Electromechanical actuator

Information

  • Patent Grant
  • 6543477
  • Patent Number
    6,543,477
  • Date Filed
    Wednesday, November 14, 2001
    22 years ago
  • Date Issued
    Tuesday, April 8, 2003
    21 years ago
Abstract
An electromechanical actuator has at least one electromagnet and an armature with a shank. The armature is mechanically coupled to at least one restoring device and it can move between a first bearing surface on the electromagnet and a further bearing surface. The shank is either completely hollow or it has a blind bore formed therein. A transmitter of a sensor is disposed in the cavity of the shank body.
Description




BACKGROUND OF THE INVENTION




Field of the Invention




The invention relate's to an electromechanical actuator, in particular an actuator for a gas exchange valve of an internal-combustion engine.




A prior art electromechanical actuator, described in U.S. Pat. No. 6,078,235 and German utility model DE 297 12 502 U1, has two electromagnets and an armature which is mechanically coupled to two springs. The armature can move between a first bearing surface on the first electromagnet and a second bearing surface on the second electromagnet. The housing is formed with recesses for accommodating the electromagnets. For an internal-combustion engine whose gas exchange valves are driven by an electromechanical actuator of this type to operate reliably and securely, it must be ensured that the armature can move very quickly from one bearing surface to the other bearing surface and back. Only in this way is it possible to ensure that the gas exchange valves of the internal-combustion engine open and close quickly and precisely.




SUMMARY OF THE INVENTION




It is accordingly an object of the invention to provide an electromechanical actuating drive, which overcomes the above-mentioned disadvantages of the heretofore-known devices and methods of this general type and which makes it possible for gas exchange valves of an internal-combustion engine to open and close rapidly while, at the same time, keeping the energy consumption required for the actuation as low as possible.




With the foregoing and other objects in view there is provided, in accordance with the invention, an electromechanical actuator, comprising:




at least one electromagnet;




an armature having a shank formed with a cavity and movably disposed between the first bearing surface on the electromagnet and a second bearing surface;




at least one restoring device mechanically coupled to the armature; and




a transmitter of a sensor disposed in the cavity in the shank.




The actuator is particularly suitable in combination with a gas exchange valve of an internal-combustion engine, where the actuator is mechanically coupled to a valve stem of the gas exchange valve.




In accordance with an added feature of the invention, the shank is a hollow tubular shaft. In an alternative embodiment, the shank is formed with a blind bore in which the transmitter is disposed.




In accordance with an additional feature of the invention, the transmitter is a permanent magnet.




In accordance with another feature of the invention, the sensor is a position sensor.




In accordance with again another feature of the invention, the transmitter is introduced into the cavity at a free end of the shank, and the shank is flanged at the free end.




In accordance with a further feature of the invention, the armature includes an armature plate formed of a cobalt-iron alloy.




In accordance with a concomitant feature of the invention, the electromagnet has a core formed of a cobalt-iron alloy.




The invention is distinguished by the fact that the shank of the armature, which is designed as a hollow body, has a significantly lower mass than a solid shank. Consequently, the armature mass which has to be moved is reduced, and therefore only small actuating forces have to be applied to move the armature plate from one armature face to the other.




Other features which are considered as characteristic for the invention are set forth in the appended claims.




Although the invention is illustrated and described herein as embodied in an electromechanical actuator, it is nevertheless not intended to be limited to the details shown, since various modifications and structural changes may be made therein without departing from the spirit of the invention and within the scope and range of equivalents of the claims.











The construction and method of operation of the invention, however, together with additional objects and advantages thereof will be best understood from the following description of specific embodiments when read in connection with the accompanying drawings.




BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a partly sectional, partly schematic view of an actuator and a control device in an internal-combustion engine;





FIG. 2

is a section taken through the armature according to the invention in a first embodiment; and





FIG. 3

is a section taken through the armature in a second embodiment.











DESCRIPTION OF THE PREFERRED EMBODIMENTS




Referring now to the figures of the drawing in detail and first, particularly, to

FIG. 1

thereof, an internal-combustion engine includes an actuator


1


which acts on a gas exchange valve


2


and is arranged in a cylinder head


31


of the internal-combustion engine. The gas exchange valve


2


is either an exhaust valve or an intake valve. The gas exchange valve


2


has a valve stem


21


and a disk or cup


22


. The actuator


1


has a housing


11


wherein a first and a second electromagnet are disposed. The first electromagnet has a first core


12


which is provided with a first coil


13


. The second electromagnet has a second core


14


which is provided with a second coil is. An armature is provided, the armature plate of which is arranged in the housing


11


such that it can move between a first bearing surface


15




a


of the first electromagnet and a second bearing surface


15




b


of the second electromagnet. The armature plate


16


can therefore move between a closed position S


maxS


and an open position S


max0


. The armature also comprises a shank


17


, which is guided through recesses in the first and second cores


12


,


14


and can be mechanically coupled to the valve stem


21


of the gas exchange valve


2


. A first restoring means


18




a


and a second restoring means


18




b


, which are preferably designed as springs, bias the armature plate


16


into the preset at-rest position S


0


, i.e., the position of repose. Preferably, a receiver


19




b


of a position sensor is arranged on or in the actuator


1


in such a way that it indirectly or directly records the position of the armature plate


16


and of the armature shank


17


.




