IP Library Granted Patent US 9,284,996
Granted Patent B2
US 9,284,996 · App. 14/061,373 · Granted Mar 15, 2016

Selective electrical control of electromechanical clutch assembly

Inventors: Elliot Kruk (Norwalk, CT); Wiiliam F. Lange (Woodbridge, CT); Michael Paul Baran (Prospect, CT)
Assignee: SIKORSKY AIRCRAFT CORPORATION
F16D27/14B64C13/503F16D28/00F16D2021/0646F16D2500/5114
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Quick Facts
Patent No.
US 9,284,996
App. No.
14/061,373
Granted
Mar 15, 2016
Kind
B2
Abstract

A clutch assembly of a vehicle includes a shaft configured to rotate around a rotation axis inside the shaft, a connection arm connected to the shaft, to a pilot-controlled mechanism, and to a mechanical servo that controls a movement of the vehicle, and at least two electromechanical actuators. The electromechanical actuators are configured to be selectively engaged with the shaft via an electromechanical clutch, such that the electromechanical actuators are disconnected from controlling a movement of the shaft and the connection arm when the electromechanical clutch is disengaged, and the electromechanical actuators are configured to control movement of the shaft and the connection arm when the electromechanical clutch is engaged.

Claims (13)

1. A clutch assembly of a vehicle, comprising:

a shaft configured to rotate around a rotation axis inside the shaft;

a connection arm connected to the shaft, to a pilot-controlled mechanism, and to a mechanical servo that controls a movement of the vehicle; and

a first electromechanical actuator configured to be selectively mechanically engaged with the shaft via a first electromechanical clutch and a second electromechanical actuator configured to be selectively mechanically engaged with the shaft via a second electromechanical clutch, such that the first and second electromechanical actuators are disconnected from controlling a movement of the shaft and the connection arm when the first and second electromechanical clutches are disengaged, and one of the first and second electromechanical actuators is configured to control movement of the shaft and the connection arm when one of the first and second electromechanical clutches is engaged, the first electromechanical actuator and second electromechanical actuator configured in a redundant configuration, such that each of the first electromechanical actuator and second electromechanical actuator is configured to engage the shaft based on receiving a shaft-position control signal, the first electromechanical clutch configured to be disengaged based on the second electromechanical clutch being engaged, the first electromechanical clutch configured to be engaged based on a failure being detected in at least one of the second electromechanical actuator and the second electromechanical clutch.

2. The clutch assembly of claim 1 , wherein the first electromechanical actuator and second electromechanical actuator are located at opposite ends of the shaft.

3. The clutch assembly of claim 1 , wherein the first electromechanical clutch includes a first inner disc configured to selectively engage a first outer disc and the second electromechanical clutch includes a second inner disc configured to selectively engage a second outer disc.

4. A method of controlling a vehicle, the vehicle including an electromechanical clutch assembly having a connection arm connected to each of a pilot-controlled mechanism, a servo to control a movement of the vehicle, and a rotation shaft of the electromechanical clutch assembly, the electromechanical clutch assembly further including an electromechanical clutch and an electromechanical actuator mechanically connected to the electromechanical clutch, the method comprising:

controlling a movement of the servo, the connection arm, and the rotation shaft with the pilot-controlled mechanism based on the electromechanical clutch being disengaged; and

controlling a movement of the servo, the connection arm, and the rotation shaft with the electromechanical actuator based on the electromechanical clutch being engaged;

wherein the electromechanical clutch assembly further includes an auxiliary electromechanical clutch connected to the rotation shaft and an auxiliary electromechanical actuator mechanically connected to the auxiliary electromechanical clutch, the method further comprising:

detecting a fault in at least one of the electromechanical clutch and the electromechanical actuator;

engaging the auxiliary electromechanical clutch based on detecting the fault in at least one of the electromechanical clutch and the electromechanical actuator; and

transmitting control signals to the auxiliary electromechanical actuator to control a movement of the vehicle based on the auxiliary clutch being engaged.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 23, 2013
From: KRUK, ELLIOT; LANGE, WILLIAM F.; BARAN, MICHAEL PAUL
To: SIKORSKY AIRCRAFT CORPORATION
Reel/Frame 031463/0071 →
Continuity (1)
Related Publication 20150107957A1 · Apr 23, 2015