IP Library Granted Patent US 9,768,663
Granted Patent B2
US 9,768,663 · App. 14/663,962 · Granted Sep 19, 2017

Rotary electromagnetic actuator

Inventor: Wladyslaw Wygnanski (Cambridgeshire, GB)
Assignee: Camcon Auto Limited
H02K7/003F01L1/185F01L1/30F01L9/04F01L2009/0411F01L2009/0432
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Quick Facts
Patent No.
US 9,768,663
App. No.
14/663,962
Granted
Sep 19, 2017
Kind
B2
Abstract

A rotary electromagnetic actuator is provided which is suitable for opening and closing a valve for example. The actuator comprises a rotor, a stator, and a biasing arrangement for applying a torque to the rotor during at least part of its rotation. A plurality of stable rest positions for the rotor are defined by forces acting on the rotor and the actuator is controllable to move the rotor from one stable rest position to another. The torque applied by the biasing arrangement varies with the rotational position of the rotor such that at a primary rest position and at least a second rest position, it is sufficiently low to enable selection of those positions, and then it increases beyond the second rest position.

Claims (16)

1. An electromagnetic actuator comprising:

a rotor;

a stator, with the rotor arranged for rotation in the stator; and

an impeller coupled to the rotor for displacement as the rotor rotates,

wherein a plurality of stable rest positions for the rotor are defined by forces acting on the rotor, and the actuator is controllable to move the rotor from one stable rest position to another,

and the displacement of the impeller resulting from movement of the rotor from a primary rest position to a second rest position is greater than the displacement resulting from movement of the rotor from the primary rest position to a third rest position, with the rotation of the rotor from the primary rest position to the second rest position and from the primary rest position to the third rest position being substantially equal and in opposite directions.

2. An actuator of claim 1 , wherein the impeller is coupled to the rotor via a linkage.

3. An actuator of claim 2 , wherein the linkage is arranged such that preventing the impeller from reaching one end of its full range of travel results in a lost motion portion in the rotation of the rotor, over which there is substantially no displacement of the impeller, with the lost motion portion including the primary rest position and being located asymmetrically with respect to the primary rest position.

4. An actuator of claim 3 , wherein the linkage comprises a resilient coupling between the rotor and the impeller which is extended over the lost motion portion of the rotor's rotation.

5. An actuator of claim 4 , wherein the linkage includes a crank coupled to an off-axis location on the rotor which is rotationally offset from the end of its travel away from the impeller when the rotor is in its primary rest position.

6. An actuator of claim 1 , comprising:

an actuation cam defining an actuation cam surface; and

an actuation cam follower associated with the actuation cam surface, with one of the actuation cam and the actuation cam follower being rotatable with or by the rotor, and the actuator being arranged such that displacement of the actuation cam follower results in displacement of the impeller.

7. An actuator of claim 6 , wherein the impeller is integral with the actuation cam follower.

8. An actuator of claim 6 , wherein the primary rest position corresponds to one end of the travel of the actuation cam follower.

9. An internal combustion engine including an actuator of claim 1 arranged to actuate a valve.

Priority Claims (2)
GB 0920152.6 · Nov 18, 2009 · national
GB 1002604.5 · Feb 16, 2010 · national
Continuity (2)
Division 13510298
Related Publication 20150194858A1 · Jul 9, 2015