Aircraft flight control system including electromechanical actuator
US-11235862-B2 · Feb 1, 2022 · US
US12374956B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12374956-B2 |
| Application number | US-202318168240-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 13, 2023 |
| Priority date | Mar 11, 2022 |
| Publication date | Jul 29, 2025 |
| Grant date | Jul 29, 2025 |
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A linear electro-mechanical actuator assembly includes a linear actuator having an output rod end, and a bell crank assembly having a bell crank that is rotatable around a central axis and that has a rod connection opening for receiving the rod end. The bell crank further includes a tube opening along the central axis for receiving a torque tube. First and second bearing plates are positioned on opposite sides of the bell crank, whereby the bank crank rotates relative to the first and second bearing plates. A connection pin provides a hinge connection of the rod end to the bell crank such that linear motion of the rod end imparts rotational motion to the bell crank. The bell crank includes bearing supports positioned on opposite sides of the bell crank body. Circular bearings are positioned within the bearing plates, and around the bearing supports, to support the rotational motion of the bell crank.
Opening claim text (preview).
What is claimed is: 1. A linear electro-mechanical actuator (EMA) assembly comprising: a linear actuator comprising an electric motor, a transmission assembly, and an actuating element having a rod end, wherein the transmission assembly converts an output of the electric motor into a linear motion of the actuating element; and a bell crank assembly comprising: a bell crank that is rotatable around a central axis and that has a rod connection opening for receiving the rod end, the bell crank further including a tube opening along the central axis for receiving a torque tube; a first bearing plate and a second bearing plate positioned on opposite sides of the bell crank, whereby the bell crank rotates relative to first bearing plate and the second bearing plate; and a connection pin to provide a hinge connection of the rod end to the bell crank such that the linear motion of the rod end imparts a rotational or articulating motion to the bell crank. 2. The linear EMA assembly of claim 1 , wherein the first bearing plate has a first internal bearing cavity and the second bearing plate has a second internal bearing cavity, and the bell crank assembly further comprises a first contact bearing that is positioned within the first internal bearing cavity and a second contact bearing that is positioned within the second internal bearing cavity, and the first contact bearing and the second contact bearing rotationally support the rotating or articulating motion of the bell crank. 3. The linear EMA assembly of claim 2 , wherein the first contact bearing and the second contact bearing are circular contact bearings, and the first bearing support and the second bearing support are circular bearing supports. 4. The linear EMA assembly of claim 2 , wherein the bell crank comprises a bell crank body that defines the rod connection opening, and a first bearing support and a second bearing support positioned on opposite sides of the bell crank body; wherein the first bearing support is positioned within the first contact bearing and the second bearing support is positioned within the second contact bearing to support the rotating or articulating motion of the bell crank. 5. The linear EMA assembly of claim 4 , wherein the first bearing support and the second bearing support are positionally separated along the central axis, with the bell crank body defining the rod connection opening between the first bearing support and the second bearing support. 6. The linear EMA assembly of claim 4 , wherein each of the first bearing support and the second bearing support includes a respective tube opening oriented along the central axis for receiving ends of respective first and second torque tubes. 7. The linear EMA assembly of claim 4 , wherein the bell crank body includes a pin opening, and the first bearing support include a first pin slot and the second bearing support includes a second pin slot that are spatially contiguous with the pin opening; wherein the rod end includes a connection hole; and wherein the connection pin extends through the pin opening, the connection pin slots, and the connection hole of the rod end to provide the hinge connection of the rod end to the bell crank. 8. The linear EMA assembly of claim 7 , wherein the pin opening and the first and second pin slots are positioned in the bell crank spaced apart from the central axis of the bell crank. 9. The linear EMA assembly of claim 1 , wherein the bell crank assembly further includes a first washer and a second washer that are positioned on opposite sides of the rod end, and the first washer and the second washer act as contact surfaces between the rod end and the bell crank. 10. The linear EMA assembly of claim 1 , wherein the linear actuator further includes an electric brake; and wherein the transmission assembly includes a speed reduction gear train mechanically coupled to the output of the electric motor, and a power screw assembly mechanically coupled between the speed reduction gear train and the actuating element and that converts the output of the electric motor into the linear motion of the actuating element. 11. A hinge line drive comprising: the linear EMA assembly accordingly to claim 1 , at least one torque tube that is fixed to the bell crank at the tube opening, wherein the rotating or articulating motion of the bell crank rotates the torque tube; and a control structure that is fixed to the torque tube at a location spaced apart from the bell crank, wherein rotation of the torque tube rotates or articulates the control structure. 12. The hinge line drive of claim 11 , further comprising at least one fixed mounting located adjacent to an end of the at least one torque tube opposite from the bell crank, wherein the at least one torque tube rotates relative to the fixed mounting. 13. The hinge line drive of claim 12 , wherein the at least one fixed mounting includes a pair of plates and a pair of bearings positioned within the pair of plates and that support rotation of the torque tube, and the control structure is positioned between the pair of plates of the fixed mounting. 14. The hinge line drive of claim 13 , wherein the at least one torque tube includes a first torque tube and a second torque tube that are fixed to and extend from opposite sides of the bell crank, and the at least one fixed mounting includes a first fixed mounting and a second fixed mounting located at respective ends of the first and second torque tubes. 15. The hinge line drive of any of claim 11 , further comprising a support frame, wherein the first bearing plate and the second bearing plate of the bell crank assembly are connected to the support frame. 16. The hinge line drive of claim 15 , further comprising: a spacer tube that extends between the first bearing plate and the second bearing plate to connect the first bearing plate and the second bearing plate to the support frame; and an additional mounting for connecting the linear actuator to the support frame. 17. An actuator assembly comprising: a linear actuator comprising an output rod end that is subject to linear extension and retraction as output of the linear actuator; and a bell crank assembly comprising: a bell crank that is rotatable around a central axis and that has a rod connection opening for receiving the rod end, the bell crank further including a tube opening along the central axis for receiving a torque tube; a first bearing plate and a second bearing plate positioned on opposite sides of the bell crank, whereby the bell crank rotates relative to first bearing plate and the second bearing plate; and a connection pin to provide a hinge connection of the rod end to the bell crank such that the linear motion of the rod end imparts a rotational or articulating motion to the bell crank; wherein the first bearing plate has a first internal bearing cavity and the second bearing plate has a second internal bearing cavity, and wherein the bell crank assembly further comprises a first contact bearing that is positioned within the first internal bearing cavity and a second contact bearing that is positioned within the second internal bearing cavity, and the first contact bearing and the second contact bearing rotationally support the rotating or articulating motion of the bell crank. 18. A bell crank assembly for use in converting a linear output of a linear actuator into a rotational or articulating motion, the bell crank assembly comprising: a bell crank that is rotatable around a central axis and that has a rod connection opening for r
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