Aircraft control surface with linear actuator
US-2023257107-A1 · Aug 17, 2023 · US
US12525849B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12525849-B2 |
| Application number | US-202418408847-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 10, 2024 |
| Priority date | Jan 13, 2023 |
| Publication date | Jan 13, 2026 |
| Grant date | Jan 13, 2026 |
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An electromechanical actuator assembly operable in a plurality of modes. The EMA assembly includes: an electrical motor having a motor shaft extending along an axis (A) of the EMA, the motor driving the shaft to rotate about the axis; a gear assembly mounted around, and in geared connection with the shaft, to rotate with the shaft; an EMA output connected to the gear assembly such that rotation of the motor shaft causes rotation of the output via the gear assembly, the output rotating at a speed which is a predetermined fraction of the speed of rotation of the motor shaft based on the gear ratio of the gear assembly.
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The invention claimed is: 1 . An electromechanical actuator (EMA), assembly operable in a plurality of modes, the EMA assembly comprising: an electrical motor having a motor shaft extending along an axis (A) of the EMA, the motor driving the shaft to rotate about the axis; a gear assembly mounted around, and in geared connection with the motor shaft, to rotate with the motor shaft; an EMA output connected to the gear assembly such that rotation of the motor shaft causes rotation of the output via the gear assembly, the output rotating at a speed which is a predetermined fraction of the speed of rotation of the motor shaft based on the gear ratio of the gear assembly; wherein the EMA output is arranged to have a neutral position and to be rotatable away from the neutral position in a first, positive, extension direction to an extension position and away from the neutral position in a second, negative, retraction direction to a retracted position; a torque limiter having a predetermined torque limit, wherein the torque limiter is arranged to limit torque transfer between the gear assembly and the output; and an anti-extension mechanism moveable between an engaged position in which it inhibits rotation of the output in the extension direction and a disengaged position wherein it allows rotation of the output in the extension direction, the anti-extension mechanism comprising: a solenoid; a ratchet wheel; and an anti-extension spring, wherein the anti-extension mechanism is in the disengaged position when the solenoid is energized to move the ratchet wheel against the force of the anti-extension spring and is in the engaged position when the solenoid is not energized; wherein, in an active mode of the plurality of modes, the solenoid is energized and wherein rotation of the output shaft in either direction of rotation drives the output to rotate; wherein in an anti-extension mode, the solenoid is not energized and, when the output is at the neutral position or in the extension position, the output shaft is connected for rotation, via the ratchet, wherein the ratchet is arranged to prevent rotation of the output shaft in the extension direction of rotation; and wherein the torque limiter disengages the anti-extension mechanism in the event that the predetermined torque limit is reached; wherein in the anti-extension mode and when the output is in the retracted position, the torque limiter is adjusted to disengage the anti-extension mechanism at a torque lower than the predetermined torque limit; and when the output position is approaching an end stop position the torque limiter is adjusted to disengage the anti-extension mechanism at a torque lower than the predetermined torque limit. 2 . The EMA assembly of claim 1 , further comprising means for providing an indication of the position of rotation of the output to the torque limiter, whereby the torque limiter is adjusted based on the indicated position. 3 . The EMA assembly of claim 1 , wherein the torque limiter includes a torque limiter spring to bias a crown, with which the ratchet wheel engages, relative to a housing of the EMA. 4 . The EMA assembly of claim 3 , wherein when the output is in the retracted position, the force of the torque limiter spring is removed to allow the gears to rotate in the anti-extension mode. 5 . The EMA assembly of claim 1 , wherein the ratchet wheel is positioned behind, and axially towards the motor, an end of the motor shaft and the anti-extension spring is located inwards of the ratchet wheel with respect to the motor axis, A, and wherein in active mode, the solenoid is energized and pushes the ratchet wheel against the force of the anti-extension spring to space the ratchet wheel away from the end of the motor shaft and in the anti-extension mode, the solenoid is not energized and the ratchet wheel is forced into engagement with the end of the motor shaft by the bias of the anti-extension spring to prevent rotation of the gears and the output in the extension direction. 6 . The EMA assembly of claim 3 , wherein the torque limiter includes an external member having a cam profile, connected to the output, such that as the output rotates, it causes rotation of the torque limiter external member cam surface relative to the torque limiter spring to vary the compression of the torque limiter spring according to the rotational position of the output. 7 . The EMA assembly of claim 1 , further comprising: mechanical stops defining an extent of rotation of the output in the first and second directions. 8 . The EMA assembly of claim 7 , wherein the torque limiter is adjusted based on detection of the rotational position of the output approaching one of the mechanical stops. 9 . The EMA assembly of claim 1 , wherein the output is connected to a lever for connection to a movable surface. 10 . The EMA assembly of claim 9 , wherein the movable surface is a spoiler of an aircraft.
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