OSCILLATION COMPENSATING METHOD AND DEVICE FOR A STEPPING WHEEL PROPULSION UNIT

Abstract

The invention relates to mechanisms for converting rotational motion into other types of motion, in particular uniform translational motion, and is intended for use as an oscillation compensator for stepping wheel propulsion units. An oscillation compensating device for a stepping wheel propulsion unit consisting of a plurality of supports fastened symmetrically to an output shaft that is fastened for transverse motion is actuated by an input shaft, the output shaft being fastened on the free end of a crank. The output shaft is set into rotation via a variator, which varies the angular velocity of the output shaft according to the current position of the crank and the angular velocity thereof. The invention obviates the need for cam mechanisms and springs in the device, reduces the coefficient of friction and the dimensions of the device and significantly reduces both spatial and speed oscillations.

Claims

1. A method of compensating for the oscillations of the wheel-stepper propulsion device is that the output shaft, on which several supports are symmetrically fixed, are fixed at the free end of the crank rotated by the input shaft, while the output shaft rotates in the same direction and plane as the crank, but the angular velocity of the output shaft is changed depending on the position and angular speed of the crank.

2. The method according to claim 1, wherein for one complete revolution of the crank, the output shaft is rotated by 1/n revolution, where n is the number of supports fixed on the output shaft.

3. The method according to claim 1, wherein the maximum angular velocity of the output shaft is developed in the upper position of the crank, in which one of the supports touching the surface is in a vertical position, and the minimum angular velocity is obtained in the lower position of the crank when the two supports simultaneously touch the surface.

4. A vibration compensation device for a wheel-stepper propulsion device, consisting of several supports symmetrically fixed on the output shaft, fixed with the possibility of transverse movements, includes: a crank driven by an input shaft, and an output shaft is fixed at the free end of the crank, while the output shaft is driven into rotation through a variator, which changes the angular speed of the output shaft depending on the current position of the crank and its angular speed.

5. The oscillation compensation device according to claim 4, further comprising an encoder that determines the position of the crank and its angular velocity, and the variator is a servo drive, including an electronic variator, which is connected to the encoder.

6. The vibration compensation device according to claim 4, wherein the variator includes a control connecting rod rotated by a crank, while the fixed axis of the connecting rod is fixed at a predetermined distance from the input shaft.

7. The vibration compensation device according to claim 4, wherein the variator includes a planetary mechanism consisting of a stationary sun gear fixed to the body of the vibration compensation device, a carrier and at least one satellite fixed to the carrier, the carrier being a crank.

8. A vibration compensation device for a wheel-stepper propulsion device, consisting of several supports symmetrically fixed on the output shaft, fixed with the possibility of transverse movements, includes: a planetary gear consisting of a stationary sun gear fixed to the body of the vibration compensation device coaxially with an input shaft, a satellite engaging with a stationary sun gear of the same size, fixed on a crank that is a carrier, a gearbox mounted on a satellite, while the output of the gearbox is connected to the output shaft, a control rod, one end of which interacts with the gearbox, and the other end is limited by an axis that is stationary relative to the body of the vibration compensation device.

9. The vibration compensation device according to claim 8, wherein the second end of the control rod is freely fixed on the axis of the input shaft, while the control rod is made with a variable length.

10. The vibration compensation device according to claim 8, wherein the gearbox is made in the form of a planetary gearbox, the end of the control rod is fixed with its carrier, one central gear is fixed with the planetary gear satellite, and the second central gear is connected to the output shaft.

11. The vibration compensation device according to claim 10, wherein when the number of supports is equal to three, the ratio of the central gears of the planetary gearbox is 3 to 2.

12. Oscillation compensation device according to claim 8, wherein the gearbox consists of: a driven gear located coaxially with the satellite and connected to the output shaft, the driving epicyclic gear, which meshes with the driven gear, while the center of the driving epicyclic gear is shifted relative to the center of the driven gear, the end of the control rod interacts with this epicyclic gear, and the axis of this epicyclic gear is eccentrically fixed on the satellite.

