Tunable Actuator Joint Modules Having Energy Recovering Quasi-Passive Elastic Actuators with Internal Valve Arrangements
US-2018194000-A1 · Jul 12, 2018 · US
US9732771B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9732771-B2 |
| Application number | US-201414547424-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 19, 2014 |
| Priority date | Feb 6, 2013 |
| Publication date | Aug 15, 2017 |
| Grant date | Aug 15, 2017 |
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A hydraulic rotary actuator including a stator housing having a through bore to position a rotor assembly. A rotor assembly includes an output shaft and at least a first rotary piston member disposed radially about the output shaft. The rotary piston member includes an vane element. A continuous seal is disposed on peripheral longitudinal faces and lateral end faces of the rotary piston element. The bore through the stator housing includes an interior cavity with surfaces adapted to receive the rotor assembly and contact the continuous seal. With rotation fluid ports blocked, the housing cavity is sealed with the continuous piston seal for hydraulic blocking, preventing actuator displacement by external forces. A method of operation and method of assembly is disclosed.
Opening claim text (preview).
What is claimed is: 1. A hydraulic rotary actuator comprising: a stator housing comprising a seamless body having a bore disposed axially therethrough, the bore having: a first end bore portion having a first diameter; a second end bore portion having a second diameter; and at least a middle bore portion disposed between the first end bore portion and the second end bore portion, said middle bore portion having: a first semi-cylindrical surface having a third diameter larger than the first diameter; a second semi-cylindrical surface having a fourth diameter less than the third diameter and larger than at least one of the first diameter and the second diameter, wherein the second semi-cylindrical surface is disposed inward radially along a portion of a perimeter of the middle bore; a first interior end surface between the middle bore portion and the first end bore portion; and a second interior end surface between said second bore portion and the middle bore portion; a rotor assembly comprising: an output shaft; a first rotary piston member disposed radially about the output shaft, said first rotary piston member having: a vane, a portion adapted to connect to the output shaft when the first rotary piston member is disposed radially about the output shaft, a first peripheral longitudinal face, a second peripheral longitudinal face, said second peripheral longitudinal face positioned axially on the vane, a first peripheral lateral face, a second peripheral lateral face, and a first continuous seal disposed on the first and second peripheral longitudinal faces and the first and second peripheral lateral faces of the first rotary piston member; and a second rotary piston member disposed radially about the output shaft, said second rotary piston member having: a vane, a portion adapted to connect to the output shaft when the second rotary piston member is disposed radially about the output shaft, a third peripheral longitudinal face, a fourth peripheral longitudinal face, said fourth peripheral longitudinal face positioned axially on the vane, a third peripheral lateral face, a fourth peripheral lateral face, and a second continuous seal disposed on the third and fourth peripheral longitudinal faces and the third and fourth peripheral lateral faces of the second rotary piston member; wherein when the rotor assembly is assembled and rotated in the bore of the stator housing, a portion of the first continuous seal positioned on the first peripheral longitudinal face contacts the second semi-cylindrical surface of the middle bore portion, a portion of the first continuous seal positioned on the second peripheral longitudinal face contacts the first semi-cylindrical surface of the middle bore portion, a portion of the first continuous seal positioned on the first peripheral lateral face contacts the first interior end surface, and a portion of the first continuous seal positioned on the second peripheral face contacts the second interior end surface. 2. The actuator of claim 1 wherein the vane of the first rotary piston member and the vane of the second rotary piston member are disposed longitudinally adjacent to each other and parallel to a longitudinal axis of the output shaft. 3. The actuator of claim 1 wherein each of the rotary piston members is adapted to pass through the first end bore portion before being coupled to the rotor output shaft in the middle bore portion. 4. The actuator of claim 3 wherein the portions of the rotary piston members include a plurality of slots adapted to receive a plurality of teeth on the output shaft thereby coupling the rotary piston members to the output shaft. 5. The actuator of claim 1 wherein at least one of the first continuous seal and the second continuous seal is selected from the group consisting of an O-ring, an X-ring, a Q-ring, a D-ring, and an energized seal. 6. The rotary actuator of claim 1 wherein the first rotary piston member and the second rotary piston member and the stator housing define two adjacent pressure chambers inside of the middle bore portion. 7. The actuator of claim 1 wherein a first external pressure source provides a fluid at a first pressure for contacting the vane of the first rotary piston member and a second external pressure source provides a fluid at a second pressure for contacting the vane of the second rotary piston member. 8. The actuator of claim 1 further including a third rotary piston member and a fourth rotary piston member each including a respective vane member, and wherein the stator housing and the first, second, third and fourth rotary piston members define four pressure chambers. 9. The actuator of claim 1 wherein the output shaft is configured to connect to a rotary valve stem. 10. The actuator of claim 1 wherein the output shaft is adapted for connection to an aircraft control surface. 11. The actuator of claim 8 wherein the first semi-cylindrical surface disposed inward radially along a portion of the middle bore includes a first terminal end adapted to contact the vane of the second rotary piston member. 12. The actuator of claim 11 wherein the middle bore portion includes a second semi-cylindrical surface disposed inward radially along a portion of the middle bore portion and opposite the first semi-cylindrical surface, said second semi-cylindrical surface having a first terminal end adapted to contact the vane of the first rotary piston member. 13. The actuator of claim 12 wherein the vanes of the first and second rotary piston members and the two semi-cylindrical surfaces are configured to define opposing pressure chambers. 14. The actuator of claim 13 wherein each pair of opposing pressure chambers defined by the housing and rotor have equal surface areas as the rotor assembly rotates within the housing. 15. The actuator of claim 13 wherein a first pair of opposing pressure chambers is adapted to be connected to a first external pressure source and a second pair of opposing pressure chambers is adapted to be connected to a second external pressure source. 16. The actuator of claim 15 wherein the first external pressure source provides a fluid at a first pressure for contacting the vane of the first rotary piston member and the second external pressure source provides a fluid for contacting the vane of the second rotary piston member. 17. The actuator of claim 12 wherein the first terminal end of the first semi-cylindrical surface further includes a first fluid port formed therethrough and the first terminal end of the second semi-cylindrical surface includes a second fluid port formed therethrough and the first fluid port is connected to a fluid provided at a first pressure and the second fluid port is connected to a fluid provided at a second pressure. 18. The actuator of claim 1 wherein the first diameter is greater than or equal to the second diameter. 19. The actuator of claim 1 wherein the second diameter is greater than or equal to the first diameter. 20. A method of rotary actuation comprising: providing a stator housing comprising a seamless body having a bore disposed axially therethrough, the bore having a first end bore portion having a first diameter, a second end bore portion having a second diameter, and at least a middle bore portion disposed between the first end bore portion and the second end bore portion, said middle bore portion having a first semi-cylindrical surface having a third diameter larger than the first diameter, a second semi-cylindrical surface
Stators · CPC title
of the oscillating-vane or curved-cylinder type · CPC title
Vane type or other rotary, e.g., fan · CPC title
forming ring or sector · CPC title
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