IP Library › Granted Patent US 11,682,513
Granted Patent B1
US 11,682,513 · App. 17/142,656 · Granted Jun 20, 2023

Linearized pull-pull electromagnetic actuators, systems, and methods

Inventor: John E. Miesner (Fairfax, VA)
Assignee: The United States of America, as represented by the Secretary of the Navy
H01F7/1615H01F7/064H01F7/066H02K33/00H02K33/12H01F7/06
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Quick Facts
Patent No.
US 11,682,513
App. No.
17/142,656
Granted
Jun 20, 2023
Kind
B1
Abstract

Electromagnetic actuators are provided, which generate bidirectional linear force output without magnetic bias from current or permanent magnets. Systems and methods based on the electromagnetic actuators are also provided. In particular, an electromagnetic actuator having a shaft, an axial bearing, coil assembly, top and bottom stationary flux returns, and top and bottom magnetic flux sensors to measure flux crossing the respective top and bottom axial air gaps.

Claims (24)

1. An electromagnetic actuator comprising:

a shaft having an axis;

an axial bearing;

a coil assembly comprising an inner flux cylinder, an outer flux cylinder, top and bottom electrical coils located radially between the inner and outer flux cylinders, a center flux return located radially between the inner and outer flux cylinders and axially between the top and bottom electrical coils, all coil assembly components being joined to move as a unit;

top and bottom stationary flux returns that support the shaft, the top and bottom stationary flux returns radially aligned with the inner and outer flux cylinders to form top and bottom axial air gaps, wherein each of the top and bottom stationary flux returns comprise annular slits positioned such that substantially all of the magnetic flux crossing the top and the bottom air gaps pass through the respective annular slits; and

top and bottom magnetic flux sensors positioned to measure magnetic flux crossing the respective top and bottom axial air gaps, and wherein the magnetic flux sensors are positioned in the annular slits in the top and bottom stationary flux returns,

wherein

the shaft is fixed within the electromagnetic actuator, the annular slits have a width of 1.5 mm, and the air gaps have a width from 3 mm to 12 mm, and

the coil assembly forms the moveable inertial mass of the electromagnetic actuator.

2. The electromagnetic actuator of claim 1 , wherein the axial bearing is attached to and slidably supports the coil assembly.

3. The electromagnetic actuator of claim 1 , wherein the coil assembly has a position that is maintained by forces produced by the top and bottom electrical coils across the top and bottom axial air gaps.

4. The electromagnetic actuator of claim 1 , wherein the shaft moves axially within the electromagnetic actuator.

5. The electromagnetic actuator of claim 4 , wherein the axial bearing is independent from the coil assembly, and slidably supports the shaft.

6. The electromagnetic actuator of claim 4 , wherein the coil assembly is affixed to the shaft, forming the moveable inertial mass of the electromagnetic actuator, and wherein the annular slits have a width of 1.5 mm, and wherein the air gaps have a width from 3 mm to 12 mm.

7. An electromagnetic actuator comprising:

a shaft having an axis;

an axial bearing;

a coil assembly comprising an inner flux cylinder, an outer flux cylinder, top and bottom electrical coils located radially between the inner and outer flux cylinders, a center flux return located radially between the inner and outer flux cylinders and axially between the top and bottom electrical coils, all coil assembly components being joined to move as a unit;

top and bottom stationary flux returns that support the shaft, the top and bottom stationary flux returns radially aligned with the inner and outer flux cylinders to form top and bottom axial air gaps; and

top and bottom magnetic flux sensors positioned to measure magnetic flux crossing the respective top and bottom axial air gaps

wherein

the shaft is fixed within the electromagnetic actuator, the annular slits have a width of 1.5 mm, and the air gaps have a width from 3 mm to 12 mm, and

the coil assembly forms the moveable inertial mass of the electromagnetic actuator.

8. The electromagnetic actuator of claim 7 wherein the magnetic flux sensors are positioned in annular slits in the top and bottom stationary flux returns, annular slits being positioned such that substantially all of the magnetic flux crossing the axial top and bottom air gaps passes through the annular slits.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 21, 2022
From: MIESNER, JOHN E.
To: THE UNITED STATES OF AMERICA, AS REPRESENTED BY THE SECRETARY OF THE NAVY
Reel/Frame 062166/0902 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 6, 2021
From: MIESNER, JOHN E., DR.
To: THE GOVERNMENT OF THE UNITED STATES OF AMERICA, AS REPRESENTED BY THE SECRETARY OF THE NAVY
Reel/Frame 054829/0547 →
Cited By (1)
US 12,211,646