13. The vibration compensation device according to claim 12, wherein when the number of supports is equal to three, the ratio of the driving epicyclic gear to the driven gear is 5 to 3.

14. Oscillation compensation device according to claim 8, wherein the gearbox consists of: a driven gear located coaxially with the satellite and connected to the output shaft, a driving gear located in a parallel plane with respect to the driven gear, the center of the driving gear is shifted relative to the center of the driven gear, while the end of the control rod is fixed to this driving gear, and the axis of this driving gear is eccentrically fixed to the satellite, at least one idler gear, which is in simultaneous engagement with the driven and driving gears, the idler gear axle is fixed to the satellite.

15. The vibration compensation device according to claim 14, wherein when the number of supports is equal to three, the ratio of the drive gear to the driven gear is 5 to 3.

16. The vibration compensation device according to claim 8, wherein the planetary mechanism consists of a fixed sun gear of an elliptical shape, a satellite engaging with a fixed sun gear of the same size and the same elliptical shape, while both gears are connected by two connecting rods of fixed length, fixed on these gears it is eccentric, one of these connecting rods is both a crank and a carrier, and the second connecting rod is a control rod.

Description

[0007] The objective of the present invention is to create a fundamentally new method and device for compensation of vibrations, in which the disadvantages of the prototype will be eliminated: high wear of parts and coefficient of friction, and also the vertical vibration of the shaft, high-speed vibrations and fluctuations in the load on the output shaft are minimized.

[0008] These tasks are achieved by the fact that in the proposed oscillation compensation device, the output shaft 1 (FIG. 1) is fixed on the crank 2, driven in rotation by the input shaft 3. Supports 4 are fixed on the output shaft 1. When the output shaft 1 rotates, one or two supports 4 touch surface 5. The output shaft 1 is driven by the variator 6. The variator 6 changes the angular velocity of the output shaft 1 depending on the current position of the crank 2 and its current angular velocity. In this case, the crank 2 and the output shaft 1 are made with the possibility of rotation in the same direction, and the output shaft 1 rotates more slowly than the crank 2, in particular, when the number of supports 4 is equal to three for one full revolution of the crank 2, the output shaft 1 must turn ⅓ of a turn but with a floating angular velocity. The variator 6 must create the maximum angular speed in the upper position of the crank 2 when one of the supports 4 touching the surface 5 is in a vertical position, and the minimum angular speed in the lower position of the crank 2 when two supports 4 simultaneously touch the surface 5. Subject to these conditions and correctly selected parameters, the solution of the assigned tasks is ensured.

[0009] If the output shaft 1 is driven by a separate drive, for example an electric servo, then an electronic variator can be used to change the angular speed of the servo. To regulate the speed of rotation of the servo—the electronic version is connected to an encoder that monitors the current position of crank 2 and its angular velocity relative to the body of the vibration compensation device.

[0010] If the output shaft 1 receives power and is driven into rotation from the input shaft 3 through the transmission and the variator 6, it is proposed to use the control rod 7 to control the variator 6 (FIG. 2). For this, the axis 8 of the connecting rod 7 must be fixed in the housing of the vibration compensation device at a predetermined distance from the input shaft 3. This distance allows you to adjust the nature of the change in the angular velocity of the output shaft 1. The other end of the connecting rod 7 passes through the axis of the output shaft 1. Thanks to this arrangement, the angle between the connecting rod 7 and the crank 2 changes in accordance with the required change in the angular velocity of the output shaft 1.

[0011] Another option for controlling the angular speed of the output shaft 1 is possible using a variator 6, consisting of a planetary gear. This planetary mechanism consists of a stationary sun gear 9 (FIG. 3), fixed on the housing of the vibration compensation device coaxially with the input shaft 3 and at least one satellite 10, fixed on the carrier. The diameter of the satellite is suggested to be the same size as the diameter of the sun gear 9. Crank 2 is used as a carrier. The rotation of the satellite can be used to change the angular velocity of the output shaft 1.

