The present invention relates to a servo valve for a hydraulic vehicle steering system.
Servo valves are known from the prior art and are typically installed in hydraulic power steering systems of vehicles to provide a hydraulic assist force for the steering movements of a driver of a vehicle. Any unevennesses in the road surface may have an effect on the chassis and therefore on the vehicle steering and may be perceived by the vehicle driver at the steering wheel as an undesirable “bumpiness of the steering”. Owing to a more direct dimensioning of the chassis and a rigid coupling between the steering gear and the chassis, the bumpiness of the steering is more strongly perceivable in power steering systems used today. In addition, energy-saving pumps are increasingly made use of in the power steering systems to reduce the energy demand. In particular when driving straight ahead, the volume flow rate of such pumps and thus also the system pressure of the power steering system are reduced. As the system pressure decreases, the pressure-dependent equivalent bulk modulus E′oil and therefore the system rigidity, which has a damping effect on the bumpiness, are also reduced. Therefore, any bumpiness in the steering occurring when driving straight ahead (i.e. in a center position of the servo valve) is especially distinctly perceptible at the steering wheel.
The bumpiness appearing needs to be dampened mechanically or hydraulically. A so-called 9-land servo valve serving this purpose is disclosed in the prior art which, upon a rotation of the valve, i.e. in a cornering of the vehicle, generates a dynamic pressure on the low pressure side, and thus dampens the bumpiness in the steering wheel.
DE 100 2006 056 350 A1 discloses a valve design, in particular for such a 9-land servo valve, in which a dynamic pressure is generated on the low pressure side and therefore the bumpiness in the steering wheel is dampened even in a center position of the valve, i.e. when the vehicle travels straight ahead.
It is a feature of the invention to provide a servo valve for vehicle steering systems in which any bumpiness occurring in the steering wheel, in particular when driving straight, is dampened even better in as simple a manner as possible and essentially irrespective of the type of valve.
In accordance with the invention, the feature is achieved by a servo valve for a hydraulic vehicle steering system, including a valve sleeve and an input shaft which is arranged within the valve sleeve and can be rotated relative to the valve sleeve about a common axis, the valve sleeve and the input shaft each having axially oriented control grooves positioned at least partially opposite each other, a first control gap being formed between a pressure port and a working port of the servo valve associated with the pressure port, and a second control gap being formed between a return port associated with the pressure port and the working port of the servo valve, the second control gap having a smaller flow cross-section than the first control gap in a center position of the valve.
The second control gap thereby acts as a hydraulic throttle in the center position of the servo valve and thus hinders the return of hydraulic fluid to a reservoir. As a consequence, a dynamic pressure builds up on the low pressure side of the servo valve, this pressure, in turn, contributing to an improved damping of the bumpiness. Furthermore, there also appears an advantageous effect in the restoring characteristic of the vehicle steering system. A typical, so-called caster of a vehicle wheel causes the steering system to be acted upon towards traveling straight ahead and to be restored by means of external driving forces. Owing to the damping of this restoring force present in the center position of the valve, an undesirable “overshoot” of the vehicle steering system beyond the straight-ahead travel thereof in the restoring motion by means of external driving forces is now prevented from occurring.
In a preferred embodiment of the servo valve, a flow cross-section of the control gaps is respectively defined by a gap length and a gap width, the gap width of the second control gap being smaller than the gap width of the first control gap in the center position of the valve. These different gap widths may be made use of for adjusting a desired flow cross-section in a simple way.
Particularly preferably, in the center position of the valve the gap width of the second control gap extends substantially in the radial direction. In the region of the valve center position, i.e. for example upon a rotation of the valve of less than 0.5° about the center position, this second control gap formed as a radial gap only shows a small change in the flow cross-section, which in turn results in an especially constant damping in this region. Any manufacturing tolerances arising in the production of the grooves also only have a very small influence on the flow cross-section of the second control gap in the region of the valve center position and, in addition, may be further minimized by a simple finishing step such as, e.g., polishing of the groove flanks.
Preferably, exactly two control gaps are provided between a pressure port and an associated return port of the servo valve. The desired damping effect can thus be achieved even with commonly used 6-land servo valves having three hydraulic bridges as well as 8-land servo valves having four hydraulic bridges.
In particular, a control groove that is in direct communication with a working port of the servo valve may, together with its two adjacent control grooves, form the first control gap and the second control gap, respectively.
In a further embodiment of the servo valve, a gap length of a respective control gap extends substantially in the axial direction, i.e. substantially parallel to the longitudinal axis of the servo valve. The gap width may extend substantially perpendicularly to the longitudinal axis of the servo valve.
Preferably, the gap width of the first and/or second control gap is substantially constant over the gap length. This, for one thing, minimizes the manufacturing expenditure in producing the control grooves in the valve sleeve and the input shaft and, for another thing, allows a simple calculation and precise adjustment of the flow cross-section.
