Hydro-magnetic linear actuator
An actuator comprising a linear electrical machine (LEM) having a stator with a stator bore and a translator axially movable within the stator bore and defining a magnetic circuit airgap therebetween, at least one fluid bearing journal formed on the translator, at least one fluid bearing providing a bearing gap adjacent the translator to allow the translator to move axially within the stator bore, a preload chamber for applying a preload force to the translator, wherein the preload chamber is defined by a side wall, a first end wall and a second end wall at least part of which is movable with the translator, and wherein the bearing gap and the magnetic circuit airgap are coaxial.
1. An actuator comprising:
a linear electrical machine (LEM) having a stator with a stator bore and a translator axially movable within the stator bore and defining a cylindrical magnetic circuit airgap therebetween;
at least one gas bearing journal formed on a surface of the translator;
at least one gas bearing acting upon the at least one gas bearing journal and providing at least one bearing gap adjacent the translator to allow the translator to move axially within the stator bore, the gas bearing and the stator forming a static assembly;
a preload chamber for applying a preload force to the translator, the preload chamber being coaxial with the stator bore and the at least one bearing gap;
one or more seal between the static assembly and the translator to limit gas flow from the preload chamber entering the magnetic circuit airgap;
wherein the preload chamber is defined by a side wall, a first end wall and a second end wall comprising a movable part movable with the translator;
wherein the at least one bearing gap and the magnetic circuit airgap are coaxial; and
wherein the at least one gas bearing journal formed on the translator also provides a sealing surface for the one or more seal.
2. The actuator of claim 1 , wherein the movement of the movable part of the second end wall is coaxial with the stator bore.
3. The actuator of claim 1 , further comprising a test subject mounting point fixed to the translator.
4. The actuator according to claim 1 , wherein the at least one gas bearing acts upon the at least one gas bearing journal on the outer surface of the translator.
5. The actuator according to claim 1 , wherein the translator is hollow and slides axially along a central core.
6. The actuator according to claim 5 , wherein the at least one gas bearing acts upon the at least one gas bearing journal on the inner surface of the translator.
7. The actuator according to claim 1 , wherein the LEM is a moving magnet machine.
8. The actuator according to claim 7 , wherein the LEM is a slotless stator machine.
9. The actuator according to claim 1 , wherein the LEM is a flux switching machine or a reluctance machine.
10. The actuator according to claim 1 , further comprising an encoder connected to the translator wherein the encoder senses one or more of position or velocity and uses at least one optical, magnetic, or mechanical sensor.
11. The actuator of claim 1 , wherein at least one bearing gap includes a plurality of axial extending arcuate cross section channels arranged around the translator.
12. The actuator according to claim 1 , wherein the at least one bearing gap is either cylindrical or includes two or more arcuate sections.
13. The actuator according to claim 1 , wherein the actuator includes an actuator housing body housing the LEM, the housing body containing one or more cooling channels.
14. The actuator according to claim 1 , further comprising a hydrodynamic bearing or a hydrostatic bearing.
15. The actuator according to claim 1 , wherein the preload chamber is adjacent the static assembly.
16. The actuator according to claim 1 , wherein the one or more seal is provided by a seal component mounted on or in the stator and/or the at least one gas bearing.
17. The actuator according to claim 1 , wherein the one or more seal is provided by the stator and/or at least one gas bearing itself.