Compact linear hydraulic actuator
In some embodiments, an actuator includes a chamber, a piston disposed within the chamber, and a tube. The chamber has a first port and a second port. The piston comprises a first surface, a second surface, and an elongated conduit coupling the first surface to the second surface. The first surface is disposed between the first port and the second port. The second surface is offset from the first surface. The tube is disposed at least partially within the elongated conduit of the piston. The tube comprises a third port disposed within the elongated conduit of the piston and a fourth port disposed outside of the elongated conduit of the piston.
1. A rotorcraft, comprising:
a body;
a rotor system coupled to the body, the rotor system comprising at least one rotor blade; and
an actuation system in mechanical communication with the rotor system, the actuation system comprising a first actuator, the first actuator comprising:
a chamber having a first port and a second port;
a piston disposed within the chamber, the piston comprising a first surface, a second surface, and an elongated conduit coupling the first surface to the second surface, the first surface being disposed between the first port and the second port, the second surface being offset from the first surface;
a tube disposed at least partially within the elongated conduit of the piston, the tube comprising a third port disposed within the elongated conduit of the piston and a fourth port disposed outside of the elongated conduit of the piston,
wherein the first surface separates the first port and the second port such that first surface, the first port, the elongated conduit, and the chamber at least partially define a first hydraulic volume,
wherein a second portion of the chamber opposite the piston from the first hydraulic volume is in fluid communication with the second port, and
wherein the second port is vented to atmosphere.
2. The rotorcraft of claim 1 , wherein a first hydraulic fluid source provides hydraulic fluid to the first hydraulic volume.
3. The rotorcraft of claim 1 , wherein increasing a hydraulic pressure of fluid within the first hydraulic volume causes the piston to move in a retract direction.
4. The rotorcraft of claim 1 , wherein the second surface, the elongated conduit, and the tube at least partially define a second hydraulic volume.
5. The rotorcraft of claim 4 , wherein a second hydraulic fluid source provides hydraulic fluid to the second hydraulic volume.
6. The rotorcraft of claim 4 , wherein increasing a hydraulic pressure of fluid within the second hydraulic volume causes the piston to move in an extend direction.
7. The rotorcraft of claim 1 , the actuator system further comprising a second actuator, a third actuator, and a yoke coupling the mechanical outputs of the first, second, and third actuators.
8. The rotorcraft of claim 1 , wherein the rotor system comprises a tiltrotor system tiltable between an airplane mode and a helicopter mode.
9. An actuator, comprising:
a chamber having a first port and a second port;
a piston disposed within the chamber, the piston comprising a first surface, a second surface, and an elongated conduit coupling the first surface to the second surface, the first surface being disposed between the first port and the second port, the second surface being offset from the first surface;
a tube disposed at least partially within the elongated conduit of the piston, the tube comprising a third port disposed within the elongated conduit of the piston and a fourth port disposed outside of the elongated conduit of the piston,
wherein the first surface separates the first port and the second port such that first surface, the first port, the elongated conduit, and the chamber at least partially define a first hydraulic volume,
wherein a second portion of the chamber opposite the piston from the first hydraulic volume is in fluid communication with the second port, and
wherein the second port is vented to atmosphere.
10. The actuator of claim 9 , wherein a first hydraulic fluid source provides hydraulic fluid to the first hydraulic volume.
11. The actuator of claim 9 , wherein increasing a hydraulic pressure of fluid within the first hydraulic volume causes the piston to move in a retract direction.
12. The actuator of claim 9 , wherein the second surface, the elongated conduit, and the tube at least partially define a second hydraulic volume.
13. The actuator of claim 12 , wherein a second hydraulic fluid source provides hydraulic fluid to the second hydraulic volume.
14. The actuator of claim 12 , wherein increasing a hydraulic pressure of fluid within the second hydraulic volume causes the piston to move in an extend direction.