IP Library Granted Patent US 11,837,401
Granted Patent B2
US 11,837,401 · App. 17/293,048 · Granted Dec 5, 2023

Actuation system to achieve soft landing and the control method thereof

Inventors: Ozkan Bebek (Istanbul, TR); Muhammad Sarmad Qureshi (Istanbul, TR); Mehmet Polat Kuntuz (Istanbul, TR); Ozgur Ertunc (Istanbul, TR); Ismail Hakki Savci (Istanbul, TR); Tahsin Hacibekir (Istanbul, TR)
Assignee: OZYEGIN UNIVERSITESI
H01F7/18H01F7/064H01F7/081
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 11,837,401
App. No.
17/293,048
Granted
Dec 5, 2023
Kind
B2
Abstract

An actuation system to achieve soft landing and the control method thereof are provided. A soft landing is achieved via an open loop control of an electromagnetic actuator. The actuation system includes a control unit, wherein the control unit controls the electromagnetic actuator. The control unit does not rely on sensor data regarding a position of an armature to achieve the soft landing. As the actuation system achieves soft landing via the open loop control of the electromagnetic actuator by the control unit, a use of the sensor data is not needed.

Claims (19)

1. An actuation system, comprising

an electromagnetic actuator, wherein the electromagnetic actuator comprises a body, at least one coil, and an armature to convert an electrical energy into a mechanical energy,

a control unit, wherein the control unit applies a voltage signal to the electromagnetic actuator on the at least one coil for an open loop control of the electromagnetic actuator to achieve a soft landing, wherein

a first portion of the voltage signal is applied to energize the at least one coil,

a second portion of the voltage signal is applied after the voltage signal is closed and an admittance time is finished to generate the soft landing of the armature ( 3 ) and,

the second portion of the voltage is applied for a period of time shorter than a period of application of the first portion of the voltage signal.

2. The actuation system according to claim 1 , wherein magnitudes of the first portion of the voltage signal and the second portion of the voltage signal are equal to each other.

3. The actuation system according to claim 1 , wherein a waiting time between the first portion and the second portion of the voltage signal is T wait and T wait is calculated by adding the period of time required to reach an admittance of the electromagnetic actuator after the first portion of the voltage signal is finished and a period of time required for a closing of the armature multiplied with a first, constant value, wherein the first constant value is determined by a manufacturer according tofirst parameters of the electromagnetic actuator.

4. The actuation system according to claim 3 , wherein the second portion of the voltage signal is applied for a period of time T width and T width and is calculated by a multiplication of a second constant value, wherein the second constant value is determined by a producer according to second parameters of the electromagnetic actuator with a time for the electromagnetic actuator to reach a maximum of the electromagnetic actuator or a movement of the armature.

5. The actuation system according to claim 4 , wherein the first constant value is 0.33 and the second constant value is 0.5.

6. A method for controlling the actuation system according to claim 1 , comprising the following steps:

applying the first portion of the voltage signal for an energization of the at least one coil by the control unit,

after an end of the application of the first portion of the voltage signal waiting for a completion of the admittance time,

after the admittance time is completed, while the armature is closing applying the second portion of the voltage signal.

7. The actuation system according to claim 2 , wherein a waiting time between the first portion and the second portion of the voltage signal is T wait and T wait is calculated by adding the period of time required to reach an admittance of the electromagnetic actuator after the first portion of the voltage signal is finished and a period of time required for a closing of the armature multiplied with a first constant value, wherein the first constant value is determined by a manufacturer according to first parameters of the electromagnetic actuator.

8. The method according to claim 6 , wherein magnitudes of the first portion of the voltage signal and the second portion of the voltage signal are equal to each other.

9. The method according to claim 6 , wherein a waiting time between the first portion and the second portion of the voltage signal is T wait and T wait is calculated by adding the period of time required to reach an admittance of the electromagnetic actuator after the first portion of the voltage signal is finished and a period of time required for a closing of the armature multiplied with a first constant value, wherein the first constant value is determined by a manufacturer according to first parameters of the electromagnetic actuator.

10. The method according to claim 9 , wherein the second portion of the voltage signal is applied for a period of time T width and T width is calculated by a multiplication of a second constant value, wherein the second constant value is determined by a producer according to second parameters of the electromagnetic actuator with a time for the electromagnetic actuator to reach a maximum of the electromagnetic actuator or a movement of the armature.

11. The method according to claim 10 , wherein the first constant value is 0.33 and the second constant value is 0.5.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 12, 2021
From: BEBEK, OZKAN; QURESHI, MUHAMMAD SARMAD; KUNTUZ, MEHMET POLAT; ERTUNC, OZGUR; SAVCI, ISMAIL HAKKI; HACIBEKIR, TAHSIN
To: OZYEGIN UNIVERSITESI
Reel/Frame 056209/0391 →
Continuity (1)
Related Publication 20210398725A1 · Dec 23, 2021