In particular, all control gaps may have substantially the same gap length, so as to further reduce the manufacturing expenditure and the costs associated therewith.
In a further embodiment of the servo valve, the gap width of the first control gap changes faster than the gap width of the second control gap when the valve is rotated in the region of the valve center position. This means that on rotating the valve in the region of the valve center position, there is a greater increase or decrease in the gap width of the first control gap than in the gap width of the second control gap. As a result, a noticeable flow control already occurs on the high pressure side of the servo valve while barely a change occurs in the flow on the low pressure side. In the final analysis, the damping thus remains almost at a constant level.
The control grooves are particularly preferably manufactured such that the gap width of the second control gap remains substantially constant when the valve is rotated in the region of the valve center position.
In a further embodiment of the servo valve, the gap width of the first control gap and the gap width of the second control gap are substantially identical as from a predefined angle of rotation of the servo valve. This results in an advantageous, even volume flow distribution inside the servo valve as from the predefined angle of rotation.
In a further embodiment, in the valve center position the flow cross-section of the second control gap is defined substantially by polished portions in the region of groove flanks of the input shaft and/or of the valve sleeve. Therefore, the flow cross-section of the second control gap can be precisely adjusted and, if required, reworked with little effort involved.
In a further embodiment, each control groove of the valve sleeve and of the input shaft communicates with two adjacent control grooves of the input shaft and of the valve sleeve, respectively, via one control gap each, preferably via exactly one control gap each. This type of design allows the valve to be manufactured particularly simply and cost-effectively.
More particularly, this control gap may be a first control gap or a second control gap. This means that all control grooves of the servo valve that are adjacent to each other communicate with one another either via a first control gap or via a second control gap. This also contributes to a simple and cost-effective valve manufacture.
Other advantages of this invention will become apparent to those skilled in the art from the following detailed description of the preferred embodiments, when read in light of the accompanying drawings.
The flow cross-section A1, A2 of a control gap 20, 22 is each defined by a gap length 1 (cf.
Since the fundamental mode of operation of a servo valve 10 having a structure of this type is known from the prior art, it will not be discussed in more detail below.
The mode of operation of the servo valve 10 according to the invention will now be explained in detail below with reference to
Generally, a respective first control gap 20 is each formed between the pressure port 24 and the two circumferentially neighboring, associated working ports 32 of the servo valve 10. Formed between the two working ports 32 and their circumferentially neighboring, associated return ports 26 of the servo valve 10 is a respective second control gap 22 each. Specifically, the control gaps 20, 22 are, of course, formed by the control grooves 16, 18, which directly communicate with the respective ports 24, 26, 32. Control grooves 16, 18 are considered to be in direct communication with ports 24, 26, 32 if the respective port 24, 26, 32 is formed directly in the control groove 16, 18 or is disposed opposite the control groove 16, 18.
In the exemplary embodiment according to
According to the illustration of
To illustrate the difference between the first control gaps 20 and the second control gaps 22 more clearly, a detail D1 of
The control groove 16, shown in
The control groove 16, shown in
In comparison with the first control gap 20 according to
Since in the present exemplary configuration the gap length 1 of all control gaps 20, 22 is substantially equal, the difference in the flow cross-sections A1, A2 in the valve center position (α=0°) results from the difference in the gaps widths b1, b2 of the first and second control gaps 20, 22.
In the region of the valve center position, that is, for example, for −0.5°<α<0.5°, the gap width b1 of the first control gaps 20 changes faster than the gap width b2 of the second control gaps 22. This becomes clear with reference to the different curve gradients at α≈0° and results from the different gap orientations of the first and second control gaps 20, 22. In fact, while upon a rotation of the valve the gap width b1 of the first control gap 20 changes rapidly owing to the circumferential or tangential component b1, b1r, the gap width b2 of the radially oriented, second control gap 22 remains almost constant.
In a preferred valve design the control grooves 16, 18 are therefore made such that the gap width b2 of the second control gaps 22 remains substantially constant when the valve is rotated in the region of the valve center position.
Furthermore, the gap geometry is preferably made such that the gap widths b1 of the first control gaps 20 and the gap widths b2 of the second control gaps 22 are identical as from a predefined angle of rotation α* of the servo valve 10. According to
A comparison of
The graph in
In accordance with the provisions of the patent statutes, the principle and mode of operation of this invention have been explained and illustrated in its preferred embodiments. However, it must be understood that this invention may be practiced otherwise than as specifically explained and illustrated without departing from its spirit or scope.
Number | Date | Country | Kind |
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10 2008 045 537.7 | Sep 2008 | DE | national |
This application is a national stage of International Application No. PCT/EP2009/007224 filed Sep. 3, 2009, the disclosures of which are incorporated herein by reference in entirety, and which claimed priority to German Patent Application No. 10 2008 045 537.7 filed Sep. 3, 2008, the disclosures of which are incorporated herein by reference in entirety.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/EP09/07224 | 9/3/2009 | WO | 00 | 5/25/2011 |