that the equiphase angle value is (a+2*2π*remainder value/K), sequentially manufacturing a fourth planetary gear, a fifth planetary gear, a sixth planetary gear, and a seventh planetary gear by analogy, and selecting an equiphase surface on a Kth planetary gear so that the equiphase angle value is (a+(K−1)*2π*remainder value/K);
- during assembly of planetary gears, the two sun gears and the planet carrier are assembled in place on the revolution axis, each mounting surface is calibrated, the equiphase surface of the first planetary gear with the equiphase angle value being a is caused to coincide with a first mounting surface, left and right equiphase points are caused to be within the reference center distance, the first planetary gear is assembled, the equiphase surface of the second planetary gear with the equiphase angle value being (a+1*2π*remainder value/K) is caused to coincide with a second mounting surface, left and right equiphase points are caused to be within the reference center distance, the second planetary gear is assembled, the equiphase surface of the third planetary gear with the equiphase angle value being (a+2*2π*remainder value/K) is caused to coincide with a third mounting surface, left and right equiphase points are caused to be within the reference center distance, the third planetary gear is assembled, the fourth planetary gear, the fifth planetary gear, the sixth planetary gear, and the seventh planetary gear are assembled by analogy, the equiphase surface of the Kth planetary gear with the equiphase angle value being (a+(K−1)*2π*remainder value/K) is caused to coincide with a Kth mounting surface, left and right equiphase points are caused to be within the reference center distance, and the Kth planetary gear is assembled;
- wherein gear reference circle radii are configured by setting a reference circle radius of the left sun gear and a reference circle radius of the left planetary gear around the reference center distance, so that the number of teeth of the left sun gear/the number of teeth of the left planetary gear=the reference circle radius of the left sun gear/the reference circle radius of the left planetary gear, and that the reference circle radius of the left sun gear+the reference circle radius of the left planetary gear=the reference center distance, and setting a reference circle radius of the right sun gear and a reference circle radius of the right planetary gear around the reference center distance, so that the number of teeth of the right sun gear/the number of teeth of the right planetary gear=the reference circle radius of the right sun gear/the reference circle radius of the right planetary gear, and that the reference circle radius of the right sun gear+the reference circle radius of the right planetary gear=the reference center distance.