The actuator


1


is rigidly connected to the cylinder head


31


of the internal-combustion engine. The intake duct


32


and a cylinder


33


with a piston


34


are provided in the internal-combustion engine. The piston


34


is coupled to a crankshaft


36


via a connecting rod


35


.




A control device


4


is provided, which records the signals from various sensors. The sensors include, for example, the position sensor and/or a rotational-speed transmitter and/or a load-recording sensor. The control device


4


energizes the first and second coils


13


,


15


of the actuator


1


as a function of the signals from the sensors.




Referring now to

FIG. 2

, the shank


17


of the armature is a hollow body. For this purpose, it has a cylindrical bore which forms a cavity


17




a


. The mass of the shank


17


is therefore small, yet the shank remains sufficiently rigid to ensure stable guidance of the armature plate


16


. A transmitter


19




a


is disposed in the region of a free end of the shank


17


. The transmitter


19




a


is preferably a permanent magnet assigned to the position sensor. The receiver


19




b


is preferably a magnetoresistive element, preferably designed as a giant-magnetoresistive element (GMR element). Particularly simple and secure fixing of the transmitter


19




a


is ensured by flanging the free end in a region


19




c.






Referring now to

FIG. 3

, in a second embodiment of the armature shank


17


, the transmitter


19




a


is arranged at a significant distance toward the armature plate


16


from the free end of the shank


17


. This makes it easy to ensure that the magnetic field generated by the transmitter


19




a


is only insignificantly interfered with by a stray magnetic field which is particularly strong at the free end of the armature shank and is caused by the magnetic circuit formed by the first or second electromagnet and the armature. Preferably, a potting compound


19




c


is introduced into the cavity


17




a


in the region of the free end and up to the transmitter


19




a


, in order to precisely fix the transmitter


19




a


. Precise fixing of the transmitter


19




a


is essential for exact recording of the position by the receiver


19




b


during a long operating period of the actuator.




Alternatively, the cavity


17




a


in the armature shank


17


may also be formed only in a partial region along the longitudinal axis of the shank, for example only in the region wherein the transmitter


19




a


is accommodated.




The moving masses of the actuator


1


are further reduced by forming the armature plate


16


from a cobalt-iron alloy. In that case, the cores


12


,


14


of the electromagnets preferably also consist of the cobalt-iron alloy. The alloy has, for example, between 17 and 50% by weight of cobalt. The cobalt-iron alloy has a significantly higher electrical resistance than, for example, iron (the electrical resistance is approximately four times as high). Consequently, the eddy-current losses in the armature are lower. Compared with the silicon-iron alloys which are customarily used in electromagnets, the cobalt-iron alloy has the advantage that the saturation is reached at a magnetic induction of approximately 2.3 tesla, which is approximately 15% higher than that of the silicon-iron alloys. It is therefore possible, particularly in the case of an actuator which is provided for a gas induction valve, to reduce the size of the armature and the core, since in this case the dimensions of the core and the armature are significantly influenced by the holding force which has to be applied while the armature is bearing against one of the bearing surfaces


15




a


,


15




b.





Claims
  • 1. An electromechanical actuator, comprising:at least one electromagnet formed with a first bearing surface; an armature having a shank formed with a cavity and movably disposed between said first bearing surface and a second bearing surface; at least one restoring device mechanically coupled to said armature; and a transmitter of a sensor disposed in said cavity in said shank.
  • 2. The actuator according to claim 1, wherein said shank is a tubular shaft.
  • 3. The actuator according to claim 1, wherein said transmitter is a permanent magnet.
  • 4. The actuator according to claim 1, wherein said sensor is a position sensor.
  • 5. The actuator according to claim 1, wherein said transmitter is introduced into said cavity at a free end of said shank, and said shank is flanged at said free end.
  • 6. The actuator according to claim 1, wherein said armature includes an armature plate formed of a cobalt-iron alloy.
  • 7. The actuator according to claim 1, wherein said electromagnet has a core formed of a cobalt-iron alloy.
  • 8. In combination with a gas exchange valve of an internal-combustion engine, the actuator according to claim 1 mechanically coupled to a valve stem of the gas exchange valve.
Priority Claims (1)
Number Date Country Kind
199 22 423 May 1999 DE
CROSS-REFERENCE TO RELATED APPLICATION

This application is a continuation of copending International Application No. PCT/DE00/01483, filed May 11, 2000, which designated the United States.

US Referenced Citations (6)
Number Name Date Kind
4682574 Kreuter Jul 1987 A
5144977 Eggerton et al. Sep 1992 A
5617417 Sathe et al. Apr 1997 A
6002670 Rahman et al. Dec 1999 A
6078235 Schebitz et al. Jun 2000 A
6193212 Ohmi et al. Feb 2001 B1
Foreign Referenced Citations (8)
Number Date Country
39 28 066 Feb 1991 DE
42 07 275 Sep 1993 DE
196 10 468 Feb 1997 DE
297 12 502 Oct 1997 DE
197 06 106 Aug 1998 DE
197 45 522 Apr 1999 DE
0 419 098 Mar 1991 EP
WO 9939468 Aug 1999 WO
Continuations (1)
Number Date Country
Parent PCT/DE00/01483 May 2000 US
Child 09/993037 US