IP Library Granted Patent US 12,337,727
Granted Patent B2
US 12,337,727 · App. 18/211,468 · Granted Jun 24, 2025

Actuator control system

Inventors: Suresh Babu Kappa Venkata (Bengaluru, IN); Srikanth Annumandla (Hyderabad, IN)
Assignee: B/E Aerospace, Inc.
B60N2/0244B60N2/02246B60N2/02253B60N2/0272
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 12,337,727
App. No.
18/211,468
Granted
Jun 24, 2025
Kind
B2
Abstract

An actuator control system for an assembly including moveable components such as a passenger seat. The system includes a first motor having a first rotating shaft, a second motor having a second rotating shaft, and a plurality of gear assemblies including a gear disposed between the shafts. A controller operates to move each gear independently between a neutral position and a rotationally engaged position with one of the rotating shafts. Each gear is coupled to a flexible shaft rotationally coupled to an actuator for moving the moveable component. In use, a singular controller and the two motors control N number of actuators.

Claims (35)

1. An actuator control system, comprising:

a first motor having a first rotating shaft;

a second motor having a second rotating shaft;

a plurality of gear assemblies each including a gear disposed between the first rotating shaft and the second rotating shaft, each gear independently movable into and out of rotational engagement with one of the first rotating shaft and the second rotating shaft, and each gear coupled to a flexible shaft rotationally coupled to an actuator positioned apart from the gear;

a controller communicatively coupled to each of the first motor, the second motor, and the plurality of gear assemblies; and

at least one sensor configured to sense a condition of the actuator and output the sensed condition of the actuator to the controller for controlling at least one of a rotational direction of the first motor, a rotational direction of the second motor, and a position of each gear relative to at least one of the first rotating shaft and the second rotating shaft.

2. The actuator control system according to claim 1 , wherein:

each gear is coupled to a common solenoid shaft disposed between a first push-pull linear solenoid assembly positioned proximal to the first rotating shaft and a second push-pull linear solenoid assembly positioned proximal to the second rotating shaft;

the first push-pull linear solenoid assembly is operative in an active push mode to push the common solenoid shaft along an axis toward the second rotating shaft to rotationally engage the gear with the second rotating shaft;

the second push-pull linear solenoid assembly is operative in an active push mode to push the common solenoid shaft along the axis toward the first rotating shaft to rotationally engage the gear with the first rotating shaft; and

the first and second push-pull solenoid assemblies are operative in a neutral mode to maintain the gear in a neutral position between and rotationally disengaged from the first and second rotating shafts.

3. The actuator control system according to claim 2 , wherein each of the first and second push-pull linear solenoid assemblies includes a coil electrically coupled to a lead wire configured to energize the coil to actively push the common solenoid shaft in the active push mode and deenergize the coil to position the common solenoid shaft in the neutral position.

4. The actuator control system according to claim 1 , wherein the first rotating shaft and the second rotation shaft are parallel.

5. The actuator control system according to claim 1 , wherein the first rotating shaft is configured to rotate in a first direction and the second rotating shaft is configured to rotate in a second direction opposite the first direction.

6. The actuator control system according to claim 1 , wherein each actuator is coupled to a moveable component.

7. A passenger seat, comprising:

a plurality of moveable components each movable by an actuator; and

an actuator control system, comprising:

a first motor having a first rotating shaft;

a second motor having a second rotating shaft;

a plurality of gear assemblies each including a gear disposed between the first rotating shaft and the second rotating shaft, each gear independently movable into and out of rotational engagement with one of the first rotating shaft and the second rotating shaft, and each gear coupled to a flexible shaft rotationally coupled to the actuator of one of the plurality of moveable components;

a controller communicatively coupled to each of the first motor, the second motor, and the plurality of gear assemblies; and

at least one sensor configured to sense a condition of the actuator and output the sensed condition of the actuator to the controller for controlling at least one of a rotational direction of the first motor, a rotational direction of the second motor, and a position of each gear relative to at least one of the first rotating shaft and the second rotating shaft.