[0012] Shown below are options in which the variator is replaced by a gearbox controlled by a connecting rod 7. In the general case, the vibration compensation device includes a planetary gear, a gearbox 11 is attached to the satellite 10 of the planetary gear, and the output shaft of the gearbox 11 is the output shaft 1. One end of the control rod 7 interacts with the gearbox 11, in particular with one of its elements, and the second end of the rod 7 is limited by an axis that is stationary relative to the body of the vibration compensation device. This axis can be the input shaft 3. In this case, the end of the connecting rod 7 has a guide with an axial slot that allows the connecting rod 7 to pass through the input shaft 3. An option is possible in which the guide passes through an axis spaced at a predetermined distance from the input shaft 3. It is also possible that the control rod 7 is made with a variable length, for example, telescopic. In this case, the second end of the connecting rod is freely mounted on the axis of the input shaft 3 or on a separate axis. A bearing can be used for free mounting. The mechanisms of interaction of the opposite end of the control rod 7 with one of the elements of the gearbox 11 depend on the type of gearbox used. Further, with specific examples, it is shown how the control rod 7 and the planetary gear can be used to control the angular speed of the output shaft 1. The options shown under the options differ in the type of gearbox 11 and the methods of fastening the control rod 7.

[0013] According to the first variant, a planetary gearbox is used as a reducer 11. A simple planetary gearbox has three main components: a center sun gear, a carrier, and an epicyclic center gear. In the example shown, the satellite 10 (FIG. 4), on which the planetary gearbox is mounted, is at the same time the central sun gear of this planetary gearbox. And the epicyclic gear 12 of the planetary gearbox is connected to the output shaft 1. In this case, the end of the control rod 7 is fixed with the carrier 13. At least one satellite 14 is attached to the carrier 13. To obtain the required gear ratio on the carrier 13, paired satellites 14 of different diameters can be used, forming a two-row planetary gearbox. In order for the planetary gear and the planetary gearbox not to interfere with each other, the satellite 10 must protrude above the sun gear 9 so that the carrier 13 with the satellite 14 can rotate around the satellite 10 without obstacles without touching the sun gear 9. With the number of supports 4 equal to three and equal to the diameter of the gears 9 and 10, the ratio of the central epicyclic gear 12 to the central sun gear of the planetary gear should be 3 to 2. This ratio makes it possible to obtain ⅓ of the revolution of the output shaft 3 for one complete revolution of the input shaft 1.

[0014] The next sub-option involves the use of a different type of gearbox 11, consisting of a driven gear 15 (FIG. 5), located coaxially with the satellite 10 and connected to the output shaft 1. The reducer also includes a driving epicyclic gear 16. The axle 17 of this gear is mounted eccentrically on the satellite 10 at a predetermined distance from the output shaft 3 and with the teeth facing inward engages with the driven gear 15. The distance from the axis 17 to the center of the driven gear 15 affects the nature of the change in the angular velocity of the output shaft 3. The end of the control rod 7 interacts with the driving epicyclic gear 16. This interaction consists in the fact that the control rod 7 sets the direction of the driving epicyclic gear 16. There are several ways how this can be done, each of them does not change the essence of the present invention. FIG. 5 shows a method in which the driving epicyclic gear 16 has two pins 17 and 18, and the control rod 7 has a groove. This groove passes through both pins 17 and 18, so any rotation of the control rod 7 automatically turns the epicyclic gear 16 at the same angle. Such a groove can be at the other end of the control rod 7, and it can pass this groove through the input shaft 3. In this case, the control rod 7 can be rigidly fixed with the epicyclic gear 16. With the number of supports 4 equal to three and equal to the diameter of the gears 9 and 10, the ratio of the driving epicyclic gear 16 to the driven gear 15 should be 5 to 3. This ratio makes it possible to obtain ⅓ of the revolution of the output shaft 3 for one complete revolution of the input shaft 1.

