Hybrid airfoil bearing with active damping
A hybrid bearing assembly is provided and includes stationary components, a shaft disposed to rotate relative to the stationary components, passive magnetic bearing components integrated into the shaft and the stationary components to generate passive magnetic force to resist radial movement of the shaft relative to the stationary components and an active damping system. The active damping system includes a stationary coil, a magnetic element rotatable with the shaft to induce current in the stationary coil and a circuit electrically coupled with the stationary coil. The circuit is configured to determine from the current an attitude change of the shaft and the magnetic element and to apply damping current to the stationary coil to resist the attitude change.
1 . A hybrid bearing assembly, comprising:
stationary components;
a shaft disposed to rotate relative to the stationary components;
passive magnetic bearing components integrated into the shaft and the stationary components to generate passive magnetic force to resist radial movement of the shaft relative to the stationary components; and
an active damping system comprising:
a stationary coil;
a magnetic element rotatable with the shaft to induce current in the stationary coil; and
a circuit electrically coupled with the stationary coil and configured to determine from the current an attitude change of the shaft and the magnetic element and to apply damping current to the stationary coil to resist the attitude change,
wherein:
the hybrid bearing assembly further comprises airfoil bearing components to supplement the passive magnetic bearing components, the airfoil bearing components comprise a top foil immediately surrounding the shaft and the passive magnetic bearing components remove a static load of the shaft on the top foil, and
the stationary components comprise a housing defining an outer bore, a bearing sleeve supported within the outer bore and a singular bump foil completely surrounding the top foil in a circumferential direction.
2 . The hybrid bearing assembly according to claim 1 , wherein the stationary coil is provided as one or more velocity sensing coils.
3 . The hybrid bearing assembly according to claim 1 , wherein the circuit is a transconductance amplified circuit.
4 . The hybrid bearing assembly according to claim 1 , wherein:
the attitude change comprises the radial movement of the shaft, and
the damping current generates a magnetic flux that interacts with the magnetic element to damp the attitude change.
5 . The hybrid bearing assembly according to claim 1 , wherein the circuit is further configured to apply the damping current to the stationary coil to damp rotor-dynamic frequency modes.
6 . The hybrid bearing assembly according to claim 1 , wherein the hybrid bearing assembly is incorporated into one or more of a thrust bearing and a journal bearing.
7 . A motor, comprising:
stationary housing components;
a shaft disposed to rotate relative to the stationary housing components; and
a hybrid bearing assembly configured to maintain a radial position of the shaft relative to the stationary housing components and comprising:
passive magnetic bearing components integrated into the shaft and the stationary housing components to generate passive magnetic force to resist radial movement of the shaft relative to the stationary housing components; and
an active damping system comprising:
a stationary coil;
a magnetic element rotatable with the shaft to induce current in the stationary coil; and
a circuit electrically coupled with the stationary coil and configured to determine from the current an attitude change of the shaft and the magnetic element and to apply damping current to the stationary coil to resist the attitude change,
wherein:
the hybrid bearing assembly further comprises airfoil bearing components to supplement the passive magnetic bearing components, the airfoil bearing components comprise a top foil immediately surrounding the shaft and the passive magnetic bearing components remove a static load of the shaft on the top foil, and
the stationary components comprise a housing defining an outer bore, a bearing sleeve supported within the outer bore and a singular bump foil completely surrounding the top foil in a circumferential direction.
8 . The motor according to claim 7 , wherein:
the attitude change comprises the radial movement of the shaft, and
the damping current generates a magnetic flux that interacts with the magnetic element to damp the attitude change.
9 . The motor according to claim 7 , wherein the circuit is further configured to apply the damping current to the stationary coil to damp rotor-dynamic frequency modes.
10 . A vehicle comprising the motor according to claim 7 , wherein the motor is a motor of one or more of a cabin air compressor, a fan and a pump.
11 . A vehicle comprising the motor according to claim 7 , wherein the motor is a motor of an air cycle machine (ACM).
12 . A motor, comprising:
stationary housing components;
a shaft disposed to rotate relative to the stationary housing components; and
a hybrid bearing assembly configured to maintain a radial position of the shaft relative to the stationary housing components and comprising:
passive magnetic bearing components integrated into the shaft and the stationary housing components to generate passive magnetic force to resist radial movement of the shaft relative to the stationary housing components;
airfoil bearing components to supplement the passive magnetic bearing components; and
an active damping system comprising:
a stationary coil;
a magnetic element rotatable with the shaft to induce current in the stationary coil; and
a circuit electrically coupled with the stationary coil and configured to determine from the current an attitude change of the shaft and the magnetic element and to apply damping current to the stationary coil to resist the attitude change,
wherein:
the airfoil bearing components comprise a top foil immediately surrounding the shaft and the passive magnetic bearing components remove a static load of the shaft on the top foil, and
the stationary housing components comprise a housing defining an outer bore, a bearing sleeve supported within the outer bore and a singular bump foil completely surrounding the top foil in a circumferential direction.
13 . The motor according to claim 12 , wherein:
the attitude change comprises the radial movement of the shaft, and
the damping current generates a magnetic flux that interacts with the magnetic element to damp the attitude change.
14 . The motor according to claim 12 , wherein the circuit is further configured to apply the damping current to the stationary coil to damp rotor-dynamic frequency modes.
15 . A vehicle comprising the motor according to claim 12 , wherein the motor is a motor of one or more of a cabin air compressor, a fan and a pump.
16 . A vehicle comprising the motor according to claim 12 , wherein the motor is a motor of an air cycle machine (ACM).