Magnetohydrodynamic inertial actuator

Patent metadata

Field	Value
Publication number	US-9994337-B2
Application number	US-201314380264-A
Country	US
Kind code	B2
Filing date	Feb 15, 2013
Priority date	Feb 21, 2012
Publication date	Jun 12, 2018
Grant date	Jun 12, 2018

Abstract

An inertial actuation magnetohydrodynamic wheel ( 2 ) comprising a torus-shaped fluid ring ( 3 ) filled with a conductive liquid, at least one effective area ( 24, 26, 28 ) for setting the liquid into motion, and at least one magnetohydrodynamic pump ( 4, 6, 8 ).
The ratio of the set back distance of any magnetic conduction element ( 24, 26, 28 ) of the air gap of any electromagnetic pump ( 4, 6, 8 ) over the internal size of the fluid ring ( 3 ) is greater than or equal to 0.5 and the fluid ring ( 3 ) comprises at least two distinct effective areas ( 24, 26 ), for setting the conductive liquid into motion, angularly spaced apart by at least 120°.

First claim

The invention claimed is:

1. An inertial actuator for pointing a platform along a predetermined direction comprising:
a fluid ring having a torus shape around a central axis, the fluid ring including a central ring hole having a diameter, the central ring hole crossed by a central axis, the fluid ring having an internal size equal to the diameter of the central ring hole, the fluid ring being filled with a conductive liquid, the fluid ring having at least one air gap portion which is defined as a portion crossed by a magnetic field, and at least one effective portion which is defined as a portion where the conductive liquid is set into motion;
at least one magnetohydrodynamic pump for setting the conductive liquid into motion around the central axis of the fluid ring,
each magnetohydrodynamic pump having only one air gap, the air gap being associated with one air gap portion of the fluid ring and with the at least one effective portion of the fluid ring that is located inside the air gap portion,
each magnetohydrodynamic pump including only one means for generating a magnetic field through the air gap thereof, and including a magnetic conduction element which, conducts and channels the magnetic field through the at least one effective area portion and is separated from the central axis by a set back distance; and
a synchronization circuit, connected to each pump of the at least one magnetohydrodynamic pump and configured for synchronising an amplitude of the magnetic field generated by each pump of the at least one magnetohydrodynamic pump so as to minimise an energy consumed by the at least one magnetohydrodynamic pump when the conductive liquid rotates at a predetermined rotational speed,
wherein the ratio of the set back distance of the magnetic conduction element over the half of the internal size of the fluid ring is greater than or equal to 0.5 and wherein
the fluid ring comprises a number P of effective portions, P being an integer greater than or equal to two, each effective portion being centered around a radial middle half-plane, one radial middle half-plane being angularly spaced apart from the next radial middle half-plane by a pitch, said pitch being equal to 360° divided by the number P of effective portions.

2. The inertial actuator according to claim 1 , wherein each pump of the at least one magnetohydrodynamic pump is a pump selected from the set formed by DC current conduction electromagnetic pumps, AC current conduction electromagnetic pumps, linear induction electromagnetic pumps, annular induction electromagnetic pumps, and spiral induction electromagnetic pumps.

3. The inertial actuator according to claim 1 , comprising
at least two distinct magnetohydrodynamic pumps, each magnetohydrodynamic pump being associated with only one air gap portion.

4. The inertial actuator according to claim 1 comprising only one magnetohydrodynamic pump which is an annular induction magnetohydrodynamic pump in which the means for generating the magnetic field is an electromechanical machine stator having several windings positioned around the central axis and along an external circumference of the fluid ring and connected to a multi-phase current source for generating alternating radial unipolar or multipolar magnetic fields that form a resulting multipolar rotating magnetic field having a number P of poles, regularly distributed angularly, and
the fluid ring comprising the number P of effective portions each effective portion being centered around a respective radial middle half-plane, which coincides with an axis of a pole of the resulting multipolar rotating magnetic field.

5. The inertial actuator according to claim 4 , further comprising a unit for regulating a frequency of an amplitude of the current provided by the multi-phase current source in order to minimise the energy consumed by the magnetohydrodynamic pump when the conductive liquid rotates at the predetermined set rotational speed.

6. The inertial actuator according to claim 1 , wherein the conductive liquid is a liquid selected from the group consisting of liquid gallium, liquid mercury and NaK.

7. The inertial actuator according to claim 1 , wherein a shape of a radial section of an envelope of the fluid ring is selected from the group consisting of circles, ellipses, rectangles, squares, rectangles with rounded angles, squares with rounded angles, polygons, polygons with rounded angles and combinations thereof.

8. The inertial actuator according to claim 1 , wherein each pump of the at least one magnetohydrodynamic pump comprises only one magnetic conduction element having a first polar end and a second polar end positioned on either side of the air gap in order to form, with the air gap, a closed magnetic circuit.

9. The inertial actuator according to claim 1 , wherein each pump of at least one magnetohydrodynamic pump comprises a first magnetic conduction magnetic element, the first and a second magnetic conduction elements being positioned on either side of the air gap in order to form a series with the air gap and the means for generating the magnetic field, a closed magnetic circuit.

10. A platform comprising a supporting structure, one or several massive pieces of equipment positioned on the supporting structure, and at least one inertial actuator according to claim 1 , and wherein the size of each of the at least one inertial actuators is between 20 centimeters and three hundred meters.

11. The platform according to claim 10 , wherein the at least one inertial actuator is
a kinetic wheel for giving a gyroscopic stiffness to the platform,
a reaction wheel for changing an angular momentum or a kinetic energy of the platform around a minimum value, or
a gyroscopic actuator for strongly changing an angular momentum of the platform.

Assignees

• Centre Nat Etd Spatiales
• Inst Nat Polytechnique Toulouse
• Centre Nat Rech Scient
• Centre Nat Rech Scient

Inventors

• Casteras Christophe
• Lefevre Yvan
• Harribey Dominique

Classifications

• B64G1/28

  using inertia or gyro effect · CPC title

• B64G1/283 Primary

  using reaction wheels · CPC title

• B64G1/285

  using momentum wheels · CPC title

• G01C19/12

  fluid driven (G01C19/14 takes precedence) · CPC title

• Y10T74/125

  by magnetic field · CPC title