[0015] The next sub-option differs from the previous one in that instead of the leading epicyclic gear 16, a gear 19 with teeth facing outward is used. Its axis is also located, but the gear 19 itself must be in a parallel plane with respect to the driven gear 15. And the drive gear 19 and the driven gear 15 interact through one or more intermediate gear 20. The axis of the idler gear 20 is attached to the satellite 10. Otherwise, this and the previous one sub-alternatives are similar to each other. With the number of supports equal to three, the ratio of the driving gear 16 to the driven gear 15 is also 5 to 3.

[0016] Another option concerns the shape of the planetary gears. It is proposed to use a stationary sun gear 21 (FIG. 7) of an elliptical shape. And the satellite 22 that engages with it is of the same elliptical shape and the same size. The use of an elliptical shape makes it possible to make the control rod 7 of a fixed size and without axial slots. Both the crank 2 and the control rod 7 in this scheme have the same size and are mounted eccentrically, at the focal points of these elliptical gears of the planetary mechanism, in opposite focuses. A gearbox 11 is mounted on the satellite 22, which is controlled by a connecting rod 7 and rotates the output shaft 1 with supports 4.

[0017] The vibration compensation method is implemented as follows, which is the same for all of the above device options: the output shaft 1 (FIG. 8) on which several supports 4 are symmetrically fixed rotates at the free end of the crank 2. The crank 2 itself is driven by the input shaft 3. In this case, the output shaft 1 is rotated in the same direction and plane as the crank 2. But the output shaft 1 rotates slower than the crank 2, in particular when the number of supports 4 is equal to three for one full revolution of the crank 2, the output shaft 1 must turn ⅓ of a turn, but with a floating angular velocity. The angular speed of the output shaft 1 is changed depending on the current position and the angular speed of the crank. The change in the angular speed is made in such a way that the maximum angular speed of the output shaft 1 is in the upper position of the crank 2, in which one of the supports 4 is in a vertical position. And the minimum angular velocity of the output shaft 1 is obtained in the lower position of the crank 2, when the support 4 touches the surface at the smallest angle. The change in the angular velocity is carried out smoothly.

[0018] For clarity, the rotation of the crank 2 in FIG. 8 is shown in the form of 4 main phases of rotation: 1st phase—turn from the upper vertical position by 45 degrees, 2nd phase—turn by another 45 degrees to the horizontal position of the crank 2. 3rd phase—turn from the horizontal position the next 45 degrees down, and finally the 4th phase—a turn of the next 45 degrees to the bottom vertical position. The greatest reduction in vibrations of both types (spatial and velocity) when using three supports 4 is observed if:

[0019] in the 1st phase, the output shaft 3 will rotate by about 22-23 degrees

[0020] in the 2nd phase, the output shaft 3 will rotate 17-18 degrees

[0021] in the 3rd phase, the output shaft 3 will rotate by about 11-12 degrees

[0022] and in the 4th phase, the output shaft 3 will rotate by about 6.5-7.5 degrees.

[0023] When the crank 2 moves from the lower position to the upper position, the rotation of the output shaft 1 is carried out in the same way—in the lower position, the smallest angle of rotation, in the upper position, the largest.

[0024] This method and all of the above options for the mechanisms of the vibration compensation device make it possible to exclude cam mechanisms and springs in the proposed device, reduce the coefficient of friction and dimensions of the device and significantly reduce vibrations, both spatial and high-speed.

[0025] Thanks to the shown solutions and optimally selected parameters, vertical vibrations can be reduced to 5% of the length of the supports, and the fluctuations in the linear speed of the reference points can be reduced to 6.5% of their average speed.