8. The passenger seat according to claim 7 , wherein:

each gear is coupled to a common solenoid shaft disposed between a first push-pull linear solenoid assembly positioned proximal to the first rotating shaft and a second push-pull linear solenoid assembly positioned proximal to the second rotating shaft;

the first push-pull linear solenoid assembly is operative in an active push mode to push the common solenoid shaft along an axis toward the second rotating shaft to rotationally engage the gear with the second rotating shaft;

the second push-pull linear solenoid assembly is operative in an active push mode to push the common solenoid shaft along the axis toward the first rotating shaft to rotationally engage the gear with the first rotating shaft; and

the first and second push-pull solenoid assemblies are operative in a neutral mode to maintain the gear in a neutral position between and rotationally disengaged from the first and second rotating shafts.

9. The passenger seat according to claim 8 , wherein each of the first and second push-pull linear solenoid assemblies includes a coil electrically coupled to a lead wire configured to energize the coil to actively push the common solenoid shaft in the active push mode and deenergize the coil to position the common solenoid shaft in the neutral position.

10. The passenger seat according to claim 7 , wherein the first rotating shaft and the second rotation shaft are parallel and the first rotating shaft is configured to rotate in a first direction and the second rotating shaft is configured to rotate in a second direction opposite the first direction.

11. The passenger seat according to claim 7 , wherein the first and second motors are positioned under a seat pan of the passenger seat.

12. The passenger seat according to claim 7 , wherein each actuator is a linear actuator or a rotary actuator.

13. The passenger seat according to claim 7 , wherein the plurality of moveable components includes at least two of a backrest, a seat pan, a leg rest, a headrest, and an armrest.

14. The passenger seat according to claim 7 , wherein the controller is configured to, responsive to receiving the output of the sensed condition of the actuator, rotationally engage the gear associated with the actuator to one of the first rotating shaft and the second rotating shaft considering the rotational direction of the first and second rotating shafts.

15. The passenger seat according to claim 7 , wherein the at least one sensor is configured to sense a position of one of the plurality of moveable components and output positional information to the controller, and the controller is configured to act to energize the coil associated with the moveable component to drive the solenoid shaft in the appropriate direction to rotationally engage the respective gear with one of the first and second rotating shafts to change the position of the moveable component.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 1, 2023
From: ROCKWELL COLLINS (INDIA) ENTERPRISES PRIVATE LIMITED
To: B/E AEROSPACE, INC.
Reel/Frame 064450/0489 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 19, 2023
From: KAPPA VENKATA, SURESH BABU; ANNUMANDLA, SRIKANTH
To: ROCKWELL COLLINS (INDIA) ENTERPRISES PRIVATE LIMITED
Reel/Frame 063986/0746 →
Priority Claims (1)
IN 202211039971 · Jul 12, 2022 · national
Continuity (1)
Related Publication 20240017643A1 · Jan 18, 2024
References Cited (24)
US 3246540A · Joseph et al. · 1966 [cited by applicant]
US 4044632A · Wildhaber · 1977 [cited by applicant]
US 5795278A · Saruwatari et al. · 1998 [cited by applicant]
US 7322710B2 · Foote et al. · 2008 [cited by applicant]
US 9789964B2 · Garing · 2017 [cited by applicant]
US 9993614B2 · Pacheco et al. · 2018 [cited by applicant]
US 10450070B2 · Beroth · 2019 [cited by applicant]
US 10895305B2 · Dalgord et al. · 2021 [cited by applicant]
US 11155185B2 · Rose et al. · 2021 [cited by applicant]
US 20010003806A1 · Swan et al. · 2001 [cited by applicant]
US 20210188134A1 · Hudson · 2021 [cited by examiner]
US 20220194595A1 · Pevida · 2022 [cited by applicant]
US 20230406168A1 · Kato · 2023 [cited by examiner]
CN 210686915U · 2020 [cited by applicant]
CN 211606314U · 2020 [cited by applicant]
EP 3301024A1 · 2018 [cited by applicant]
EP 3385112A1 · 2018 [cited by applicant]
GB 2497332A · 2013 [cited by applicant]
KR 100461315B1 · 2004 [cited by applicant]
KR 20190121670A · 2019 [cited by applicant]
KR 102239250B1 · 2021 [cited by applicant]
WO 2012123487A1 · 2012 [cited by applicant]
“What is a Toroidal Transmission”, Mar. 23, 2018; www.go4trans.com/technical-transmission-general-articles/what-is-a-toroidal-transmission/. [cited by applicant]
Extended European Search Report dated Oct. 20, 2023; European Application No. 23185107.2. [cited by applicant]