This application claims priority to European Patent Application No. 17172300.0 filed May 22, 2017, the entire contents of which is incorporated herein by reference.
The present disclosure relates to servo spool valves.
Servovalves are well-known in drive or actuator systems for converting input power into mechanical drive power. Conventional servo spool valves comprise a spool, linearly moveable within a bore or sleeve in a valve cylinder or housing in response to a control input, such as to vary hydraulic fluid flow paths through the valve to a control port to provide output drive power.
Conventionally, rotational motion of a motor is converted into linear motion of the spool. Torque motor driven servo spool valves are well-known, and find application in a wide range of technical fields. A rotary torque motor has a drive member extending eccentrically from the motor rotor, which comes into contact with an end of the spool causing the spool to move linearly within the bore, thus controlling the flow of fluid to the valve control port.
The contact mechanism between the eccentric member and the spool can take various forms such as ball-type, which provides a point contact, and pin/roller type, which provides a linear contact.
Direct drive valves (DDVs) are also known in which the eccentric drive member is directly connected to the spool with a flexible metal rod.
Safety, precision and reliability of spool valves is crucially important, particularly in e.g. the aircraft industry where such valves are extensively used, and where faults or failure can have catastrophic consequences. Therefore, with conventional valves, very close manufacturing tolerances and alignment between the eccentric drive member and the spool are necessary to prevent backlash and hysteresis. Further, in arrangements with a point or line contact between the eccentric member and the spool, the contact area is small, thus resulting in high local pressures. This can lead to premature wear which can, in turn, lead to breakdown. High contact pressures at the contact surfaces limit shear (breakout) force and poor lubrication of the valve drive mechanism, leading to unpredictable friction forces and valve performance.
There is a need for an improved servo spool valve arrangement that overcomes these problems and that may permit greater manufacturing tolerances.
Accordingly, there is provided a spool valve arrangement comprising a spool arranged for linear movement within a bore to regulate flow of fluid through the bore according to the linear position of the spool relative to the bore, the spool having an end arranged to be engaged, in use, by a drive member to cause the linear movement, the spool valve arrangement further comprising a sliding block component moveably attached to the spool end and arranged to engage with the drive member, in use, such that the drive member engages with the spool end via the sliding block component and the sliding block component moves relative to the spool to compensate for non-linear movement of the drive member.
Preferred embodiments will now be described, by way of example only, with reference to the drawings.
Referring briefly to
The present disclosure improves the contact mechanism between the eccentric drive member and the spool to overcome the problems described in the background.
Embodiments will be described with reference to
Referring first to
End caps 7 are provided as seals, and to retain the sleeves 2. In a tandem structure, the position of the sleeves 2 can be adjusted by appropriate shimming 6 to ensure flow matching between the two sides. A spool 3 is mounted for linear movement within each sleeve 2.
The linear movement of the spool(s) 3 is caused by an eccentric drive member 5 of a torque motor (see
As best seen in
Returning now to
The sliding block 4 is configured to be moveably attached to the end 4a of the spool(s) 3 and also to engage with the eccentric drive member 5, in use, so as to act as an interface between the eccentric drive member and the spool(s) 3. In the example shown, where the valve arrangement has two spools 3, 3′ having their respective inner ends directed toward each other, the eccentric drive member 5 extends intermediate these ends to opposingly linearly move the spools 3, 3′ and so the sliding block 4 will be located between the two inner ends. In a valve arrangement with only one spool, the sliding block 4 is arranged at the end 4a of the spool 3 which is to be contacted by the eccentric drive member 5.
The attachment of the sliding block 4 to the spool end(s) can be realised in any way provided there is scope for some movement of the sliding block 4 relative to the spool to compensate for the rise and fall effect of the eccentric drive member 5 as it rotates. In the preferred example, a slot (not shown) is provided in the end of the spool(s) 3 and the sliding block 4 is inserted/mounted in the slot(s).
The engagement between the eccentric drive member 5 and the sliding block 4 can also be realised in various ways. In the embodiment shown, a hole or recess 40 is provided in the sliding block 4 dimensioned to receive the end of the eccentric drive member 5. The result is that the end of the eccentric drive member 5 has a greater contact surface area, due to the end being mounted in a sliding block 4, than the conventional point, linear or direct contact with the spool end. This essentially creates a hydrostatic bearing. The dimensional relationship between the eccentric end of the motor shaft and sliding block 4 is such as to provide minimal frictional forces, near zero backlash and a large contact area which assists in meeting high chip shear force requirements. Additionally, because the motor rotor, bearings and sliding block will usually be immersed in return pressure hydraulic fluid this ensures enhanced hydrostatic lubrication. Sealing to external environment is preferably provided by a motor membrane and by O-rings at the spool sleeve ends 8.
The sliding block 4 is preferably made of a material having good bearing properties e.g. bronze. The sliding block can be coated with a friction reducing coating.
Number | Date | Country | Kind |
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17172300 | May 2017 | EP | regional |
Number | Name | Date | Kind |
---|---|---|---|
4672992 | Vanderlaan | Jun 1987 | A |
4793377 | Haynes et al. | Dec 1988 | A |
4825904 | Grau et al. | May 1989 | A |
5504409 | Elrod | Apr 1996 | A |
5551481 | Elrod | Sep 1996 | A |
6000678 | Coakley | Dec 1999 | A |
7828245 | Suisse et al. | Nov 2010 | B2 |
8210206 | Coakley | Jul 2012 | B2 |
Number | Date | Country |
---|---|---|
1216533 | Dec 1970 | GB |
S60164003 | Aug 1985 | JP |
H0581511 | Nov 1993 | JP |
H09257137 | Sep 1997 | JP |
9002884 | Mar 1990 | WO |
2005111431 | Nov 2005 | WO |
Entry |
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Extended European Search Report for International Application No. 17172300.0 dated Sep. 29, 2017, 7 pages. |
Number | Date | Country | |
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20180335162 A1 | Nov 2018 | US |